L3Harris Aviation Products Technical Publications Catalog
Last update: 7/12/2025
| Product | Type | Pub Part Number | ATA Number | Revision | Revision Date | Title | Subject/Description | Product Part Number |
|---|---|---|---|---|---|---|---|---|
| 612RIU | Component Maintenance Manual | AD009A0480 | 0 | 2/1/1982 | Installation and Maintenance Manual | 612 RIU Remote Interface Unit | 805D0480 | |
| 7100 CVDR | Component Maintenance Manual | 0040-28002-01 | 23-70-75 | 04 | 5/7/2024 | SRVIVR25 (7100) CVDR CMM | Cockpit Voice and Flight Data Recorder (SRVIVR25) CVDR | 7100-3000-00, 7100-3900-00, 7102-3900-00, 7104-3000-00, 7104-3700-00 |
| 7100 CVDR | Component Maintenance Manual | L3HARRIS7100-25583-00001-00 | 31-34-01 | 009 | 11/13/2023 | Component Maintenance Publication (CMP) | Cockpit Voice and Flight Data Recorder (Dual - Deployable), 7100-0200-00 (Supersedes CMM 165E6493-00) | 7100-0200-00 |
| 7100 CVDR | Installation Manual | 0040-28001-07 | 23-70-79 | 02 | 3/20/2023 | Installation and Operation Manual | Cockpit Voice and Flight Data Recorder (SRVIVR25) CVDR, PN 7104-3700-00 | 7104-3700-00 |
| 7100 CVDR | Installation Manual | 165E6493-01 | 31-34-02 | 03 | 4/30/2020 | Installation and Operation Manual, 7100-0200-00 | Cockpit Voice and Flight Data Recorder (Dual - Deployable), 7100-0200-00 | 7100-0200-00 |
| 7100 CVDR | Installation Manual | 0040-28001-01 | 23-70-76 | 04 | 1/19/2023 | Installation and Operation Manual | Cockpit Voice and Flight Data Recorder (SRVIVR25) CVDR | 7102-3900-00 |
| 7100 CVDR | Installation Manual | 0040-28001-02 | 23-70-77 | 01 | 3/14/2024 | Installation and Operation Manual | Cockpit Voice and Flight Data Recorder (SRVIVR25) CVDR, 7100-3900-00 | 7100-3900-00 |
| 7100 CVDR | Installation Manual | 0040-28001-20 | 23-70-80 | 01 | 1/19/2023 | Installation & Operation Manual, SRVIVR25 (7100) | SRVIVR25 Cockpit Voice and Flight Data Recorder ARINC 757 Variant RIPS Capable | 7104-3000-00 |
| 7100 CVDR | Instruction Manual | 905-E6493-22 | 01 | 11/30/2021 | Accident Investigation Procedure. 7100CVDR (dual-deployable) | Accident Investigation Procedure | 7100-0200-00 | |
| 7100 CVDR | Service Bulletin | SB002-SVR7100CVDR | SVR7100CVDR-23-6000 | 00 | 2/28/2022 | Software Release 1.4 | Software Release 1.4 | 7100-3000-00, 7102-3900-00 |
| 7100 CVDR | Service Bulletin | SB001-SVR7100CVDR-EMB | SVR7100CVDR-23-0001 | 00 | 3/31/2022 | MOD 1 – New Aircraft Interface CCA | MOD 1 – New Aircraft Interface CCA | 7104-3700-00, SVR7100CVDR-23-0001 |
| 7100 CVDR | Service Bulletin | SB003-SVR7100CVDR | SVR7100CVDR-23-6001 | 00 | 6/20/2022 | Software Release 1.5 | Software Release 1.5 | 7100-3000-00, 7102-3900-00 |
| 7100 CVDR | Service Letter | SIL-001-7100 | 00 | 10/5/2021 | SRVIVR25 CVR/CVDR Greenwich Mean Time (GMT) date and time mismatch. | SRVIVR25 CVR/CVDR Greenwich Mean Time (GMT) date and time mismatch | 7100-xxxx-xx | |
| 7100 CVDR | Service Letter | SIL-002-7100 | 00 | 9/11/2024 | Possible delamination of circuit card conformal coating. | Provide customers information on circuit card assembly coating for affected serial numbers. | 7100-0200-00 | |
| 7100 CVR | Component Maintenance Manual | 0040-28002-02 | 23-70-70 | 11 | 8/14/2024 | SRVIVR25 (7100) CMM | Cockpit Voice Recorder (SRVIVR25) CVR | 7100-1000-00, 7100-1000-12, 7100-1000-30, 7100-1000-31, 7100-1000-70, 7100-1100-20, 7100-1900-30, 7100-1900-31, 7102-1000-00, 7102-1000-20, 7102-1100-00, 7102-1900-30, 7104-1000-00, 7104-1000-20, 7104-1100-00, 7104-1100-20, 7104-1900-00, 7104-1900-20 |
| 7100 CVR | Installation Manual | 0040-28001-12 | 23-70-85 | 01 | 8/12/2024 | Installation and Operation Manual, 7102-1900-30 | Cockpit Voice Recorder (SRVIVR25) CVR, ARINC 757 Variant | 7102-1900-30 |
| 7100 CVR | Installation Manual | 0040-28001-13 | 23-70-86 | 04 | 12/5/2024 | Installation and Operation Manual | Cockpit Voice Recorder (SRVIVR25) CVR, 7104-1100-20, 7104-1900-20 | 7104-1100-20, 7104-1900-20 |
| 7100 CVR | Installation Manual | 0040-28001-06 | 23-70-73 | 01 | 3/1/2023 | Installation and Operation Manual | Cockpit Voice Recorder (SRVIVR25) CVR, 7100-1000-70 | 7100-1000-70 |
| 7100 CVR | Installation Manual | 0040-28001-15 | 23-70-87 | 01 | 2/15/2024 | Installation and Operation Manual | Cockpit Voice Recorder (SRVIVR25) CVR, 7100-1000-12 | 7100-1000-12 |
| 7100 CVR | Installation Manual | 0040-28001-19 | 23-70-90 | 05 | 2/15/2024 | Installation and Operation Manual, SRVIVR25 (7100) | Cockpit Voice Recorder (SRVIVR25) CVR, ARINC 757 Variant | 7100-1000-00, 7100-1100-00 7102-1000-00, 7102-1100-00 7104-1000-00, 7104-1100-00 |
| 7100 CVR | Installation Manual | 0040-28001-04 | 23-70-71 | 02 | 11/13/2024 | Installation and Operation Manual | Cockpit Voice Recorder (SRVIVR25) CVR | 7100-1000-30, 7100-1000-31 |
| 7100 CVR | Installation Manual | 0040-28001-05 | 23-70-72 | 02 | 11/20/2024 | Installation and Operation Manual | Cockpit Voice Recorder (SRVIVR25) CVR | 7100-1900-30, 7100-1900-31 |
| 7100 CVR | Installation Manual | 0040-28001-18 | 23-70-89 | 01 | 11/25/2024 | Installation and Operation Manual | Cockpit Voice Recorder (SRVIVR25) , CVR, ARINC 757, DC Only, No RIPS, Short, Common Grounds, Std Memory | 7100-1100-20, 7102-1000-20, 7104-1000-20 |
| 7100 CVR | Installation Manual | 0040-28001-21 | 23-70-60 | 01 | 4/10/2024 | Installation and Operation Manual | Cockpit Voice Recorder (SRVIVR25) CVR, 7104-1900-00 | 7104-1900-00 |
| 7100 CVR | Instructions for Continued Airworthiness iCA | 8210686-600 | C | 4/30/2023 | Instructions for Continued Airworthiness for the Bombardier CRJ-200/900 SRVIVR25 CVR with RIPS Recorder System | Instructions for Continued Airworthiness for the Bombardier CRJ-200/900 SRVIVR25 CVR with RIPS Recorder System | Recorder Cockpit Voice Recorder, 7100 | |
| 7100 CVR | Instructions for Continued Airworthiness iCA | 8210691-600 | - | 8/10/2022 | DE HAVILLAND DHC-8-100/-300 SRVIVR25 CVR NSTRUCTIONS FOR CONTINUED AIRWORTHINESS | DE HAVILLAND DHC-8-100/-300 SRVIVR25 CVR NSTRUCTIONS FOR CONTINUED AIRWORTHINESS | Recorder Cockpit Voice Recorder, 7100 | |
| 7100 CVR | Instructions for Continued Airworthiness iCA | 8210693-600 | C | 12/18/2023 | DE HAVILLAND DHC-8-400 SRVIVR25 CVR INSTRUCTIONS FOR CONTINUED AIRWORTHINESS | DE HAVILLAND DHC-8-400 SRVIVR25 CVR INSTRUCTIONS FOR CONTINUED AIRWORTHINESS | Recorder Cockpit Voice Recorder, 7100 | |
| 7100 CVR | Instructions for Continued Airworthiness iCA | 8010116-600 | B | 7/25/2023 | Instructions for Continued Airworthiness for the Boeing 737NG SRVIVR25 CVR with RIPS Recorder System | Instructions for Continued Airworthiness for the Boeing 737NG SRVIVR25 CVR with RIPS Recorder System | Recorder Cockpit Voice Recorder, 7100 | |
| 7100 CVR | Service Bulletin | SB002-SVR7100CVR | SVR7100CVR-23-6000 | 01 | 4/14/2022 | Software Release 1.4 | Software Release 1.4 | 7102-1000-00, SVR7100CVR-23-6000 |
| 7100 CVR | Service Bulletin | SB001-SVR7100CVR | SVR7100CVR-23-0000 | 00 | 3/31/2022 | MOD 1 – New Aircraft Interface CCA | MOD 1 – New Aircraft Interface CCA | 7100-1000-12 |
| 7100 CVR | Service Bulletin | SB001-7100CVR-AB | SVR7100CVR-23-0001 | 01 | 6/9/2025 | ADMT A - New Aircraft Interface CCA | ADMT A - New Aircraft Interface CCA | 7100-1000-30, 7100-1000-31, 7100-1900-30, 7100-1900-31, SVR7100CVR-23-0001 |
| 7100 CVR | Service Bulletin | SB001-SVR7100CVR-ABC | SVR7100CVR-23-0003 | 00 | 3/31/2022 | ADMT A - New Aircraft Interface CCA | ADMT A - New Aircraft Interface CCA | 7102-1900-30, SVR7100CVR-23-0003 |
| 7100 CVR | Service Bulletin | SB001-SVR7100CVR-BA | SVR7100CVR-23-0002 | 00 | 3/31/2022 | MOD 1 – New Aircraft Interface CCA | MOD 1 – New Aircraft Interface CCA | 7104-1100-20, 7104-1900-20 |
| 7100 CVR | Service Bulletin | SB002-SVR7100CVR-BA | SVR7100CVR-23-6001 | 00 | 4/14/2022 | Software Release 1.4 | Software Release 1.4 | 7104-1100-20, 7104-1900-20, SVR7100CVR-23-6001 |
| 7100 CVR | Service Bulletin | SB003-SVR7100CVR | SVR7100CVR-23-6001 | 00 | 6/20/2022 | Software Release 1.5 | Software Release 1.5 | 7102-1000-00 |
| 7100 CVR | Service Letter | SIL-001-7100 | 00 | 10/5/2021 | SRVIVR25 CVR/CVDR Greenwich Mean Time (GMT) date and time mismatch. | SRVIVR25 CVR/CVDR Greenwich Mean Time (GMT) date and time mismatch | 7100-xxxx-xx | |
| 7100 CVR | Supplemental Type Certificate | ST02721LA | A | 4/14/2023 | Bombardier / MHI for CVR | ST02721LA MHI/Bombardier | 7100- | |
| 7100 CVR | Supplemental Type Certificate | ST04560CH | A | 2/13/2023 | DE HAVILLAND DHC-8-400 - CVR | ST04560CH DE HAVILLAND DHC-8-400 | 7100- | |
| 7100 CVR | Supplemental Type Certificate | ST02719LA | B | 10/5/2022 | BOEING B737-700 B737-800 - CVR | STC ST02719LA BOEING B737-700 B737-800 | 7100-xxxx-xx | |
| 7100 CVR | Supplemental Type Certificate | ST04559CH | C | 1/5/2023 | DE HAVILLAND DHC-8-100/300 - CVR | STC for DE HAVILLAND DHC-8-100/300 Rev C: Add TCCA approval certificate | 7100- | |
| 7100 FDR | Component Maintenance Manual | 0040-28002-03 | 31-30-70 | 05 | 5/7/2024 | SRVIVR25 (7100) FDR CMM | Flight Data Recorder (SRVIVR25) FDR | 7100-2400-00, 7100-2400-12, 7100-2700-00, 7100-2700-20, 7100-2700-30, 7100-4400-00, 7100-4400-70 |
| 7100 FDR | Installation Manual | 0040-28001-14 | 31-30-75 | 00 | 11/16/2020 | Installation and Operation Manual | Flight Data Recorder (SRVIVR25) FDR, 7100-2400-12 | 7100-2400-12 |
| 7100 FDR | Installation Manual | 0040-28001-10 | 31-30-73 | 01 | 5/15/2023 | Installation and Operation Manual | Flight Data Recorder (SRVIVR25) FDR, 7100-4400-70 Specific, ARINC 747 Variant, no RIPS | 7100-4400-70 |
| 7100 FDR | Installation Manual | 0040-28001-08 | 31-30-71 | 03 | 5/23/2024 | Installation and Operation Manual | Flight Data Recorder (SRVIVR25) FDR | 7100-2400-00, 7100-2700-00 |
| 7100 FDR | Installation Manual | 0040-28001-09 | 31-30-72 | 03 | 12/27/2023 | Installation and Operation Manual | Flight Data Recorder (SRVIVR25), FDR, 7100-4400-00 | 7100-4400-00 |
| 7100 FDR | Installation Manual | 0040-28001-03 | 23-70-78 | 03 | 3/14/2024 | Installation and Operation Manual | Cockpit Voice and Flight Data Recorder (SRVIVR25) FDR, 7100-3000-00 | 7100-3000-00 |
| 7100 FDR | Installation Manual | 0040-28001-11 | 31-30-74 | 01 | 11/12/2024 | Installation and Operation Manual | Flight Data Recorder (SRVIVR25) FDR | 7100-3700-30 |
| 7100 FDR | Installation Manual | 0040-28001-17 | 31-30-76 | 01 | 12/9/2024 | Installation and Operation Manual, SRVIVR25 (7100) | Flight Data Recorder (SRVIVR25) FDR, 7100-2400-20, 7100-2700-20 | 7100-2400-20, 7100-2700-20 |
| 7100 FDR | Service Bulletin | SB002-SVR7100FDR | SVR7100FDR-31-6000 | 00 | 2/28/2022 | Software Release 1.4 | Software Release 1.4 | 7100-4400-00 |
| 7100 FDR | Service Bulletin | SB003-SVR7100FDR | SVR7100FDR-31-6001 | 00 | 6/20/2022 | Software Release 1.5 | Software Release 1.5 | 7100-2400-00, 7100-2700-00, 7100-4400-00 |
| 7100 FDR | Service Bulletin | SB001-SVR7100FDR | SVR7100FDR-31-0000 | 00 | 3/31/2022 | MOD 1 – New Aircraft Interface CCA | MOD 1 – New Aircraft Interface CCA | 7100-2400-12 |
| 7100 FDR | Service Bulletin | SB001-SVR7100FDR-EMB | SVR7100FDR-31-0001 | 00 | 3/31/2022 | MOD 1 – New Aircraft Interface CCA | MOD 1 – New Aircraft Interface CCA | 7100-2400-00, 7100-2700-00, SVR7100FDR-31-0001 |
| 7100 FDR | Service Bulletin | SB001-SVR7100FDR-ABC | SVR7100FDR-31-0002 | 00 | 3/31/2022 | AMDT A – New Aircraft Interface CCA | AMDT A – New Aircraft Interface CCA | 7100-2700-30, SVR7100FDR-31-0002 |
| A100 -IRIS | Drawings / SPEC | A46PM5048 | D | 12/8/2006 | IRIS ICAW | IRIS ICAW | 9200-18000-01 9200-18000-02 9200-18000-03 9200-18000-0 | |
| A100 -IRIS | Installation Manual | 0040-18001-01 | D | 4/3/2012 | Installation Manual | Install Manual | 9200-18000-( ), 9200-18000-01 | |
| A100 -IRIS | Pilot Guide | 0040-18000-01 | B | 4/27/2007 | Pilots Guide for the Infrared Imaging System IRIS Model A100 | Pilots Guide | 9200-18000-( ), 9200-18000-01 | |
| A100 -IRIS | Service Letter | SL-228 | A | 7/21/2007 | Permission to use STC | Permission to use STC | 9200-18000-( ), 9200-18000-01 | |
| A100 -IRIS | Service Letter | SL-232 | A | 4/9/2008 | PMA APPROVAL LIST FOR A-100 IRIS | PMA APPROVAL LIST FOR IRIS A-100 | 9200-18000-01 | |
| A100A | Component Maintenance Manual | 165E010200 | 23-70-11 | Initial | 8/1/1989 | GA100 Component Maintenance Manual | GA100 CMM by special request only. Contact Avionics.TechPubs@L3Harris.com | GA100-0000, GA150-0000 |
| A100A | Component Maintenance Manual | 165E010100 | 23-70-01 | 3 | 3/4/2004 | A100 / A100A CVR CMM | Acron Aviation | 93A100, 93A151, 93A152, 93A055 |
| A100A | Installation Manual | 165E280700 | 23-70-01 | 02 | 7/1/2002 | A100 / A100A Installation & Operation Manual | A100 / A100A Installation & Operation Manual, Acron Aviation | 93A10010, 93A10011, 93A10011, 93A10030, 93A10031, 93A10032, 93A10033, 93A10080, 93A10081, 93A10082, 93A10083, 93A10084, 93A10085, 93A15100, 93A15101, 93A15120, 93A15130, 93A15140, 93A15150, 93A15200, 93A15201, 93A15204, 93A15220, 93A15225, 93A15230, 93A15235, 93A15240, 93A15250, 93A15260, 93A15270, 93A05500, 93A05510, 93A05520, 93A05530, 93A05540, 93A05545, 93A05550, 93A05555, 93A05560, 93A05565, 93A05566, 93A05567, 93A05595, 93A15020 |
| A100A | Miscellaneous | A100 Recorder Service Letters | n/a | 11/18/2021 | UntitledLetters provide information on A100 obsolescence and replacement options. | Letters provide information on A100 obsolescence and replacement options. | n/a | |
| A100A | Service Letter | A100/A100A CVR 025 | Orig | 8/13/2014 | ACCESS TO A100/A100A TECHNICAL PUBLICATIONS | ACCESS TO A100/A100A TECHNICAL PUBLICATIONS | 93A100, 93A151, 93A152, 93A055 | |
| A100S | Component Maintenance Manual | 165E094800 | 23-70-02 | 03 | 7/1/2005 | A100S Component Maintenance Manual | Acron Aviation | S100–0080–00, S100–0080–01, 93A15101, 93A15120, 93A15130, 93A15140, 93A15150, 93A15200, 93A15201, 93A15204, 93A15220, 93A15225, 93A15230, 93A15235, 93A15240, 93A15250, 93A15260, 93A15270, 93A05500, 93A05503, 93A05510, 93A05520, 93A05530, 93A05550, 93A05555, 93A05540, 93A05545, 93A05560, 93A05565, 93A05566, 93A05567, 93A05595, 9300A165, 9300A16501 |
| A100S | Installation Manual | 165E2712-00 | 23-70-02 | Initial | 8/1/1993 | A100S Installation & Operation Manual | A100S Installation & Operation Manual (previously FAR04611238), Acron Aviation | S100–0080–00, S100–0080–01, 93A15101, 93A15120, 93A15130, 93A15140, 93A15150, 93A15200, 93A15201, 93A15204, 93A15220, 93A15225, 93A15230, 93A15235, 93A15240, 93A15250, 93A15260, 93A15270, 93A05500, 93A05503, 93A05510, 93A05520, 93A05530, 93A05550, 93A05555, 93A05540, 93A05545, 93A05560, 93A05565, 93A05566, 93A05567, 93A05595, 9300A165, 9300A16501 |
| A100S | Miscellaneous | A100 Recorder Service Letters | n/a | 11/18/2021 | UntitledLetters provide information on A100 obsolescence and replacement options. | Letters provide information on A100 obsolescence and replacement options. | n/a | |
| A100S | Service Letter | A100S SSCVR SIL006 | Orig | 8/23/1996 | CUSTOMER ACCESS TO A100S SSCVR PUBLICATIONS | CUSTOMER ACCESS TO A100S SSCVR PUBLICATIONS | A100S | |
| A200S | Component Maintenance Manual | 165E123300 | 23-70-03 | 5 | 3/1/2005 | A200S Component Maintenance Manual | A200S CMM, Acron Aviation | S200–0012–00, S200–0003–00, S200–0003–90, S200–0012–91, S200–0003–91 |
| A200S | Service Bulletin | A200S SSCVR SB009 | 23‐70‐03-009 | 00 | 2/2/2015 | MD 4 & 5: Introduction of 90 Day ULB | A200S SSCVR MD 4 & 5: Introduction of 90 Day ULB, Acron Aviation | S200–00XX–XX |
| A200S | Service Letter | A200S SSCVR 003 | 01 | 8/23/2006 | NOTIFICATION OF OBSOLESCENCE | NOTIFICATION OF OBSOLESCENCE, Acron Aviation | S200-0003-xx S200-0012-xx S200-xxxx-xx | |
| A200S | Service Letter | A200S SSCVR 004 | Orig | 2/3/2011 | NOTIFICATION OF DISCONTINUED PARTS SUPPORT - A200S | NOTIFICATION OF DISCONTINUED PARTS SUPPORT, Acron Aviation | S200-0003-XX S200-0012-XX | |
| AC-111 | Service Bulletin | SB501-1038-1 | Orig | 1/15/1973 | Replace diodes on interconnect PC board and removal of C5 from solid state synchronizer board. | 501-1038-( ) | ||
| AC-111 | Service Bulletin | SB501-1038-2 | Orig | 1/15/1973 | Replace diodes on interconnect PC board and removal of C5 from solid state synchronizer board. | 501-1038-( ) | ||
| AC-111 | Service Bulletin | SB501-1038-3 | A | 8/1/1974 | Modification of solid state synchronizer board. | 501-1038-( ) | ||
| AC-111 | Service Bulletin | SB501-1038-4 | D | 8/5/1983 | To retrofit Flight Controller for 6 degree per second Roll Rate Limiter. (Model change) | 501-1038-( ) | ||
| AC-111 | Service Bulletin | SB501-1038-5 | D | 9/24/1984 | Retrofit flight controller to limit pitch command capability to 20 deg/UP and 10 deg/down. (Model change) | 501-1038-( ), 501-1038-01, 501-1038-02 | ||
| AC-111 | Service Bulletin | SB501-1038-6 | Orig | 8/4/1983 | Resistor Replacement on Command Limiter Circuit Card Assembly. | 501-1038-( ) | ||
| AC-111 | Service Bulletin | SB501-1038-7 | Orig | 6/29/1984 | Resistor Replacement on Command Limiter Circuit Card Assembly. | 501-1038-( ) | ||
| AC-111 | Service Bulletin | SB501-1042-1 | Orig | 1/15/1973 | Replace diodes on interconnect PC board and removal of C5 from solid state synchronizer board. | 501-1042-( ) | ||
| AC-111 | Service Bulletin | SB501-1042-2 | Orig | 1/15/1973 | Replace diodes on interconnect PC board and removal of C5 from solid state synchronizer board. | 501-1042-( ) | ||
| AC-111 | Service Bulletin | SB501-1042-3 | A | 8/1/1974 | Modification of solid state synchronizer board. | 501-1042-( ) | ||
| AC-111 | Service Bulletin | SB501-1042-4 | D | 8/5/1983 | To retrofit Flight Controller for 6 degree per second Roll Rate Limiter. (model change) | 501-1042-( ) | ||
| AC-111 | Service Bulletin | SB501-1042-5 | D | 9/24/1984 | Retrofit flight controller to limit pitch command capability to 20 deg/UP and 10 deg/down. (Model change) | 501-1042-( ) | ||
| AC-111 | Service Bulletin | SB501-1042-6 | Orig | 8/4/1983 | Resistor Replacement on Command LImiter Circuit Card Assemlby. | 501-1042-( ) | ||
| AC-111 | Service Bulletin | SB501-1042-7 | Orig | 6/29/1984 | Resistor Replacement on Command Limiter Circuit Card Assembly. | 501-1042-( ) | ||
| AC-111 | Service Bulletin | SB501-1047-1 | Orig | 1/15/1973 | Replace diodes on interconnect PC board and removal of C5 from solid state synchronizer board. | 501-1047-( ) | ||
| AC-111 | Service Bulletin | SB501-1047-2 | Orig | 1/15/1973 | Replace diodes on interconnect PC board and removal of C5 from solid state synchronizer board. | 501-1047-( ) | ||
| AC-111 | Service Bulletin | SB501-1047-3 | A | 8/1/1974 | Modification of solid state synchronizer board. | 501-1047-( ) | ||
| AC-111 | Service Bulletin | SB501-1047-4 | D | 8/5/2004 | To retrofit Flight Controller for 6 degree per second Roll Rate Limiter. (Model change) | 501-1047-( ) | ||
| AC-111 | Service Bulletin | SB501-1047-5 | D | 9/24/1984 | Retrofit flight controller to limit pitch command capability to 20 deg/UP and 10 deg/down. (Model change) | 501-1047-( ) | ||
| AC-111 | Service Bulletin | SB501-1047-6 | Orig | 8/4/1983 | Resistor Replacement on Command Limiter Circuit Card Assembly. | 501-1047-( ) | ||
| AC-111 | Service Bulletin | SB501-1047-7 | Orig | 5/29/1984 | Resistor Replacement on Command Limiter Circuit Card Assemlby. | 501-1047-( ) | ||
| AC-111 | Service Bulletin | SB501-1048-1 | Orig | 1/15/1973 | Replace diodes on interconnect PC board and removal of C5 from solid state synchronizer board. | 501-1048-( ) | ||
| AC-111 | Service Bulletin | SB501-1048-2 | Orig | 1/15/1973 | Replace diodes on interconnect PC board and removal of C5 from solid state synchronizer board. | 501-1048-01 | ||
| AC-111 | Service Bulletin | SB501-1048-3 | A | 8/1/1974 | Modification of solid state synchronizer board. | 501-1048-01 | ||
| AC-111 | Service Bulletin | SB501-1048-4 | D | 8/5/1983 | To retrofit Flight Controller for 6 degree per second Roll Rate Limiter. (Model Change) | 501-1048-01, 501-1048-03 | ||
| AC-111 | Service Bulletin | SB501-1048-5 | D | 9/24/1984 | Retrofit flight controller to limit pitch command capability to 20 deg/UP and 10 deg/down. (Model change) | 501-1048-( ), 501-1048-01, -02 | ||
| AC-111 | Service Bulletin | SB501-1048-6 | Orig | 8/4/1983 | Resistor Replacement on Command Limiter Circuit Card Assemlby. | 501-1048-( ) | ||
| AC-111 | Service Bulletin | SB501-1048-7 | Orig | 7/26/2005 | Resistor Replacement on Command Limiter Circuit Card Assemlby. | 501-1048-( ) | ||
| AC-111 | Service Bulletin | SB501-1072-1 | Orig | 1/15/1973 | Replace diodes on interconnect PC board and removal of C5 from solid state synchronizer board. | 501-1072-01 | ||
| AC-111 | Service Bulletin | SB501-1072-2 | Orig | 1/15/1973 | Replace diodes on interconnect PC board and removal of C5 from solid state synchronizer board. | 501-1072-01 | ||
| AC-111 | Service Bulletin | SB501-1072-3 | A | 8/1/1974 | Modification of solid state synchronizer board. | 501-1072-01 | ||
| AC-111 | Service Bulletin | SB501-1072-4 | D | 8/5/1983 | To retrofit Flight Controller for 6 degree per second Roll Rate Limiter. (Model change) | 501-1072-01, 501-1072-03 | ||
| AC-111 | Service Bulletin | SB501-1072-5 | D | 9/24/1984 | Retrofit flight controller to limit pitch command capability to 20 deg/UP and 10 deg/down. (Model change) | 501-1072-01, 501-1072-02 | ||
| AC-111 | Service Bulletin | SB501-1072-6 | Orig | 8/4/1983 | Resistor Replacement on Command Limiter Circuit Card Assembly. | 501-1072-( ) | ||
| AC-111 | Service Bulletin | SB501-1072-7 | Orig | 6/29/1984 | Resistor Replacement on Command Limiter Circuit Card Assembly. | 501-1072-( ) | ||
| AC-111 | Service Bulletin | SB501-1073-1 | Orig | 1/15/1973 | Replace diodes on interconnect PC board and removal of C5 from solid state synchronizer board. | 501-1073-01 | ||
| AC-111 | Service Bulletin | SB501-1073-2 | Orig | 1/15/1973 | Replace diodes on interconnect PC board and removal of C5 from solid state synchronizer board. | 501-1073-01 | ||
| AC-111 | Service Bulletin | SB501-1073-3 | A | 8/1/1974 | Modification of solid state synchronizer board. | 501-1073-01 | ||
| AC-111 | Service Bulletin | SB501-1073-4 | D | 8/5/1983 | To retrofit Flight Controller for 6 degree per second Roll Rate Limiter. (model change) | 501-1073-01, 501-1073-03 | ||
| AC-111 | Service Bulletin | SB501-1073-5 | D | 9/24/1984 | Retrofit flight controller to limit pitch command capability to 20 deg/UP and 10 deg/down. (Model change) | 501-1073-01, 501-1073-02 | ||
| AC-111 | Service Bulletin | SB501-1073-6 | Orig | 8/4/1983 | Resistor Replacement on Command Limiter Circuit Card Assembly. | 501-1073-( ) | ||
| AC-111 | Service Bulletin | SB501-1073-7 | Orig | 6/29/1984 | Resistor Replacement on Command Limiter Curcuit Card Assemlbly. | 501-1073-( ) | ||
| AC-111 | Service Bulletin | SB501-1074-1 | Orig | 1/15/1973 | Replace diodes on interconnect PC board and removal of C5 from solid state synchronizer board. | 501-1074-01 | ||
| AC-111 | Service Bulletin | SB501-1074-2 | Orig | 1/15/1973 | Replace diodes on interconnect PC board and removal of C5 from solid state synchronizer board. | 501-1074-01 | ||
| AC-111 | Service Bulletin | SB501-1074-3 | A | 8/1/1974 | Modification of solid state synchronizer board. | 501-1074-01 | ||
| AC-111 | Service Bulletin | SB501-1074-4 | D | 8/5/1983 | To retrofit Flight Controller for 6 degree per second Roll Rate Limiter. (Model Change) | 501-1074-01, 501-1074-03 | ||
| AC-111 | Service Bulletin | SB501-1074-5 | D | 9/24/1984 | Retrofit flight controller to limit pitch command capability to 20 deg/UP and 10 deg/down. (Model change) | 501-1074-01, 501-1074-02 | ||
| AC-111 | Service Bulletin | SB501-1074-6 | Orig | 8/4/1983 | Resistor Replacement on Command Limiter Circuit Card Assemlby. | 501-1074-( ) | ||
| AC-111 | Service Bulletin | SB501-1074-7 | Orig | 6/29/1984 | Resisitor Replacement on Command Limiter Circuit Card Assemlby. | 501-1074-( ) | ||
| AC-111 | Service Bulletin | SB501-1254-1 | D | 8/5/1983 | To retrofit Flight Controller for 6 degree per second Roll Rate Limiter. (Model Change) | 501-1254-01, 501-1254-02, 501-1254-05, 501-1254-06 | ||
| AC-111 | Service Bulletin | SB501-1254-2 | D | 9/24/1984 | Retrofit flight controller to limit pitch command capability to 20 deg/UP and 10 deg/down. (Model change) | 501-1254-01, 501-1254-02, 501-1254-07, 501-1254-08 | ||
| AC-111 | Service Bulletin | SB501-1254-3 | Orig | 8/1/1983 | To replace resistor to provide increase ROLL SERVO BALANCE adjustment range. | 501-1254-03, 501-1254-04, 501-1254-07, 501-1254-08 | ||
| AC-111 | Service Bulletin | SB501-1254-4 | Orig | 6/1/1984 | To replace resistor on Command Limiter Circuit Card Assembly. | 501-1254-03, 501-1254-04, 501-1254-05, 501-1254-06 | ||
| Accelerometer | Component Maintenance Manual | 165E4878-01 | 31-20-01 | 05 | 8/6/2015 | Multi-Axial Accelerometer CMM | Multi-Axial Accelerometer, Acron Aviation | 17A717-03-00 |
| Accelerometer | Installation Manual | 165E4878-00 | 05 | 8/12/2014 | Multi-Axial Accelerometer Installation and Operation Manual w/IPC | Multi-Axial Accelerometer, Acron Aviation | 17A542-03-00 | |
| Accelerometer | Installation Manual | 165E4878-02 | 02 | 8/12/2014 | Multi-Axial Accelerometer (High Sensitivity) Installation & Operation Manual w/IPC | Multi-Axial Accelerometer (High Sensitivity) Installation & Operation Manual w/IPC, Acron Aviation | 17A542-03-01, ARINC 542 / TRI AXIS, Multi-Axial Accelerometer (High Sensitivity) | |
| Accelerometer | Service Bulletin | SB002-17A717 | 17A717-31-002 | 01 | 9/24/2024 | Service Bulletin (Label Update) | Hardware – Product Identification Label Update for TSO-C124c and ED-112A. Acron Aviation | 17A717-03-00 |
| ADC-3000 | Service Bulletin | SB501-1797-3 | B | 12/3/2008 | To eliminate intermittent air data invalidities after extended period of flight. | To eliminate intermittent air data invalidities after extended period of flight. | 501-1797-(), 501-1797-00 thru -64, 501-1797-66, 501-1797-68 thru -76, 501-1797-78 | |
| ADC-3000 | Service Bulletin | SB501-1797-1 | A | 3/14/2003 | Stabilize air data sensors. | Stabilize air data sensors. | 501-1797-( ), 501-1797-01 thru -61 | |
| ADC-3000 | Service Bulletin | SB501-1797-2 | B | 2/11/2009 | Correct intermittent air data invalidities. [Inspect for Mod D or higher identification on Rosemount ID plate]. | Correct intermittent air data invalidities. | 501-1797-01 thru -71 | |
| ADC-3000 | Service Bulletin | SB501-1890-1 | Orig | 2/12/2003 | Eliminates erratic altitude display. | Incorporation of MOD 1 by inspecting for MOD A on Rosemount ID Plate." | 501-1890-( ) | |
| ADC-3000 | Service Letter | SL-243 | B | 1/9/2018 | Replacement of ADC-3000 with ADC-4000 | Replacement of ADC-3000 with ADC-4000 | 501-1797-( ), 9200-30000-( ) | |
| ADC-3000 | Service Letter | SL-176 | K | 1/9/2023 | Factory generated tolerance settings of altitude accuracy for certified repair stations. | Provide factory generated tolerance settings of altitude accuracy for certified repair stations. | 501-1797-(), 501-1841-(), 501-1881-(), 501-1890-() 9200-30000 | |
| ADC-3000 | Service Letter | SL-185 | Orig | 1/20/2004 | Inform customers of the Cessna Citation Bravo Series Aircraft of Airdata problem. | 501-1741-( ) | ||
| ADC-3001 | Service Letter | SL-176 | K | 1/9/2023 | Factory generated tolerance settings of altitude accuracy for certified repair stations. | Provide factory generated tolerance settings of altitude accuracy for certified repair stations. | 501-1797-(), 501-1841-(), 501-1881-(), 501-1890-() 9200-30000 | |
| ADC-3100 | Service Letter | SL-176 | K | 1/9/2023 | Factory generated tolerance settings of altitude accuracy for certified repair stations. | Provide factory generated tolerance settings of altitude accuracy for certified repair stations. | 501-1797-(), 501-1841-(), 501-1881-(), 501-1890-() 9200-30000 | |
| ADC-3100 | Service Letter | SL-338 | A | 11/12/2018 | End of Manufacturing Life | Service Letter | 501-1841- | |
| ADC-4000 | Installation Manual | 0040-34401-01 | AE | 5/27/2025 | GH-3900.2, Installation Manual | GH-3900.2 Electronic Standby Instrument System with Release 1.0, 1.1, 1.2, 1.3, 1.4, 1.5, 1.6, 1.7 , 1.8 & 1.9. Includes the ADC-4000 Air Data Computer and MAG-3000 or MAG-3100 Magnetometer. Details on Simulator unit’s P/N 9200-34701-( ) and 9200-34901-( ) are also provided. | 9200-34400-( ) 9200-34500-( ) 9200-34600-( ) 9200-34700-( ) 9200-34800-( ) 9200-34900-( ) 9200-34402-( ) 9200-34502-( ) 9200-34602-( ) 9200-34702-( ) 9200-34802-( ) 9200-34410-( ) | |
| ADC-4000 | Installation Manual | 0040-30001-01 | D | 1/20/2023 | Installation Manual, ADC-4000 | Air Data Computer | 9200-30000 | |
| ADC-4000 | Service Bulletin | SB9200-30000-1 | A | 5/6/2009 | Eliminate spurious faults due to stale data built-in-test failure | , Acron Aviation | 9200-30000-205, 9200-30000-206 | |
| ADC-4000 | Service Bulletin | SB9200-30000-2 | A | 5/3/2010 | Enable automatic recovery when a recoverable fault is detected | , Acron Aviation | ADC-4000 | |
| ADC-4000 | Service Letter | SL-255 | A | 12/22/2015 | ADC-4000 Status Indicator | To provide operational information on ADC-4000 Status Indicator (LED) | 9200-30000 | |
| ADC-4000 | Service Letter | SL-243 | B | 1/9/2018 | Replacement of ADC-3000 with ADC-4000 | Replacement of ADC-3000 with ADC-4000 | 501-1797-( ), 9200-30000-( ) | |
| ADC-4000 | Service Letter | SL-176 | K | 1/9/2023 | Factory generated tolerance settings of altitude accuracy for certified repair stations. | Provide factory generated tolerance settings of altitude accuracy for certified repair stations. | 501-1797-(), 501-1841-(), 501-1881-(), 501-1890-() 9200-30000 | |
| ADI-330 | Component Maintenance Manual | TP-435 | 34-20-33 | 4 | 2/17/2017 | Component Maintenance Manual | Pub# TP-435 | 501-1566-01, 501-1566-02, 501-1566-03, 501-1566-04, 501-1566-05, 501-1566-06, 501-1566-07, 501-1566-08, 501-1566-09, 501-1566-10, 501-1566-11, 501-1566-12, 501-1566-13, 501-1566-14, 501-1566-15, 501-1566-16, 501-1566-17, 501-1566-18, 501-1566-19, 501-1566-20, 501-1566-21 |
| ADI-330 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 2 | 9/26/2024 | Component Maintenance Manual | Rotor Housing Assemblies Manual contains repair information for JET commercial rotor assemblies. | 502-1015-01, 502-1015-02, 502-1025-04, 502-1044-01, 502-1044-02, 502-1153-04, 502-1154-07, 502-1154-08, 502-1177-01, 502-1177-04, 502-1177-07, 502-1177-08, 502-1177-11, 502-1177-12, 502-1177-13, 502-1177-15, 502-1241-02, 502-1253-01, 502-1378-01, 502-1378-04, 502-1378-06, 502-1449-01, 502-1490-01 |
| ADI-330 | Installation Manual | TP-434 | 34-20-29 | A | 8/23/2017 | Installation and Operation Manual | Pub# TP-434 | 501-1566-01, 501-1566-02, 501-1566-03, 501-1566-04, 501-1566-05, 501-1566-06, 501-1566-07, 501-1566-08, 501-1566-09, 501-1566-10, 501-1566-11, 501-1566-12, 501-1566-13, 501-1566-14, 501-1566-15, 501-1566-16, 501-1566-17, 501-1566-18, 501-1566-19, 501-1566-20, 501-1566-21 |
| ADI-330 | Service Bulletin | SB501-1566-1 | B | 9/1/1993 | To prevent possible degradation of flag relay contacts which may result in improper or intermittent flag operation. | 501-1566-01, 501-1566-02, 501-1566-03, 501-1566-04, 501-1566-05, 501-1566-06, 501-1566-07, 501-1566-08, 501-1566-09, 501-1566-10, 501-1566-11, 501-1566-12, 501-1566-13, 501-1566-14, 501-1566-15, 501-1566-16, 501-1566-19 | ||
| ADI-330 | Service Bulletin | SB501-1566-2 | A | 1/1/1995 | MOD 5 prevents possible intermittent flags due of over voltage conditions at the input to the attitude indicator. | 501-1566-() | ||
| ADI-330 | Service Bulletin | SB501-1566-3 | Orig | 7/1/1997 | To replace caging shaft with stronger, standardized part on the 502-1380-() indicator assemblies. | GYRO | 501-1566-() | |
| ADI-330 | Service Bulletin | SB501-1566-4 | Orig | 1/1/1999 | To prevent loss of caging shaft retaining rings. | 501-1566-() | ||
| ADI-330 | Service Bulletin | SB501-1566-5 | Orig | 7/19/2002 | Reduce possibility of gear slippage. | 501-1566-() | ||
| ADI-330 | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| ADI-331 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 2 | 9/26/2024 | Component Maintenance Manual | Rotor Housing Assemblies Manual contains repair information for JET commercial rotor assemblies. | 502-1015-01, 502-1015-02, 502-1025-04, 502-1044-01, 502-1044-02, 502-1153-04, 502-1154-07, 502-1154-08, 502-1177-01, 502-1177-04, 502-1177-07, 502-1177-08, 502-1177-11, 502-1177-12, 502-1177-13, 502-1177-15, 502-1241-02, 502-1253-01, 502-1378-01, 502-1378-04, 502-1378-06, 502-1449-01, 502-1490-01 |
| ADI-331 | Component Maintenance Manual | TP-438 | 34-20-35 | B | 1/13/2025 | Component Maintenance Manual | JET® Attitude Indicator | 501-1567-01, 501-1567-02, 501-1567-03, 501-1567-04, 501-1567-05, 501-1567-06, 501-1567-07, 501-1567-08, 501-1567-09, 501-1567-10, 501-1567-11, 501-1567-12, 501-1567-13, 501-1567-14 |
| ADI-331 | Installation Manual | TP-437 | A | 8/31/2003 | Installation and Operation Manual | Pub# TP-437 | 501-1567-01, 501-1567-02, 501-1567-03, 501-1567-04, 501-1567-05, 501-1567-06, 501-1567-07, 501-1567-08, 501-1567-09, 501-1567-10, 501-1567-11, 501-1567-12, 501-1567-13, 501-1567-14 | |
| ADI-331 | Service Bulletin | SB501-1567-1 | Orig | 9/1/1999 | To prevent possible undesirable flag and pointer activity caused by induced noise upon activation of power failure flag switching circuit when caging the indicator. | 501-1567-( ) | ||
| ADI-331 | Service Bulletin | SB501-1567-2 | Orig | 2/1/1997 | To replace caging shaft with stronger, standardized part on the 502-1381-01 indicator assembly. | 501-1567-( ) | ||
| ADI-331 | Service Bulletin | SB501-1567-3 | Orig | 1/8/1999 | Incorporation of MOD 4 by cutting pads joining leads of A2L5. Change restores EMI protection to qualified configuration. | 501-1567-( ) | ||
| ADI-331 | Service Bulletin | SB501-1567-5 | Orig | 6/16/2002 | Reduce possibility of Gear slippage by the incorporation of MOD 4 or 5 (model dependant) by replacing Face Gear P/N: 571-1550-01 with P/N: 571-1741-01. | 501-1567-( ) | ||
| ADI-331 | Service Bulletin | SB501-1567-6 | B | 10/23/2009 | Incorporation of MOD 5 or 6 (dependant on unit part number) to prevent spurious Watchdog Interrupts, which causes G/S andILS Flags to flutter | 501-12567-( ) | ||
| ADI-331 | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| ADI-332 | Component Maintenance Manual | TP-459 | 34-20-41 | A | 12/6/2018 | Component Maintenance Manual | Pub# TP-459 | 501-1656-01, 501-1656-02, 501-1656-03, 501-1656-04, 501-1656-05 |
| ADI-332 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 2 | 9/26/2024 | Component Maintenance Manual | Rotor Housing Assemblies Manual contains repair information for JET commercial rotor assemblies. | 502-1015-01, 502-1015-02, 502-1025-04, 502-1044-01, 502-1044-02, 502-1153-04, 502-1154-07, 502-1154-08, 502-1177-01, 502-1177-04, 502-1177-07, 502-1177-08, 502-1177-11, 502-1177-12, 502-1177-13, 502-1177-15, 502-1241-02, 502-1253-01, 502-1378-01, 502-1378-04, 502-1378-06, 502-1449-01, 502-1490-01 |
| ADI-332 | Installation Manual | TP-458 | 34-20-40 | Reis | 3/19/1998 | Installation and Operation Manual | Pub# TP-458 | 501-1656-01, 501-1656-02, 501-1656-03, 501-1656-04, 501-1656-05 |
| ADI-332 | Service Bulletin | SB501-1656-1 | B | 8/1/1995 | Mod 1 prevents possible degradation of flag relay contacts, which may result in improper or intermittent flag operation. Mod 2 prevents possible degradation of back course engage relay contacts, which may result when switching from back course mode annunc | 501-1656-( ) | ||
| ADI-332 | Service Bulletin | SB501-1656-2 | A | 8/1/1995 | Mod 3 prevents a possible short circuit condition between Meter Switching Circuit Card Assembly (A8) power ground and housing and plate assembly, which may cause undesirable chassis ground connections. | 501-1656-( ) | ||
| ADI-332 | Service Bulletin | SB501-1656-3 | A | 8/1/1995 | Mod 5 prevents possible intermittent flags due to over voltage conditions at the input to the attitude indicator. | 501-1656-( ) | ||
| ADI-332 | Service Bulletin | SB501-1656-4 | Orig | 6/1/1995 | Mod 4 prevents possible failure of the ILS function switch and bracket assembly because of switch damage or shaft separation, which is normally caused by excessive force on the ILS function knob during ILS mode selection. | 501-1656-( ) | ||
| ADI-332 | Service Bulletin | SB501-1656-5 | Orig | 2/1/1997 | To replace caging shaft with stronger, standardized part on the 502-1413-01 thru -04 indicator assemblies. | 501-1656-( ) | ||
| ADI-332 | Service Bulletin | SB501-1656-6 | A | 1/22/2003 | To prevent loss of caging shaft retaining rings. | 501-1656-( ) | ||
| ADI-332 | Service Bulletin | SB501-1656-7 | Orig | 3/14/2003 | Reduce possibility of gear slippage. | 501-1656-( ), 501-1656-01, 501-1656-02, 501-1656-03, 501-1656-04, 501-1656-05 | ||
| ADI-332 | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| ADI-333 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 2 | 9/26/2024 | Component Maintenance Manual | Rotor Housing Assemblies Manual contains repair information for JET commercial rotor assemblies. | 502-1015-01, 502-1015-02, 502-1025-04, 502-1044-01, 502-1044-02, 502-1153-04, 502-1154-07, 502-1154-08, 502-1177-01, 502-1177-04, 502-1177-07, 502-1177-08, 502-1177-11, 502-1177-12, 502-1177-13, 502-1177-15, 502-1241-02, 502-1253-01, 502-1378-01, 502-1378-04, 502-1378-06, 502-1449-01, 502-1490-01 |
| ADI-333 | Component Maintenance Manual | TP-512 | 34-20-62 | A-4 | 2/20/2017 | Component Maintenance Manual, 501-1657-02 | ADI-333B | 501-1657-02 |
| ADI-333 | Component Maintenance Manual | TP-446 | 34-20-37 | 2 | 8/13/2018 | Component Maintenance Manual, 501-1657-01 | ADI-333A | 501-1657-01 |
| ADI-333 | Installation Manual | TP-445 | 34-20-67 | A | 12/23/2005 | Installation and Operation Manual, 501-1657-( ) | ADI-333A, ADI-333B | 501-1657-01, 501-1657-02 |
| ADI-333 | Intermediate Maintenance Manual | TP-639 | 24-20-76 | A | 7/16/2012 | intermediate Maintenance Manual, ADI-333B | Bench level test. No open box repair information. ADI-333B | 501-1657-02 |
| ADI-333 | Pilot Guide | TP-444 | C | 12/23/2005 | Pilot's Guide | Pub# TP-444 | 501-1657-02 | |
| ADI-333 | Service Bulletin | SB501-1567-4 | Orig | 6/16/2002 | To prevent loss of caging shaft retaining rings. | 501-1567-02, 501-1567-10 | ||
| ADI-333 | Service Bulletin | SB501-1657-2 | B | 1/22/2003 | To replace the caging shaft with stronger, standardized part on indicator assembly (P/N 502-1414-01). | 501-1657-01 | ||
| ADI-333 | Service Bulletin | SB501-1657-3 | A | 9/6/2002 | To prevent loss of caging shaft retaining ring. | 501-1657-01, 501-1657-02 | ||
| ADI-333 | Service Bulletin | SB501-1657-4 | B | 1/22/2003 | Reduce possibility of bearing damaging sphere housing. | 501-1657-02 | ||
| ADI-333 | Service Bulletin | SB501-1657-5 | A | 9/22/2003 | Improve gear tooth engagement to reduce occurrence of slipped Spheres. | 501-1657-02 | ||
| ADI-333 | Service Bulletin | SB501-1657-6 | B | 7/20/2009 | To reduce oscillation on the 15V and 5V power supplies. | 501-1657-02 | ||
| ADI-333 | Service Bulletin | SB501-1657-7 | Orig | 9/24/2003 | Improve gear tooth engagement to reduce occurrence of slipped Spheres and to ensure that the screws are replaced to prevent them from backing out. | 501-1657-02 | ||
| ADI-333 | Service Bulletin | SB501-1657-8 | B | 10/23/2009 | Incorporation of MOD 4 to prevent spurious Watchdog Interrupts, which causes G/S andILS Flags to flutter | 501-1657-01 | ||
| ADI-333 | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| ADI-333 | Service Letter | SL-208 | A | 5/24/2006 | To provide instructions for replacing caution label. | To provide instructions for replacing caution label. | 501-1657-02 | |
| ADI-333 | Service Letter | SL-217 | A | 1/2/2007 | To provide a means of monitoring temperature of units in the field and to provide guidance of the location of the temperature tag. | 501-1657-02 | ||
| ADI-334 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 2 | 9/26/2024 | Component Maintenance Manual | Rotor Housing Assemblies Manual contains repair information for JET commercial rotor assemblies. | 502-1015-01, 502-1015-02, 502-1025-04, 502-1044-01, 502-1044-02, 502-1153-04, 502-1154-07, 502-1154-08, 502-1177-01, 502-1177-04, 502-1177-07, 502-1177-08, 502-1177-11, 502-1177-12, 502-1177-13, 502-1177-15, 502-1241-02, 502-1253-01, 502-1378-01, 502-1378-04, 502-1378-06, 502-1449-01, 502-1490-01 |
| ADI-334 | Installation Manual | TP-477 | 34-20-52 | Reis | 8/15/1994 | Installation and Operation Manual | Pub# TP-477 | 501-1704-01, 501-1704-02, 501-1704-03, 501-1704-04 |
| ADI-334 | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| ADI-335 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 2 | 9/26/2024 | Component Maintenance Manual | Rotor Housing Assemblies Manual contains repair information for JET commercial rotor assemblies. | 502-1015-01, 502-1015-02, 502-1025-04, 502-1044-01, 502-1044-02, 502-1153-04, 502-1154-07, 502-1154-08, 502-1177-01, 502-1177-04, 502-1177-07, 502-1177-08, 502-1177-11, 502-1177-12, 502-1177-13, 502-1177-15, 502-1241-02, 502-1253-01, 502-1378-01, 502-1378-04, 502-1378-06, 502-1449-01, 502-1490-01 |
| ADI-335 | Installation Manual | TP-490 | 34-20-49 | C | 11/24/2010 | Installation and Operation Manual | Pub# TP-490 | 501-1753-01, 501-1753-02, 501-1753-03, 501-1753-04, 501-1753-05, 501-1753-06, 501-1753-07, 501-1753-08, 501-1753-09, 501-1753-10, 501-1753-11, 501-1753-12, 501-1753-13, 501-1753-14, 501-1753-15, 501-1753-16, 501-1753-17, 501-1753-18 |
| ADI-335 | Pilot Guide | TP-493 | B | 1/27/2005 | Pilot's Guide | Pub# TP-493 | 501-1753-01, 501-1753-02, 501-1753-03, 501-1753-04, 501-1753-05, 501-1753-06, 501-1753-07, 501-1753-08, 501-1753-09, 501-1753-10 | |
| ADI-335 | Service Bulletin | SB501-1753-1 | Orig | 5/1/1997 | Manufacturers discontinuation of the (A-K) light sensitive resistor in auto dimming control of display brightness. | 501-1753-( ) | ||
| ADI-335 | Service Bulletin | SB501-1753-2 | Orig | 5/1/1997 | Provide the proper operation of DME (A-K) hold function when unit is operated with scanning DME in conjunction with ARINC output type equipment. | 501-1753-( ) | ||
| ADI-335 | Service Bulletin | SB501-1753-3 | Orig | 5/22/2001 | Change caging shaft for increased strength. | 501-1753-( ) | ||
| ADI-335 | Service Bulletin | SB501-1753-4 | Orig | 5/22/2001 | Prevent possible undesirable flag/pointer activity caused by induced noise upon activation of power failure flag switching circuit when caging indicator. | 501-1753-( ) | ||
| ADI-335 | Service Bulletin | SB501-1753-5 | B | 1/23/2008 | Replace possibility of gear slippage MOD 6 | Replace possibility of gear slippage | 501-1753-01, 501-1753-02, 501-1753-03, 501-1753-04, 501-1753-05, 501-1753-06, 501-1753-07, 501-1753-08, 501-1753-09, 501-1753-10, 501-1753-11, 501-1753-12, 501-1753-13, 501-1753-14, 501-1753-15, 501-1753-16, 501-1753-17, 501-1753-18 | |
| ADI-335 | Service Bulletin | SB501-1753-6 | A | 1/23/2008 | Limited quantity of non-conforming parts | Limited quantity of non-conforming parts | 501-1753-04 | |
| ADI-335 | Service Letter | SL-163 | A | 12/14/2004 | To provide flight personnel with general information concerning operation of AI/ADI-33 (X) Attitude Indicators. | To provide flight personnel with general information concerning operation of AI/ADI-33 (X) Attitude Indicators. | 501- | |
| ADI-335 | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| ADI-350 | Component Maintenance Manual | TP-442 | 34-20-34 | 2 | 6/27/2018 | Component Maintenance Manual, 501-1617-01 | Pub# TP-442 | 406-375-220-101, 501-1617-01 |
| ADI-350 | Component Maintenance Manual | TP-545 | A C1 | 9/3/2002 | Maintenance Manual with IPL, 501-1742-01 | Pub# TP-545 | 501-1742-01 | |
| ADI-350 | Component Maintenance Manual | TP-403 | 34-20-22 | Orig | 9/1/1986 | Intermediate Maintenance Manual, 501-1442-01 | Pub# TP-403 | 501-1442-01 |
| ADI-350 | Component Maintenance Manual | TP-390 | 34-20-10 | Orig | 12/1/1983 | Maintenance Manual with IPL, 501-1284-01 | Pub# TP-390 | 501-1284-01 |
| ADI-350 | Component Maintenance Manual | TP-220 | 34-20-11 | Orig | 5/22/1985 | Operation, Installation, and Maintenance Manual | Pub# TP-220 | 501-1243-01, 501-1458-01 |
| ADI-350 | Installation Manual | TP-532 | B C1 | 8/30/2002 | Installation and Operation Manual, 501-1809-01 | Pub# TP-532 | 501-1809-01 | |
| ADI-350 | Pilot Guide | TP-271 | A | 1/31/2005 | Pilot's Guide | Pub# TP-271 | 501-1218-01, 501-1277-01, 501-1278-01, 501-1442-01, 501-1598-01 | |
| ADI-350 | Pilot Guide | TP-272 | A | 2/1/2005 | Pilot's Guide | Pub# TP-272 | 501-1230-01, 501-1519-01, 501-1583-01 | |
| ADI-350 | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| ADLP - software | Instruction Manual | 165E3596-03 | 02 | 4/12/2024 | ADLP Software v3.6, v3.7 Operator's Manual | Operator's Manual for ADLP software version 3.6 & 3.7 | 17TES0436 | |
| ADLP - software | Service Bulletin | SB005-ADLP | 00 | 4/12/2024 | ADLP Software v3.7 Release | ADLP Software v3.7 Release Service Bulletin, Acron Aviation | 17TES0436 | |
| AFIRS 228S - Iridium | Component Maintenance Manual | 165E5733-10 | 23-28-01 | 09 | 12/12/2023 | AFIRS 228S Iridium CMM | Level 1 Maintenance | 228E5733-00, 228E5733-01, 418E5733-00, 418E5733-01 |
| AFIRS 228S - Iridium | Installation Manual | 165E5733-02 | D | 12/12/2023 | AFIRS 228S Installation Manual for A220 Series | For A220 Series A/C | 418E5733-01, 228E5733-00, 228E5733-01, 418E5733-00 | |
| AFIRS 228S - Iridium | Installation Manual | 165E5733-00 | 06 | 12/12/2023 | AFIRS 228S Installation Manual for A320/A330 | For A320/A330 Series A/C | 228E5733-00, 228E5733-01, 23-28-01, 418E5733-00 | |
| AFIRS 228S - Iridium | Instruction Manual | 165E5733-21 | B | 11/30/2022 | AFIRS 228S Welcome Package and Quick Start Guide for A220 Series | A220 Series Aircraft. Welcome Package and Quick Start Guide | 228E5733-00 | |
| AFIRS 228S - Iridium | Instruction Manual | 165E5733-20 | 03 | 11/30/2022 | AFIRS 228S Welcome Package and Quick Start Guide for A320/A320 Series | A320/A320 Series Aircraft. Welcome Package and Quick Start Guide | 228E5733-00, 418E5733-00, SDU Configuration Module | |
| AFIRS 228S - Iridium | Pilot Guide | 165E5733-41 | A | 5/28/2019 | AFIRS 228S Pilot’s Guide for A220 Series | For A220 Series A/C | 418E5733-01, 228E5733-00 | |
| AFIRS 228S - Iridium | Service Bulletin | SB010-Iridium | SDU228-23-0005 | 01 | 6/5/2024 | SDU Part Number Conversion to 228E5733-01 ADMT B, Repair Station Only | SDU Part Number Conversion to 228E5733-01 ADMT B, Acron Aviation | 228E5733-01 |
| AFIRS 228S - Iridium | Service Bulletin | Iridium-SB001 | 23-28-01-001AB | 00 | 7/11/2016 | Software Revision 17 | Software Revision 17, Acron Aviation | 228E5733-00 |
| AFIRS 228S - Iridium | Service Bulletin | Iridium-SB002 | 23-28-01-002AB | 07 | 5/11/2018 | MOD 1. fix several field issues | MOD 1, Acron Aviation | 228E5733-00 |
| AFIRS 228S - Iridium | Service Bulletin | Iridium-SB004 | 00 | 8/20/2019 | SDU functionality , Repair Station Only | ADMT D To increase SDU functionality by adding simultaneous transmission of voice and data. This SB no longer applies to new production units since there has been a revision change from -00 to -01. Repairs are still possible. | 228E5733-00 | |
| AFIRS 228S - Iridium | Service Bulletin | Iridium-SB003 | 23-28-01-003AB | 00 | 9/23/2019 | Software (OFP) 840E5733-18 | Software Revision 18, Acron Aviation | 228E5733-00 |
| AFIRS 228S - Iridium | Service Bulletin | SB005-Iridium | SDU-23-0000 | 00 | 9/30/2020 | Remove and Replace Data Modem Instructions, Repair station only | Remove and Replace Data Modem Instructions. | 228E5733-00 |
| AFIRS 228S - Iridium | Service Bulletin | SB006-Iridium | SDU228-23-0002 | 05 | 9/5/2023 | Software (OFP) 840E5733-20 | Customer notification of Software 20. Acron Aviation | 228E5733-00, 228E5733-01 |
| AFIRS 228S - Iridium | Service Bulletin | SB008-Iridium | SDU228-23-0001 | 06 | 9/1/2023 | Introduction to New Iridium SDU Part Number 228E5733-01 and -01 AMDT A | Introduction to New Iridium SDU Part Number 228E5733-01 and -01 AMDT A ( Iridium), Acron Aviation | 228E5733-00, 228E5733-01, 228E5733-01 AMDT A, |
| AFIRS 228S - Iridium | Service Bulletin | SB009-Iridium | SDU228-23-0004 | 01 | 9/6/2022 | SDU Part Number Conversion to 228E5733-01 ADMT A, Repair Station Only | SDU Part Number Conversion to 228E5733-01 ADMT A, Acron Aviation | 228E5733-00, 228E5733-01 |
| AFIRS 228S - Iridium | Software | 840E5733-20 | 0 | 5/25/2021 | Software for hardware PN 228E5733-01 | Operation SW 20 | 228E5733-01 | |
| AFIRS 228S - Iridium | Software | 840E5733-20 | 00 | 5/25/2021 | 840-E5733-20 | Operation Software 20 | 228E5733-01 | |
| AI-330 | Component Maintenance Manual | TP-431 | 34-20-27 | A ch | 5/14/2019 | Component Maintenance Manual | 501-1568-01, 501-1568-02, 501-1568-03, 501-1568-04, 501-1568-05, 501-1568-06, 501-1568-07, 501-1568-08, 501-1568-09, 501-1568-10, 501-1568-11, 501-1568-12, 501-1568-13, 501-1568-15, 501-1568-21, 501-1568-28, 501-1568-30, 501-1568-33, 501-1568-34, 501-1568-38, 501-1568-40, 501-1568-43 | |
| AI-330 | Component Maintenance Manual | TP-450 | 34-20-38 | B | 5/15/2018 | Component Maintenance Manual | Pub# TP-450 | 501-1568-14, 501-1568-16, 501-1568-17, 501-1568-18, 501-1568-19, 501-1568-20, 501-1568-22, 501-1568-24, 501-1568-26, 501-1568-27, 501-1568-39, 501-1568-41, 501-1568-47, 501-1568-51, 501-1568-55, 501-1568-57, 501-1568-58 |
| AI-330 | Component Maintenance Manual | TP-488 | 34-20-48 | A C1 | 4/3/2018 | Component Maintenance Manual | Pub# TP-488 | 501-1568-29, 501-1568-44 |
| AI-330 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 2 | 9/26/2024 | Component Maintenance Manual | Rotor Housing Assemblies Manual contains repair information for JET commercial rotor assemblies. | 502-1015-01, 502-1015-02, 502-1025-04, 502-1044-01, 502-1044-02, 502-1153-04, 502-1154-07, 502-1154-08, 502-1177-01, 502-1177-04, 502-1177-07, 502-1177-08, 502-1177-11, 502-1177-12, 502-1177-13, 502-1177-15, 502-1241-02, 502-1253-01, 502-1378-01, 502-1378-04, 502-1378-06, 502-1449-01, 502-1490-01 |
| AI-330 | Drawings / SPEC | JET SPECIFICATION 579 | F | 8/28/1995 | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Gyro - general | |
| AI-330 | Installation Manual | TP-454 | 34-20-51 | C | 2/5/2018 | Installation and Operation Manual | Pub# TP-454 | 501-1568-01, 501-1568-02, 501-1568-03, 501-1568-04, 501-1568-05, 501-1568-06, 501-1568-07, 501-1568-08, 501-1568-09, 501-1568-10, 501-1568-11, 501-1568-12, 501-1568-13, 501-1568-14, 501-1568-15, 501-1568-16, 501-1568-17, 501-1568-18, 501-1568-19, 501-1568-20, 501-1568-21, 501-1568-22, 501-1568-24, 501-1568-25, 501-1568-26, 501-1568-27, 501-1568-28, 501-1568-29, 501-1568-30, 501-1568-31, 501-1568-33, 501-1568-34, 501-1568-37, 501-1568-38, 501-1568-39, 501-1568-40, 501-1568-41, 501-1568-43, 501-1568-44, 501-1568-45, 501-1568-46, 501-1568-47, 501-1568-48, 501-1568-49, 501-1568-51, 501-1568-54, 501-1568-55, 501-1568-56 |
| AI-330 | Installation Manual | TP-480 | 34-20-54 | A | 4/3/2018 | Installation and Operation Manual | Pub# TP-480 | 501-1568-29, 501-1568-44 |
| AI-330 | Pilot Guide | TP-573 | D | 2/5/2018 | Pilot's Guide | Pub# TP-573 | 501-1568-() | |
| AI-330 | Service Bulletin | SB501-1568-1 | D | 10/11/1999 | To prevent intermittent flags due to overvoltage condition. | 501-1568-( ) | ||
| AI-330 | Service Bulletin | SB501-1568-2 | A | 5/1/1997 | To replace caging shaft with stronger, standardized part on the 502-1364-( ) and 502-1448-( ) indicator assemlbies. | 501-1568-( ) | ||
| AI-330 | Service Bulletin | SB501-1568-10 | A | 12/26/2007 | Planning Information | 501-1568-01, 501-1568-28 | ||
| AI-330 | Service Bulletin | SB501-1568-10 | A | 12/13/2007 | Limited Quantity of non-conforming parts | 501-1568-01, 501-1568-28 | ||
| AI-330 | Service Bulletin | SB501-1568-3 | C | 3/14/2003 | To prevent loss of caging shaft retaining rings. | 501-1568-( ) | ||
| AI-330 | Service Bulletin | SB501-1568-4 | A | 5/1/2001 | To reduce tendency of erector weight to stick. | 501-1568-48 | ||
| AI-330 | Service Bulletin | SB501-1568-5 | A | 9/15/2011 | Incorporation ID plates with bar code information. | 501-1568-34 | ||
| AI-330 | Service Bulletin | SB501-1568-6 | Orig | 5/1/2001 | Improve reliability of erection system. | 501-1568-48 | ||
| AI-330 | Service Bulletin | SB501-1568-7 | A | 7/19/2002 | To improve paint adhesion. | 501-1568-28, 501-1568-56 | ||
| AI-330 | Service Bulletin | SB501-1568-8 | Orig | 7/19/2002 | Remove lacquer paint from bezel and knob to eliminate peeling paint during tape test. | 501-1568-28, 501-1568-56 | ||
| AI-330 | Service Bulletin | SB501-1568-9 | Orig | 7/19/2002 | Reduce possibility of gear slippage. | 501-1568-() | ||
| AI-330 | Service Bulletin | SB501-1657-1 | A | 1/22/2003 | To prevent switch damage and shaft separation. | To prevent switch damage and shaft separation. | 501-1657-01 | |
| AI-330 | Service Letter | SL-163 | A | 12/14/2004 | To provide flight personnel with general information concerning operation of AI/ADI-33 (X) Attitude Indicators. | To provide flight personnel with general information concerning operation of AI/ADI-33 (X) Attitude Indicators. | 501- | |
| AI-330 | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| AI-330 | Supplemental Type Certificate | SA5852NM | Reis | 1/25/1993 | Installation of a BFGoodrich Jet Electronics AI-330 standby altitude indicator. | Installation of a BFGoodrich Jet Electronics AI-330 standby altitude indicator. | ||
| AI-330 | Supplemental Type Certificate | SA5853NM | Reis | 12/11/1992 | Installation of a BF Goodrich Jet electronics AI-330 standby attitude indicator. | Installation of a BF Goodrich Jet electronics AI-330 standby attitude indicator. | ||
| AI-330 | Supplemental Type Certificate | SA7083NM | Orig | 4/22/1994 | Installation of BF Goodrich Aerospace, Jet Electronics and Technology Inc. Model AI-330 standby attitude indicator and associated indicator power supply. | Installation of BF Goodrich Aerospace, Jet Electronics and Technology Inc. Model AI-330 standby attitude indicator and associated indicator power supply. | ||
| AI-330 | Supplemental Type Certificate | SA8044NM | Orig | 12/15/1994 | Installation of BF Goodrich, Jet Electronics Model AI-330 standby indicator | Installation of BF Goodrich, Jet Electronics Model AI-330 standby indicator | ||
| AI-330 | Supplemental Type Certificate | SA97-25 | Orig | 2/6/1997 | Installation of BF Goodrich Aerospace, Jet Electronics and Technology Inc. Model AI-330 standby attitude indicator and associated indicator power supply. | Installation of BF Goodrich Aerospace, Jet Electronics and Technology Inc. Model AI-330 standby attitude indicator and associated indicator power supply. | ||
| AI-330 | Supplemental Type Certificate | SA5853NM | Orig | 4/10/1995 | Installation of Jet Electronics and Technology Inc. AI-330 Standby Indicator. | Installation of Jet Electronics and Technology Inc. AI-330 Standby Indicator. | ||
| AI-340 | Component Maintenance Manual | TP-423 | 34-20-25 | 2C1 | 9/10/2014 | AI-340 B & C CMM | AI-340 B & C CMM | 501-1539, 501-1539-01, 501-1539-02 |
| AI-340 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 2 | 9/26/2024 | Component Maintenance Manual | Rotor Housing Assemblies Manual contains repair information for JET commercial rotor assemblies. | 502-1015-01, 502-1015-02, 502-1025-04, 502-1044-01, 502-1044-02, 502-1153-04, 502-1154-07, 502-1154-08, 502-1177-01, 502-1177-04, 502-1177-07, 502-1177-08, 502-1177-11, 502-1177-12, 502-1177-13, 502-1177-15, 502-1241-02, 502-1253-01, 502-1378-01, 502-1378-04, 502-1378-06, 502-1449-01, 502-1490-01 |
| AI-340 | Drawings / SPEC | JET SPECIFICATION 579 | F | 8/28/1995 | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Gyro - general | |
| AI-340 | Installation Manual | TP-441 | 34-20-32 | Reis | 5/20/1995 | Installation and Operation Manual | Pub# TP-441 | 501-1539-01, 501-1539-02 |
| AI-340 | Service Bulletin | SB501-1539-1 | A | 4/13/1994 | Reduce roll slip ring and brush block current | Reduce roll slip ring and brush block current | 501-1539, 501-1539-01, 501-1539-02 | |
| AI-340 | Service Bulletin | SB501-1539-2 | Ori | 9/11/1995 | To prevent possible interference between lighting wedge and inclinometer | 501-1539, 501-1539-01, 501-1539-02 | ||
| AI-340 | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| AI-350 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 2 | 9/26/2024 | Component Maintenance Manual | Rotor Housing Assemblies Manual contains repair information for JET commercial rotor assemblies. | 502-1015-01, 502-1015-02, 502-1025-04, 502-1044-01, 502-1044-02, 502-1153-04, 502-1154-07, 502-1154-08, 502-1177-01, 502-1177-04, 502-1177-07, 502-1177-08, 502-1177-11, 502-1177-12, 502-1177-13, 502-1177-15, 502-1241-02, 502-1253-01, 502-1378-01, 502-1378-04, 502-1378-06, 502-1449-01, 502-1490-01 |
| AI-350 | Component Maintenance Manual | TP-482 | 34-20-46 | A | 4/17/2018 | Component Maintenance Manual | Pub# TP-482 | 501-1745-01 |
| AI-350 | Component Maintenance Manual | TP-543 | B | 4/3/2018 | Maintenance Manual with IPL | Pub# TP-543 | 501-1833-01, 501-1856-01, 501-1861-01 | |
| AI-350 | Component Maintenance Manual | TP-673 | A1 | 6/27/2018 | Maintenance Manual | Pub#TP-673 | 501-1757-01, 501-1790-01 | |
| AI-350 | Component Maintenance Manual | TP-674 | A2 | 12/3/2024 | Maintenance Manual | Pub#TP-674 | 501-1817-01, 501-1817-02 | |
| AI-350 | Drawings / SPEC | JET SPECIFICATION 579 | F | 8/28/1995 | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Gyro - general | |
| AI-350 | Installation Manual | TP-507 | 34-20-63 | Orig | 10/31/1996 | Installation and Operations Manual | Pub# TP-507 | 501-1790-01 |
| AI-350 | Installation Manual | TP-514 | 34-20-65 | A | 9/15/2004 | Installation and Operation Manual | Pub# TP-514 | 501-1817-01, 501-1817-02 |
| AI-350 | Installation Manual | TP-595 | A | 12/19/2003 | Installation and Operation Manual | Pub# TP-595 | 501-1833-03 | |
| AI-350 | Installation Manual | TP-596 | A | 12/19/2003 | Installation and Operation Manual | Pub# TP-596 | 501-1757-01 | |
| AI-350 | Service Bulletin | SB501-1757-1 | Orig | 7/24/2000 | Reduce the possibility of bearing damaging sphere housing. | 501-1757-01 | ||
| AI-350 | Service Bulletin | SB501-1757-2 | Orig | 9/6/2002 | Reduce possibility of gear slippage. | 501-1757-01, 501-1757-02, 501-1757-03 | ||
| AI-350 | Service Bulletin | SB501-1790-1 | Orig | 7/1/2000 | Reduce the possibility of bearing damaging sphere housing. | 501-1790-01 | ||
| AI-350 | Service Bulletin | SB501-1817-1 | Orig | 7/1/2000 | Reduce the possibility of bearing damaging sphere housing. | 501-1817-01 | ||
| AI-350 | Service Bulletin | SB501-1817-2 | Orig | 6/11/2002 | Improve gear tooth engagement to reduce occurrence of slipped spheres. | 501-1817-01 | ||
| AI-350 | Service Bulletin | SB501-1817-3 | B | 7/14/2005 | To reduce the possibilty of stress craking of erection switches during temperature extremes an adhesive is being used to secure leads. | 501-1817-01, 501-1817-02 | ||
| AI-350 | Service Bulletin | SB501-1745-1 | Orig | 12/1/1996 | To replace caging shaft with stronger, standardized part on the 502-1457-01 indicator assembly. | 501-1745-01 | ||
| AI-350 | Service Bulletin | SB501-1745-2 | Orig | 7/25/2003 | Reduce possibility of gear slippage. | 501-1745-01 | ||
| AI-350 | Service Bulletin | SB501-1856-01 | A | 1/23/2012 | Reduce the possibility of bearing damaging sphere housing. | 501-1856-01 | ||
| AI-350 | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| AI-360 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 2 | 9/26/2024 | Component Maintenance Manual | Rotor Housing Assemblies Manual contains repair information for JET commercial rotor assemblies. | 502-1015-01, 502-1015-02, 502-1025-04, 502-1044-01, 502-1044-02, 502-1153-04, 502-1154-07, 502-1154-08, 502-1177-01, 502-1177-04, 502-1177-07, 502-1177-08, 502-1177-11, 502-1177-12, 502-1177-13, 502-1177-15, 502-1241-02, 502-1253-01, 502-1378-01, 502-1378-04, 502-1378-06, 502-1449-01, 502-1490-01 |
| AI-360 | Drawings / SPEC | JET SPECIFICATION 579 | F | 8/28/1995 | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Gyro - general | |
| AI-360 | Installation Manual | TP-564 | E | 7/12/2007 | Installation and Operation Manual | TP-564 | 501-1874-( ), 501-1874-01, 501-1874-02, 501-1874-03, 501-1874-04, 501-1874-05, 501-1874-06, 501-1874-08, 501-1874-09, 501-1874-10, 501-1874-11, 501-1874-14, 501-1874-16, 501-1874-17 | |
| AI-360 | Installation Manual | TP-625 | A | 11/10/2006 | Installation and Operation Manual | J.E.T.® Model AI-360 With NVIS Lighting | 501-1874-( ), 501-1874-12, 501-1874-13, 501-1874-15 | |
| AI-360 | Pilot Guide | TP-565 | E | 1/26/2005 | Pilot's Guide | Pub# TP-565 | 501-1874-() | |
| AI-360 | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| AI-360 | Service Letter | SIL-001-AI-360 | 00 | 11/25/2024 | Service Information Letter | To inform customers that the AI-360 has reached manufacturing end of life and will no longer be available for sale. | 501-1874-xx 501-1874-01 501-1874-06 501-1874-14 501-1874-02 501-1874-08 501-1874-16 501-1874-03 501-1874-09 501-1874-17 501-1874-04 501-1874-10 501-1874-05 501-1874-11 501-1874-12 501-1874-13 501-1874-15 | |
| AI-803 | Component Maintenance Manual | TP-513 | 34-20-64 | A C3 | 2/10/2016 | Component Maintenance Manual | Changed from ITAR to EAR | 501-1674-01 |
| AI-803 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 2 | 9/26/2024 | Component Maintenance Manual | Rotor Housing Assemblies Manual contains repair information for JET commercial rotor assemblies. | 502-1015-01, 502-1015-02, 502-1025-04, 502-1044-01, 502-1044-02, 502-1153-04, 502-1154-07, 502-1154-08, 502-1177-01, 502-1177-04, 502-1177-07, 502-1177-08, 502-1177-11, 502-1177-12, 502-1177-13, 502-1177-15, 502-1241-02, 502-1253-01, 502-1378-01, 502-1378-04, 502-1378-06, 502-1449-01, 502-1490-01 |
| AI-803 | Component Maintenance Manual | TP-549 | B1 | 1/24/2019 | Maintenance Manual with IPL | Changed from ITAR to EAR | 501-1857-01 | |
| AI-803 | Component Maintenance Manual | TP-439 | 34-20-31 | 1 | 2/8/2016 | Maintenance Manual | Pub# TP-439 | 501-1647-01 |
| AI-803 | Component Maintenance Manual | TP-380 | 34-20-03 | A C4 | 2/16/2016 | Maintenance Manual | Pub# TP-380 | 501-1131-01, 501-1131-02, 501-1219-01, 501-1386-01, 501-1423-01, 501-1646-01 |
| AI-803 | Component Maintenance Manual | TP-601 | B | 2/25/2016 | Maintenance Manual with IPL | Pub# TP-601 | 501-1845-01 | |
| AI-803 | Component Maintenance Manual | TP-548 | B C1 | 2/10/2016 | AI-803BG Maintenance Manual | 501-1604-03 | ||
| AI-803 | Component Maintenance Manual | TP-677 | A | 3/16/2016 | CMM for AI-803V | CMM for AI-803V | 501-1239-51 | |
| AI-803 | Component Maintenance Manual | TP-678 | A | 3/23/2016 | CMM for AI-803CG | CMM for AI-803CG | 501-1646-02 | |
| AI-803 | Component Maintenance Manual | TP-679 | A | 3/23/2016 | CMM fo AI-803CJ | CMM fo AI-803CJ | 501-1795-01 | |
| AI-803 | Component Maintenance Manual | TP-681 | A | 5/31/2016 | AI-803DF | 501-1893-01 | ||
| AI-803 | Component Maintenance Manual | TP-680 | A | 5/31/2016 | AI-803DA CMM | AI-803DA CMM | 501-1832-01 | |
| AI-803 | Drawings / SPEC | JET SPECIFICATION 579 | F | 8/28/1995 | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Gyro - general | |
| AI-803 | Installation Manual | TP-675 | D | 2/4/2016 | Installation and Operation Manual, 501-1907-01 | AI-803DJ | 501-1907-01 | |
| AI-803 | Installation Manual | TP-537 | C | 2/4/2016 | Installation and Operation Manual, 501-1804-01 | Install manual for AI-803CK | 501-1804-01 | |
| AI-803 | Installation Manual | TP-590 | C | 2/4/2016 | Installation and Operation Manual, 501-1832-01 | Install Manual for AI-803DA | 501-1832-01 | |
| AI-803 | Pilot Guide | TP-591 | E | 2/4/2016 | Pilot's Guide | Changed from ITAR to EAR | 501-1832-01 | |
| AI-803 | Pilot Guide | TP-307 | C | 2/4/2016 | Pilot's Guide | Pub# TP-307 | 501-1022-01, 501-1032-01, 501-1049-51, 501-1086-01, 501-1098-01, 501-1101-01, 501-1101-02, 501-1131-01, 501-1131-02 | |
| AI-803 | Pilot Guide | TP-308 | B | 2/4/2016 | Pilot's Guide | changed from ITAR to EAR | 501-1087-01 | |
| AI-803 | Pilot Guide | TP-479 | B | 2/4/2016 | Pilot's Guide | 501-1710-01 | ||
| AI-803 | Service Bulletin | SB501-1821-2 | Orig | 5/1/2001 | Improve reliability of erection system. | 501-1821-01 | ||
| AI-803 | Service Bulletin | SB501-1857-1 | Orig | 4/17/2002 | Reliability improvement. New part has strengthened locking tang. | 501-1857-01 | ||
| AI-803 | Service Bulletin | SB501-1806-1 | A | 12/1/2000 | New erector is a simplified design. | 501-1806-01 | ||
| AI-803 | Service Bulletin | SB501-1806-2 | Orig | 12/1/2000 | Improve reliability of erection system. | 501-1806-01 | ||
| AI-803 | Service Bulletin | SB501-1845-1 | Orig | 4/17/2002 | Reliability improvement. New part has strengthened locking tang. | 501-1845-01 | ||
| AI-803 | Service Bulletin | SB501-1821-1 | Orig | 5/15/2001 | Reduce tendency of erector weight to stick. | 501-1821-01 | ||
| AI-803 | Service Bulletin | SB501-1832-1 | A | 12/13/2007 | Limited Quantity of Non-Conforming Parts | Limited Quantity of Non-Conforming Parts | 501-1832-01 | |
| AI-803 | Service Bulletin | SB501-1845-2 | A | 12/13/2007 | Limited Quantity of Non-Conforming Parts | Limited Quantity of Non-Conforming Parts | 501-1845-01 | |
| AI-803 | Service Bulletin | SB501-1857-02 | A | 12/13/2007 | Limited Quantity of Non-Conforming Parts | Limited Quantity of Non-Conforming Parts | 501-1857-01 | |
| AI-803 | Service Bulletin | SB501-1710-1 | Orig | 12/3/1999 | Removal of external label from unit. | 501-1710-01 | ||
| AI-803 | Service Bulletin | SB501-1857-2 | A | 12/13/2007 | Limited quantity of non-conforming parts installed. High temp performance affected (mod 2) | Limited quantity of non-conforming parts installed. High temp performance affected (mod 2) | 501-1857-01 | |
| AI-803 | Service Letter | SL-162 | Orig | 6/10/1999 | To establish authorization to remove lead seal and replace with safety wire. | |||
| AI-803 | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| AI-804 | Component Maintenance Manual | TP-624 | 34-20-73 | A C2 | 2/8/2016 | AI-804CD CMM | AI-804CD CMM | 501-1748-01 |
| AI-804 | Component Maintenance Manual | TP-218 | 34-20-01 | B C8 | 9/22/2022 | Component Maintenance Manual | PUB#TP-218 | 501-1036-01, 501-1036-02, 501-1036-03, 501-1036-04, 501-1036-05, 501-1036-06, 501-1036-07, 501-1105-01, 501-1105-02, 501-1105-03, 501-1105-04, 501-1105-05, 501-1105-06, 501-1105-07, 501-1105-08, 501-1105-09, 501-1105-10, 501-1105-11, 501-1197-01, 501-1197-02, 501-1197-03, 501-1197-04, 501-1197-05, 501-1197-06, 501-1197-07, 501-1197-08, 501-1197-09, 501-1197-10, 501-1197-11, 501-1197-12, 501-1197-14, 501-1197-15, 501-1197-16, 501-1197-17, 501-1197-18, 501-1197-19, 501-1197-21, 501-1197-22, 501-1197-23, 501-1197-24, 501-1197-25, 501-1197-26, 501-1197-27, 501-1197-28, 501-1197-29, 501-1197-31, 501-1197-32, 501-1197-33, 501-1197-34, 501-1295-01, 501-1296-01, 501-1296-02, 501-1296-03, 501-1296-04, 501-1296-05, 501-1296-06, 501-1296-07, 501-1296-08, 501-1412-01, 501-1412-02, 501-1412-03, 501-1412-04, 501-1412-05, 501-1412-06, 501-1455-01, 501-1648-02, 501-1748-02, 501-1798-01, 501-1811-01, 501-1812-01, 501-1828-01, 501-1838-01, 501-1844-01, 501-1848-01, 501-1850-01, 501-1882-01 |
| AI-804 | Component Maintenance Manual | TP-464 | 34-20-42 | A | 6/29/2016 | Maintenance Manual | This revision corrects major volumes of text | 501-1648-01 |
| AI-804 | Component Maintenance Manual | TP-555 | 34-20-01A | B | 6/29/2016 | Component Maintenance Manual | This Revision corrects major volumes of text | 501-1197-20 |
| AI-804 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 2 | 9/26/2024 | Component Maintenance Manual | Rotor Housing Assemblies Manual contains repair information for JET commercial rotor assemblies. | 502-1015-01, 502-1015-02, 502-1025-04, 502-1044-01, 502-1044-02, 502-1153-04, 502-1154-07, 502-1154-08, 502-1177-01, 502-1177-04, 502-1177-07, 502-1177-08, 502-1177-11, 502-1177-12, 502-1177-13, 502-1177-15, 502-1241-02, 502-1253-01, 502-1378-01, 502-1378-04, 502-1378-06, 502-1449-01, 502-1490-01 |
| AI-804 | Drawings / SPEC | JET SPECIFICATION 579 | F | 8/28/1995 | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Gyro - general | |
| AI-804 | Installation Manual | TP-599 | C | 2/4/2016 | Installation and Operation | Pub# TP-599 | 501-1748-01 | |
| AI-804 | Installation Manual | TP-326 | 34-20-02 | H | 9/9/2013 | Installation and Operation Manual | Pub# TP-326 | 501-1036-01, 501-1036-02, 501-1036-03, 501-1036-04, 501-1036-05, 501-1036-06, 501-1036-07, 501-1063-01, 501-1063-02, 501-1063-03, 501-1063-04, 501-1063-05, 501-1063-06, 501-1063-07, 501-1063-08, 501-1078-01, 501-1078-02, 501-1078-03, 501-1078-04, 501-1078-05, 501-1078-06, 501-1078-07, 501-1078-08, 501-1078-09, 501-1078-10, 501-1078-11, 501-1078-12, 501-1078-13, 501-1105-01, 501-1105-02, 501-1105-03, 501-1105-04, 501-1105-05, 501-1105-06, 501-1105-07, 501-1105-08, 501-1105-09, 501-1105-10, 501-1105-11, 501-1170-01, 501-1170-02, 501-1170-03, 501-1170-04, 501-1170-05, 501-1170-06, 501-1170-07, 501-1170-08, 501-1170-09, 501-1170-10, 501-1170-11, 501-1170-12, 501-1170-13, 501-1170-14, 501-1170-15, 501-1170-16, 501-1170-17, 501-1170-18, 501-1170-19, 501-1170-20, 501-1170-21, 501-1170-22, 501-1170-23, 501-1170-24, 501-1170-25, 501-1170-26, 501-1170-27, 501-1170-28, 501-1170-29, 501-1170-30, 501-1170-31, 501-1170-32, 501-1170-33, 501-1170-35, 501-1170-36, 501-1170-37, 501-1170-38, 501-1170-39, 501-1170-40, 501-1170-41, 501-1170-42, 501-1197-01, 501-1197-02, 501-1197-03, 501-1197-04, 501-1197-05, 501-1197-06, 501-1197-07, 501-1197-08, 501-1197-09, 501-1197-10, 501-1197-11, 501-1197-12, 501-1197-14, 501-1197-15, 501-1197-16, 501-1197-17, 501-1197-18, 501-1197-19, 501-1197-20, 501-1197-21, 501-1197-22, 501-1197-23, 501-1197-24, 501-1197-25, 501-1197-26, 501-1197-27, 501-1197-28, 501-1197-29, 501-1197-31, 501-1197-32, 501-1197-33, 501-1197-34, 501-1237-01, 501-1237-02, 501-1242-01, 501-1242-02, 501-1242-03, 501-1242-04, 501-1242-05, 501-1242-06, 501-1242-07, 501-1242-08, 501-1257-01, 501-1295-01, 501-1296-01, 501-1296-02, 501-1296-03, 501-1296-04, 501-1296-05, 501-1296-06, 501-1296-07, 501-1296-08, 501-1297-01, 501-1412-01, 501-1412-02, 501-1412-03, 501-1412-04, 501-1412-05, 501-1412-06, 501-1413-01, 501-1413-02, 501-1426-01, 501-1455-01, 501-1648-01, 501-1748-02, 501-1798-01, 501-1811-01, 501-1812-01, 501-1828-01, 501-1838-01, 501-1844-01, 501-1848-01, 501-1849-01, 501-1850-01, 501-1876-01, 501-1882-01, 501-1889-01, 501-1895-01, 501-1896-01 |
| AI-804 | Instruction Manual | TP-630 | A | 2/12/2009 | Instruction Manual, Level 1 Maintenance, AI-804 | This manual contains functional bench test instructions for the AI-804 Attitude Indicator. | 501-1036, 501-1105, 501-1197, 501-1295, 501-1296, 501-1412, 501-1455, 501-1648-02, 501-1748-02, 501-1798, 501-1811-01, 501-1812-01, 501-1828-01, 501-1838-01, 501-1844-01, 501-1848-01, 501-1849-01, 501-1895-01, 501-1896-01, 501-1902-01 | |
| AI-804 | Pilot Guide | TP-325 | C | 1/27/2005 | Pilot's Guide | Pub# TP-325 | 501-1036-01, 501-1036-02, 501-1036-03, 501-1036-04, 501-1036-05, 501-1036-06, 501-1036-07, 501-1063-01, 501-1063-02, 501-1063-03, 501-1063-04, 501-1063-05, 501-1063-06, 501-1063-07, 501-1063-08, 501-1078-(), 501-1078-01, 501-1078-02, 501-1078-03, 501-1078-04, 501-1078-05, 501-1078-06, 501-1078-07, 501-1078-08, 501-1078-09, 501-1078-10, 501-1078-11, 501-1078-12, 501-1078-13, 501-1105-01, 501-1105-02, 501-1105-03, 501-1105-04, 501-1105-05, 501-1105-06, 501-1105-07, 501-1105-08, 501-1105-09, 501-1105-10, 501-1105-11, 501-1170-01, 501-1170-02, 501-1170-03, 501-1170-04, 501-1170-05, 501-1170-06, 501-1170-07, 501-1170-08, 501-1170-09, 501-1170-10, 501-1170-11, 501-1170-12, 501-1170-13, 501-1170-14, 501-1170-15, 501-1170-16, 501-1170-17, 501-1170-18, 501-1170-19, 501-1170-20, 501-1170-21, 501-1170-22, 501-1170-23, 501-1170-24, 501-1170-25, 501-1170-26, 501-1170-27, 501-1170-28, 501-1170-29, 501-1170-30, 501-1170-31, 501-1170-32, 501-1170-33, 501-1170-35, 501-1170-36, 501-1170-37, 501-1197-01, 501-1197-02, 501-1197-03, 501-1197-04, 501-1197-05, 501-1197-06, 501-1197-07, 501-1197-08, 501-1197-09, 501-1197-11, 501-1197-12, 501-1197-14, 501-1197-15, 501-1197-16, 501-1197-17, 501-1197-18, 501-1237-01, 501-1242-01, 501-1242-02, 501-1242-03, 501-1242-04, 501-1242-05, 501-1242-06, 501-1242-07, 501-1242-08, 501-1257-01, 501-1295-01, 501-1296-01, 501-1296-02, 501-1296-03, 501-1296-04, 501-1296-05, 501-1296-06, 501-1297-01, 501-1412-01, 501-1412-02, 501-1413-01, 501-1413-02, 501-1426-01, 501-1455-01, 501-1648-(), 501-1798-(), 501-1811-(), 501-1812-(), 501-1828-(), 501-1838-(), 501-1844-(), 501-1848-(), 501-1850-() | |
| AI-804 | Service Bulletin | SB501-1811-1 | A | 5/1/2001 | Reduce tendency of erector weight to stick. | 501-1811-01 | ||
| AI-804 | Service Bulletin | SB501-1811-2 | Orig | 5/1/2001 | Improve reliability of erection system. | 501-1811-01 | ||
| AI-804 | Service Bulletin | SB501-1812-1 | A | 5/1/2001 | Reduce tendency of erector weight to stick. | 501-1812-01 | ||
| AI-804 | Service Bulletin | SB501-1812-2 | Orig | 5/1/2001 | Improve reliability of erection system. | 501-1812-01 | ||
| AI-804 | Service Bulletin | SB501-1828-1 | A | 12/1/2000 | Reduce tendency of erector weight to stick. | 501-1828-01 | ||
| AI-804 | Service Bulletin | SB501-1828-2 | Orig | 12/1/2000 | Improve reliability of erection system. | 501-1828-01 | ||
| AI-804 | Service Bulletin | SB501-1828-3 | Orig | 4/22/2002 | Reliability improvement. New part has strengthened locking tang. | 501-1828-01 | ||
| AI-804 | Service Bulletin | SB501-1844-1 | A | 12/1/2000 | New erector is a simplified design. | 501-1844-01 | ||
| AI-804 | Service Bulletin | SB501-1844-2 | Orig | 12/1/2000 | Improve reliability of erection system. | 501-1844-01 | ||
| AI-804 | Service Bulletin | SB501-1844-3 | Orig | 4/22/2002 | Reliability improvement. New part has strengthened locking tang. | 501-1844-01 | ||
| AI-804 | Service Bulletin | SB501-1798-1 | A | 12/1/2000 | New erector is a simplified design. | 501-1798-01 | ||
| AI-804 | Service Bulletin | SB501-1798-2 | Orig | 12/1/2000 | Improve reliability of erection system. | 501-1798-01 | ||
| AI-804 | Service Bulletin | SB501-1798-3 | Orig | 4/22/2002 | Reliability improvement. New part has strengthened locking tang. | 501-1798-01 | ||
| AI-804 | Service Bulletin | SB501-1848-1 | A | 12/6/2000 | Reduce tendency of erector weight to stick. | 501-1848-01 | ||
| AI-804 | Service Bulletin | SB501-1848-2 | Orig | 12/6/2000 | Improve reliability of erection system. | 501-1848-01 | ||
| AI-804 | Service Bulletin | SB501-1849-1 | Orig | 4/17/2002 | Reliability improvement. New part has strengthened locking tang. | 501-1849-01 | ||
| AI-804 | Service Bulletin | SB501-1850-1 | A | 5/1/2001 | Reduce tendency of erector weight to stick. | 501-1850-01 | ||
| AI-804 | Service Bulletin | SB501-1850-2 | Orig | 5/1/2001 | Improve reliability of erection system. | 501-1850-01 | ||
| AI-804 | Service Bulletin | SB501-1748-1 | A | 2/8/2016 | Replace Airplane P/N 565-1709-07 with Airplane P/N 565-1709-08. | 501-1748-01 | ||
| AI-804 | Service Bulletin | SB501-1748-2 | B | 2/8/2016 | Reduce tendency of erector weight to stick. | 501-1748-01 | ||
| AI-804 | Service Bulletin | SB501-1748-3 | A | 2/8/2016 | Improve reliability of erection system. | 501-1748-01 | ||
| AI-804 | Service Bulletin | SB501-1748-4 | A | 2/8/2016 | Reliability improvement. New part has strengthened locking tang. | 501-1748-01 | ||
| AI-804 | Service Bulletin | SB501-1648-1 | A | 12/1/2000 | New erector is a simplified design. | 501-1648-01, 501-1648-02 | ||
| AI-804 | Service Bulletin | SB501-1648-2 | Orig | 12/1/2000 | Improve reliability of erection system. | 501-1648-01, 501-1648-02 | ||
| AI-804 | Service Bulletin | SB501-1648-3 | Orig | 4/17/2002 | Reliability improvement. New part has strengthened locking tang. | 501-1648-01, 501-1648-02 | ||
| AI-804 | Service Bulletin | SB501-1296-1 | Orig | 8/1/1997 | To incorporate lighting system with longer life. | 501-1296-04 | ||
| AI-804 | Service Bulletin | SB501-1296-2 | A | 12/1/2000 | New erector is a simplified design. | 501-1296-( ) | ||
| AI-804 | Service Bulletin | SB501-1296-3 | Orig | 12/1/2000 | Improve reliability of erection system. | 501-1296-( ) | ||
| AI-804 | Service Bulletin | SB501-1296-4 | Orig | 4/22/2002 | Reliability improvement. New part has strengthened locking tang. | 501-1296-( ) | ||
| AI-804 | Service Bulletin | SB501-1412-1 | Orig | 10/1/1995 | To insure proper connection between chassis ground pin of J1 and case of unit. | 501-1412-( ) | ||
| AI-804 | Service Bulletin | SB501-1412-2 | A | 12/1/2000 | New erector is a simplified design. | 501-1412-( ) | ||
| AI-804 | Service Bulletin | SB501-1412-3 | Orig | 12/1/2000 | Improve reliability of erection system. | 501-1412-( ) | ||
| AI-804 | Service Bulletin | SB501-1412-4 | Orig | 4/22/2002 | Reliability improvement. New part has strengthened locking tang. | 501-1412-( ) | ||
| AI-804 | Service Bulletin | SB501-1197-1 | A | 1/1/1993 | To provide an attitude indicator with a longer caging knob. | 501-1197-05 | ||
| AI-804 | Service Bulletin | SB501-1197-2 | A | 12/1/2000 | Reduce tendency of erector weight to stick. (superceded) | 501-1197-20 | ||
| AI-804 | Service Bulletin | SB501-1197-3 | A | 12/1/2000 | New erector is a simplified design. | 501-1197-( ) | ||
| AI-804 | Service Bulletin | SB501-1197-4 | Orig | 12/1/2000 | Improve reliability of erection system. | 501-1197-( ) | ||
| AI-804 | Service Bulletin | SB501-1197-5 | Orig | 4/30/2002 | Reliability improvement. New part has strengthened locking tang. | 501-1197-( ) | ||
| AI-804 | Service Bulletin | SB501-1648-4 | A | 12/13/2007 | Limited quantity of non-conforming parts | Limited quantity of non-conforming parts | 501-1648-02 | |
| AI-804 | Service Bulletin | SB501-1748-5 | B | 2/8/2016 | Limited quantity of non-conforming parts installed. High temp performance affected (mod 5) | Limited quantity of non-conforming parts installed. High temp performance affected (mod 5) | 501-1748-01 | |
| AI-804 | Service Bulletin | SB501-1197-6 | A | 12/13/2007 | Planning Information | Planning Information | 501-1197-28, 501-1197-29, 501-1197-32 | |
| AI-804 | Service Bulletin | SB501-1828-4 | A | 12/13/2007 | Limited quantity of non-conforming parts installed. High temp performance affected. | 501-1828-01 | ||
| AI-804 | Service Bulletin | SB501-1849-2 | A | 12/13/2007 | Limited quantity of non-conforming parts installed. High temp performance affected. | 501-1849-01 | ||
| AI-804 | Service Letter | SL-172 | Orig | 4/12/2001 | To inform Authorized Repair Facilities of correct manual use when repairing the AI-804 () Attitude Indicator. | |||
| AI-804 | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| AI-804 | Service Letter | SL-12 | E | 4/23/2010 | To provide Attitude Indicator operation information. | |||
| AI-903 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 2 | 9/26/2024 | Component Maintenance Manual | Rotor Housing Assemblies Manual contains repair information for JET commercial rotor assemblies. | 502-1015-01, 502-1015-02, 502-1025-04, 502-1044-01, 502-1044-02, 502-1153-04, 502-1154-07, 502-1154-08, 502-1177-01, 502-1177-04, 502-1177-07, 502-1177-08, 502-1177-11, 502-1177-12, 502-1177-13, 502-1177-15, 502-1241-02, 502-1253-01, 502-1378-01, 502-1378-04, 502-1378-06, 502-1449-01, 502-1490-01 |
| AI-903 | Component Maintenance Manual | TP-643 | A | 1/29/2019 | Component Maintenance Manual, 501-1509-01 | 3" Attitude Indicator | 501-1509-01 | |
| AI-903 | Drawings / SPEC | JET SPECIFICATION 579 | F | 8/28/1995 | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Gyro - general | |
| AI-903 | Pilot Guide | TP-306 | A | 2/1/2005 | Pilot's Guide | Pub# TP-306 | 501-1077-01, 501-1152-01, 501-1153-01, 501-1154-01, 501-1190-01, 501-1190-02 | |
| AI-903 | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| AI-903 | Service Letter | SL-184 | Orig | 12/5/2003 | Proper Operation of Caging Knob | |||
| AI-904 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 2 | 9/26/2024 | Component Maintenance Manual | Rotor Housing Assemblies Manual contains repair information for JET commercial rotor assemblies. | 502-1015-01, 502-1015-02, 502-1025-04, 502-1044-01, 502-1044-02, 502-1153-04, 502-1154-07, 502-1154-08, 502-1177-01, 502-1177-04, 502-1177-07, 502-1177-08, 502-1177-11, 502-1177-12, 502-1177-13, 502-1177-15, 502-1241-02, 502-1253-01, 502-1378-01, 502-1378-04, 502-1378-06, 502-1449-01, 502-1490-01 |
| AI-904 | Component Maintenance Manual | TP-216 | 34-20-06 | 6 | 10/9/2012 | Component Maintenance Manual | Pub# TP-216 | 501-1063-01, 501-1063-02, 501-1063-03, 501-1063-04, 501-1063-05, 501-1063-06, 501-1063-07, 501-1063-08, 501-1078-01, 501-1078-02, 501-1078-03, 501-1078-04, 501-1078-05, 501-1078-06, 501-1078-07, 501-1078-08, 501-1078-09, 501-1078-10, 501-1078-11, 501-1078-12, 501-1078-13, 501-1170-01, 501-1170-02, 501-1170-03, 501-1170-04, 501-1170-05, 501-1170-06, 501-1170-07, 501-1170-08, 501-1170-09, 501-1170-10, 501-1170-11, 501-1170-12, 501-1170-13, 501-1170-14, 501-1170-15, 501-1170-16, 501-1170-17, 501-1170-18, 501-1170-19, 501-1170-20, 501-1170-21, 501-1170-22, 501-1170-23, 501-1170-24, 501-1170-25, 501-1170-26, 501-1170-27, 501-1170-28, 501-1170-29, 501-1170-30, 501-1170-31, 501-1170-32, 501-1170-33, 501-1170-35, 501-1170-36, 501-1170-37, 501-1170-38, 501-1170-39, 501-1170-40, 501-1237-01, 501-1242-01, 501-1242-02, 501-1242-03, 501-1242-04, 501-1242-05, 501-1242-06, 501-1242-07, 501-1242-08, 501-1413-01, 501-1413-02, 501-1426-01 |
| AI-904 | Component Maintenance Manual | TP-356 | 3 | 10/16/2012 | Overhaul Manual and Parts Breakdown | Pub# TP-356 | 501-1297-01 | |
| AI-904 | Drawings / SPEC | JET SPECIFICATION 579 | F | 8/28/1995 | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Gyro - general | |
| AI-904 | Installation Manual | TP-326 | 34-20-02 | H | 9/9/2013 | Installation and Operation Manual | Pub# TP-326 | 501-1036-01, 501-1036-02, 501-1036-03, 501-1036-04, 501-1036-05, 501-1036-06, 501-1036-07, 501-1063-01, 501-1063-02, 501-1063-03, 501-1063-04, 501-1063-05, 501-1063-06, 501-1063-07, 501-1063-08, 501-1078-01, 501-1078-02, 501-1078-03, 501-1078-04, 501-1078-05, 501-1078-06, 501-1078-07, 501-1078-08, 501-1078-09, 501-1078-10, 501-1078-11, 501-1078-12, 501-1078-13, 501-1105-01, 501-1105-02, 501-1105-03, 501-1105-04, 501-1105-05, 501-1105-06, 501-1105-07, 501-1105-08, 501-1105-09, 501-1105-10, 501-1105-11, 501-1170-01, 501-1170-02, 501-1170-03, 501-1170-04, 501-1170-05, 501-1170-06, 501-1170-07, 501-1170-08, 501-1170-09, 501-1170-10, 501-1170-11, 501-1170-12, 501-1170-13, 501-1170-14, 501-1170-15, 501-1170-16, 501-1170-17, 501-1170-18, 501-1170-19, 501-1170-20, 501-1170-21, 501-1170-22, 501-1170-23, 501-1170-24, 501-1170-25, 501-1170-26, 501-1170-27, 501-1170-28, 501-1170-29, 501-1170-30, 501-1170-31, 501-1170-32, 501-1170-33, 501-1170-35, 501-1170-36, 501-1170-37, 501-1170-38, 501-1170-39, 501-1170-40, 501-1170-41, 501-1170-42, 501-1197-01, 501-1197-02, 501-1197-03, 501-1197-04, 501-1197-05, 501-1197-06, 501-1197-07, 501-1197-08, 501-1197-09, 501-1197-10, 501-1197-11, 501-1197-12, 501-1197-14, 501-1197-15, 501-1197-16, 501-1197-17, 501-1197-18, 501-1197-19, 501-1197-20, 501-1197-21, 501-1197-22, 501-1197-23, 501-1197-24, 501-1197-25, 501-1197-26, 501-1197-27, 501-1197-28, 501-1197-29, 501-1197-31, 501-1197-32, 501-1197-33, 501-1197-34, 501-1237-01, 501-1237-02, 501-1242-01, 501-1242-02, 501-1242-03, 501-1242-04, 501-1242-05, 501-1242-06, 501-1242-07, 501-1242-08, 501-1257-01, 501-1295-01, 501-1296-01, 501-1296-02, 501-1296-03, 501-1296-04, 501-1296-05, 501-1296-06, 501-1296-07, 501-1296-08, 501-1297-01, 501-1412-01, 501-1412-02, 501-1412-03, 501-1412-04, 501-1412-05, 501-1412-06, 501-1413-01, 501-1413-02, 501-1426-01, 501-1455-01, 501-1648-01, 501-1748-02, 501-1798-01, 501-1811-01, 501-1812-01, 501-1828-01, 501-1838-01, 501-1844-01, 501-1848-01, 501-1849-01, 501-1850-01, 501-1876-01, 501-1882-01, 501-1889-01, 501-1895-01, 501-1896-01 |
| AI-904 | Pilot Guide | TP-325 | C | 1/27/2005 | Pilot's Guide | Pub# TP-325 | 501-1036-01, 501-1036-02, 501-1036-03, 501-1036-04, 501-1036-05, 501-1036-06, 501-1036-07, 501-1063-01, 501-1063-02, 501-1063-03, 501-1063-04, 501-1063-05, 501-1063-06, 501-1063-07, 501-1063-08, 501-1078-(), 501-1078-01, 501-1078-02, 501-1078-03, 501-1078-04, 501-1078-05, 501-1078-06, 501-1078-07, 501-1078-08, 501-1078-09, 501-1078-10, 501-1078-11, 501-1078-12, 501-1078-13, 501-1105-01, 501-1105-02, 501-1105-03, 501-1105-04, 501-1105-05, 501-1105-06, 501-1105-07, 501-1105-08, 501-1105-09, 501-1105-10, 501-1105-11, 501-1170-01, 501-1170-02, 501-1170-03, 501-1170-04, 501-1170-05, 501-1170-06, 501-1170-07, 501-1170-08, 501-1170-09, 501-1170-10, 501-1170-11, 501-1170-12, 501-1170-13, 501-1170-14, 501-1170-15, 501-1170-16, 501-1170-17, 501-1170-18, 501-1170-19, 501-1170-20, 501-1170-21, 501-1170-22, 501-1170-23, 501-1170-24, 501-1170-25, 501-1170-26, 501-1170-27, 501-1170-28, 501-1170-29, 501-1170-30, 501-1170-31, 501-1170-32, 501-1170-33, 501-1170-35, 501-1170-36, 501-1170-37, 501-1197-01, 501-1197-02, 501-1197-03, 501-1197-04, 501-1197-05, 501-1197-06, 501-1197-07, 501-1197-08, 501-1197-09, 501-1197-11, 501-1197-12, 501-1197-14, 501-1197-15, 501-1197-16, 501-1197-17, 501-1197-18, 501-1237-01, 501-1242-01, 501-1242-02, 501-1242-03, 501-1242-04, 501-1242-05, 501-1242-06, 501-1242-07, 501-1242-08, 501-1257-01, 501-1295-01, 501-1296-01, 501-1296-02, 501-1296-03, 501-1296-04, 501-1296-05, 501-1296-06, 501-1297-01, 501-1412-01, 501-1412-02, 501-1413-01, 501-1413-02, 501-1426-01, 501-1455-01, 501-1648-(), 501-1798-(), 501-1811-(), 501-1812-(), 501-1828-(), 501-1838-(), 501-1844-(), 501-1848-(), 501-1850-() | |
| AI-904 | Service Bulletin | SB501-1297-1 | Orig | 2/1/1987 | To install hardened gear train. | 501-1297-01 | ||
| AI-904 | Service Bulletin | SB501-1237-1 | Orig | 7/1/1978 | To insure power warning flag operation when used with PS-823C or D Emergency Power Supply. | 501-1237-01 | ||
| AI-904 | Service Bulletin | SB501-1237-2 | B | 12/15/2000 | Conversion of Model AI-904W (part number 501-1237-01) to AI-904AZ (part number 501-1237-02). | 501-1237-01 | ||
| AI-904 | Service Bulletin | SB501-1242-1 | Orig | 7/1/1978 | To insure power warning flag operation when used with PS-823C or D Emergency Power Supply. | 501-1242-( ) | ||
| AI-904 | Service Bulletin | SB501-1078-1 | 7/30/1973 | Unknown | ||||
| AI-904 | Service Bulletin | SB501-1078-2 | Orig | 9/1/1981 | To prevent dynamic braking of indicator gyro caused by back EMF. | , Acron Aviation | 501-1078-( ) | |
| AI-904 | Service Bulletin | SB501-1170-1 | A | 2/1/1985 | To convert listed AI-904 models to models for helicopter use. | 501-1170-09, 501-1170-10, 501-1170-13, 501-1170-14 | ||
| AI-904 | Service Bulletin | SB501-1170-2 | Orig | 2/1/1985 | To provide instructions necessary for relocation of C1 capacitor which will permit installation of the replacement circuit card assembly. | 501-1170-( ), 501-1413-01 | ||
| AI-904 | Service Bulletin | SB501-1170-3 | Orig | 4/1/1985 | To incorporate gears with hard finish. | 501-1170-( ) | ||
| AI-904 | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| AI-904 | Service Letter | SL-12 | E | 4/23/2010 | To provide Attitude Indicator operation information. | |||
| AI-930 | Drawings / SPEC | JET SPECIFICATION 579 | F | 8/28/1995 | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Calibration of Pitch & Bank Indicators used in Fixed Wing High Speed Aircraft Applications. | Gyro - general | |
| AI-930 | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| AP General Files | Drawings / SPEC | AutoPilot Service | D | 3/9/2017 | Change location of DN-104 repairs | Change location of DN-104 repairs | 501- | |
| AP General Files | Installation Manual | TP-336, TP-352, TP-447, TP-470 | x.x | 4/17/2023 | IOM - Service Information Letter Manual transfer to Extant Aerospace | The production and service of this product has been transferred to Extant Aerospace. The technical manuals and service literature will no longer be accessible from the L3Harris Aviation Products technical publications website after 04/17/2023. See SIL-008. The following rev/date was last L3H AP releases prior to transfer to Extant. [PS-823, TP-336, rev R, 9/26/22 PS-835, TP-352, reissue, 6/10/1987 PS-834, TP-447, rev B, date 5/8/06 PS-850/855, TP-470 rev K, date 8/22/17] | 501-1075-( ), 501-1228-( ), 501-1682-( ), 501-1712-( ), 501-1719-( ) | |
| AP General Files | Installation Manual | 0040-21453-01 | N | 8/8/2011 | Installation Manual | Sold product. The ADR-7050 transfer has been transferred to Genesys aerosystems. https://genesys-aerosystems.com/ | ADR-7050 Part Numbers: 9200-21453-01 9200-21453-02 9200-21453-03 ADR-7050 Mounting Tray Part Numbers: 9010-21453-01 9010-21457-01 | |
| AP General Files | Miscellaneous | FC-xxx Flight Control and system components | B | 5/13/2015 | Notice of Transfer of Service | LearJet Updates See SL-280 | n/a | |
| AP General Files | Miscellaneous | A100 Recorder Service Letters | n/a | 11/18/2021 | UntitledLetters provide information on A100 obsolescence and replacement options. | Letters provide information on A100 obsolescence and replacement options. | n/a | |
| AP General Files | Miscellaneous | 2023 SAP Migration | 00 | 5/22/2023 | 2023 SAP Migration Letter | The purpose of this letter is to provide information concerning a forthcoming Enterprise Resource Planning (ERP), Manufacturing Execution System (MES) and time keeping systems transition. Following more than 20 years in our current systems; Impressa, Visual and Eshop; the size and scale of our business and the growing complexities in our end to end value chains necessitates that we upgrade our infrastructure in order to best serve our many stakeholders. We are currently in the process of upgrading our existing ERP systems to the latest version of SAP S/4 HANA, our MRP system to SAP Shopfloor and our timekeeping system to Auto Time. This change will be implemented across all of our Commercial Avionics locations in Grand Rapids, St. Petersburg and Phoenix with a current Go Live target date of July 5th, 2023. | None | |
| AP General Files | Miscellaneous | ADR-7050 | 0 | 5/25/2023 | Information on ADR-7050 | The ADR-7050 transfer has been transferred to Genesys aerosystems. https://genesys-aerosystems.com/ | 9200-21453-01 9200-21453-02 9200-21453-03 | |
| AP General Files | Miscellaneous | 2024-Repair-Price | JAN2024 | 5/30/2024 | L3Harris commercial avionics: repair and aftermarket services catalog | Repair and aftermarket services catalog | All L3H AP and ACSS | |
| AP General Files | Miscellaneous | 2023-Repair-Policy-Announcement | 2023-01 | 2/15/2023 | Streamlining of Repair and Overhaul Process/Standard Repair Use | We have streamlined our repair and overhaul process to accelerate the shop processing of customer repairs. This means that for standard repairs and no-fault-found recertification, the returned units will be processed, final tested, shipped, and invoiced without seeking approval for standard repairs. | L3H AP and ACSS | |
| AP General Files | Pilot Guide | 0040-21454-01 | A | 5/5/2006 | Pilot's Guide | The ADR-7050 transfer has been transferred to Genesys aerosystems. https://genesys-aerosystems.com/ | 9200-21453-01 9200-21453-02 9200-21453-03 | |
| AP General Files | Service Letter | SL-153 | A | 5/16/2018 | Elimination of Internal Moisture in Attitude Indicators. | Elimination of Internal Moisture in Attitude Indicators. | All P/N 501-xxxx-xx, models AI- and ADI- | |
| AP General Files | Service Letter | SL-156 | B | 2/27/2019 | Define the L3 Aviation Products Exchange/Overhaul Program and acceptable/unacceptable exchange core to the field. | L3 Aviation Products Exchange Program | n/a | |
| AP General Files | Service Letter | SL-159 | Orig | 3/8/1999 | Establishment of policy requiring use of clean room environment during disassembly, repair, and assembly for all AI/ADI/VG and DG products. | n/a | ||
| AP General Files | Service Letter | SL-1 | F | 5/16/2018 | Provide general repair instructions for circuit card assembies. | Provide general repair instructions for circuit card assembies. | All | |
| AP General Files | Service Letter | SL-10 | T | 10/8/2018 | Gyro Handling, Storage and Packaging | To provide all service facilities and aircraft operators information concerning gyro handling, storage, packaging, and shipping. | ADI-330, ADI-331, ADI-332, ADI-333, ADI-334, ADI-335, ADI-336, ADI-350, ADI-363,, AI-330, AI-350, AI-360, AI-803( ), AI-804( ), AI-903, AI-904, DG-110, DG-710, DN-101, DN-104, DN-501, DN-600, RG-225, RG-227, VG-204, VG-206, VG-208, VG-301, VN-202 | |
| AP General Files | Service Letter | SL-175 | F | 3/23/2023 | Cross-reference of Avaition Products chemical part numbers to vendor and vendor numbers. | Chemical part numbers cross-reference. (Rev F adds new and replaced RTV refences) | general | |
| AP General Files | Service Letter | SL-49 | F | 5/16/2018 | To provide BFG customers with information concerning the latest moisture/fungus proofing materials/methods being used. | Moisture/Fungus Proofing | general | |
| AP General Files | Service Letter | SL-234 | B | 10/15/2009 | Part Number Clarification | Part Number Claification | multi- | |
| AP General Files | Service Letter | SL-299 | B | 8/27/2015 | Service Letter - Service transfer of SKYWATCH to Extant Aerospace | Transfer of Service SKY497 and SKY899 | 805-10800-( ) 805-11900-( ) | |
| AP General Files | Service Letter | SIL-008 | 02 | 4/18/2023 | Service Information Letter Service/Manual transfer to Extant Aerospace | The transfer of technical manuals, service literature, production, and service to Extant Aerospace is effective April 17, 2023. This includes spares and piece part sales. Orders received after this date by L3Harris will not be accepted. Repair units received by L3Harris Aviation Products from that date and later will be returned. | 501-1873-01 Adapter Charger 501-1334-01 Adapter Phase Lock 501-1334-02 Adapter Phase Lock 501-1334-03 Adapter Phase Lock 501-1043-01 Emergency Power Supply 501-1043-02 Emergency Power Supply 501-1075-01 Emergency Power Supply 501-1075-02 Emergency Power Supply 501-1075-03 Emergency Power Supply 501-1075-04 Emergency Power Supply 501-1075-05 Emergency Power Supply 501-1075-06 Emergency Power Supply 501-1075-07 Emergency Power Supply 501-1075-08 Emergency Power Supply 501-1075-09 Emergency Power Supply 501-1075-10 Emergency Power Supply 501-1075-11 Emergency Power Supply 501-1075-12 Emergency Power Supply 501-1075-13 Emergency Power Supply 501-1075-14 Emergency Power Supply 501-1075-15 Emergency Power Supply 501-1075-16 Emergency Power Supply 501-1228-01 Emergency Power Supply 501-1228-02 Emergency Power Supply 501-1228-03 Emergency Power Supply 501-1228-04 Emergency Power Supply 501-1228-05 Emergency Power Supply 501-1228-06 Emergency Power Supply 501-1228-07 Emergency Power Supply 501-1682-01 Emergency Power Supply 501-1682-02 Emergency Power Supply 501-1686-01 Emergency Power Supply 501-1712-01 Emergency Power Supply 501-1712-02 Emergency Power Supply 501-1712-03 Emergency Power Supply 501-1712-04 Emergency Power Supply 501-1719-01 Emergency Power Supply 501-1719-02 Emergency Power Supply 501-1179-01 Phase Lock Assembly 501-1179-02 Phase Lock Assembly 501-1318-01 Static Converter 201-1001-001 Static Inverter 501-1128-01 Static Inverter 501-1130-01 Static Inverter 501-1148-01 Static Inverter 501-1148-02 Static Inverter 501-1167-01 Static Inverter 501-1167-02 Static Inverter 501-1178-01 Static Inverter 501-1205-01 Static Inverter 501-1205-02 Static Inverter 501-1206-01 Static Inverter 501-1235-01 Static Inverter 501-1240-01 Static Inverter 501-1240-02 Static Inverter 501-1249-01 Static Inverter 501-1265-01 Static Inverter 501-1329-01 Static Inverter 501-1330-01 Static Inverter 501-1331-01 Static Inverter 501-1475-01 Static Inverter 501-1666-01 Static Inverter 501-1666-02 Static Inverter 501-1724-01 Static Inverter 24E508294G01 Transformer Rectifier 24E508294G02 Transformer Rectifier 3S2060DC168B1 Generator Control Unit 3S2060DC168D1 Generator Control Unit 3S2060DM169A1 Battery Charger 3S2060DM169A3 Battery Charger 3S2060DM169B1 Battery Charger 44B258051P002 Feeder Protection Relay | |
| AP General Files | Service Letter | SL-346 | A | 12/18/2019 | Service Letter - Service transfer of Stormscope to Extant Aerospace | Stormscope® Series II Weather Mapping System | WX-1000 ( ), P/N 78-8060-( )-( ), 78-8051-( )-( ) WX-500, P/N 805-11500-001 WX-900, P/N 78-8060-( )-( ) WX-950 ( ), P/N 805-10950-( ), 805-10951-( ) WX-110, P/N 78-8060-6045-1 (System P/N 78-8060-6040-2) WX-PA, (Portable Analyzer) WX-SM, (Skinmapper) NY163, Antenna, P/N 805-10930-( ) Display Unit, P/N 78-8060-5900-8, 78-8060-5900-9 | |
| AP General Files | Service Letter | SL-336 | A | 9/4/2018 | Notification of NGT- Product transfer | Customers of Lynx® Series of Products To inform customers that technical manuals, software, databases, and STC’s for the Lynx® Series product line are to be obtained from Aviation Communications and Surveillance Systems (ACSS) for the products listed in Table 1 and Table 2, effective September 15, 2018. | 9200- | |
| AP General Files | Service Letter | SIL-006 | 02 | 3/15/2023 | Service Information Letter Product and Service transfer to Extant Aerospace | To inform customers that the production and service of Servo/Actuator and associated products listed in the service letter have been transferred to Extant Aerospace. | 501-1076-01 Sensor Pitch Force 501-1123-02 Sensor Position 501-1123-03 Sensor Position 501-1123-04 Sensor Position 501-1132-01 Mach Trim Computer Assembly 501-1132-02 Mach Trim Computer Assembly 501-1132-04 Mach Trim Computer Assembly 501-1132-05 Mach Trim Computer Assembly 501-1133-01 Spoileron Computer Assembly 501-1133-02 Spoileron Computer Assembly 501-1133-03 Spoileron Computer Assembly 501-1133-05 Spoileron Computer Assembly 501-1133-06 Spoileron Computer Assembly 501-1133-07 Spoileron Computer Assembly 501-1133-08 Spoileron Computer Assembly 501-1133-09 Spoileron Computer Assembly 501-1133-10 Spoileron Computer Assembly 501-1133-11 Spoileron Computer Assembly 501-1142-04 Air Data Sensor 501-1142-05 Air Data Sensor 501-1142-07 Air Data Sensor 501-1258-01 Capstan Assembly 501-1258-02 Capstan Assembly 501-1259-03 Servo Actuator Assembly 501-1259-04 Servo Actuator Assembly 501-1259-05 Servo Actuator Assembly 501-1321-01 Battery Charger 501-1321-02 Battery Charger 501-1420-01 Servo Actuator 501-1421-01 Capstan Assembly 501-1478-01 Servo Actuator 501-1478-02 Servo Actuator 501-1478-03 Servo Actuator 501-1478-04 Servo Actuator 501-1478-05 Servo Actuator 501-1482-01 Controller Assembly Autopilot 501-1483-01 Servo Actuator 501-1483-02 Servo Actuator 501-1505-01 Capstan Assembly 501-1505-02 Capstan Assembly 501-1535-01 Servo Actuator 501-1535-04 Servo Actuator 501-1661-03 Computer Amplifier Nose Steering 501-1661-04 Computer Amplifier Nose Steering 501-1661-05 Computer Amplifier Nose Steering 501-1662-01 Servo Actuator 501-1679-01 Autopilot Controller 501-1679-02 Autopilot Controller 501-1679-03 Autopilot Controller 501-1684-01 Servo Actuator 501-1684-02 Servo Actuator 501-1684-03 Servo Actuator 501-1684-04 Servo Actuator 501-1685-05 Capstan Assembly 501-1708-02 Computer Amplifier Nose Steering 501-1708-03 Computer Amplifier Nose Steering 501-1711-02 Servo Actuator 501-1770-01 Pusher Actuator Assembly 501-1770-02 Pusher Actuator Assembly 501-1770-03 Pusher Actuator Assembly 501-1770-04 Pusher Actuator Assembly 501-1770-05 Pusher Actuator 501-1771-01 Capstan Assembly 501-1771-02 Capstan Assembly 501-1771-03 Capstan Assembly 501-1771-04 Capstan Assembly 501-1771-05 Capstan Assembly 501-1772-01 Stick Pusher System 501-1772-02 Stick Pusher System 501-1772-03 Stick Pusher System 501-1772-04 Stick Pusher System 501-1772-05 Stick Pusher System 501-1814-01 Stick Pusher System 501-1814-02 Stick Pusher System 501-1864-01 Capstan Assembly 509-1005-01 Follow-Up, Position Sensor 509-1005-02 Follow-Up, Position Sensor | |
| AP General Files | Service Letter | SIL-007 | 02 | 3/15/2023 | Service Information Letter Manual transfer to Extant Aerospace | Transfer of Publications from L3Harris Aviation Products. See SIL-007 for specific model and part numbers affected by this Transfer of Publications. | 501-1076-01 Sensor Pitch Force 501-1123-02 Sensor Position 501-1123-03 Sensor Position 501-1123-04 Sensor Position 501-1132-01 Mach Trim Computer Assembly 501-1132-02 Mach Trim Computer Assembly 501-1132-04 Mach Trim Computer Assembly 501-1132-05 Mach Trim Computer Assembly 501-1133-01 Spoileron Computer Assembly 501-1133-02 Spoileron Computer Assembly 501-1133-03 Spoileron Computer Assembly 501-1133-05 Spoileron Computer Assembly 501-1133-06 Spoileron Computer Assembly 501-1133-07 Spoileron Computer Assembly 501-1133-08 Spoileron Computer Assembly 501-1133-09 Spoileron Computer Assembly 501-1133-10 Spoileron Computer Assembly 501-1133-11 Spoileron Computer Assembly 501-1142-04 Air Data Sensor 501-1142-05 Air Data Sensor 501-1142-07 Air Data Sensor 501-1258-01 Capstan Assembly 501-1258-02 Capstan Assembly 501-1259-03 Servo Actuator Assembly 501-1259-04 Servo Actuator Assembly 501-1259-05 Servo Actuator Assembly 501-1321-01 Battery Charger 501-1321-02 Battery Charger 501-1420-01 Servo Actuator 501-1421-01 Capstan Assembly 501-1478-01 Servo Actuator 501-1478-02 Servo Actuator 501-1478-03 Servo Actuator 501-1478-04 Servo Actuator 501-1478-05 Servo Actuator 501-1482-01 Controller Assembly Autopilot 501-1483-01 Servo Actuator 501-1483-02 Servo Actuator 501-1505-01 Capstan Assembly 501-1505-02 Capstan Assembly 501-1535-01 Servo Actuator 501-1535-04 Servo Actuator 501-1661-03 Computer Amplifier Nose Steering 501-1661-04 Computer Amplifier Nose Steering 501-1661-05 Computer Amplifier Nose Steering 501-1662-01 Servo Actuator 501-1679-01 Autopilot Controller 501-1679-02 Autopilot Controller 501-1679-03 Autopilot Controller 501-1684-01 Servo Actuator 501-1684-02 Servo Actuator 501-1684-03 Servo Actuator 501-1684-04 Servo Actuator 501-1685-05 Capstan Assembly 501-1708-02 Computer Amplifier Nose Steering 501-1708-03 Computer Amplifier Nose Steering 501-1711-02 Servo Actuator 501-1770-01 Pusher Actuator Assembly 501-1770-02 Pusher Actuator Assembly 501-1770-03 Pusher Actuator Assembly 501-1770-04 Pusher Actuator Assembly 501-1770-05 Pusher Actuator 501-1771-01 Capstan Assembly 501-1771-02 Capstan Assembly 501-1771-03 Capstan Assembly 501-1771-04 Capstan Assembly 501-1771-05 Capstan Assembly 501-1772-01 Stick Pusher System 501-1772-02 Stick Pusher System 501-1772-03 Stick Pusher System 501-1772-04 Stick Pusher System 501-1772-05 Stick Pusher System 501-1814-01 Stick Pusher System 501-1814-02 Stick Pusher System 501-1864-01 Capstan Assembly 509-1005-01 Follow-Up, Position Sensor 509-1005-02 Follow-Up, Position Sensor | |
| AP General Files | Service Letter | SL-297 | D | 9/27/2018 | AIM ® Series product. Sold Product | Sold Product (Attitude Indicator) To inform customers that technical manuals for the AIM ® Series product line are to be obtained from Extant Aerospace for the products listed in Table 1, effective January 31, 2015. | 205-, 210-, 305-, 500-, 505-, 540- | |
| AP General Files | Service Letter | SL-302 | A | 9/14/2015 | To inform customers that technical manuals for the SKYWATCH ® Series. SKY497 / SKY899 | To inform customers that technical manuals for the SKYWATCH ® Series product line are to be obtained from Extant Aerospace for the products listed in Table 1, effective September 21, 2015. | 805-11900-xx, 805-10800-xx | |
| AP General Files | Service Letter | SL-347 | A | 12/18/2019 | To inform customers that technical manuals for the Stormscope® Series II product lines are to be obtained from Extant Aerospace | Sold Product (Stormscope) To inform customers that technical manuals for the Stormscope® Series II product lines are to be obtained from Extant Aerospace for the products listed in Table 1, effective December 13, 2019. | 78-8060-( )-( ), 78-8051-( )-( ), 805-11500-001, 78-8060-6045-1, 78-8060-6040-2, 78-8060-( )-( ), 805-10950-( ), 805-10951-( ) | |
| AP General Files | Service Letter | SL-348 | A | 12/18/2019 | New location for repair and service. CD800 | Transfer of service to Extant Aerospace | 805-11800-002 | |
| AP General Files | Service Letter | SL-349 | A | 12/18/2019 | To inform customers that technical manuals for the CD800 Control Display Unit product lines are to be obtained from Extant Aerospace | To inform customers that technical manuals for the CD800 product lines are to be obtained from Extant Aerospace for the products listed in Table 1, effective December 13, 2019. | Control Display Unit | |
| AP General Files | Service Letter | SL-299 | B | 8/27/2015 | Transfer of Service (Extant Aerospace). SKY497 / SKY899 | Transfer of Service (Extant Aerospace) Repair and service of the SKY497 and SKY899 is being transferred to Extant Aerospace | 805-10800-, 805-11900- | |
| AP General Files | Service Letter | SIL-004 | 05 | 4/22/2025 | Support Logistics Services Partners | To provide general information and contact information of Global Support partners. Acron Aviation and Aviation Communication & Surveillance Systems (ACSS) Global Support Logistics Services. | General | |
| AP General Files | Service Letter | PI/2-001 | 03 | 2/12/2024 | Notification of discontinued product. | Notification of discontinued product. | 17TES0062, 17TES0065, 17TES0066, 17TES0092 | |
| AP General Files | Service Letter | SIL-002 | 00 | 7/1/2020 | Change of manufacturers Cage Code. | Change of manufacturers Cage Code. | general | |
| AP General Files | Service Letter | SIL-001 | 00 | 5/1/2020 | Cleaning and disinfecting guidance. | Cleaning and disinfecting guidance. | N/A | |
| AP General Files | Service Letter | SIL-003 | 00 | 5/25/2021 | To provide customers a means of identifying legacy Recorder product part numbers | L3H AP legacy Recorders product line Part Number Clarification | general | |
| AP General Files | Service Letter | SL-335 | A | 10/23/2019 | To provide customers with instructions for Return Materials Authorization (RMA). | Return Materials Authorization (RMA) procedure | general | |
| AP General Files | Service Letter | SL-240 | B | 11/21/2011 | Discontinued support of products | To inform customers of discontinued support of products owned by Avionics Systems. Effective September 1, 2009 Avionics Systems will no longer support the repair and service of the products listed in Table 1 | general | |
| AP General Files | Service Letter | SL-353 | A | 2/4/2020 | Discontinued Literature Package Distribution | Discontinued Literature Package Distribution | n/a | |
| AP General Files | Service Letter | SL-344 | A | 7/29/2019 | Pilot’s Guide Distribution | To inform customers that L3 Aviation Products will no longer be providing hard copies of product Pilot’s Guides. | general | |
| AP General Files | Service Letter | ARF SIL007 | Orig | 3/16/2018 | FACTORY AND REPAIR STATION MOVE FROM SARASOTA, FLORIDA TO GRAND RAPIDS, MICHIGAN | FACTORY AND REPAIR STATION MOVE FROM SARASOTA, FLORIDA TO GRAND RAPIDS, MICHIGAN | n/a | |
| AP General Files | Service Letter | SL-307 | A | 2/29/2016 | Maintenance Manual Revision Packets | Discontinue issuing of Revision Packets | Multi- | |
| AP General Files | Service Letter | SL-261 | H | 7/30/2024 | Shipping Instructions for International Customers | Part 145 (Repairs) and Part 21 (RMA) shipping instructions for international customers. | General | |
| AP General Files | Service Letter | SL-280 | D | 9/6/2018 | Autopilot product line sold to Butler Avionics | Service Letter | FC-110, FC-200, FC-530, FC-535, FC-550 | |
| AP General Files | Service Letter | SL-294 | D | 9/11/2018 | Transfer of Service to Butler Avionics for SA-400A | New location for repair and overhaul | 501-1212-01 | |
| AP General Files | Service Letter | SL-298 | B | 9/11/2018 | Product sold to Butler Avionics | Transfer of Service Nose Wheel Computer CA-400 ( ) and Altitude Preselect Computer PC-500 ( ) | 501-1211-( ), 501-1288-( ) | |
| AP General Files | Service Letter | SL-8, SL-80, SL-120, SL-170 | x.x | 4/17/2023 | Service Information Letter Manual transfer to Extant Aerospace | The production and service of this product has been transferred to Extant Aerospace. The technical manuals and service literature will no longer be accessible from the L3Harris Aviation Products technical publications website after April 17, 2023. See SIL-008. The following rev/date was last L3H AP releases prior to transfer to Extant. [PS-823, SL-8, rev U, date 6/22/11. PS-835, SL-80, rev AD, date 4/11/18. PS-834, SL-120, rev F, date 11/30/09. PS-850 / PS-855, rev K, date 7/23/14. | 501-1075-( ), 501-1228-( ), 501-1682-( ), 501-1712-( ), 501-1719-( ) | |
| AP General Files | Service Letter | TP-202, TP-329, TP-475, TP-483 | x.x | 4/17/2023 | CMM - Service Information Letter Manual transfer to Extant Aerospace | The production and service of this product has been transferred to Extant Aerospace. The technical manuals and service literature will no longer be accessible from the L3Harris Aviation Products technical publications website after 04/17/2023. See SIL-008. The following rev/date was last L3H AP releases prior to transfer to Extant. [PS-823, TP-202, rev B date 8/01/2018], [PS-834, TP-475, rev B date 04/23/2018], [PS-835, TP-329, rev C5 date 3/30/2020], [PS-850 / PS-855, TP-483, rev C5 date 04/16/2019] | 501-1075-( ), 501-1228-( ), 501-1682-( ), 501-1712-( ), 501-1719-( ) | |
| AP General Files | Service Letter | SIL-001-ACSS | - | 4/18/2023 | Transfer of Service - ACSS TCAS II and Mode S Transponder | Repair and service of both the TCAS II and Mode S Transponder is being transferred to Penta Avionics. L3Harris Aviation Products / ACSS will no longer offer any repair support or testing of the part numbers listed in the Effectivity as of March 31, 2023. | 4066010-901, 4066010-902, 4066010-903, 4066010-904, 4066010-905, 4066010-907, 4066010-910, 4066010-911, 4066010-912, 4066010-913, 4066010-914, 4066010-954, 4066010-984 4061400-901, 4061400-902, 4061400-903, 4061400-904, 4061400-905 | |
| AP General Files | Service Letter | SIL-002-ACSS | 00 | 2/28/2024 | Transfer of Service - ACSS DV-910 VSI/TRA and TCAS Control Panel | Repair and service of both the DV-910 VSI/TRA and TCAS Control Panel is being transferred to Penta Avionics. L3Harris Aviation Products / ACSS will no longer offer any repair support or testing of the part numbers listed in the Effectivity as of December 4, 2023. | DV-910 VSI/TRA, 4067241-801, 4067241-802, 4067241-803, 4067241-804, 4067241-805, 4067241-806, 4067241-840, 4067241-841, 4067241-842, 4067241-843, 4067241-844, 4067241-845, 4067241-860, 4067241-861, 4067241-862, 4067241-863, 4067241-864, 4067241-865, 4067241-880, 4067241-881, 4067241-882, 4067241-883, 4067241-884, 4067241-885, 4067241-890, 4067241-891, 4067241-892, 4067241-893, 4067241-894, 4067241-895. TCAS Control Panel, 4052190-902, 4052190-903, 4052190-904, 4052190-905, 4052190-906, 4052190-907, 4052190-908, 4052190-909 | |
| AP General Files | Service Letter | SIL-004-ULB | 00 | 1/23/2025 | Notification of Dukane Seacom Service Information Letter. | Reports of internal battery spring discoloration within the DK120/90 have been reported by service technicians performing field battery replacement activities in accordance with Technical Manual 03-TM-0063 Section V. | P/N 266E5542-00 (Dukane DK120/90) | |
| AP General Files | Service Letter | SIL-009 | 00 | 4/8/2025 | Acron Aviation Announcement | To provide general information and contact information for Acron Aviation. | General | |
| AP General Files | Service Letter | SIL-002-ULB | 00 | 9/16/2024 | Battery Information for 90 Day Underwater Locator Beacon (ULB). | Provide Composition Information on Ingredients and Transportation Rules information on 90-day ULB. NOTE: The battery is considered a battery inside a contained product (i.e., ULB). | P/N 266E5542-00 (Dukane DK120/90) P/N 9080-10036-01 (Dukane DK290-11) P/N 266E6914-00 (Novega 22960-00, GREEN90) | |
| AP General Files | Service Letter | SL-293 | F | 5/6/2025 | spare piece part sales | To provide sales policy related to spare piece part sales for Acron Aviation. | Multi- | |
| BTP-1634 | Installation Manual | 009-10140-001 | C | 6/2/2008 | Instruction Manual | Pub# 009-10140-001 | 805-10045-001 | |
| BTP-1634 | Service Bulletin | SB001-BTP-1634 | 00 | 4/3/2023 | MOD A: Add TACAN+ Compatibility. | Bench Test Panel for AN/ARN-154 (V) TACAN System MOD A: Add TACAN+ Compatibility to BTP-1634. | 805-10045-001, 805-10045-002, 805-10045-003 | |
| CA-2001 | Service Bulletin | SB501-1200-1 | Orig | 4/1/1978 | To prevent possible false VNAV CAPTURE indication. | To prevent possible false VNAV CAPTURE indication | 501-1200-03, 501-1200-04 | |
| CA-2001 | Service Bulletin | SB501-1200-2 | Orig | 4/1/1978 | To prevent inadvertent localizer engagement of receiver when RNAV power is off. | To prevent inadvertent localizer engagement of receiver when RNAV power is off. | 501-1200-03, 501-1200-04 | |
| CATS - Software | Installation Aircraft Tools | n/a | x.x | 10/26/2021 | CVR AUTOMATED TEST STATION/ RECORDER INTERFACE UNIT (CATS/RIU) | CATS 2.4. | 17TES0420 | |
| CATS - Software | Instruction Manual | 165E4127-01 | Init | 4/19/2013 | CVR Automated Test Station (CATS) / Recorder Interface Unit (RIU) Operator's Manual | CATS / RIU Operator's Manual | 17TES0700, 17TES0710 | |
| CATS - Software | Service Bulletin | SB002-CATS | Initial | 6/15/2017 | CVR Automatic Test Station (CATS) Software v2.2 | CVR Automatic Test Station (CATS) Software v2.2, Acron Aviation | 17TES0420 | |
| CATS - Software | Service Bulletin | SB003-CATS | Initial | 10/30/2023 | CVR Automatic Test Station (CATS) Software v2.4 | CVR Automatic Test Station (CATS) Software v2.4, Acron Aviation | 17TES0420 | |
| CATS - Software | Service Letter | SIL-001-CATS | 00 | 6/20/2023 | Service Information Letter | FA2100 CVR (P/N 2100-1227-02) failing power consumption test when using CATS software. | 17TES0700, 2100-1227-02, 17TES0710 | |
| CATS - Software | Service Letter | SIL-001-L3AP | 00 | 5/27/2021 | CVR audio data. | If synchronized CVR audio data is required, the .CVR format must be downloaded from the recorder. The .CVR format will produce synchronized audio between all channels | n/A | |
| CD-2001 | Service Bulletin | SB501-1172-1 | 7/26/2005 | SB501-1172-1 | 501-1172-( ) | |||
| CD-2001 | Service Bulletin | SB501-1172-2 | Orig | 10/1/1977 | To replace lamp overlay plate. | 501-1172-01, 501-1172-02 | ||
| CD605 | Service Bulletin | SB805-10007-1 | A | 12/14/2005 | An inspection modification to verify the RNG and TEST push button backlighting is NVIS Type I, Class B compatible (i.e., NVIS green backlighting). | , Acron Aviation | 805-10007-013 | |
| CD605 | Service Letter | SL-266 | A | 3/21/2011 | Recommended Alternate Display Options | 805-10007-005, 805-10007-006, 805-10007-007, 805-10007-008 | ||
| CDU-600 | Miscellaneous | ETM-600 N/A | x.x | 1/1/2023 | Information on ETM-600 | Engine Temperature Monitor - Discontinued product. | 501-1460-01 501-1513-01 | |
| CICC/3 | Installation Manual | 165E4049-00 | 01 | 10/25/2007 | CICC/3 Installation Sheet | Installation Instructions for using CICC3 The CICC/3 requires Rose 3.8 or higher on a PC running Windows XP SP2. | 17TES0075 | |
| CICC/3 | Service Bulletin | CICC2-SB001 | original | 11/26/2007 | Service Bulletin, CICC/3, MOD 1 | Customers using the CICC/3 with the 45-foot extension cable, p/n 17TES0039, occasional downloading errors were occurring. This service bulletin introduces a software modification to remedy this problem. Acron Aviation | 17TES0075 | |
| CICC/3 | Service Bulletin | CICC2-SB002 | original | 3/23/2017 | Service Bulletin, CICC/3, MOD 2 | When using the CICC/3 with FA2100 NAND memory CVRs, CVDRs or FDRs, occasional downloading errors were occurring. Refer to Table 1 for information on the NAND memory, Acron Aviation upgrades to the FA2100s | 17TES0075 | |
| CICC/3 | Service Bulletin | SB003-CICC3 | 00 | 3/28/2023 | Service Bulletin, CICC/3, MOD 3 | Update Portable Interface CCIC/3 to replace obsolete cable with new external interconnect cable assembly. Acron Aviation | 17TES0075 | |
| CICC/4 | Service Letter | CICC4-001 | 02 | 8/4/2021 | Notification of obsolescence | Service Information Letter | 17TES0073 | |
| CM-710 | Component Maintenance Manual | TP-407 | 34-20-21 | 4 | 7/17/2017 | Maintenance Manual | Pub# TP-407 | 501-1515-01, 501-1515-02, 501-1516-01, 501-1517-01, 501-1517-02, 501-1518-01, 501-1518-02, 501-1518-03 |
| DB682 | Installation Manual | 009-10099-001 | Orig | 12/8/1995 | Installation Manual | Pub# 009-10099-001 | 805D0650-01, 805D0650-02, 805D0650-03 | |
| DB682 | Pilot Guide | 002A0652 | 2 | 11/21/1995 | Pilot's Guide | Pub# 002A0652 | 805D0650-01, 805D0650-02, 805D0650-03 | |
| DCM | Installation Manual | TP-582 | G | 3/4/2010 | Installation and Operation Manual, GH-3100, sw 4.0 | Pub# TP-582 | 501-1826-01, 501-1860-0102, 501-1860-0104, 501-1870-( ) | |
| DCM | Installation Manual | TP-559 | K | 3/30/2017 | Installation and Operation Manual, GH-3100, SW 3.0 | This manual contains installation and operating information for the GH Electronic Standby Instrument System. Information in this manual includes the following products: GH-3100 Electronic Standby Indicator (with 1.3, 1.4 or 3.0 software), DCM-3100 Detachable configuration Module, and MAG-3000 / MAG-3100 Magnetometer. This information is supplemented and kept current by revisions, service letters and service bulletins. | 501-1826-01, 501-1826-02, 501-1860-0101, 501-1860-0103, 501-1860-0201, 501-1860-0203, 501-1860-0301, 501-1860-0303, 501-1860-0401, 501-1860-0403, 501-1860-0501, 501-1860-0503, 501-1860-0601, 501-1860-0603, 501-1860-0701, 501-1860-0703, 501-1860-1101, 501-1860-1103, 501-1860-1201, 501-1860-1203, 501-1860-1301, 501-1860-1303, 501-1860-1401, 501-1860-1403, 501-1860-1501, 501-1860-1503, 501-1860-1601, 501-1860-1603, 501-1860-1701, 501-1860-1703, 501-1860-1801, 501-1860-1803, 501-1860-2101, 501-1860-2103, 501-1860-2201, 501-1860-2203, 501-1870-( ) | |
| DCM | Service Bulletin | SB501-1803-1 | A | 5/10/2010 | To provide missing labeling information | 501-1803 | ||
| DCM | Service Bulletin | SB9230-34004-1 | A | 3/22/2012 | Missing TSO markings | To provide instructions on incorporating TSO markings on the OCM. | 9230-34004-01 | |
| DCM | Service Bulletin | SB9230-34012-1 | A | 7/31/2012 | Missing TSO markings | To provide instructions on incorporating TSO markings on the Configuration Module. | 9230-34012-01 | |
| DCM | Service Letter | SL-262 | A | 11/24/2010 | The customer (IS&S) requested a change to the -143 configuration data on their Detachable Configuration Module | 501-1870-143 | ||
| DCM | Service Letter | SL-259 | A | 7/12/2010 | The DCM-3100 may not be recognized by the GH-310 Electronic Standby Indicator at startup. | 501-1870-() | ||
| DG-110 | Component Maintenance Manual | TP-255 | 1 C4 | 4/6/1983 | DG-106D Overhaul Manual | DG-106D | 501-1149-01 | |
| DGS-710 | Component Maintenance Manual | TP-407 | 34-20-21 | 4 | 7/17/2017 | Maintenance Manual | Pub# TP-407 | 501-1515-01, 501-1515-02, 501-1516-01, 501-1517-01, 501-1517-02, 501-1518-01, 501-1518-02, 501-1518-03 |
| DGS-710 | Component Maintenance Manual | TP-474 | 1 | 7/20/1994 | Component Maintenance Manual | Pub# TP-474 | 510-1140-01, 510-1140-02 | |
| DGS-710 | Installation Manual | TP-429 | 34-20-26 | Orig | 12/1/1989 | Installation Manual | Pub# TP-429 | 501-1518-01, 501-1518-02 |
| DGS-710 | Service Bulletin | SB501-1517-1 | B | 10/1/1995 | Installation of new thread forming inserts into the Integrally Illuminated Information Panel that prevents panel and inserts from separating. | 501-1517-01, 501-1517-02 | ||
| DGS-710 | Service Bulletin | MOD 1 and 2 | A | 12/8/2015 | SB501-1515-13 | To incorporate the cut-and-jumper modifications from Mod 1 and Mod 2 into the Computer CCA layout | 501-1515-01 | |
| DI681 | Component Maintenance Manual | 009A0550 | Orig | 8/1/1985 | Installation and Maintenance Manual | Pub# 009A0550 | 805D0500, 805D0520, 805D0530, 805D0550-( ), 805D0570, 805D0580 | |
| DI681 | Service Bulletin | SB-50 | Orig | 10/1/1984 | Sperry EFIS interface modification | , Acron Aviation | 805D0570 | |
| DI681 | Service Bulletin | SB-46 | Orit | 9/1/1984 | To eliminate wavering left/right needle and erratic OBS operation. | , Acron Aviation | 805D0550 | |
| DI681 | Service Bulletin | SB-44 | Orig | 6/1/1984 | To allow the RNC601 to communicate with the DI681 DataBase. | , Acron Aviation | 805D0550 | |
| DI681 | Service Bulletin | SB-57 | Orig | 2/1/1988 | To allow DI681 to operate as DI681A with RNC601B. | , Acron Aviation | 805D0570 | |
| DM58 | Installation Manual | 165E5822-00 | 03 | 11/15/2023 | Installation and Operation Instruction Manual, DM58 | MODEL DM58 PRE−AMPLIFIED DIGITAL MICROPHONE, Acron Aviation | DM58-0048-10 DM58-0148-00 | |
| DME | Installation Manual | 009A0305 | C1 | 12/1/1990 | Installation Manual | Pub# 009A0305 | 805C0604-0x, 805C0620-4x | |
| DME | Installation Manual | 009A0601 | Orig | 1/1/1986 | Installation Manual | Pub# 009A0601 | ||
| DME | Pilot Guide | 009A0602 | 0 | 7/26/2005 | Operations Manual | Pub# 009A0602 | ||
| DME | Pilot Guide | 009A0302 | Orig | 8/1/1988 | TCN 970 Pilot Guide | TCN 970 Pilot Guide | 805D0602, 805D0602-00, 805D0602-01, 805D0602-02 | |
| DME675 | Installation Manual | 009A0305 | C1 | 12/1/1990 | Installation Manual | Pub# 009A0305 | 805C0604-0x, 805C0620-4x | |
| DN-10 | Service Bulletin | SB5-2000-10 | CXL | 7/26/2005 | SB5-2000-10 | |||
| DN-10 | Service Bulletin | SB5-2000-11 | Orig | 11/1/1975 | To remove yaw sync operation during initial starting cycle. | 5-2000-01, 5-2000-02, 5-2000-03, 5-2000-04, 5-2000-05, 5-2000-06 | ||
| DN-10 | Service Bulletin | SB5-2000-12 | Orig | 7/1/1977 | To modify Slaving Pre-amp and Servo amp to provide linear annunciation output of "4/ into 1K 200 micro amp meter. | 5-2000-01, 5-2000-02, 5-2000-03, 5-2000-04, 5-2000-05, 5-2000-06, 5-2000-07 | ||
| DN-10 | Service Bulletin | SB5-2000-13 | A | 1/1/1988 | To minimize introduction of moisture and provide short-circuit protection. | 5-2000-01, 5-2000-02, 5-2000-03, 5-2000-04, 5-2000-05, 5-2000-06, 5-2000-07 | ||
| DN-10 | Service Bulletin | SB5-2000-14 | A | 12/1/1977 | To verify proper wattage resistors on servo amp boards. | 5-2000-07 | ||
| DN-10 | Service Bulletin | SB5-2000-15 | A | 2/1/1987 | To replace fuse with slow blow fuse. | 5-2000-01, 5-2000-02, 5-2000-03, 5-2000-04, 5-2000-05, 5-2000-06, 5-2000-07 | ||
| DN-10 | Service Bulletin | SB5-2000-16 | A | 4/24/2003 | To insure proper HSI flag voltage is maintained when using Relay Circuit Card Assembly part number 542-1964-02. | 5-2000-(), 5-2000-01, 5-2000-02, 5-2000-03, 5-2000-04, 5-2000-05, 5-2000-06, 5-2000-07 | ||
| DN-10 | Service Bulletin | SB5-2000-5 | Orig | 2/1/1969 | To provide two flag capability for Directisyns with single flag capability. | 5-2000-01, 5-2000-02, 5-2000-03, 5-2000-04, 5-2000-05, 5-2000-06, 5-2000-07 | ||
| DN-10 | Service Bulletin | SB5-2000-6 | B | 3/1/1988 | To provide for slaving adjustment. | 5-2000-01, 5-2000-02, 5-2000-03, 5-2000-04, 5-2000-05, 5-2000-06, 5-2000-07 | ||
| DN-10 | Service Bulletin | SB5-2000-7 | Orig | 4/1/1970 | To provide for solid state time delay. | 5-2000-01, 5-2000-02, 5-2000-03, 5-2000-04, 5-2000-05, 5-2000-06, 5-2000-07 | ||
| DN-10 | Service Bulletin | SB5-2000-8 | A | 11/1/1975 | To minimize heading error during turns. | 5-2000-01, 5-2000-02, 5-2000-03, 5-2000-04, 5-2000-05, 5-2000-06, 5-2000-07 | ||
| DN-10 | Service Bulletin | SB5-2000-9 | Orig | 9/1/1975 | To provide gyro with solid state synchronizer. | 5-2000-01, 5-2000-02, 5-2000-03, 5-2000-04, 5-2000-05, 5-2000-06, 5-2000-07 | ||
| DN-501 | Component Maintenance Manual | TP-395 | 7/26/2005 | Maintenance Manual | Pub# TP-395 | 501-1359-02 | ||
| DN-501 | Installation Manual | TP-394 | 34-20-19 | Revision 1 | 11/15/1989 | Installation Manual | Directisyn | 501-1359-02 |
| DU-42 | Installation Manual | 0040-38501-01 | D | 6/2/2016 | DU-42 Installation Manual | Rev C, Incorporate minor changes to mating connector & details on pull up resistor for dimming control | 9200-38500, 9200-38600 | |
| DU-42 | Pilot Guide | 0040-38500-01 | D | 3/17/2023 | DU-42 Pilots Guide | Pilots Guide | 9200-38500 9200-38600 | |
| DU-42 | Printer Copies | 0040-38500-01PC | D | 3/17/2023 | DU-42 Pilots Guide | Printer copy DU-42 PG | 9200-38500-( ) 9200-38600-( ) | |
| DU-42 | Service Bulletin | SB9200-38600-1 | A | 5/12/2015 | DU-42 - MOD A | To prevent counter-rotation of the rear connector standoffs when disconnecting the mating connector. Acron Aviation | 9200-38600-0201 | |
| DU-42 | Service Bulletin | SB9200-38500-1 | A | 5/12/2015 | DU-42 - MOD A | To prevent counter-rotation of the rear connector standoffs when disconnecting the mating connector. Acron Aviation | 9200-38500-0201 | |
| DU-42 | Service Bulletin | SB9200-38500-2 | A | 3/15/2016 | DU-42 MOD B | Incorporation of MOD B, Acron Aviation | 9200-38500, 9200-38500-0201 | |
| DU-42 | Service Bulletin | SB9200-38600-2 | A | 3/15/2016 | DU-42 MOD B | Incorporates MOD B to the DU-42, Acron Aviation | 9200-38600, 9200-38600-0201 | |
| DU-42 | Service Bulletin | SB9200-38500-5 | A | 8/14/2017 | Inspection MOD | , Acron Aviation | 9200-38500-0201 | |
| DU-42 | Service Bulletin | SB9200-38600-5 | A | 8/14/2017 | Inspection MOD | , Acron Aviation | 9200-38600-0201 | |
| DU-42 | Service Bulletin | SB9200-38500-3 | A | 4/19/2016 | To improve engagement of the rear connector standoffs to connector J3 | , Acron Aviation | 9200-38500-0201 | |
| DU-42 | Service Bulletin | SB9200-38600-3 | A | 4/19/2016 | DU-42 - MOD C | Improve engagement of the rear connector standoffs to Connector J3. Acron Aviation | 9200-38600-0201 | |
| DU-42 | Service Bulletin | SB9200-38600-4 | A | 8/25/2016 | DU-42 - MOD D | Thermal pads remain in a compressed state after assembly. When the label is removed from A3 per Mod B, the thermal pads must also be replaced to ensure proper heat dissipation from A3 to the cover. Acron Aviation | 9200-38600-0201 | |
| EBDI-4000 | Installation Manual | TP-566 | C | 1/31/2018 | Installation and Operation Manual | Pub# TP-566 | 501-1871-0101, 501-1871-0201 | |
| EBDI-4000 | Service Bulletin | SB501-1871-1 | Orig | 5/15/2003 | Correct length of screw. | 501-1871-0101, 501-1871-0201 | ||
| EBDI-4000 | Service Bulletin | SB501-1871-2 | B | 4/18/2007 | New DSP FPGA release to improve timing margins. | 501-1871-0101, 501-1871-0201 | ||
| EBDI-4000 | Service Bulletin | SB501-1871-3 | C | 1/3/2006 | To reduce the possibility of the display blanking or failing at start up. | 501-1871-0101, 501-1871-0201 | ||
| EBDI-4000 | Service Bulletin | SB501-1871-4 | B | 2/12/2009 | Provide replacement display due to diminishing source. | 501-1871-0101, 501-1871-0201 | ||
| EFB | Pilot Guide | 165E4860-02 | 4 | 2/17/2015 | Operation Manual | L-3 CrewMate 840 Electronic Flight Bag OPERATOR’S MANUAL | DISPLAY UNIT N01A10000X AIRCRAFT INTERFACE UNIT N01A20000X DOCKING STATION N01A30000X DOCKING CABLE N01A40000X HOTEL KIT N01A50000X | |
| EFB | Service Letter | EFB-SIL-005 | 00 | 1/18/2024 | Service Information Letter | Obsolescence Notice for the Crewmate 840 Electronic Flight Bag (EFB) | Display Unit N01A10000X Aircraft Interface Unit N01A20000X Docking Station N01A30000X Docking Cable N01A40000X Hotel Kit N01A50000X | |
| EFD-750 | Drawings / SPEC | 0100-15753-01 | D | 2/17/2023 | Interface Control Document (Platform), EFD-750 | The purpose of this document is to describe pin level interfaces to the hardware of the L3Harris Aviation Products, Inc., Model EFD-750. This data is generated for customer use at the engineering level. | 9200-15750-01 | |
| EFD-750 | Installation Aircraft Tools | 576-6343-04 (rev 01) | A | 4/22/2025 | ACM Tool for Software 1.4 (EFD-750) | ACM Tool for Software 1.4 (EFD-750) aircraft configuration file version (1.03), ACM Tool (revision 1.00 and 1.01) | 9200-15753-0101 9200-15754-0101 9200-15754-0201 9200-15754-0301 9200-15756-0301 | |
| EFD-750 | Installation Aircraft Tools | 576-6343-04 | A | 2/17/2023 | ACM Tool for Software 1.3 (EFD-750) | ACM Tool for Software 1.3 (EFD-750) aircraft configuration file version (1.03), ACM Tool (revision 1.00) | 9200-15753-0101 9200-15754-0101 9200-15754-0201 9200-15754-0301 | |
| EFD-750 | Installation Aircraft Tools | 576-6343-02 | A | 6/26/2019 | ACM Tool for Software 1.1 (EFD-750) | ACM Tool for Software 1.1 (EFD-750) aircraft configuration file version (1.01), ACM Tool (revision 1.00) | 576-6343-02, 9200-15753-0101, 9200-15754-0101, 9200-15754-0201 | |
| EFD-750 | Installation Aircraft Tools | 576-6343-03 | A | 12/12/2019 | ACM Tool for Software 1.2 (EFD-750) | ACM Tool for Software 1.2 (EFD-750) aircraft configuration file version (1.02), ACM Tool (revision 1.00) | 9200-15753-0101, 9200-15754-0101, 9200-15754-0201 | |
| EFD-750 | Installation Aircraft Tools | 576-6343-01 | A | 2/7/2019 | ACM Tool for Software 1.0 (EFD-750) | ACM Tool for Software 1.0 (EFD-750) aircraft configuration file version (1.00), ACM Tool (revision 1.00) | 576-6343-01, 9200-15750-0101, 9200-15751-0101, 9200-15751-0201, 9200-15753-0101, 9200-15754-0101, 9200-15754-0201 | |
| EFD-750 | Installation Aircraft Tools | 576-6439-02 | A | 9/23/2020 | ACM Tool | Aircraft Configuration Module Tool, SIM-750 Simulator | ||
| EFD-750 | Installation Manual | 0040-15751-01 | G | 4/14/2025 | Installation Manual, EFD-750 / MAG-500 | Electronic Flight Display System EFD-750 Electronic Flight Display MAG-500 Magnetometer | 9200-15751-0101, 9200-15753-0101, 9200-15754-0101, 9200-15754-0201, 9200-15750-0101, 9200-15751-0201, 9200-15754-0301, 9200-15756-0301. 9200-15500-0101, 9200-15500-0201 | |
| EFD-750 | Installation Manual | 0040-15800-01 | 01 | 4/21/2025 | Installation Manual, SIM-750 | Electronic Flight Display Simulator Model: SIM-750 (Acron Aviation) | 9200-15800-0101 9200-15800-0301 | |
| EFD-750 | Pilot Guide | 0040-15750-01 | E | 4/14/2025 | Operation Manual, EFD-750 | Electronic Flight Display System | 9200-15753-0101, 9200-15754-0101, 9200-15754-0201, 9200-15751-0101, 9200-15751-0201, 9200-15750-0101, 9200-15756-0301. | |
| EFD-750 | Service Bulletin | SB004-EFD-750 | EFD750-34-6002 | 00 | 4/14/2025 | Service Bulletin, Release 1.4 | System Software Release 1.4 | 9200-15753-0101, 9200-15754-0101, 9200-15754-0201, 9200-15754-0301 |
| EFD-750 | Service Bulletin | SB003-EFD-750 | EFD750-34-6001 | 01 | 4/21/2025 | Service Bulletin, Release 1.3 | System Software Release 1.3 incorporates new functions listed below. • New option to allow an alternate color scheme for Airspeed Awareness Color Bar depiction for Part 27/29. • New option to allow an alternate Aircraft Reference Symbol depiction (Acron Aviation) | 9200-15753-0101, 9200-15754-0101, 9200-15754-0201, 9200-15754-0301 |
| EFD-750 | Service Bulletin | SB002-EFD-750 | 02 | 4/21/2025 | MOD A – Operational Improvement in Cold Environments | MOD A provides improved reliability, especially during operation at cold ambient temperatures of -15 Celsius and below. Acron Aviation | 9200-15750-0101, 9200-15751-0101, 9200-15751-0201, 9200-15753-0101, 9200-15754-0101, 9200-15754-0201 | |
| EFD-750 | Service Bulletin | SB001-EFD-750 | B | 4/21/2025 | Service Bulletin, Release 1.2 | System Software Release 1.2. Acron Aviation | 9200-15753-0101, 9200-15754-0101, 9200-15754-0201 | |
| EFD-750 | Service Letter | SIL-001-EFD-750 | 01 | 4/21/2025 | Service Information Letter | The Skylight Avionics NAV/CONV Navigation Signal Converter is an optional navigation source called out in AML STC ST02718LA used for VOR/ILS presentation on the EFD-750 flight display. (Acron Aviation) | 9200-15753-0101 and 9200-15754-0101 | |
| EFD-750 | Software | 8010-15750-0104 | A | 4/18/2025 | System Software Version 1.4 | Software Executable Object Code, EFD-750 | 9200-15753-0101 9200-15754-0101 9200-15754-0201 9200-15754-0301 9200-15756-0301 | |
| EFD-750 | Software | EFD-750 Software 1.1 | 0 | 6/26/2019 | EFD-750 Software 1.1 | System Software 1.1 | 576-6343-02, 8010-15750-0101, 9200-15753-0101, 9200-15754-0101, 9200-15754-0201 | |
| EFD-750 | Software | EFD-750 Software 1.2 | 0 | 12/12/2019 | EFD-750 Software 1.2 | System Software 1.2 | 8010-15750-0102, 9200-15753-0101, 9200-15754-0101, 9200-15754-0201 | |
| EFD-750 | Software | 8010-15750-0103 | 1.3 | 2/17/2023 | System Software Version 1.3 | Software Executable Object Code, EFD-750 | 9200-15753-0101 9200-15754-0101 9200-15754-0201 9200-15754-0301 | |
| EFD-750 | Supplemental Type Certificate | 9002455-001 | C | 12/20/2021 | Supplemental Type Certificate AML ST02718LA, EFD-750 | Installation of EFD-750 Electronic Flight Display (0031-15750-01) | 0031-15750-01, 9002455-001 | |
| EFI-650 | Component Maintenance Manual | 13131-A037 | 2 | 8/9/2017 | EFI-650 Component Maintenance Manual (level 1) ATR | EFI-650 Component Maintenance Manual (level 1) ATR | E57A000-00-000 | |
| EFI-650 | Component Maintenance Manual | 13131-A903 | 1 | 11/3/2016 | EFI-650 Component Maintenance Manual | EFI-650 Component Maintenance Manual (level 1) | E57A000-00-000, E57A000-00-100, E57A000-00-200 | |
| EFI-650 | Component Maintenance Manual | 0040-E57A2-01 | A | 12/20/2019 | Maintenance Manual | EFI-650 Component Maintenance Manual (level 2) EHA Repair | E57A000-00-200, E57A000-00-000, E57A000-00-100 | |
| EFI-650 | Component Maintenance Manual | 0040-E57A0-01 | H | 4/16/2024 | Component Maintenance Manual | EFI-650 Component Maintenance Manual (level 2) | E57A000-00-000, E57A000-00-100, E57A000-00-200 | |
| EFI-650 | Installation Manual | 13131‐A907 | C | 5/23/2019 | Installation and Operation Manual | EFI-650 Installation and Operation Manual | E57A000-00-000, E57A000-00-100, E57A000-00-200 | |
| EFI-650 | Installation Manual | 13131‐A908 | A | 5/23/2019 | Installation and Operation Manual (ATR), EFI-650 | EFI-650 Installation and Operation Manual (ATR) | E57A000‐00‐000 | |
| EFI-650 | Installation Manual | 0040-E57A1-01 | A | 9/25/2019 | TroubleShooting Guide | Aircraft Level Troubleshooting Procedures | E57A000-00-000, E57A000-00-100, E57A000-00-200 | |
| EFI-650 | Service Bulletin | SB001-EFI-650 | 00 | 3/7/2024 | Service Bulletin, MOD A (PN E57A000-00-000, ATR) | Modification A to remove diodes from rear connector circuit card assembly. | E57A000-00-000 | |
| EFI-650 | Service Bulletin | SB002-EFI-650 | 00 | 4/10/2024 | Service Bulletin, MOD A (PN E57A000-00-100, E57A000-00-200) | Modification A to remove diodes from rear connector circuit card assembly. | E57A000-00-100, E57A000-00-200 | |
| EHSI-4000 | Installation Manual | TP-580 | B | 12/6/2007 | Installation and Operation Manual | Pub# TP-580 | 501-1879-0101, 501-1879-0201 | |
| EHSI-4000 | Pilot Guide | TP-581 | B | 8/12/2008 | Pilot's Guide | Pub# TP-581 | 501-1879-0101 | |
| EHSI-4000 | Pilot Guide | TP-627 | A | 4/15/2008 | EHSI-4000 REL 2.X | EHSI-4000 Pilots Guide | 501-1879-0102 | |
| EHSI-4000 | Printer Copies | TP-627PC | A | 4/15/2008 | Pilot's Guide | Printer copy EHSI-4000 PG | 501-1879-0102 | |
| EHSI-4000 | Service Bulletin | SB501-1879-4 | B | 2/12/2009 | Provide replacement display due to diminishing source. | 501-1879-0101 | ||
| EHSI-4000 | Service Bulletin | SB501-1879-5 | A | 2/12/2009 | Provide replacement display due to dimminishing source | Provide replacement display due to dimminishing source | 501-1879-0101, 501-1879-0102 | |
| EHSI-4000 | Service Bulletin | SB501-1879-5 | A | 2/12/2009 | Provide replacement display due to diminishing source | Provide replacement display due to diminishing source | 501-1879-0101, 501-1879-0102 | |
| EHSI-4000 | Service Bulletin | SB501-1879-3 | B | 2/3/2006 | To reduce the possibility of the display blanking or failing at start up. | 501-1879-0101 | ||
| EHSI-4000 | Service Bulletin | SB501-1879-1 | A | 8/15/2003 | Correct length of screw. | 501-1879-0101 | ||
| EHSI-4000 | Service Bulletin | SB501-1879-2 | A | 8/15/2003 | To prevent shorting of diode during lightning testing which removed reversed input protection. | 501-1879-0101 | ||
| EHSI-4900 | Component Maintenance Manual | 0040-25002-01 | A | 1/21/2019 | EHSI-4900 MM | Electronic Horizontal Situation Indicator | 9200-25000-0201 | |
| EHSI-4900 | Installation Manual | 0040-25001-01 | A | 1/21/2019 | EHSI-4900 IOM | Electronic Horizontal Situation Indicator | 9200-25000-0201 | |
| EHSI-4900 | Intermediate Maintenance Manual | 0040-25003-01 | A | 1/21/2019 | EHSI-4900 IMM | Electronic Horizontal Situation Indicator | 9200-25000-0201 | |
| ESI-1000 | Installation Manual | 0040-32001-01 | U | 10/13/2017 | ESI-1000 Installation Manual | Electronic Standby System This manual contains installation instructions and recommended flightline maintenance information for the ESI-1000 Electronic Standby Indicator Release 1.0, 1.1, 2.0 and 2.1. | 9200-32000-0101 9200-32000-( ) 9200-32100-( ) | |
| ESI-1000 | Instructions for Continued Airworthiness iCA | E08046-3400-B002 | A | 6/10/2009 | Instructions for Continued Airworthiness ESI-1000 | Instructions for Continued Airworthiness ESI-1000 | ESI-1000, 9200-32000, 9200-21200-01 | |
| ESI-1000 | Pilot Guide | 0040-32000-01 | G | 10/24/2017 | ESI-1000 Pilots Guide | PUB# 0040-32000-01 | 9200-34000-0101 | |
| ESI-1000 | Printer Copies | 0040-32000-01PC | G | 10/24/2017 | ESI-1000 Pilots Guide | Printer copy ESI-1000 PG | 9200-32000-( ) 9200-32100-( ) | |
| ESI-1000 | Service Bulletin | SB9200-32000-7 | A | 9/15/2016 | To prevent rate sensor loopback failure at start up. | To prevent rate sensor loopback failure at start up, Acron Aviation | 9200-32000-0101, 9200-32000-0201, 9200-32000-0301, 9200-32000-0401, 9200-32000-0701, 9200-32000-0801 | |
| ESI-1000 | Service Bulletin | SB9200-32100-6 | A | 9/14/2016 | To prevent rate sensor loopback failure at Startup | To prevent rate sensor loopback failure at Startup, Acron Aviation | 9200-32100-0101, 9200-32100-0201, 9200-32100-1001, 9200-32100-3203 | |
| ESI-1000 | Service Bulletin | SB9200-32100-4 | A | 3/18/2016 | Eliminate the possibility of power supply test-points (TP16, TP18, and TP21) being shorted against the top cover threaded plate (Mod D) | Eliminate the possibility of power supply test-points (TP16, TP18, and TP21) being shorted against the top cover threaded plate (Mod D), Acron Aviation | 9200-32100-1001 | |
| ESI-1000 | Service Bulletin | SB9200-32100-5 | A | 4/1/2016 | Eliminate the possibility of Power Supplyt Test points being shorted | Eliminate the possibility of Power Supplyt Test points being shorted, Acron Aviation | 9200-32100-0201 | |
| ESI-1000 | Service Bulletin | SB9200-32000-3 | A | 3/29/2012 | To standardize DSP boards across ESI product line | 9200-32000-0101, 9200-32000-0201, 9200-32000-0601 | ||
| ESI-1000 | Service Bulletin | SB9200-32000-4 | A | 4/9/2012 | Replace obsolete LED Backlight assembly | , Acron Aviation | 9200-32000-0101, 9200-32000-0201, 9200-32000-0301, 9200-32000-0401, 9200-32000-0701, 9200-32000-0801 | |
| ESI-1000 | Service Bulletin | SB9200-32000-5 | A | 8/23/2012 | Improve backlight low end brightness characteristics | , Acron Aviation | 9200-32000-0101, 9200-32000-0201, 9200-32000-0301, 9200-32000-0401, 9200-32000-0701, 9200-32000-0801 | |
| ESI-1000 | Service Bulletin | SB9200-32100-3 | A | 8/23/2012 | Improve backlight low end brightness characteristics | , Acron Aviation | 9200-32100-0101, 9200-32100-0201, 9200-32100-1001 | |
| ESI-1000 | Service Bulletin | SB9200-32000-6 | A | 12/17/2012 | Incorporation of 1.1 Software | , Acron Aviation | 9200-32000-0301, 9200-32000-0401, 9200-32000-0701, 9200-32000-0801 | |
| ESI-1000 | Service Bulletin | SB9200-32100-1 | A | 12/22/2010 | LED Backlight is obsolete | , Acron Aviation | 9200-32100-0101, 9200-32100-0201, 9200-32100-1001 | |
| ESI-1000 | Service Bulletin | SB9200-32000-1 | A | 5/3/2010 | Revise night lighting color from blue to white | , Acron Aviation | 9200-32000-0301, 9200-32000-0401 | |
| ESI-1000 | Service Bulletin | SB9200-32000-2 | B | 8/6/2012 | Incorporation of Mod 2 | , Acron Aviation | 9200-32000-0101, 9200-32000-0201, 9200-32000-0301, 9200-32000-0401 | |
| ESI-1000 | Service Bulletin | SB9200-32100-2 | A | 4/4/2011 | Incorporation of Mod B | , Acron Aviation | 9200-32100-0101, 9200-32100-0201, 9200-32100-1001 | |
| ESI-1000 | Service Letter | SL-273 | A | 9/28/2011 | ESI-1000 Corrected Vmo Table Definition data | 9200-32100-1001 | ||
| ESI-1000 | Service Letter | SL-277 | A | 8/21/2013 | Trilogy Congiuration Tool | Trilogy Configuration Tool | 9200-32100-0101, 9200-32100-0201, 9200-32100-1001, 9200-32500, 9200-32500-0011, 9200-32500-0021, 9200-32500-0031, 9200-32500-0041, 9200-32500-0051, 9200-32500-0061, 9200-32500-0071, 9200-32500-0081, 9200-32500-0121 | |
| ESI-1000 | Service Letter | SL-254 | E | 2/5/2013 | ESI-1000/2000 AML STC | ESI-1000/2000 AML STC | 9200-32000-0101, 9200-32000-0201, 9200-32100-0101, 9200-32100-0201, 9200-32500-0011, 9200-32500-0021 | |
| ESI-1000 | Service Letter | SL-327 | B | 7/27/2017 | ESI-1000/2000 end of production | ESI-1000/2000 end of production | 9200-32000, 9200-32100, 9200-32500 | |
| ESI-1000 | Supplemental Type Certificate | SA02738CH | 0 | 2/15/2022 | ESI-1000 and ESI-2000 - Permission to Use AML STC | ESI-1000 and ESI-2000 | 0 | |
| ESI-2000 | Installation Manual | 0040-32501-01 | L | 8/1/2018 | ESI-2000 Installation Manual | Rev L corrections only. | 9200-32500-0011, 9200-32500-0021, 9200-32500-0031, 9200-32500-0041 | |
| ESI-2000 | Pilot Guide | 0040-32500-01 | E | 3/25/2011 | ESI-2000 Pilots Guide | Pub# 0040-32500-01 | 9200-32500-() | |
| ESI-2000 | Service Bulletin | SB9200-32500-4 | A | 9/14/2016 | To prevent rate sensor loopback failure at statrt up | To prevent rate sensor loopback failure at statrt up. Acron Aviation | 9200-32500-0011, 9200-32500-0021, 9200-32500-0031, 9200-32500-0041, 9200-32500-0051, 9200-32500-0061, 9200-32500-0071, 9200-32500-0081, 9200-32500-0121 | |
| ESI-2000 | Service Bulletin | SB9200-32500-1 | A | 11/11/2010 | Release of new software | Software 1.12, Acron Aviation | 9200-32500-0011, 9200-32500-0021, 9200-32500-0031, 9200-32500-0041 | |
| ESI-2000 | Service Bulletin | SB9200-32500-3 | A | 8/23/2012 | Improve backlight low end brightness | Improve backlight low end brightness, Acron Aviation | 9200-32500-0011, 9200-32500-0021, 9200-32500-0031, 9200-32500-0041, 9200-32500-0061, 9200-32500-0081, 9200-32500-0121 | |
| ESI-2000 | Service Bulletin | SB9200-32500-2 | A | 4/4/2011 | Incorporate Mod B by adding washers and updating software to Version 1.2 | Incorporate Mod B by adding washers and updating software to Version 1.2, Acron Aviation | 9200-32500-0011, 9200-32500-0021, 9200-32500-0031, 9200-32500-0041 | |
| ESI-2000 | Service Letter | SL-268 | A | 6/7/2011 | To provide information on the installation of the ESI-2000 (P/N 9200-32500-0121) on a Piper Cheyenne II, Type Certificate Data Sheet (TCDS): A8EA | 9200-32500-0121 | ||
| ESI-2000 | Service Letter | SL-277 | A | 8/21/2013 | Trilogy Congiuration Tool | Trilogy Configuration Tool | 9200-32100-0101, 9200-32100-0201, 9200-32100-1001, 9200-32500, 9200-32500-0011, 9200-32500-0021, 9200-32500-0031, 9200-32500-0041, 9200-32500-0051, 9200-32500-0061, 9200-32500-0071, 9200-32500-0081, 9200-32500-0121 | |
| ESI-2000 | Service Letter | SL-286 | C | 4/1/2016 | Annual battery maintenance | ESI-2000 Battery Maintenance | 9200-32500, 9200-32501 | |
| ESI-2000 | Service Letter | SL-254 | E | 2/5/2013 | ESI-1000/2000 AML STC | ESI-1000/2000 AML STC | 9200-32000-0101, 9200-32000-0201, 9200-32100-0101, 9200-32100-0201, 9200-32500-0011, 9200-32500-0021 | |
| ESI-2000 | Service Letter | SL-327 | B | 7/27/2017 | ESI-1000/2000 end of production | ESI-1000/2000 end of production | 9200-32000, 9200-32100, 9200-32500 | |
| ESI-2000 | Software | ESI-2000 Config S/W | 1.0 | 9/12/2013 | ESI-2000 Configuration S/W | ESI-2000 Configuration S/W | 576-6217-01, 9200-32500 | |
| ESI-2000 | Supplemental Type Certificate | SA02738CH | 0 | 2/15/2022 | ESI-1000 and ESI-2000 - Permission to Use AML STC | ESI-1000 and ESI-2000 | 0 | |
| ESI-500 | Installation Manual | 0040-15001-01 | K | 4/29/2025 | ESI-500 /MAG-500 Installation Manual | Electronic Standby Indicator | 9200-15000-0101, 9200-15500-0101 | |
| ESI-500 | Pilot Guide | 0040-15000-01 | G | 4/28/2025 | Pilot Guide, ESI-500 | Electronic Standby Instrument System, Acron Aviation | 9200-15000-0101, 9200-15500-0101 | |
| ESI-500 | Pilot Guide | 0040-15000-01 Printcopy | G | 4/28/2025 | Pilot Guide, ESI-500 Print copy | Electronic Standby Instrument System, Acron Aviation | 9200-15000-0101, 9200-15500-0101 | |
| ESI-500 | Service Bulletin | SB9200-15000-1 | B | 4/29/2025 | MOD A | Applies to S/N 1021; 1025; 1029; 1030; &1032 | 9200-15000-0101 | |
| ESI-500 | Service Bulletin | SB9200-15000-5 | B | 4/29/2025 | ESI-500 MOD C | To correct a problem where the unit may restart and operate from the battery immediately after shutdown. | 9200-15000-0101 | |
| ESI-500 | Service Bulletin | SB9200-15000-3 | B | 4/29/2025 | The units airspeed sensor output may shift | 9200-15000-0101 | ||
| ESI-500 | Service Bulletin | SB9200-15000-2 | B | 4/29/2025 | Information on ESI-500 Software 1.2 | 9200-15000-0101 | ||
| ESI-500 | Service Bulletin | SB9200-15000-4 | B | 4/29/2025 | Informs customers of 1.3 Software release | Informs customers of 1.3 Software release | 9200-15000-0101 | |
| ESI-500 | Service Bulletin | SB9200-15000-6 | B | 4/29/2025 | ESI-500 MOD D | The vertical speed output from the ESI-500 can potentially exceed the tolerances specified for an air data computer | 9200-15000-0101 | |
| ESI-500 | Service Letter | SL-329 | A | 1/11/2018 | ESI-500 Battery Calibration | Battery Calibration | 9200-15000-0101 | |
| ESI-500 | Service Letter | SL-316 | B | 4/29/2025 | 68DC & 71DC Database Subscription | 68DC & 71DC Database Subscription | 9200-15000-0101 | |
| ESI-500 | Service Letter | SL-323 | B | 4/29/2025 | Setting The Real Time Clock | Setting the Real Time Clock | 9200-15000-0101 | |
| ESI-500 | Service Letter | SL-305 | B | 4/29/2025 | To Prevent damage to MicroSD Card | To Prevent damage to MicroSD Card | 9200-15000-0101 | |
| ESI-500 | Service Letter | SL-309 | C | 4/29/2025 | ESI-500 Battery Maintenance | Battery Pack Maintenance and Shipping Information for the ESI-500 | 9200-15000-0101 | |
| ESI-500 | Service Letter | SL-345 | A | 8/1/2019 | Synthetic Vision Obstacles Causing Unit Restart | Synthetic Vision Obstacles Causing Unit Restart | 9200-15000-0101 | |
| ESI-500 | Software | ESI-500 Software 1.1 with ACM Tool | 1.1 | 11/18/2015 | ESI-500 Software 1.1 with ACM Tool | ESI-500 Software 1.1 with ACM Tool | 576-6294-01, 9200-15000-0101 | |
| ESI-500 | Software | ESI-500 Software 1.3 W/ ACM Tool | 1.3 | 12/15/2016 | ESI-500 Software 1.3 W/ ACM Tool | ESI-500 Software 1.3 W/ ACM Tool | 9200-15000-0101 | |
| ESI-500 | Software | ESI-500-15000-R01.01 | 1.1 | 11/18/2015 | ESI-500-15000-R01.01 | ESI-500 S/W 1.1 (R01.01) with ACM tool 576-6294-01 | 576-6294-01, 9200-15000-0101, 972-6294-01 | |
| ESI-500 | Software | ESI-500-15000-R01.02 | 1.2 | 4/21/2016 | Software 1.2 With ACM Tool | Software 1.2 With ACM Tool | 576-6294-02, 9200-15000-0101 | |
| ESI-500 | Software | ESI-500-15000-R01.03 | 1.3 | 12/15/2016 | Software 1.3 w/ACM Tool | Software 1.3 w/ACM Tool | 576-6294-03, 9200-15000-0101 | |
| ESI-500 | Supplemental Type Certificate | SA04046CH | D | 9/2/2020 | AML STC for ESI-500 | ESI-500 AML STC Package with ICA & AFMS (part 23) | 9200-15000-0101, 9200-15500-0101 | |
| ESI-500 | Supplemental Type Certificate | SR2487AK | 0 | 11/12/2016 | ESI-500 RW STC (part 27) | ESI-500 RW STC (part 27) | 9200-15000-01 | |
| ESIS-5000 | Installation Manual | 0040-43001-01 | J | 10/11/2023 | Installation Manual | Electronic Standby Instrument System with Touch Screen Revision J adds SW1.3. | 9200-43000-0201 | |
| ESIS-5000 | Intermediate Maintenance Manual | 0040-43003-01 | G | 10/11/2023 | Intermediate Maintenance Manual, Lvl 1 | Standby Display with Touch Screen Level 1 Maintenance Revision G adds software release 1.3 | 9200-43000-0201 | |
| ESIS-5000 | Pilot Guide | 0040-43000-01 | D | 10/11/2023 | Pilots Guide, ESIS-5000 | Standby Display with Touch Screen Revision D includes Software Release 1.3 | 9200-43000-0201 | |
| ESIS-5000 | Service Bulletin | SB9200-43000-3 | A | 2/27/2017 | Software Release 1.1 | Software Release 1.1, Acron Aviation | 9200-43000-0201 | |
| ESIS-5000 | Service Bulletin | SB9200-43000-5 | A | 3/1/2019 | Implement new supplier for bonded display assembly. | Implement new supplier for bonded display assembly. , Acron Aviation | 9200-43000-0201 | |
| ESIS-5000 | Service Bulletin | SB9200-43000-1 | A | 9/24/2015 | Planning MOD | improve the RS-232 transceiver performance at cold temperature, Acron Aviation | 9200-43000-0201 | |
| ESIS-5000 | Service Bulletin | SB9200-43000-2 | A | 3/16/2016 | ESIS-5000 Mod B | Improve the I/O Power Circuit Card Assembly , Acron Aviation | 9200-43000-0201 | |
| ESIS-5000 | Service Bulletin | SB9200-43000-4 | A | 10/16/2018 | MOD C | To remove component interference between I/O Power board and EMI board., Acron Aviation | 9200-43000-0201 | |
| ESIS-5000 | Service Bulletin | SB9200-43000-6 | 00 | 10/13/2020 | MOD E provides information on new Bezel Assembly. | MOD E provides information on new Bezel Assembly., Acron Aviation | 9200-43000-0201 | |
| ESIS-5000 | Service Bulletin | SB9200-43000-7 | 00 | 9/8/2021 | To inform customers of System Software Release 1.2 (version R01.02). | Software Release 1.2 , Acron Aviation | 9200-43000-0201 | |
| ESIS-5000 | Service Bulletin | SB9200-43000-9 | 00 | 10/11/2023 | To inform customers of System Software Release 1.3 (version R01.03). | Software Release 1.3 To correct VOR/TACAN functionality., Acron Aviation | 9200-43000-0201 | |
| ETC-404 | Component Maintenance Manual | TP-399 | 77-30-02 | 1 | 4/12/1990 | Maintenance Manual | Pub# TP-399 | 501-1506-01, 501-1506-02, 501-1506-03, 501-1506-04, 501-1506-05 |
| ETC-404 | Service Letter | SL-119 | Orig | 9/20/1993 | Service Letter, ETC-404 repair | To provide all current repair centers for Model ETC-404E Engine Temperature Cycle Counter with the procedures required to assemble U17 (P/N 545-1016-01) Programmed Microcircuit to A1 Computer Circuit Card Assembly (CCA) (P/N 542-1728-05). | 501-1506-05 | |
| ETM-600 | Miscellaneous | ETM-600 N/A | x.x | 1/1/2023 | Information on ETM-600 | Engine Temperature Monitor - Discontinued product. | 501-1460-01 501-1513-01 | |
| ETM-600 | Service Bulletin | SB501-1460-1 | Orig | 7/26/2005 | To improve power distribution and insure proper operaton. | 501-1460-01 | ||
| ETM-600 | Service Bulletin | SB501-1460-2 | Orig | 12/1/1986 | To improve power distribution and insure proper operation. | 501-1460-01 | ||
| F1000 | Component Maintenance Manual | 165E0503-00 | 31-30-02 | TR6 | 5/12/2017 | F1000 Component Maintenance Manual | F1000 CMM by special request only, Acron Aviation | S903-2000-00, S903-2000-01, S903-2000-02, S603-1000-00, S603-1000-01, S703-1000-00, S703-1000-01, S800-2000-00, S800-2000-01, S800-2000-02, S800-3000-00, S800-3000-01, S800-3000-02, S903-3000-00 |
| F1000 | Installation Manual | 165E235000 | 31-30-02 | Initial | 7/1/2001 | F1000 Installation & Operation Manual S800-2000 / 3000 / 3500 | F1000 IO for S800-2000, S800-3000, S800-3500, Obsolete, Acron Aviation | S800-2000-00, S800-2000-01, S800-2000-02, S800-3000-00, S800-3000-01, S800-3000-02 |
| F1000 | Installation Manual | 165E235001 | 31-30-02 | Initial | 7/1/2001 | F1000 Installation & Operation Manual S603, S703, S903 | F1000 IO for S603-1000, S703-1000, S903-2000, S903-3000, Obsolete, Acron Aviation | S903-2000-00, S903-2000-01, S903-2000-02, S603-1000-00, S603-1000-01, S703-1000-00, S703-1000-01, S903-3000-00 |
| F1000 | Service Bulletin | F1000 SSFDR SB032 | 31-30-02-032 | 01 | 4/27/2011 | Introduction of Refurbished Flash Crash Survivable Store Unit (FCSSU) | Introduction of Refurbished Flash Crash Survivable Store Unit (FCSSU) Part Numbers: 253U1290–00, 253U1290–01 & 253U1290–02, Acron Aviation | s603-xxxx-xx, s703-xxxx-xx, s800-xxxx-xx, s903-xxxx-xx |
| F1000 | Service Bulletin | F1000 SSFDR SB033 | 31-30-02-033 | 01 | 10/11/2000 | Upgrade from to 64/128 WPS, Conversion S800‐2000‐00 to S800‐3000‐00 | Upgrade from to 64/128 WPS, Conversion S800‐2000‐00 to S800‐3000‐00, Acron Aviation | s603-xxxx-xx, s703-xxxx-xx, s800-xxxx-xx, s903-xxxx-xx |
| F1000 | Service Letter | F1000 SSFDR SIL006 | 00 | 10/31/2012 | Discontinued Production of the F1000 SSFDR | Discontinued Production of the F1000 SSFDR, Acron Aviation | s603-xxxx-xx, s703-xxxx-xx, s800-xxxx-xx, s903-xxxx-xx | |
| F1000 | Service Letter | F1000 SSFDR SIL004 | 00 | 2/18/2003 | Part Number Interchangeability for F1000 SSFDR S800 | Part Number Interchangeability for F1000 SSFDR S800, Acron Aviation | s800-xxxx-xx | |
| F1000 | Service Letter | F1000 SSFDR SIL007 | Orig | 8/12/2014 | Access to F1000 Publications | Access to F1000 Publications, Acron Aviation | s603-xxxx-xx, s703-xxxx-xx, s800-xxxx-xx, s903-xxxx-xx | |
| F1000 | Service Letter | PI/2-001 | 03 | 2/12/2024 | Notification of discontinued product. | Notification of discontinued product. | 17TES0062, 17TES0065, 17TES0066, 17TES0092 | |
| F1000 | Service Letter | SIL-001-RAU | 00 | 1/14/2021 | Notification of end of production and sale of the ROSE Analysis Unit. | Notification of end of production and sale of the ROSE Analysis Unit. | 17TES0055, 17TES0060, 17TES0063, 17TES0068 | |
| F3000 | Service Bulletin | SB004-F3000 | 31-40-04-005 | 00 | 5/23/2023 | Service Bulletin for Software 02 | Introduction to New Software P/N 840-E4190-02. To provide new software to upgrade the ARINC 429 interface. Acron Aviation | 3000-1100-00, 3000-1100-01 |
| F3849 | Installation Manual | 009A0301 | 1 | 8/1/1988 | Installation Manual | Pub# 009A0301 | 805C0620-( ), 805D0602-( ), 805D0660-( ), 805D0661-( ), 805D0662-( ), 805D0663-( ) | |
| F3849 | Miscellaneous | F3849 TACAN Control Unit | x.x | 1/1/2023 | Information on F3849 TACAN Control Unit | The F3849 is the TACAN and TACAN+ system. TACAN Control Unit | 805D0660-( ) 805D0665-( ) | |
| F6444 | Installation Manual | 009A0301 | 1 | 8/1/1988 | Installation Manual | Pub# 009A0301 | 805C0620-( ), 805D0602-( ), 805D0660-( ), 805D0661-( ), 805D0662-( ), 805D0663-( ) | |
| F6555 | Installation Manual | 009A0301 | 1 | 8/1/1988 | Installation Manual | Pub# 009A0301 | 805C0620-( ), 805D0602-( ), 805D0660-( ), 805D0661-( ), 805D0662-( ), 805D0663-( ) | |
| F6555 | Miscellaneous | F6555 TACAN Control Unit | x.x | 1/1/2023 | Information on F6555 TACAN Control Unit | TACAN Control Units F3849, F3849A, F6444, & F6555 Series See IOM 0040-35001-01 See CMM 009-10065-001 | 805D0663-() | |
| F6555 | Service Bulletin | SB805D0663-200 | A | 2/10/2005 | Removing Rubber boots from switches | , Acron Aviation | 805D0663-31 | |
| F800 | Component Maintenance Manual | 165E0049-00 | 31-30-01 | 2 | 1/31/1994 | F800 Component Maintenance Manual | Acron Aviation | 17M303–266, 17M303–281, 17M303–282, 17M600–00, 17M600–00A, 17M600–274, 17M603–00, 17M603–261, 17M603–274, 17M603–277, 17M604–00, 17M700–00, 17M700–00A, 17M700–274, 17M703–00, 17M703–01, 17M703–261, 17M703–274, 17M703–275, 17M703–277, 17M800–00, 17M800–00A, 17M800–01A, 17M800–251, 17M800–252, 17M800–253, 17M800–258, 17M800–261, 17M800–262, 17M900–00, 17M900–00A, 17M900–251, 17M900–274, 17M903–00, 17M903–01, 17M903–02, 17M903–261, 17M903–263, 17M903–266, 17M903–274, 17M903–275, 17M903–276, 17M903–277, 17M903–278, 17M903–279, 17M903–281, 17M903–282 |
| F800 | Installation Manual | 165E335200 | 31-30-01 | 01 | 10/1/2003 | F800 17-M900 Installation & Operation Manual | F800 17-M900 Installation & Operation Manual | 17M900–00, 17M900–00A, 17M900–251, 17M900–274 |
| F800 | Installation Manual | 165E335300 | 31-30-01 | 01 | 10/1/2003 | F800 17-M604 Installation & Operation Manual | F800 17-M604 Installation & Operation Manual | 17M604–00 |
| F800 | Installation Manual | 165E335400 | 31-30-01 | Initial | 8/1/2003 | F800 17-M303 Installation & Operation Manual | F800 17-M303 Installation & Operation Manual | 17M303–266, 17M303–281, 17M303–282 |
| F800 | Installation Manual | 165E335500 | 31-30-01 | Initial | 8/1/2003 | F800 17-M703 Installation & Operation Manual | F800 17-M703 Installation & Operation Manual | 17M703–00, 17M703–01, 17M703–261, 17M703–274, 17M703–275, 17M703–277 |
| F800 | Installation Manual | 165E335600 | 31-30-01 | 01 | 10/1/2003 | F800 17-M600 Installation & Operation Manual | F800 17-M600 Installation & Operation Manual | 17M600–00, 17M600–00A, 17M600–274 |
| F800 | Installation Manual | 165E335700 | 31-30-01 | Initial | 8/1/2003 | F800 17-M603 Installation & Operation Manual | F800 17-M603 Installation & Operation Manual | 17M603–00, 17M603–261, 17M603–274, 17M603–277 |
| F800 | Installation Manual | 165E335800 | 31-30-01 | Initial | 8/1/2003 | F800 17-M903 Installation & Operation Manual | F800 17-M903 Installation & Operation Manual | 17M903–00, 17M903–01, 17M903–02, 17M903–261, 17M903–263, 17M903–266, 17M903–274, 17M903–275, 17M903–276, 17M903–277, 17M903–278, 17M903–279, 17M903–281, 17M903–282 |
| F800 | Installation Manual | 165E335900 | 31-30-01 | 01 | 10/1/2003 | F800 17-M800 Installation & Operation Manual | F800 17-M800 Installation & Operation Manual | 17M800–00, 17M800–00A, 17M800–01A, 17M800–251, 17M800–252, 17M800–253, 17M800–258, 17M800–261, 17M800–262 |
| F800 | Installation Manual | 165E337000 | 31-30-01 | 01 | 10/1/2003 | F800 17-M700 Installation & Operation Manual | F800 17-M700 Installation & Operation Manual | 17M700–00, 17M700–00A, 17M700–274 |
| F800 | Service Letter | F800 DFR007 | Orig | 8/12/2014 | Access to F800 technical publications | Access to F800 technical publications | ||
| FA2100 CVDR | Component Maintenance Manual | 165E1747-00 | 23-70-05 | 11 | 4/23/2024 | ED-56A Control Units Pre Amplifiers & Microphones CMM | ED−56A CONTROL UNITS, PREAMPLIFIER MODULE, AND MICROPHONE MODULES FOR SOLID−STATE COCKPIT VOICE RECORDERS (SSCVR) SCVR CONTROL UNITS MODELS S151/S161, S152/S162, AND S251/S261 SSCVR PREAMPLIFIER MODULE MODEL S150/S160 SSCVR MICROPHONE MODULES MODELS S055, S056 AND S058 CONTROL UNIT MICROPHONE PREAMPLIFIER MODULE REMOTE MICROPHONE MODULES, Acron Aviation | S151−0020−00 S161−0020−00 S162−0020−00 S151−0030−00 S161−0020−10 S162−0030−00 S151−0040−00 S161−0030−00 S162−0040−00 S151−0050−00 S161−0040−00 S251−1120−00 S151−0060−00 S161−0050−00 S251−1130−00 S152−0020−00 S161−0060−00 S251−1170−00 S152−0020−01 S161−0080−00 S261−1120−00 S152−0030−00 S161−0090−00 S261−1130−00 S152−0030−01 S161−0090−02 S261−0050−00 S152−0040−00 S161−1120−10 S261−1121−00 S161−1390−01 S161−1390−02 S161−1390−03 S161−1090−20 S150−0020−00 S160−0020−00 S150−0020−00 S160−0030−00 S055−0030−00 S056−0048−00 S058−0048−00 S055−0065−00 S056−0048−10 S058−0048−01 S055−0066−00 S056−0048−15 S058−0148−10 S055−0067−00 S056−0049−00 S055−0067−01 S056−0050−00 S055−0068−00 S056−0051−00 S056−0030−00 S056−1048−00 S056−0047−00 |
| FA2100 CVDR | Component Maintenance Manual | 165E1690-90 | 23-70-90 | 04 | 4/30/2025 | FA2100 CVDR CMM | FA2100 CVDR Component Maintenance Manual | 2100-3083-51, 2100-3083-93, 2100-3084-93, 2100-5083-51, 2100-5283-51 |
| FA2100 CVDR | Component Maintenance Manual | 165E1690-00 | 23-70-07 | 10 | 4/30/2025 | FA2100 CVDR CMM | Cockpit Voice and Data Recorder Model: FA2100 CVDR | 2100-3073-00 2100-3073-51 (Obsolete) 2100-3083-00 2100-3083-10 2100-3083-50 2100-3083-51 2100-3084-00 2100-3084-50 2100-3283-10 2100-3283-50 |
| FA2100 CVDR | Installation Aircraft Tools | n/a | x.x | 10/26/2021 | CVR AUTOMATED TEST STATION/ RECORDER INTERFACE UNIT (CATS/RIU) | CATS 2.4. | 17TES0420 | |
| FA2100 CVDR | Installation Aircraft Tools | 17TES0436 | Orig | 12/14/2020 | ADLP Software V3.6 | Software - ADLP V3.6 | 17TES0436 | |
| FA2100 CVDR | Installation Manual | 165E1847-10 | 01 | 4/30/2025 | FA2100 CVDR Install Manual | FA2100CVDR Install Manual | 2100-3083-10 2100-3283-10 | |
| FA2100 CVDR | Installation Manual | 165E1847-01 | 04 | 12/30/2024 | FA2100 CVDR Installation and Operation Manual, ARINC 757 | FA2100CVDR INSTALLATION & OPERATION INSTRUCTION MANUAL | 2100-3083-50, 2100-3083-51, 2100-3084-50, 2100-3283-50 | |
| FA2100 CVDR | Installation Manual | 165E1847-00 | 7 | 4/30/2025 | FA2100 CVDR Installation Manual | FA2100 CVDR Install Manual for 2100-30XX-00 | 2100-3073-00 2100-3083-00 2100-3084-00 | |
| FA2100 CVDR | Miscellaneous | 905-E6407-07 | D | 9/26/2019 | FA2100 90 day Beacon, Lithium Battery Information Sheet | FA2100 90 day Beacon | 2100- | |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB020 | 23-70-07-20 | 03 | 12/27/2016 | SB020-MD14: Introduction of L-3AR 90 Day ULB | Mod Dot 14, 90 Day ULB | 2100−3283−10, 2100−3283−50, 2100−5283−51 |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB018 | 23-70-07-18 | 02 | 7/30/2024 | SB018-MD13-Intro of New CSMU and SW Revision | MD13: INTRODUCTION OF NEW CRASH SURVIVABLE MEMORY UNIT AND SW REVISION | 2100-3073-00, 2100-3083-xx, 2100-3084-00, 2100-5083-51 |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB022 | 23-70-02 | 01 | 5/18/2018 | SB022-MD17-Intro of New CSMU Part Number | MOD DOT 17 INTRODUCTION OF NEW CSMU PART NUMBER | 2100-3073-00, 2100-3083-00, 2100-3083-10, 2100-3083-50, 2100-3083-51, 2100-3084-00, 2100-3084-93, 2100-3283-10, 2100-3283-50, 2100-5083-51, 2100-5283-51 |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB001 | 23-70-07-01 | Initial | 8/1/2003 | SB001-MD01-SW02-Intro of Enhanced AP PWA and Software Revision | INTRODUCTION OF THE ENHANCED ACQUISITION PROCESSOR, PRINTED WIRING ASSEMBLY P/N 205E1931–00 AND SOFTWARE REVISION R2 | 2100-3073-00 |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB002 | 23-70-07-02 | Initial | 8/1/2003 | SB002-MD02-Moisture-Resistant Seals | MOISTURE-RESISTANT SEALS | 2100-3073-00 |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB005 | 23-70-07-05 | Initial | 4/5/2005 | SB005-MD04-Intro of AP PWA PN 205E2502−11 | INTRODUCTION OF ACQUISITION PROCESSOR PWA, P/N: 205E2502−11 | 2100-3073-00 |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB008 | 23-70-07-08 | Initial | 9/20/2007 | SB008-MD06-Application of Chassis Seam Sealing | APPLICATION OF CHASSIS SEAM SEALING ON FA2100-3083-00 | 2100-3083-00 |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB009 | 23-70-07-09 | Initial | 11/6/2007 | SB009-MD01-SW02-Intro of New AC PWA, PN 205E3977-10 and 3V CSMU PN 253E1568-36 | INTRODUCTION OF NEW AUDIO COMPRESSOR PWA, PN 205E3977-10 AND NEW 3V CSMU PN 253E1568-36 FOR 30-MINUTE FA2100CVDRS | 2100-3073-00 |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB011 | 23-70-07-11 | Initial | 9/4/2008 | SB011-MD07-Intro of New AI, AP, AC PWAs and New W001, W002 and W003 Cable Assemblies | INTRODUCTION OF NEW AIRCRAFT INTERFACE (AI), ACQUISITION PROCESSOR (AP), AUDIO COMPRESSOR (AC) PRINTED WIRING ASSEMBLIES, NEW W001, W002 and W003 CABLE ASSEMBLIES | 2100-3083-50, 2100-3083-51 |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB012 | 23-70-07-12 | Initial | 9/4/2008 | SB012-MD09-Installation of Mounting Bracket to Support Storage Capacitor | INSTALLATION OF MOUNTING BRACKET TO SUPPORT STORAGE CAPACITOR | 2100-3073-00, 2100-3073-51, 2100-3083-00, 2100-3083-10, 2100-3083-50, 2100-3083-51 |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB013 | 23-70-07-13 | Initial | 11/9/2010 | SB013-MD10-Intro of Improved Storage Capacitor | INTRODUCTION OF IMPROVED STORAGE CAPACITOR | 2100-3073-XX, 2100-3083-XX, 2100-3084-XX, 2100-5083-XX |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB014 | 23-70-07-14 | 01 | 1/31/2011 | SB014-SW06-Intro of Software Revision 06 | INTRODUCTION OF SOFTWARE REVISION 06 | 2100-3083-50 |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB015 | 23-70-07-15 | 03 | 5/28/2014 | SB015-Replacement of Non−Conforming Hardware | REPLACEMENT OF NON−CONFORMING HARDWARE | 2100−3073−00, 2100−3083−00, 2100−3083−50, 2100−3083−51, 2100−3084−50 |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB016 | 23-70-07-16 | 01 | 1/31/2011 | SB016-SW07-Intro of Software Revision 07 | INTRODUCTION OF SOFTWARE REVISION 07 | 2100‐3083‐10 |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB017 | 23-70-07-17 | 01 | 5/2/2013 | SB017-SW07 & SW08-Intro of Software Revision 07 and 08 | INTRODUCTION OF SOFTWARE REVISION 07 AND 08 | 2100−3083−00, 2100−3083−10, 2100−3083−50 |
| FA2100 CVDR | Service Bulletin | 23‐70‐05‐001 | 23‐70‐05 | Initial | 8/22/2013 | SB001-Introduction of S152−0020−01 Control Unit | SB001-Introduction of S152−0020−01 Control Unit Used in Boeing NG Aircraft. | S152−0020−01 |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB023 | 23-70-07-23 | 00 | 7/30/2024 | SB023-SW MD 06: P/N 2100-3084-50 | DATA RECORDERS - INTRODUCTION OF SOFTWARE MOD 06 | 2100-3084-50 |
| FA2100 CVDR | Service Bulletin | FA2100CVDR-SB021 | 23-70-07 | 01 | 5/18/2018 | Service Bulletin, intro to SW and CSMU | INTRODUCTION OF NEW SOFTWARE REVISION AND CSMU PART NUMBER. | 2100-3073-00 2100-2082-51 2100-3283-10 2100-3083-00 2100-3083-93 2100-3283-50 2100-3083-10 2100-3084-00 2100-5083-51 2100-3083-5 2100-3084-93 3100-5283-51 |
| FA2100 CVDR | Service Letter | SIL-003-ULB | 02 | 3/6/2025 | Service Information Letter, NTO for ULB | No Technical Objection (NTO) FA2100 and FA5000 Recorder Models for alternate Underwater Locator Beacon (ULB) installation. TSO-C142B Compliant Devices: • P/N 9080-10036-01. DK290-11, Dukane (Non-Restricted Class 9 Lithium Battery) • P/N 266-E6914-00. Green90, Novega P/N: 22960−00 (Lithium Free Battery) | ALL FA2100, FA5000 ULB: 9080-10036-01 ULB: 266-E6914-00 | |
| FA2100 CVDR | Service Letter | FA2100CVDR-SIL001 | Init | 8/19/2014 | SIL001-New Underwater Locator Beacon to Provide 90 Days of Operation | SIL001-New Underwater Locator Beacon to Provide 90 Days of Operation | 2100-3XXX-XX | |
| FA2100 CVDR | Service Letter | PI/2-001 | 03 | 2/12/2024 | Notification of discontinued product. | Notification of discontinued product. | 17TES0062, 17TES0065, 17TES0066, 17TES0092 | |
| FA2100 CVR | Component Maintenance Manual | 165E1689-90 | 23-70-90 | 03 | 1/30/2025 | Component Maintenance Manual, FA2100 CVR | COCKPIT VOICE AND DATA RECORDER MODEL FA2100 CVR | 2100−1020−91, 2100−1020−93 |
| FA2100 CVR | Component Maintenance Manual | 165E1747-00 | 23-70-05 | 11 | 4/23/2024 | ED-56A Control Units Pre Amplifiers & Microphones CMM | ED−56A CONTROL UNITS, PREAMPLIFIER MODULE, AND MICROPHONE MODULES FOR SOLID−STATE COCKPIT VOICE RECORDERS (SSCVR) SCVR CONTROL UNITS MODELS S151/S161, S152/S162, AND S251/S261 SSCVR PREAMPLIFIER MODULE MODEL S150/S160 SSCVR MICROPHONE MODULES MODELS S055, S056 AND S058 CONTROL UNIT MICROPHONE PREAMPLIFIER MODULE REMOTE MICROPHONE MODULES, Acron Aviation | S151−0020−00 S161−0020−00 S162−0020−00 S151−0030−00 S161−0020−10 S162−0030−00 S151−0040−00 S161−0030−00 S162−0040−00 S151−0050−00 S161−0040−00 S251−1120−00 S151−0060−00 S161−0050−00 S251−1130−00 S152−0020−00 S161−0060−00 S251−1170−00 S152−0020−01 S161−0080−00 S261−1120−00 S152−0030−00 S161−0090−00 S261−1130−00 S152−0030−01 S161−0090−02 S261−0050−00 S152−0040−00 S161−1120−10 S261−1121−00 S161−1390−01 S161−1390−02 S161−1390−03 S161−1090−20 S150−0020−00 S160−0020−00 S150−0020−00 S160−0030−00 S055−0030−00 S056−0048−00 S058−0048−00 S055−0065−00 S056−0048−10 S058−0048−01 S055−0066−00 S056−0048−15 S058−0148−10 S055−0067−00 S056−0049−00 S055−0067−01 S056−0050−00 S055−0068−00 S056−0051−00 S056−0030−00 S056−1048−00 S056−0047−00 |
| FA2100 CVR | Component Maintenance Manual | 165E1689-00 | 23-70-04 | 28 | 4/30/2025 | Component Maintenance Manual, FA2100 CVR | COCKPIT VOICE RECORDER (CVR) | 2100−1010−00, 2100−1010−50, 2100−1010−51, 2100−1020−00, 2100−1020−02, 2100−1020−50, 2100−1020−51, 2100−1020−90, 2100−1025−02, 2100−1025−12, 2100−1025−22, 2100−1025−24, 2100−1026−02, 2100−1027−02, 2100−1220−00, 2100−1220−02, 2100−1225−22, 2100−1225−24, 2100−1225−60, 2100−1226−02, 2100−1227−02, 2100−1228−02, 2100−1925−22, 2100−1925−23 |
| FA2100 CVR | Installation Aircraft Tools | n/a | x.x | 10/26/2021 | CVR AUTOMATED TEST STATION/ RECORDER INTERFACE UNIT (CATS/RIU) | CATS 2.4. | 17TES0420 | |
| FA2100 CVR | Installation Aircraft Tools | 17TES0436 | Orig | 12/14/2020 | ADLP Software V3.6 | Software - ADLP V3.6 | 17TES0436 | |
| FA2100 CVR | Installation Manual | 165E1846-00 | 23-70-06 | 31 | 4/30/2025 | Installation and Operation Manual, FA2100 CVR | MODEL FA2100CVR COCKPIT VOICE RECORDER | 2100–1010–00, 2100–1020–00, 2100–1020–02, 2100−1020−90, 2100–1025–02, 2100−1025−12, 2100–1025–12, 2100–1025–22, 2100–1025–24, 2100−1025−60, 2100–1026–02, 2100–1027–02, 2100–1220–00, 2100–1220–02, 2100–1225–22, 2100–1225–24, 2100–1225–60, 2100–1226–02, 2100–1227–02, 2100−1228−02, 2100–1925–22, 2100−1925−23, 2100-1020-90 |
| FA2100 CVR | Installation Manual | 165E1846-01 | 05 | 4/30/2025 | Installation and Operation Manual, FA2100 CVR | COCKPIT VOICE RECORDER | 2100−1024−92, 2100−1224−92 | |
| FA2100 CVR | Installation Manual | 165E1848-00 | 4 | 4/30/2008 | Installation & Operation Instruction Manual, FA2100 GACVR | FA2100 General Aviation CVR Installation Manual | 2100-1010-5X 2100-1020-5X | |
| FA2100 CVR | Miscellaneous | 905-E6407-07 | D | 9/26/2019 | FA2100 90 day Beacon, Lithium Battery Information Sheet | FA2100 90 day Beacon | 2100- | |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB018 | 23-70-04 | 04 | 5/28/2014 | SB018-Replacement of Non-Conforming Hardware | SB018-Replacement of Non-Conforming Hardware | 2100-1010-XX 2100-1020-XX 2100-1025-XX 2100-1026-02 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB019 | 23-70-04-19 | 06 | 5/19/2025 | SB019-MD14-Introduction of New CSMU and SW Revision | SB019-MD14-Introduction of New Crash Survivable Memory Unit and Software Revision | 2100-1010-00 2100-1010-50 2100-1010-51 2100-1020-00 2100-1020-02 2100-1020-50 2100-1020-51 2100-1020-90 2100-1020-93 2100-1020-98 2100-1020-99 2100-1025-12 2100-1025-22 2100-1025-24 2100-1025-90 2100-1026-02 2100-1226-02 and 2100-1228-02 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB020 | 23-70-04 | Initial | 1/10/2013 | SB020-SW06-Introduction of Software Revision | SB020-SW06-Introduction of Software Revision | 2100-1010-XX 2100-1020-XX |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB021 | 23-70-04-21 | 02 | 4/8/2025 | SB021-Introduction of New SW Revision | INTRODUCTION OF NEW SOFTWARE REVISION. Note: Part Numbers listed in this bulletin with NAND memory (MOD DOT 14) CSMUs. | 2100-1010-00 2100-1010-50 2100-1010-51 2100-1020-00 2100-1020-02 2100-1020-50 2100-1020-51 2100-1020-90 2100-1020-93 2100-1020-98 2100-1020-99 2100-1025-12 2100-1025-24 2100-1025-22 2100-1026-02 2100-1925-22 2100-1220-02 2100-1225-22 2100-1227-02 2100-1226-02 and 2100-1228-02 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB023 | 23-70-04 | 04 | 9/15/2023 | SB023-MD/SW-Introduction of New SW Revision and CSMU PN | SB023-MD/SW-Introduction of New Software Revision and Crash Survivable Memory Unit Part Number | 2100-1020-00 2100-1020-02 2100-1020-50 2100-1020-51 2100-1020-90 2100-1025-22 2100-1025-24 2100-1026-02 2100-1220-00 2100-1220-02 2100-1225-22 2100-1226-02 2100-1227-02 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB025 | 23-70-04 | 02 | 1/9/2019 | SB025-Conversion Instructions for 90-Day ULB | SB025-Conversion Instructions for 90-Day Underwater Locator Beacon | 2100-1025-22 2100-1925-22 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB027 | 23-70-04 | 01 | 9/20/2018 | SB027-Conversion Instructions for 90-Day ULB | SB027-Conversion Instructions for 90-Day Underwater Locator Beacon | 2100-4045-22 2100-4945-22 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB028 | 23-70-04 | Initial | 3/27/2020 | SB028-SW04-Introduction of New SW Revision | SB028-SW04-Introduction of New Software Revision | 2100-1225-24 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB029 | 23-70-04 | Initial | 11/30/2020 | SB029-Part Number Conversion | SB029-Part Number Conversion 2100-1925-22 to 2100-1925-23. | 2100-1925-22 2100-1925-23 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB031 | 23-70-04-031 | 05 | 2/19/2025 | SB031-MOD 19, New Perylene Coated CCA | MOD 19-New Perylene Coated Circuit Card Assemblies. | (NAND memory) 2100-1020-00, 2100-1020-02, 2100-1025-02, 2100-1025-22, 2100-1026-02, 2100-1220-02, 2100-1225-22, 2100-1225-60, 2100-1226-02, 2100-1227-02, 2100-1228-02. (NOR memory) 2100-1020-00, 2100-1020-02, 2100-1025-12, 2100-1026-02. |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB001 | 23-70-04-001 | Initial | 9/8/1998 | SB001-MD01-Modified AI PWA PN 205E1593-00 | SB001-MD01-Modified Aircraft Interface PWA PN 205E1593-00 | 2100-1010-00 2100-1020-00 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB002 | 23-70-04-002 | Initial | 4/30/2000 | SB002-MD02 SW01-Introduction of Enhanced AP PWA PN 205E1931-00 | SB002-MD02 SW01-Introduction of Enhanced Acquisition Processor PWA PN 205E1931-00 | 2100-1010-00 2100-1020-00 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB003 | 23-70-04-003 | Initial | 8/15/2001 | SB003-MD03-Modified AC PWA PN 205E1849-03 | SB003-MD03-Modified Audio Compressor PWA P/N 205E1849–03 | 2100-1020-02 2100-1020-98 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB004 | 23-70-04 | 02 | 7/26/2011 | SB004-MD04-Moisture Resistant Seals | SB004-MD04-Moisture Resistant Seals | 2100-1010-00 2100-1020-00 2100-1020-02 2100-1020-9X |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB005 | 23-70-04 | Initial | 4/16/2002 | SB005-SW02-Introduction of New Software | SB005-SW02-Introduction of New Software | 2100-1010-00 2100-1010-50 2100-1010-51 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB006 | 23-70-04 | 01 | 11/1/2004 | SB006-MD05-Introduction of AP PWA PN 205E2502-10 or 205E2502-11 | SB006-MD05-Introduction of Acquisition Processor PWA PN 205E2502-10 or 205E2502-11 | 2100-1010-00 2100-1010-50 2100-1010-51 2100-1020-00 2100-1020-02 2100-1020-50 2100-1020-51 2100-1020-90 2100-1020-91 2100-1020-93 2100-1020-98 2100-1020-99 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB007 | 23-70-04 | 01 | 10/11/2004 | SB007-SW04-Introduction of SW Revision | SB007-SW04-Introduction of Software Revision 04 | 2100-1010-00 2100-1010-50 2100-1010-51 2100-1020-00 2100-1020-02 2100-1020-50 2100-1020-51 2100-1020-90 2100-1020-91 2100-1020-93 2100-1020-98 2100-1020-99 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB008 | 23-70-04 | 01 | 3/12/2008 | SB008-MD06-Introduction of CSMU Containing 3V Memory | SB008-MD06-Introduction of Crash Survivable Memory Unit Containing 3V Memory | 2100-1010-00 2100-1010-50 2100-1010-51 2100-1020-00 2100-1020-02 2100-1020-50 2100-1020-51 2100-1020-90 2100-1020-91 2100-1020-93 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB010 | 23-70-04 | 01 | 12/4/2008 | SB010-SW05-Introduction of SW Revision to Support 3V CSMU | SB010-SW05-Introduction of Software Revision 05 to Support 3V Crash Survivable Memory Unit and 2-Hour High Quality Audio Recording | 2100-1010-00 2100-1010-50 2100-1010-51 2100-1020-00 2100-1020-02 2100-1020‐50 2100-1020‐51 2100-1020‐90 2100-1020‐91 2100-1020‐93 2100-1020‐98 2100-1020‐99 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB011 | 23-70-04 | Initial | 9/20/2007 | SB011-SW05-Introduction of Software Revision 03 | SB011-SW05-Introduction of Software Revision 03 | 2100-1025-02 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB012 | 23-70-04 | 01 | 10/17/2007 | SB012-MD08-Introduction of MOD DOT 8 Factory Tracking ID | SB011-MD08-Introduction of MOD DOT 8 Factory Tracking Identification | 2100-1010-00 2100-1010-50 2100-1010-51 2100-1020-00 2100-1020-02 2100-1020-50 2100-1020-51 2100-1020-90 2100-1020-91 2100-1020-98 2100-1020-99 2100-1020-93 2100-1025-02 2100-1025-12 2100-1025-22 2100-1025-90 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB013 | 23-70-04 | Initial | 12/14/2007 | SB013-MD09-Introduction of New AP PWA PN 205E2502-52 | SB013-MD09-Introduction of New Acquistion Processor PWA PN 205E2502-52 | 2100-1010-50 2100-1010-51 2100-1020-50 2100-1020-51 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB014 | 23-70-04 | Initial | 11/26/2007 | SB014-SW04-Introduction of Software Revision 04 | SB014-SW04-Introduction of Software Revision 04 | 2100-1025-02 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB015 | 23-70-04 | 01 | 2/19/2009 | SB015-MD06-Intro of New AI, AC, and AP PWAs. New W001, W002, and W003 Cables. | SB015-MD06-Introduction of New Aircraft Interface, Audio Compressor, and Acquistion Processor PWAs. New W001, W002, and W003 Cables. | 2100-1010-00 2100-1010-50 2100-1010-51 2100-1020-00 2100-1020-02 2100-1020-50 2100-1020-51 2100-1020-90 2100-1020-98 2100-1020-99 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB016 | 23-70-04 | Initial | 9/4/2008 | SB016-MD11-Installation of Mounting Bracket to Support Storage Capacitor | SB016-MD11-Installation of Mounting Bracket to Support Storage Capacitor | 2100-1010-00 2100-1010-50 2100-1010-51 2100-1020-00 2100-1020-02 2100-1020-50 2100-1020-51 2100-1020-90 2100-1020-98 2100-1020-99 2100-1025-02 2100-1025-12 2100-1025-22 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB017 | 23-70-04-017 | 02 | 4/8/2025 | SB017-MD12/13-Introduction of Improved Storage Capacitor | SB017-MD12 or 13-Introduction of Improved Storage Capacitor | 2100-1010-XX 2100-1020-XX 2100-1025-XX 2100-1026-XX 2100-1226-02 and 2100-1228-02 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB022 | 23-70-04-022 | 08 | 3/15/2023 | SB022-MD15-Introduction of 90 Day ULB | MOD DOT 15 INTRODUCTION OF L3H AP 90−DAY UNDERWATER LOCATOR BEACON PART NUMBER 266E5542−00 | 2100-1020-00, 2100-1020-02, 2100-1020-50, 2100-1020-90, 2100-1020-93, 2100-1024-92, 2100-1026-02, 2100-1025-02, 2100-1025-12, 2100-1025-22, 2100-1025-24, 2100-1027-02 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB024 | 23-70-04 | 04 | 9/15/2023 | SB024-MD17-Introduction of New CSMU PN | MOD DOT 17 INTRODUCTION OF NEW CSMU PART NUMBERMOD DOT 17 INTRODUCTION OF NEW CSMU PART NUMBER | 2100-1xxx-xx, ATA 23-70-04 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB008-AB | 23-70-04 | 01 | 7/11/2019 | SB008AB-SW Revision to Remove Larsen Noise During CVR Test | NEW PART NUMBER AND SOFTWARE REVISION TO REMOVE LARSEN NOISE DURING CVR TEST | 2100−1026−02 2100−1228−02 (new) |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB033 | 23-70-04-033 | 05 | 9/4/2024 | SB033-SW12-Introduction of New SW12 for Units with MD17 | INTRODUCTION OF NEW SOFTWARE REVISION 12 FOR UNITS WITH HARDWARE MOD 17. | 2100-1925-22 2100-1925-23 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB009 | 23-70-04 | orig | 12/15/2005 | SB009-Introduction of a New Audio Compressor PWA PN 205E3977–10, –12, –13, & –14 | INTRODUCTION OF A NEW AUDIO COMPRESSOR PRINTED WIRING ASSEMBLY (PWA), P/N: 205E3977–10, –12, –13, & –14 | 2100-1010-xx, 2100-1020-xx, 2100-1xxx-xx |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB030 | 23-70-04-030 | 08 | 2/19/2025 | SB030-MD18-Chassis Assembly Update | Mod 18. Chassis Assembly Update to Incorporate Moisture Prevention Countermeasure. | (NAND memory) memory) 2100-1020-00, 2100-1020-02, 2100-1025-02, 2100-1026-02, 2100-1220-02, 2100-1225-22, 2100-1225-60, 2100-1226-02, 2100-1227-02, 2100-1228-02.. (NOR memory) 2100-1020-00, 2100-1020-02, 2100-1025-12, 2100-1026-02. |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB032 | 23-70-04 | 00 | 7/15/2021 | SB032-MD20–Introduction of CSMU PN 253-E5675-06 | HARDWARE MOD 20 – INTRODUCTION OF CSMU PART NO. 253-E5675-06 | 2100-1225-24 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB-001ATR | 23-70-04 | Initial | 6/26/2019 | SB001ATR-New PN 2100−1225−60 for ATR Operators to Improve Reliability | new part number, 2100−1225−60, for ATR operators to improve reliability. | 2100-1225-22, 2100-1225-60 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB035 | 23-70-04-035 | 02 | 4/30/2025 | SB035-MD20-Replaces AI CCA Due to Obsolescence | COMMUNICATIONS - DATA RECORDERS - HARDWARE MOD 20 REPLACES AIRCRAFT INTERFACE CCA DUE TO OBSOLESCENCE | 2100-1020-90, 2100-1024-92 |
| FA2100 CVR | Service Bulletin | 23‐70‐05‐001 | 23‐70‐05 | Initial | 8/22/2013 | SB001-Introduction of S152−0020−01 Control Unit | SB001-Introduction of S152−0020−01 Control Unit Used in Boeing NG Aircraft. | S152−0020−01 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB034 | 23-70-04 | 00 | 8/15/2023 | SB034-SW05-Introduction of New SW05 for P/N 2100-1025-02 | INTRODUCTION OF NEW SOFTWARE REVISION 05 FOR P/N 2100-1025-02 | 2100-1025-02 |
| FA2100 CVR | Service Letter | SIL-001-CATS | 00 | 6/20/2023 | Service Information Letter | FA2100 CVR (P/N 2100-1227-02) failing power consumption test when using CATS software. | 17TES0700, 2100-1227-02, 17TES0710 | |
| FA2100 CVR | Service Letter | SIL-003-ULB | 02 | 3/6/2025 | Service Information Letter, NTO for ULB | No Technical Objection (NTO) FA2100 and FA5000 Recorder Models for alternate Underwater Locator Beacon (ULB) installation. TSO-C142B Compliant Devices: • P/N 9080-10036-01. DK290-11, Dukane (Non-Restricted Class 9 Lithium Battery) • P/N 266-E6914-00. Green90, Novega P/N: 22960−00 (Lithium Free Battery) | ALL FA2100, FA5000 ULB: 9080-10036-01 ULB: 266-E6914-00 | |
| FA2100 CVR | Service Letter | SIL-041-FA2100CVR | 00 | 6/30/2024 | SIL041-Permission to allow the application of RTV | This Service Information Letter (SIL) gives permission to allow the application of RTV, P/N 060-12-00006 to the FA2100 CVR chassis cover seal. | 2100-1XXXX-XX | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL001 | Orig | 3/1/2001 | SIL001-FA2100CVR Upgrade for A100/A100A | SIL for Model FA2100CVR Upgrade for A100/A100A Installations | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | PI/2-001 | 03 | 2/12/2024 | Notification of discontinued product. | Notification of discontinued product. | 17TES0062, 17TES0065, 17TES0066, 17TES0092 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL002 | 01 | 1/15/2002 | SIL002-FA2100CVR Upgrade for TSO-84 Installations | SIL002-FA2100CVR Upgrade for TSO-84 Installations for BOEING 737, All Series | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL003 | 01 | 1/22/2002 | SIL003-FA2100CVR Upgrade for A100/A100A Installations | SIL003-FA2100CVR Upgrade for A100/A100A Installations for BOEING 757, All Series | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL004 | 01 | 1/22/2002 | SIL004-FA2100CVR Upgrade for A100/A100A Installations | SIL003-FA2100CVR Upgrade for A100/A100A Installations for BOEING 767, All Series | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL005 | Initial | 4/10/2001 | SIL005-FA2100CVR Upgrade for A100/A100A Installations | SIL003-FA2100CVR Upgrade for A100/A100A Installations for BOEING 747, 100/200/300 Series | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL006 | 01 | 1/22/2002 | SIL006-FA2100CVR Upgrade for A100/A100A Installations | SIL006-FA2100CVR Upgrade for A100/A100A Installations for BOEING DC-9, All Series | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL007 | Initial | 4/10/2001 | SIL007-FA2100CVR Upgrade for A100/A100A Installations | SIL003-FA2100CVR Upgrade for A100/A100A Installations for BOEING DC-10, All Series | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL008 | Initial | 10/17/2001 | SIL008-FA2100CVR Upgrade for TSO-C84/C123 Installations | SIL008-FA2100CVR Upgrade for TSO-C84/C123 Installations for BOEING B747-400 | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL009 | Initial | 9/10/2001 | SIL009-No Charge L-3 Factory Modification of FA2100CVR | SIL009-No Charge L-3 Factory Modification of FA2100CVR, p/n: 2100-1020-00 | 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL010 | Initial | 10/1/2001 | SIL010-FA2100CVR Upgrade for TSO-84 Installations | SIL010-FA2100CVR Upgrade for TSO-84 Installations for BOEING MD-11, All Series | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL011 | Initial | 10/1/2001 | SIL011-FA2100CVR Upgrade for TSO-84 Installations | SIL011-FA2100CVR Upgrade for TSO-84 Installations for Fokker 70 | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL012 | 01 | 1/2/2002 | SIL012-FA2100CVR Upgrade for TSO-84 Installations | SIL012-FA2100CVR Upgrade for TSO-84 Installations for Fokker 100 | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL013 | 01 | 1/22/2002 | SIL013-FA2100CVR Upgrade for TSO-84 Installations | SIL013-FA2100CVR Upgrade for TSO-84 Installations for Airbus A300, All Series | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL014 | Initial | 10/3/2001 | SIL014-FA2100CVR Upgrade for TSO-84 Installations | SIL014-FA2100CVR Upgrade for TSO-84 Installations for BOEING B747-SP | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL015 | Initial | 11/13/2001 | SIL015-Control Unit and Remote Microphone Upgrade | SIL015-Control Unit and Remote Microphone Upgrade for Cessna Citation, All Series | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL016 | Initial | 7/31/2002 | SIL016-FA2100CVR Upgrade for TSO-C84 CVR Installations | SIL016-FA2100CVR Upgrade for TSO-C84 CVR Installations for Bombardier Challenger CL-600-2B16 | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL017 | Initial | 9/10/2002 | SIL017-FA2100CVR Upgrade for TSO-C84 CVR Installations | SIL017-FA2100CVR Upgrade for TSO-C84 CVR Installations for SAAB 340B | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL018 | Initial | 7/25/2003 | SIL018-Application of CSMU Moisture Resistant Seal and RTV Application | SIL018-Application of CSMU Moisture Resistant Seal and RTV Application for GACVR | 2100-1010-50 2100-1010-51 2100-1020-50 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL019 | Initial | 2/19/2004 | SIL019-FA2100CVR Upgrade for TSO-C123 A100S SSCVR Installations | SIL019-FA2100CVR Upgrade for TSO-C123 A100S SSCVR Installations for Hawker 800 | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL020 | Initial | 9/21/2004 | SIL020-Discontinuation of the S056 Remote Microphone Protective Shipping Cover | SIL020-Discontinuation of the S056 Remote Microphone Protective Shipping Cover | 2100-1010-00 2100-1020-00 S056-0030-00 S152-0020-00 S056-0047-00 S152-0030-00 S056-0048-00 S152-0030-01 S056-0048-10 S152-0040-00 S056-0049-00 S162-0020-00 S056-0050-00 S162-0030-00 S056-0051-00 S162-0040-00 S056-1048-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL021 | Initial | 10/4/2004 | SIL021-FA2100CVR Upgrade for TSO-84 Installations | SIL021-FA2100CVR Upgrade for TSO-84 Installations for BOEING 727, All Series | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL023 | Initial | 4/14/2005 | SIL023-FA2100CVR Upgrade for TSO-84 Installations | SIL023-FA2100CVR Upgrade for TSO-84 Installations for L410E9 | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL024 | Initial | 4/20/2005 | SIL024-FA2100CVR Upgrade for TSO-84 Installations for Fokker 50 | SIL024-FA2100CVR Upgrade for TSO-84 Installations for Fokker 50 | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL025 | Initial | 6/17/2005 | SIL025-FA2100CVR Upgrade for TSO-84 Installations for Embraer 110 Bandeirante | SIL025-FA2100CVR Upgrade for TSO-84 Installations for Embraer 110 Bandeirante | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL026 | Initial | 8/9/2005 | SIL026-FA2100CVR Upgrade for TSO-84 Installations for Airbus A300-600 | SIL026-FA2100CVR Upgrade for TSO-84 Installations for Airbus A300-600 | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL027 | Initial | 8/9/2005 | SIL027-FA2100CVR Upgrade for TSO-84 Installations for Airbus A310 | SIL027-FA2100CVR Upgrade for TSO-84 Installations for Airbus A310 | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL028 | Initial | 8/9/2005 | SIL028-FA2100CVR Upgrade for TSO-84 Installations for DC-9 Series, MD-88 | SIL028-FA2100CVR Upgrade for TSO-84 Installations for DC-9 Series, MD-88 | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL029 | Initial | 10/25/2005 | SIL029-FA2100CVR Upgrade for TSO-84 Installations for DC-8 | SIL029-FA2100CVR Upgrade for TSO-84 Installations for DC-8 | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL030 | Initial | 7/19/2006 | SIL030-FA2100CVR Upgrade for TSO-84 Installations for Embraer 120 | SIL030-FA2100CVR Upgrade for TSO-84 Installations for Embraer 120 | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL031 | Initial | 8/19/2008 | SIL031-FA2100CVR Upgrade for TSO-84 Installations for Hawker Beechcraft 1990C and 1900D | SIL031-FA2100CVR Upgrade for TSO-84 Installations for Hawker Beechcraft 1990C and 1900D | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL032 | Initial | 8/26/2008 | SIL032-FA2100CVR Upgrade for TSO-84 Installations for Dassault Mystere Falcon 50, Mystere Falcon 900, Falcon 900EX | SIL032-FA2100CVR Upgrade for TSO-84 Installations for Dassault Mystere Falcon 50, Mystere Falcon 900, Falcon 900EX | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL033 | 01 | 9/1/2015 | SIL033-CVR Conversion to 2-Hour, High Quality Audio Recording and/or Non-Datalink to Datalink | SIL033-CVR Conversion to 2-Hour, High Quality Audio Recording and/or Non-Datalink to Datalink | 2100-1010-00 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL034 | Initial | 3/5/2010 | SIL034-Unique Behavior of Monitor Output from Airbus Specific SSCVRs During the Preflight Check | SIL034-Unique Behavior of Monitor Output from Airbus Specific SSCVRs During the Preflight Check | 2100-1025-02 2100-1026-02 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL035 | Initial | 10/4/2012 | SIL035-Introduction of the ROC/7 for Shop Maintenance | SIL035-Introduction of the ROC/7 for Shop Maintenance | 2100-1XXX-XX 2100-2XXX-XX | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL036 | Initial | 8/19/2014 | SIL036-New Underwater Locator Beacon to Provide 90 Days of Operation | SIL036-New Underwater Locator Beacon to Provide 90 Days of Operation | 2100-1XXX-XX 2100-2XXX-XX | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL037 | Initial | 3/11/2015 | SIL037-New Conformal Coating Process for Acquisition Processor Circuit Card Assembly | SIL037-New Conformal Coating Process for Acquisition Processor Circuit Card Assembly | 2100-1XXX-XX 2100-2XXX-XX | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL038 | 01 | 9/18/2018 | SIL038-Interim Authorization for Alternative Return-to-Service Testing of PN 2100-1228-02 | SIL038-Interim Authorization for Alternative Return-to-Service Testing of PN 2100-1228-02 | 2100-1228-02 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL039 | 01 | 9/18/2018 | SIL039-Interim Authorization for Alternative Return-to-Service Testing of PN 2100-1020-00 | SIL039-Interim Authorization for Alternative Return-to-Service Testing of PN 2100-1020-00 | 2100-1020-00 | |
| FA2100 CVR | Service Letter | FA2100CVR-SIL040 | Initial | 4/8/2019 | SIL040-Authorization for Software Load Procedure (SLP) | SIL040-Authorization for Software Load Procedure (SLP) | 2100-1X24-92 2100-1X25-2X 2100-1X25-6X 2100-1X26-XX 2100-1X27-XX 2100-1X28-XX | |
| FA2100 FDR | Component Maintenance Manual | 165E1688-00 | 31-30-03 | 22 | 5/15/2025 | Component Maintenance Manual, FA2100 FDR | FLIGHT DATA RECORDER (FDR) | 2100-2042-00, 2100-2043-00, 2100-2043-01, 2100-2043-12, 2100-2044-00, 2100-2044-01, 2100-2044-51, 2100-2045-00, 2100-2045-22, 2100-2045-23, 2100-2243-00, 2100-2244-00, 2100-2245-22, 2100-4042-00, 2100-4043-00, 2100-4043-02, 2100-4044-00, 2100-4045-00, 2100-4045-22, 2100-4045-60, 2100-4243-00, 2100-4245-00, 2100-4245-22, 2100-4245-60, 2100-4945-22, 2100-4945-23 |
| FA2100 FDR | Installation Aircraft Tools | n/a | x.x | 10/26/2021 | CVR AUTOMATED TEST STATION/ RECORDER INTERFACE UNIT (CATS/RIU) | CATS 2.4. | 17TES0420 | |
| FA2100 FDR | Installation Aircraft Tools | 17TES0436 | Orig | 12/14/2020 | ADLP Software V3.6 | Software - ADLP V3.6 | 17TES0436 | |
| FA2100 FDR | Installation Manual | 165E1845-00 | 18 | 6/30/2025 | Installation Manual, FA2100 FDR | Flight Data Recorder Model: FA2100 FDR ARINC 747 | 2100-2042-00, 2100-2043-00, 2100-2043-01, 2100-2043-12, 2100-2044-00, 2100-2044-01, 2100-2044-51, 2100-2045-00, 2100-2045-22, 2100-2243-00, 2100-2244-00, 2100-2245-22, 2100-4042-00, 2100-4043-00, 2100-4043-02, 2100-4044-00, 2100-4045-00, 2100-4045-22, 2100-4045-60, 2100-4065-51, 2100-4243-00, 2100-4245-00, 2100-4245-22, 2100-4245-60, 2100-4945-22, 2100-4945-23 | |
| FA2100 FDR | Miscellaneous | 905-E6407-07 | D | 9/26/2019 | FA2100 90 day Beacon, Lithium Battery Information Sheet | FA2100 90 day Beacon | 2100- | |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB001 | 31-30-03-001 | 01 | 9/28/2018 | SB001-MD01-Modified AI PWA PN 205E1592-00 | SB001-MD01-Modified AI PWA PN 205E1592-00, Acron Aviation | 2100-2042-XX 2100–4042-XX 2100-2043-XX 2100-4043-XX |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB002 | 31-30-03-002 | 01 | 9/28/2018 | SB002-SW01-Incorporation of Software Revision 1 | SB002-SW01-Incorporation of Software Revision 1, Acron Aviation | 2100-2042-XX 2100-2043-XX 2100-4042-XX 2100-4043-XX |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB003 | 31-30-03-003 | 01 | 9/28/2018 | SB003-MD02-Introduction of New AI PWA PN 205E1592-01 | SB003-Introduction of New AI PWA PN 205E1592-01, Acron Aviation | 2100-20XX-XX 2100-40XX-XX |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB004 | 31-30-03-004 | 01 | 9/28/2018 | SB004-MD03-Introduction of Rear Panel GSE Access Capability | SB004-MD03-Introduction of Rear Panel GSE Access Capability, Acron Aviation | 2100-4042-00 |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB005 | 31-30-03-005 | 02 | 9/28/2018 | SB005-MD04-Moisture Resistant Seals | SB005-MD04-Moisture Resistant Seals, Acron Aviation | 2100-20XX-XX 2100-40XX-XX |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB006 | 31-30-03-006 | 01 | 10/3/2002 | SB006-SW02-Incorporation of Software Revision 2 | SB006-SW02-Incorporation of Software Revision 2, Acron Aviation | 2100-2042-00 2100-2042-99 2100-4042-00 2100-4042-99 2100-2043-00 2100-2043-01 2100-4043-00 2100-4043-99 2100-4043-02 2100-4043-98 |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB007 | 31-30-03-007 | 02 | 8/30/2018 | SB007-MD05 SW03-Introduction of Advanced AP PWA PN 205E2502-11 and Software Revision 3 | SB007-MD05 SW03-Introduction of Advanced AP PWA PN 205E2502-11 and Software Revision 3, Acron Aviation | 2100–2042–00 2100–2043–00 2100–4043–00 2100–4043–02 2100–4043–98 2100–4043–99 |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB014 | 31-30-03-014 | 02 | 9/28/2018 | SB014-MD09-Intro of New Aircraft Interface, Acquisition Processor PWAs and New W001 Cable Assembly | SB014-MD09-Intro of New Aircraft Interface, Acquisition Processor PWAs and New W001 Cable Assembly, Acron Aviation | 2100-2042-00 2100-2043-00 2100-2043-01 2100-2043-12 2100-2044-00 2100-2044-01 2100-2045-00 2100-2045-22 2100-4042-00 2100-4042-99 2100-4043-00 2100-4043-02 2100-4043-98 2100-4043-99 2100-4044-00 2100-4045-00 |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB015 | 31-30-03-015 | 02 | 9/28/2018 | SB015-MD10-Intro of Factory Tracking Identification | SB015-MD10-Intro of Factory Tracking Identification, Acron Aviation | 2100-2042-00 2100-2043-00 2100-2043-01 2100-2043-12 2100-2044-00 2100-2044-01 2100-2045-00 2100-2045-22 2100-4042-00 2100-4042-53 2100-4042-99 2100-4043-00 2100-4043-02 2100-4043-98 2100-4043-99 2100-4044-00 2100-4045-00 |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB008 | 31-30-03-008 | 01 | 9/28/2018 | SB008-MD05 SW04-Intro of Advanced Acquistion Processor PWA, PN 205E2502-13 | SB008-MD05 SW04-Intro of Advanced Acquistion Processor PWA, PN 205E2502-13, Acron Aviation | 2100-4042-00 2100-4042-99 |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB009 | 31-30-03-009 | 01 | 9/28/2018 | SB009-MD05-Intro of Advanced Acquistion Processor PWA, PN 205E2502-11 | SB009-MD05-Intro of Advanced Acquistion Processor PWA, PN 205E2502-11, Acron Aviation | 2100-2044-00 2100-4044-00 |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB010 | 31-30-03-010 | 01 | 9/28/2018 | SB010-MD06-Modification of Advanced Acquistion Processor PWA, PN 205E2502-13 to Improve RSU Operation | SB010-MD06-Modification of Advanced Acquistion Processor PWA, PN 205E2502-13 to Improve RSU Operation, Acron Aviation | 2100-4042-00 2100-4042-99 |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB011 | 31-30-03-011 | 01 | 9/28/2018 | SB011-MD07-Intro of Replacement CSMU Containing 3v Memory | SB011-MD07-Intro of Replacement CSMU Containing 3v Memory, Acron Aviation | 2100-2042–00 2100-4042-00 2100-4042-53 2100-2043-00 2100-4043-00 2100-4043-01 2100-4043-02 2100-2044-00 2100-4044-00 |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB012 | 31-30-03 | Initial | 11/5/2006 | SB012-MD07 SW01-Intro of Replacement CSMU Containing 3v Memory | SB012-MD07 SW01-Intro of Replacement CSMU Containing 3v Memory, Acron Aviation | 2100-4042-53 |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB013 | 31-30-03 | Initial | 7/12/2007 | SB013-MD08 SW01-Modification to Acquisition Processor PWA 205E2502-17 to Correct Timing Issue | SB013-MD08 SW01-Modification to Acquisition Processor PWA 205E2502-17 to Correct Timing Issue, Acron Aviation | 2100-4042-53 |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB027 | 02 | 1/9/2019 | SB027-Part Number Conversion Instructions for 90-Day ULB | FA2100 FDR Service Bulletin 27 for P/N Conversion from 2100-4045-22 to 2100-4945-22 after 90-Day ULB Installation | 2100-4045-22, 2100-4945-22 | |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB019 | 31-30-03-019 | 01 | 9/28/2018 | SB019-Introduction of Improved Storage Capacitor | Introduction of Improved Storage Capacitor, Acron Aviation | 2100-2042-XX , 2100-2043-XX, 21002044-XX, 2100-2045-XX, 2100-4042-XX, 2100-4043-XX , 2100-4044-XX and 2100-4045-XX, 2100-4065-XX |
| FA2100 FDR | Service Bulletin | SB033-FA2100FDR | FA2100FDR-31-0033 | 01 | 7/30/2024 | SB033-Service Bulletin for New Accelerometer TSO | HARDWARE – PRODUCT IDENTIFICATION LABEL UPDATE FOR TSO-C124c and ED-112A | 2100-4245-00 or 2100-4245-60 |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB017 | 31-30-03-017 | 01 | 9/28/2018 | SB017-Installation of Mounting Bracket to Support Storage Capacitor | Service Bulletin 17 for FA2100 FDR. MOD DOT 11., Acron Aviation | 2100-2042-00 2100-2043-XX 2100-2044-XX 2100-2045-XX 2100-4042-XX 2100-4043-XX 2100-4044-XX 2100-4045-XX |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB028 | 31-30-03-028 | 11 | 4/8/2025 | SB028- MOD 18 – Chassis Assembly Update to apply moisture prevention countermeasure. | HW MOD 18. Update to chassis assembly. Incorporate moisture prevention countermeasure. | (Short Case) 2100-2042-00, 2100-2045-00, 2100-2043-12 (Long Case) 2100-4042-00, 2100-4043-00, 2100-4043-02, 2100-4044-00, 2100-4045-00, 2100-4045-60, 2100-4243-00, 2100-4245-00, 2100-4245-22, 2100-4245-60 |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB025 | 08 | 8/15/2022 | SB025-Introduction of New Software Revision and CSMU Part Number | Introduction of New Software Revision and CSMU Part Number | 2100-2xxx-xx, 2100-4xxx-xx | |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB026 | 02 | 8/15/2022 | SB026-MOD-DOT 17: INTRODUCTION OF NEW CSMU PART NUMBER | MOD-DOT 17: INTRODUCTION OF NEW CSMU PART NUMBER | 2100-XXXX-XX | |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB029 | 31-30-03-029 | 08 | 4/8/2025 | SB029 - MOD 19 - New Parylene Coated CCA | HW MOD 19. Incorporate moisture prevention countermeasure. | short case 2100-2042-00, 2100-2043-12 2100-2044-51 2100-2045-00 2100-2243-00 long case 2100-4042-00 2100-4043-00 2100-4043-02 2100-4044-00 2100-4045-00 2100-4045-60 2100-4243-00 2100-4245-00 2100-4245-22 2100-4245-60 |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB031 | 01 | 8/15/2022 | SB031-SOFTWARE MOD 06 | SOFTWARE MOD 06 | 2100-4945-22 | |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB030 | 01 | 9/30/2021 | SB030-Convert P/N 2100-4945-22 to P/N 2100-4945-23 | Convert P/N 2100-4945-22 to P/N 2100-4945-23 | 2100-4945-22, 2100-4945-23 | |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB020 | 06 | 3/15/2022 | SB020-REPLACEMENT OF NON−CONFORMING HARDWARE | REPLACEMENT OF NON−CONFORMING HARDWARE | 2100- | |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB032 | 00 | 12/23/2021 | SB032-Convert P/N 2100-2045-00 to P/N 2100-2045-23 | Convert P/N 2100-2045-00 to P/N 2100-2045-23 | 2100-2045-00, 2100-2045-23 | |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB024 | 07 | 10/15/2022 | SB024-INTRODUCTION OF L3AP 90-DAY UNDERWATER LOCATOR BEACON PART NUMBER 266E5542-00 | INTRODUCTION OF L3AP 90-DAY UNDERWATER LOCATOR BEACON PART NUMBER 266E5542-00 | 2100-2042, 2100-2043, 2100-2044, 2100-2045, 2100-4042, 2100-4043, 2100-4044, 2100-4045, 2100-4065 | |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB018 | 31-30-03-018 | 01 | 9/28/2018 | SB018-Software Revision 02 | FA2100 FDR Service Bulletin 18, Software Revision 02, Acron Aviation | 2100-2045-00, 2100-4045-00, 2100-4045-22 |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB022 | 31-30-03-022 | 02 | 9/28/2018 | SB022-SW MOD DOT | INTRODUCTION OF NEW SOFTWARE, Acron Aviation | 2100-2042-xx, 2100-2044-xx, 2100-2045-xx, 2100-4042-xx, 2100−4043−xx, 2100−4044−xx, 2100−4045−xx and 2100−4065−xx |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB023 | 31-30-03-023 | 01 | 9/28/2018 | SB023-SW MOD DOT | INTRODUCTION OF NEW SOFTWARE, Acron Aviation | 2100-2042-xx, 2100-2043-xx, 2100-2044-xx, 2100-2045-xx, 2100-4042-xx, 2100−4043−xx, 2100−4044−xx, 2100−4045−xx and 2100−4065−xx |
| FA2100 FDR | Service Letter | SIL-003-ULB | 02 | 3/6/2025 | Service Information Letter, NTO for ULB | No Technical Objection (NTO) FA2100 and FA5000 Recorder Models for alternate Underwater Locator Beacon (ULB) installation. TSO-C142B Compliant Devices: • P/N 9080-10036-01. DK290-11, Dukane (Non-Restricted Class 9 Lithium Battery) • P/N 266-E6914-00. Green90, Novega P/N: 22960−00 (Lithium Free Battery) | ALL FA2100, FA5000 ULB: 9080-10036-01 ULB: 266-E6914-00 | |
| FA2200 MADRAS | Component Maintenance Manual | 165E1900-00 | 31-30-04 | 04 | 4/15/2025 | FA22XX FDR-MADRAS CMM | Modular Airborne Data Recording/Acquisition System Flight Data Recorder ARINC 404A | 2202-1100-00 2202-1101-00 2202-1300-00 2202-1300-01 2202-2000-00 |
| FA2200 MADRAS | Installation Manual | 165E1901-02 | 01 | 4/15/2025 | FA220x MADRAS/FDR Installation & Operation Manual for 2202-2000-00 | FA2200 Modular Airborne Data Recording/Acquisition System Flight Data Recorder ARINC 404A | 2202-2000-00 | |
| FA2200 MADRAS | Installation Manual | 165E1901-00 | 05 | 4/15/2025 | FA22xx FDR-MADRAS Installation Manual | FA22xx Modular Airborne Data Recording Acquisition System Flight Data Recorder ARINC 404A | 2202–1100–00 2202−1101−00 2204–1000–00 | |
| FA2200 MADRAS | Installation Manual | 165E1901-07 | 01 | 4/15/2025 | FA2200 MADRAS/CVDR Installation Manual for 2202-1301-00 | FA220x MADRAS/FDR Installation & Operation Manual for 2202-1301-00 ARINC 747 | 2202-1301-00 | |
| FA2200 MADRAS | Installation Manual | 165E1901-03 | 01 | 4/15/2025 | FA220x MADRAS/FDR Installation & Operation Manual for 2202-2100-00 | FA220x Modular Airborne Data Recording/Acquisition System Flight Data Recorder ARINC 404A | 2202-2100-00 | |
| FA2200 MADRAS | Installation Manual | 165E1901-04 | 01 | 4/15/2025 | FA220x MADRAS/FDR Installation & Operation Manual for 2202-2300-00 | FA220x Modular Airborne Data Recording/Acquisition System Flight Data Recorder ARINC 747 | 2202-2300-00 | |
| FA2200 MADRAS | Installation Manual | 165E1901-05 | 02 | 4/15/2025 | FA2200 MADRAS/CVDR Installation & Operation Manual for 2202-2600-00 | FA220x MADRAS/FDR Installation & Operation Manual for 2202-2600-00 ARINC 747 | 2202-2600-00 | |
| FA2200 MADRAS | Installation Manual | 165E1901-01 | 02 | 4/15/2025 | FA22xx MADRAS/FDR Installation & Operation Manual for 2202-1300-XX | FA2200 Modular Airborne Data Recording/Acquisition System Flight Data Recorder ARINC 747 | 2202−1300−00 2202−1300−01 | |
| FA2200 MADRAS | Service Bulletin | SB2202-1300-00-013 | FA2202-31-0000 | 00 | 10/6/2020 | Part Number Conversion 2202-1300-00 to 2202-1300-01 | Part Number Conversion 2202-1300-00 to 2202-1300-01 | 2202-1300-00, 2202-1300-01 |
| FA2300 MADRAS | Installation Manual | 165E1903-24 | Init | 3/15/2011 | FA23XX MADRAS CVDR for the AAI Bell 412, 2316-1203-01 | FA23XX MADRAS CVDR for the AAI Bell 412, 2316-1203-01 | 2316-1203-01 | |
| FA2300 MADRAS | Installation Manual | 165E1903-09 | 09 | 6/30/2025 | FA2300 MADRAS CVDR Installation Manual for 2306-1401-01, 2306-1403-01 | Modular Airborne Data Recording/Acquisition System Cockpit Voice and Data Recorder Model: FA2300 MADRAS CVDR ARINC 404A | 2306-1401-01, 2306-1403-01 | |
| FA2300 MADRAS | Installation Manual | 165E1903-14 | Initial | 7/15/2009 | FA23XX MADRAS CVDR Installation Manual for 2306-1402-01 | FA23XX MADRAS CVDR Installation Manual for 2306-1402-01 | 2306-1402-01 | |
| FA2300 MADRAS | Installation Manual | 165E1903-33 | 02 | 4/30/2023 | Installation and Operation Manual, FA2300 | Modular Airborne Data Recording/Acquisition System Cockpit Voice And Data Recorder For The Beechcraft King Air | 2312−8500−02, 2312−8500−03 | |
| FA2300 MADRAS | Installation Manual | 165E1903-06 | 02 | 2/15/2010 | Installation Manual | Modular Airborne Data Recording/Acquisition Systems Cockpit Voice And Data Recorder For The Gulf Bell 412 | 2306-1202-00 | |
| FA2300 MADRAS | Installation Manual | 165E1903-03 | 05 | 10/15/2011 | Installation and Operation Manual, FA2300 | Cockpit Voice and Data Recorder | 2316-1600-00, S056-0048-00, S261-1130-00 | |
| FA2300 MADRAS | Installation Manual | 165E1903-36 | 01 | 8/30/2021 | Installation & Operation Instruction Manual, FA2300 | Cockpit Voice and Data Recorder | 2312−8500−94 | |
| FA2300 MADRAS | Installation Manual | 165E1903-05 | 05 | 5/15/2025 | Installation and Operation Instruction Manual, FA2300 | Cockpit Voice and Data Recorder | 2306-1800-00 | |
| FA2300 MADRAS | Service Bulletin | SB022-FA2316CVDR | A2316-23-0001 | 00 | 5/15/2024 | Service Bulletin, MOD 20, PN 2316-1501-01 | HARDWARE MOD 20 REPLACES CHASSIS ASSEMBLY, PART NO. 253E3825-05 WITH 253E3825-27, REV A (OR AFTER) | 2316-1501-01 |
| FA5000 CVDR | Component Maintenance Manual | 165E5906-02 | 23-70-43 | 01 | 11/15/2024 | FA5000 MADRAS CVDR CMM | COCKPIT VOICE AND DATA RECORDER MODEL FA5000 MADRAS CVDR | 5311−6143−21, 5311−6143−22 |
| FA5000 CVDR | Component Maintenance Manual | 165E5327-12 | 23-70-42 | 01 | 12/30/2021 | FA5013 DVDR Digital Voice and Data Recorder (CMM) | FA5013 DVDR CMM | 165E5327−12, 5013-6100-01 |
| FA5000 CVDR | Component Maintenance Manual | 165E6554-00 | 23-70-42 | 04 | 12/30/2022 | FA5000 CVDR CMM | FA5000 CVDR CMM | 5011-6133-11, 5051-6133-11 500-4030-000 |
| FA5000 CVDR | Component Maintenance Manual | 165E1689-01 | 23-70-31 | 04 | 4/30/2024 | Component Maintenance Manual, FA5000 CVDR | Cockpit Voice and Data Recorder | Recorder 5003-6100-00, 5003-6100-50, 5013-6100-50 RIPS 500−4030−000 |
| FA5000 CVDR | Installation Manual | 165E6554-01 | 05 | 1/15/2023 | FA5000 CVDR Installation & Operation Manual | FA5000 CVDR with Datalink and Cockpit Image Recording Model: FA5000 CVDR Recorder P/N 5011-6133-11, 5051-6133-11 Recorder Independent Power Supply (RIPS) P/N 500-4030-000 Cockpit Area Microphone P/N S056-0048-10 | 5011-6133-11, 5051-6133-11 | |
| FA5000 CVDR | Installation Manual | 165E5327-01 | 15 | 4/15/2024 | FA5000 CVDR Installation and Operation Instruction Manual | FA5000 CVDR Short Case IOM | 5001-6103-11, 5001-6133-11, 5003-6103-11, 5011-6103-11 500-4030-000 | |
| FA5000 CVDR | Installation Manual | 165E5327−13 | 03 | 12/30/2021 | FA5013 DVDR Digital Voice and Data Recorder (IOM) | FA5013 DVDR Digital Voice and Data Recorder (IOM) | 500−4030−000, 5013-6100-01 | |
| FA5000 CVDR | Installation Manual | 165E5327-04 | 02 | 4/30/2024 | Installation and Operation Instruction Manual, FA5000 CVDR | COCKPIT VOICE AND DATA RECORDER MODEL FA5000 CVDR ARINC 757 | 5003−6100−00 RIPS Part Number: 500−4030−000 | |
| FA5000 CVDR | Installation Manual | 165E5327-21 | 03 | 5/15/2024 | Installation & Operation Instruction Manual, FA5000 CVDR, PN 5011-8103-11 | COCKPIT VOICE AND DATA RECORDER | 5011-8103-11 | |
| FA5000 CVDR | Installation Manual | 165E5327−04 | 01 | 2/28/2024 | FA5000 CVDR Digital Voice and Data Recorder (IOM) | FA5000 CVDR Digital Voice and Data Recorder (IOM) | 5003-6100-00 RIPS: 500−4030−000, | |
| FA5000 CVDR | Installation Manual | 165E5327-01-R14-TR-01 | TR-01 | 2/15/2024 | FA5000 CVDR Installation and Operation Instruction Manual | FA5000 CVDR Short Case IOM Temporary Revision for 165E5327-01 rev 14 | 5001-6103-11, 5001-6133-11, 5003-6103-11, 5011-6103-11 | |
| FA5000 CVDR | Installation Manual | 165E5327-55 | 04 | 5/30/2024 | INSTALLATION & OPERATION INSTRUCTION MANUAL (GA CVDR) FA5003/FA5013 | INSTALLATION & OPERATION INSTRUCTION MANUAL MODEL FA5003 & FA5013 CVDR COCKPIT VOICE & DATA RECORDER for GENERAL AVIATION 1/2-ATR SHORT CASE | 5003−6100−50, 5013−6100−50 500-4030-000 | |
| FA5000 CVDR | Service Bulletin | SB003-FA5013 | FA5013-23-0001 | 00 | 12/30/2021 | HARDWARE MOD 08 | Update the aircraft interface PWA HARDWARE MOD 08 – UPDATE THE AIRCRAFT INTERFACE PWA, PART NO. 205-E6227-00 TO REVISION J, Acron Aviation | 5013-6100-01 |
| FA5000 CVDR | Service Bulletin | SB002-FA5000 | 01 | 1/30/2025 | Hardware MOD 03 and 04 | Hardware MOD 03 and 04, Acron Aviation | 5003-6100-00 5003-6100-50 5013-6100-50 5001-6103-11 5001-6133-11 5003-5000-00 5003-5001-50 5013-5001-50 5003-3100-01 5013-3100-00 5003-3103-11 5001-5003-11 5003-5003-11 5033-5003-11 5011-6103-11 | |
| FA5000 CVDR | Service Bulletin | SB002-FA5000CVDR | FA5000CVDR-23-0001 | 00 | 7/15/2022 | CONVERSION OF PART NO. 5011-6133-11 TO PART NO. 5051-6133-11 | CONVERSION OF PART NO. 5011-6133-11 TO PART NO. 5051-6133-11, Acron Aviation | 23-70-35, 5011-6133-11, 5051-6133-11 |
| FA5000 CVDR | Service Bulletin | 50x1-6103-11-001 | 23-70-40-01 | 02 | 7/30/2022 | HARDWARE MOD 02 – IMPROVED MAIN PROCESSOR | HARDWARE MOD 02 – IMPROVED MAIN PROCESSOR, Acron Aviation | 5001-6103-11 |
| FA5000 CVDR | Service Bulletin | SB003-FA5000CVDR | FA5000CVDR-23-0002 | 00 | 7/30/2022 | MOD 06 – CSMU PRODUCTION IMPROVEMENT | MOD 06 – CSMU PRODUCTION IMPROVEMENT, Acron Aviation | 5011-6133-11, |
| FA5000 CVDR | Service Bulletin | SB001-FA5000 | FA5000-70-6000 | 06 | 4/3/2025 | Introduction of Software MOD 12 | Introduction of Software MOD 12 Software MOD 12 (SW 2.6) ensure capability with new SDRAM component on the FA5000 Main Processor PWA and power anomalies possible at startup. Acron Aviation | 5001-6103-11 5003-6103-11 5013-6100-50 5011-6103-11 5011-8103-11 5013-6100-01 5003-5003-11 5033-5003-11 5003-5000-01 5013-5000-30 5013-5001-50 5003-3100-01 5013-3100-00 5013-3100-30 |
| FA5000 CVDR | Service Bulletin | SB004-FA5000 | 03 | 7/16/2024 | Service Bulletin, MOD 7 | Hardware MOD 7 to release new Main Processor PWA with update firmware. note: Revision 03 adds new part number to the SB. | (FDR), P/N: 5003-3100-00, 5003-3100-01, 5003-3103-11, 5003-6100-50, 5013-3100-00, 5031-3103-11. (CVR), P/N: 5001-5003-11, 5003-5001-50, 5003-5003-11, 5013-5001-50, 5033-5003-11, 5053-5003-11. (CVDR), P/N: 5001-6103-11, 5003-6100-00, 5003-6103-11, 5011-6103-11, 5011-8103-11, 5013-6100-50. | |
| FA5000 CVDR | Service Letter | SIL-003-FA5000 | 00 | 12/19/2023 | Service Information Letter | Anomalies in downloaded flight data. | CVDR: 5001-6103-11, 5003-6103-11, 5013-6100-50, 5011-6103-11, 5011-8103-11, 5013-6100-01. CVR: 5003-5003-11, 5033-5003-11, 5003-5000-01, 5013-5000-30, 5013-5001-50 FDR: 5003-3100-01, 5013-3100-00, 5013-3100-30 DVR: 5011-6133-11 | |
| FA5000 CVDR | Service Letter | SIL-003-ULB | 02 | 3/6/2025 | Service Information Letter, NTO for ULB | No Technical Objection (NTO) FA2100 and FA5000 Recorder Models for alternate Underwater Locator Beacon (ULB) installation. TSO-C142B Compliant Devices: • P/N 9080-10036-01. DK290-11, Dukane (Non-Restricted Class 9 Lithium Battery) • P/N 266-E6914-00. Green90, Novega P/N: 22960−00 (Lithium Free Battery) | ALL FA2100, FA5000 ULB: 9080-10036-01 ULB: 266-E6914-00 | |
| FA5000 CVDR | Service Letter | SIL-004-FA5000 | 00 | 3/18/2025 | Service Information Letter | Temporary Approval for Return-to-Service exception / Required Compliance – Channel Balance Tests. | 5003-6100-00, 5003-6100-50, 5013-6100-50 | |
| FA5000 CVDR | Service Letter | PI/2-001 | 03 | 2/12/2024 | Notification of discontinued product. | Notification of discontinued product. | 17TES0062, 17TES0065, 17TES0066, 17TES0092 | |
| FA5000 CVR | Component Maintenance Manual | 165E5398-00-R10-TR01 | 23-70-35 | TR-01 | 2/15/2024 | Model FA5000 Cockpit Voice Recorder CMM | FA5000 CVR CMM Temp revision for 165E5398-00, Revision 10. | 5001-5003-11, 5003-5003-11, 5033-5003-11, 5053-5003-11 |
| FA5000 CVR | Component Maintenance Manual | 165E5398-00 | 23-70-40 | 11 | 4/15/2024 | Model FA5000 Cockpit Voice and Data Recorder CMM | FA5000 CVDR CMM | 5001-6103-11, 5001-6133-11, 5003-6103-11, 500-4030-000, 5011-6103-11, 5011-8103-11 |
| FA5000 CVR | Component Maintenance Manual | 165E5398-01 | 23-70-35 | 05 | 1/30/2025 | FA5000 Cockpit Voice Recorder CMM | FA5000 CVR CMM RIPS | 5001-5003-11, 5003-5003-11, 5033-5003-11, 5053-5003-11. 500−4030−000 |
| FA5000 CVR | Component Maintenance Manual | 165E1689-02 | 23-70-30 | 08 | 3/31/2025 | FA5000 Cockpit Voice Recorder, CMM | FA5000 CVR CMM | 5003-5000-00, 5003-5000-01, 5003-5000-30, 5003-5001-50, 500-4030-00, 5013-5000-30, 5013-5001-50 |
| FA5000 CVR | Installation Manual | 165E5327-00 | 07 | 3/31/2025 | FA5000 Cockpit Voice Recorder 1/2 ATR Short Case IOM | FA5000 Short Case IOM | 5001-6103-11, 5003-5000-00, 5003-5000-01 500-4030-000 | |
| FA5000 CVR | Installation Manual | 165E5850-01 | INT | 5/19/2016 | FA5013 CVR 1/2 Short Case Installation & Operation Manual | FA5013 CVR 1/2 Short Case Installation & Operation Manual | 5013-5000-30 | |
| FA5000 CVR | Installation Manual | 165E5327-11 | 09 | 1/30/2025 | FA5000 CVR Installation & Operation Manual | FA5000 CVR RIPS 500−4030−000 | 5001-5003-11, 5003-5003-11, 5053-5003-11 500-4030-000 | |
| FA5000 CVR | Installation Manual | 165E5328-11 | 04 | 11/30/2023 | FA5033 CVR Installation & Operation Manual | COCKPIT VOICE RECORDER MODEL FA5033 CVR | 5033−5003−11 | |
| FA5000 CVR | Installation Manual | 165E5327-50 | 04 | 1/5/2024 | FA5000 Cockpit Voice Recorder IOM | FA5000 CVR ARINC 757, 757A | 5000-5001-50, 5003-5001-50, 5013-5001-50, 5013-5001-50 | |
| FA5000 CVR | Installation Manual | 165E5278-11 | 07 | 1/30/2025 | Installation Manual, FA5033, CVR | COCKPIT VOICE RECORDER MODEL FA5033 CVR | 5033−5003−11 | |
| FA5000 CVR | Installation Manual | 165E5327-97 | 07 | 5/29/2014 | Installation and Operation Instruction Manual, FA5003-5000-97CVR | MODEL FA5003- 5000- 97CVR COCKPIT VOICE RECORDER 1/2-ATR SHORT CASE | 5003-5000-97 rips 500- 4030- 000 | |
| FA5000 CVR | Service Bulletin | SB50X3-5003-11-001 | 23-70-35 | 00 | 7/13/2018 | INTRODUCTION OF SOFTWARE VERSION 06 | SOFTWARE VERSION 06, Acron Aviation | 5003−5003−11, 5033−5003−11 |
| FA5000 CVR | Service Bulletin | SB006-FA5003 | FA5003-23-0001 | 00 | 8/30/2021 | CONVERSION OF PART NO. 5003-5003-11 TO PART NO. 5053-5003-11 | This service bulletin implements hardware modifications to the FA5000 Cockpit Voice Recorder. CONVERSION OF PART NO. 5003-5003-11 to PART NO. 5053-5003-11, Acron Aviation | 5003-5003-11, 5053-5003-11, FA5000, FA5003, FA5053 |
| FA5000 CVR | Service Bulletin | SB007-FA5000CVR | FA5000CVR-23-0003 | 00 | 6/15/2022 | HARDWARE MOD 05 – UPDATES TO MAIN PROCESSOR PWA | HARDWARE MOD 05 – UPDATES TO MAIN PROCESSOR PWA, Acron Aviation | 23-70-30, 5003-5000-01, 5013-5000-30 |
| FA5000 CVR | Service Bulletin | SB007-FA5003 | FA5003-23-0002 | 00 | 8/15/2022 | HARDWARE MOD 06 – UPDATE WITH NEW CSMU | HARDWARE MOD 06 – UPDATE WITH NEW CSMU, Acron Aviation | 23-70-35, 5001-5003-11, 5003-5003-11 |
| FA5000 CVR | Service Bulletin | SB002-FA5000 | 01 | 1/30/2025 | Hardware MOD 03 and 04 | Hardware MOD 03 and 04, Acron Aviation | 5003-6100-00 5003-6100-50 5013-6100-50 5001-6103-11 5001-6133-11 5003-5000-00 5003-5001-50 5013-5001-50 5003-3100-01 5013-3100-00 5003-3103-11 5001-5003-11 5003-5003-11 5033-5003-11 5011-6103-11 | |
| FA5000 CVR | Service Bulletin | SB005-FA5003 | FA5003-31-6000 | 01 | 2/16/2021 | Introduction of Software MOD 11 | Software MOD 11 (SW 2.5) removes the DHCP option to obtain IP Addresses for the recorder, improve the record only mode protection, and update the Datalink record function, Acron Aviation | 5003-5000-01 |
| FA5000 CVR | Service Bulletin | SB001-FA5000 | FA5000-70-6000 | 06 | 4/3/2025 | Introduction of Software MOD 12 | Introduction of Software MOD 12 Software MOD 12 (SW 2.6) ensure capability with new SDRAM component on the FA5000 Main Processor PWA and power anomalies possible at startup. Acron Aviation | 5001-6103-11 5003-6103-11 5013-6100-50 5011-6103-11 5011-8103-11 5013-6100-01 5003-5003-11 5033-5003-11 5003-5000-01 5013-5000-30 5013-5001-50 5003-3100-01 5013-3100-00 5013-3100-30 |
| FA5000 CVR | Service Bulletin | FA5000-SB004 | 02 | 3/16/2015 | Introduction of 90 Day ULB | Introduction of 90 Day ULB | 50xx-xxxx-xx (FDR), P/N: 5003-3100-00, 5003-3100-01, 5003-3103-11, 5003-6100-50, 5013-3100-00, 5031-3103-11. (CVR), P/N: 5001-5003-11, 5003-5000-00, 5003-5000-01, 5003-5001-50, 5003-5003-11, 5013-5000-50, 5013-5000-30, 5013-5001-50, 5033-5003-11, 5053-5003-11. (CVDR), P/N: 5001-6103-11, 5003-6100-00, 5003-6103-11, 5011-6103-11, 5011-8103-11, 5013-6100-50 | |
| FA5000 CVR | Service Bulletin | SB004-FA5000 | 03 | 7/16/2024 | Service Bulletin, MOD 7 | Hardware MOD 7 to release new Main Processor PWA with update firmware. note: Revision 03 adds new part number to the SB. | (FDR), P/N: 5003-3100-00, 5003-3100-01, 5003-3103-11, 5003-6100-50, 5013-3100-00, 5031-3103-11. (CVR), P/N: 5001-5003-11, 5003-5001-50, 5003-5003-11, 5013-5001-50, 5033-5003-11, 5053-5003-11. (CVDR), P/N: 5001-6103-11, 5003-6100-00, 5003-6103-11, 5011-6103-11, 5011-8103-11, 5013-6100-50. | |
| FA5000 CVR | Service Letter | SIL-003-FA5000 | 00 | 12/19/2023 | Service Information Letter | Anomalies in downloaded flight data. | CVDR: 5001-6103-11, 5003-6103-11, 5013-6100-50, 5011-6103-11, 5011-8103-11, 5013-6100-01. CVR: 5003-5003-11, 5033-5003-11, 5003-5000-01, 5013-5000-30, 5013-5001-50 FDR: 5003-3100-01, 5013-3100-00, 5013-3100-30 DVR: 5011-6133-11 | |
| FA5000 CVR | Service Letter | SIL-003-ULB | 02 | 3/6/2025 | Service Information Letter, NTO for ULB | No Technical Objection (NTO) FA2100 and FA5000 Recorder Models for alternate Underwater Locator Beacon (ULB) installation. TSO-C142B Compliant Devices: • P/N 9080-10036-01. DK290-11, Dukane (Non-Restricted Class 9 Lithium Battery) • P/N 266-E6914-00. Green90, Novega P/N: 22960−00 (Lithium Free Battery) | ALL FA2100, FA5000 ULB: 9080-10036-01 ULB: 266-E6914-00 | |
| FA5000 CVR | Service Letter | PI/2-001 | 03 | 2/12/2024 | Notification of discontinued product. | Notification of discontinued product. | 17TES0062, 17TES0065, 17TES0066, 17TES0092 | |
| FA5000 FDR | Component Maintenance Manual | 165E5398-04 | 31-30-35 | 03 | 10/15/2024 | Component Maintenance Manual, FDR, FA5001/FA5003/FA5031 | 5001−3103−11, 5003−3103−11, 5031−3103−11 FDR Flight Data Recorder | 5001-3103-11 5003-3103-11 5031-3103-11 |
| FA5000 FDR | Component Maintenance Manual | 165E1689-03 | 31-30-30 | 06 | 4/30/2024 | Component Maintenance Manual, FA5000 FDR | Flight Data Recorder Model Variant: FA5003 and FA5013 | 5003-3100-00, 5003-3100-01, 5013-3100-00, 5013-3100-30 |
| FA5000 FDR | Installation Manual | 165E5326-00 | 06 | 4/30/2024 | Installation & Operation Instruction Manual, FA5003 & FA5013 FDR | FA5003 & FA5013 Flight Data Recorder Installation & Operation Manual | 5003−3100−00, 5003−3100−01, 5013−3100−00 | |
| FA5000 FDR | Installation Manual | 165E5850-02 | 01 | 4/30/2024 | FA5000 FDR IOM. FA5013 | FA5013 FDR IOM | 5013-3100-30 | |
| FA5000 FDR | Installation Manual | 165E5327-10 | 08 | 10/15/2024 | Installation and Operation Instruction Manual. P/N 5001−3103−11, 5003−3103−11 | MODEL FA5000 FDR FLIGHT DATA RECORDER | 5001−3103−11, 5003−3103−11 | |
| FA5000 FDR | Installation Manual | 165E5278-10 | 04 | 5/15/2024 | Installation Manual, FA5031, FDR | MODEL FA5031 FDR FLIGHT DATA RECORDER | 5031-3103-11 | |
| FA5000 FDR | Service Bulletin | SB004-FA5000 | 03 | 7/16/2024 | Service Bulletin, MOD 7 | Hardware MOD 7 to release new Main Processor PWA with update firmware. note: Revision 03 adds new part number to the SB. | (FDR), P/N: 5003-3100-00, 5003-3100-01, 5003-3103-11, 5003-6100-50, 5013-3100-00, 5031-3103-11. (CVR), P/N: 5001-5003-11, 5003-5001-50, 5003-5003-11, 5013-5001-50, 5033-5003-11, 5053-5003-11. (CVDR), P/N: 5001-6103-11, 5003-6100-00, 5003-6103-11, 5011-6103-11, 5011-8103-11, 5013-6100-50. | |
| FA5000 FDR | Service Bulletin | SB009-FA5000FDR | FA5000FDR-31-0009 | 00 | 10/15/2024 | HARDWARE MOD 06 REPLACES CSMU FOR RELIABILITY, P/N 5003-3103-11 | This service bulletin implements hardware modifications to the FA5000 FDR, P/N 5003-3103-11. Hardware MOD 06 Updates the Crash Survival Memory Unit (CSMU) P/N 253-E5856-00 to 253-E5856-01 for reliability. The new CSMU incorporates a new silicone cord seal, silicone gasket, and insulated housing for improve mounting of the beacon bracket. | 5003-3103-11 |
| FA5000 FDR | Service Bulletin | SB002-FA5000 | 01 | 1/30/2025 | Hardware MOD 03 and 04 | Hardware MOD 03 and 04, Acron Aviation | 5003-6100-00 5003-6100-50 5013-6100-50 5001-6103-11 5001-6133-11 5003-5000-00 5003-5001-50 5013-5001-50 5003-3100-01 5013-3100-00 5003-3103-11 5001-5003-11 5003-5003-11 5033-5003-11 5011-6103-11 | |
| FA5000 FDR | Service Bulletin | SB001-FA5013 | FA5013-31-0000 | 03 | 1/8/2024 | Hardware MOD 7 to update Firmware on CCA Main Processor board. | Instructions for the installation of Firmware Part No. 840-E5479-04. Acron Aviation | 5013-3100-30 |
| FA5000 FDR | Service Bulletin | SB002-FA5013 | FA5013-23-0000 | 01 | 6/3/2021 | Instructions for the installation of Firmware Part No. 840-E5479-04. | MOD 7. This modification improves the ARINC 429 OMS output speed | 5013-5000-30 |
| FA5000 FDR | Service Bulletin | SB001-FA5000 | FA5000-70-6000 | 06 | 4/3/2025 | Introduction of Software MOD 12 | Introduction of Software MOD 12 Software MOD 12 (SW 2.6) ensure capability with new SDRAM component on the FA5000 Main Processor PWA and power anomalies possible at startup. Acron Aviation | 5001-6103-11 5003-6103-11 5013-6100-50 5011-6103-11 5011-8103-11 5013-6100-01 5003-5003-11 5033-5003-11 5003-5000-01 5013-5000-30 5013-5001-50 5003-3100-01 5013-3100-00 5013-3100-30 |
| FA5000 FDR | Service Bulletin | SB004-FA5003 | FA5003-23-6000 | 01 | 2/16/2021 | Introduction of Software MOD 11 | Software MOD 11 (SW 2.5) removes the DHCP option to obtain IP Addresses for the recorder, improve the record only mode protection, and update the Datalink record function, Acron Aviation | 5003-3100-01 |
| FA5000 FDR | Service Letter | SIL-003-FA5000 | 00 | 12/19/2023 | Service Information Letter | Anomalies in downloaded flight data. | CVDR: 5001-6103-11, 5003-6103-11, 5013-6100-50, 5011-6103-11, 5011-8103-11, 5013-6100-01. CVR: 5003-5003-11, 5033-5003-11, 5003-5000-01, 5013-5000-30, 5013-5001-50 FDR: 5003-3100-01, 5013-3100-00, 5013-3100-30 DVR: 5011-6133-11 | |
| FA5000 FDR | Service Letter | SIL-003-ULB | 02 | 3/6/2025 | Service Information Letter, NTO for ULB | No Technical Objection (NTO) FA2100 and FA5000 Recorder Models for alternate Underwater Locator Beacon (ULB) installation. TSO-C142B Compliant Devices: • P/N 9080-10036-01. DK290-11, Dukane (Non-Restricted Class 9 Lithium Battery) • P/N 266-E6914-00. Green90, Novega P/N: 22960−00 (Lithium Free Battery) | ALL FA2100, FA5000 ULB: 9080-10036-01 ULB: 266-E6914-00 | |
| FA5000 MADRAS | Installation Manual | 165E5906-01 | 04 | 11/15/2024 | Installation and Operation Instruction Manual | COCKPIT VOICE AND DATA RECORDER MODEL FA5000 MADRAS CVDR | 5311−6143−21, 5311−6143−22 | |
| FA5000 MADRAS | Service Bulletin | SB001-FA5311 | 00 | 11/18/2020 | Service Bulletin, MOD 6 | Firmware Update - Hardware MOD 06, Acron Aviation | 5311-6143-21 | |
| FA5000 MADRAS | Service Letter | SIL-003-ULB | 02 | 3/6/2025 | Service Information Letter, NTO for ULB | No Technical Objection (NTO) FA2100 and FA5000 Recorder Models for alternate Underwater Locator Beacon (ULB) installation. TSO-C142B Compliant Devices: • P/N 9080-10036-01. DK290-11, Dukane (Non-Restricted Class 9 Lithium Battery) • P/N 266-E6914-00. Green90, Novega P/N: 22960−00 (Lithium Free Battery) | ALL FA2100, FA5000 ULB: 9080-10036-01 ULB: 266-E6914-00 | |
| GA100 | Component Maintenance Manual | 165E010200 | 23-70-11 | Initial | 8/1/1989 | GA100 Component Maintenance Manual | GA100 CMM by special request only. Contact Avionics.TechPubs@L3Harris.com | GA100-0000, GA150-0000 |
| GA100 | Installation Manual | FAR04229004 | 23-70-11 | 2 | 1/27/1993 | GA100 Installation & Operation Manual | GA100 Installation & Operation Manual | GA100-0000, GA150-0000 |
| GE - Power Conditioning | Component Maintenance Manual | TP-569 | 24-30-21 | B C2 | 7/30/2014 | Component Maintenance Manual with IPL | Overhaul Manual for Transformer Rectifier | GEK-9107A |
| GE - Power Conditioning | Component Maintenance Manual | GEI-42518C | C | 10/1/1969 | Instructions with IPL | Pub# GEI-42518C | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-46981 | Orig | 7/26/2005 | Instructions | Pub# GEI-46981 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-47017 | Orig | 4/1/1963 | Instructions | Pub# GEI-47017 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-47162B | B | 7/26/2005 | Instructions | Pub# GEI-47162B | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-47252A | A | 1/1/1967 | Instructions | Pub# GEI-47252A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-47276B | B | 8/5/1963 | Instructions | Pub# GEI-47276B | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-47289 | Orig | 11/1/1960 | Instructions with IPL | Pub# GEI-47289 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-47329 | Orig | 7/1/1963 | Instructions with IPL | Pub# GEI-47329 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-47365 | Orig | 7/26/2005 | Instructions with IPL | Pub# GEI-47365 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-47390B | B | 7/26/2005 | Instructions with IPL | Pub# GEI-47390B | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-86820A | A | 7/26/2005 | Instructions | Pub# GEI-86820A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-86820B | B | 7/26/2005 | Instructions | Pub# GEI-86820B | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-86821A | 1 | 9/15/1972 | Instructions | Pub# GEI-86821A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-86823B | B | 8/12/1963 | Instructions | Pub# GEI-86823B | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-86840 | Orig | 7/26/2005 | Instructions | Pub# GEI-86840 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-86862A | A | 8/2/1963 | Instructions with IPL | Pub# GEI-86862A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-86896C | C | 7/26/2005 | Instructions with IPL | Pub# GEI-86896C | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-86969 | Orig | 7/26/2005 | Instructions with IPL | Pub# GEI-86969 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-86971 | Orig | 3/15/1963 | Instructions | Pub# GEI-86971 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-93104 | Orig | 7/26/2005 | Instruction | Pub# GEI-93104 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-93109C | 3 | 7/31/1967 | Maintenance and Overhaul Manual | Pub# GEI-93109C | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-93119B | 3 | 7/31/1967 | Maintenance and Overhaul Manual | Pub# GEI-93119B | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-93124B | B | 5/1/1972 | Instruction | Pub# GEI-93124B | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-93148 | Orig | 7/26/2005 | Preliminary Issue [No distribution] | Pub# GEI-93148 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-93151 | Orig | 3/15/1963 | Illustrated Parts Breakdown | Pub# GEI-93151 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-93232A | A | 7/26/2005 | Instructions | Pub# GEI-93232A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-93239 | Orig | 7/26/2005 | Instruction with IPL | Pub# GEI-93239 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-93268B | 1 | 9/7/1967 | Instruction with IPL | Pub# GEI-93268B | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-93269A | A | 7/26/2005 | Instruction with IPL | Pub# GEI-93269A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-98121 | Orig | 7/26/2005 | Instruction with IPL | Pub# GEI-98121 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-98255A | A | 3/1/1968 | Maintenance and Overhaul Manual | Pub# GEI-98255A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-98258B | 2 | 11/15/1966 | Maintenance and Overhaul Manual | Pub# GEI-98258B | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-98279A | A | 7/26/2005 | Instructions with IPL | Pub# GEI-98279A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-98282B | 1 | 9/1/1965 | Instruction Manual | Pub# GEI-98282B | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-98285A | A | 9/15/1969 | Maintenance and Overhaul Manual | Pub# GEI-98285A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12422 | Orig | 10/1/1967 | Field Maintenance with IPL | Pub# GEK-12422 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12423 | Orig | 10/1/1967 | Overhaul | Pub# GEK-12423 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12424 | Orig | 6/30/1967 | Illustrated Parts Breakdown | Pub# GEK-12424 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12426A | A | 11/1/1968 | Maintenance and Overhaul Manual | Pub# GEK-12426A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12433 | Orig | 7/26/2005 | Instructions with IPL | Pub# GEK-12433 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12437 | 24-30 | 2 | 2/15/1967 | Overhaul and Maintenance Manual | Pub# GEK-12437 | |
| GE - Power Conditioning | Component Maintenance Manual | GEK-12438 | Orig | 7/26/2005 | Instructions with Parts Breakdown | Pub# GEK-12438 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12439 | Orig | 3/1/1967 | Maintenance Manual with Parts Breakdown | Pub# GEK-12439 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12501A | A | 12/1/1968 | Field Maintenance Manual | Pub# GEK-12501A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12502 | Orig | 7/26/2005 | Field Maintenance Manual | Pub# GEK-12502 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12506 | Orig | 8/6/1959 | Operating and Maintenance Instruction | Pub# GEK-12506 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12507 | Orig | 10/1/1968 | Instructions | Pub# GEK-12507 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12560 | Orig | 4/1/1967 | Field Maintenance Manual | Pub# GEK-12560 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12561A | A | 7/26/2005 | Field Maintenance Manual | Pub# GEK-12561A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12566A | A | 1/11/1968 | Maintenance and Overhaul Manual | Pub# GEK-12566A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12568 | Orig | 7/26/2005 | Maintenance and Overhaul Manual | Pub# GEK-12568 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12571 | 24-30-xx | 11/1/1967 | Maintenance and Overhaul Manual | Pub# GEK-12571 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12572 | Orig | 7/26/2005 | Field Maintenance Manual | Pub# GEK-12572 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-12574 | 2 | 7/11/1990 | Maintenance/Overhaul Manual | Pub# GEK-12574 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-14790 | 1/25/1999 | Operations and Maintenance Instruction | Pub# GEK-14790 | |||
| GE - Power Conditioning | Component Maintenance Manual | GEK-14792 | Orig | 7/26/2005 | Instructions with IPL | Pub# GEK-14792 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-14797 | 24-30-04 | 1 | 4/1/1976 | Overhaul Manual with IPL | Pub# GEK-14797 | |
| GE - Power Conditioning | Component Maintenance Manual | GEK-14800 | 24-30-03 | Orig | 9/1/1969 | Overhaul Manual with IPL | Pub# GEK-14800 | |
| GE - Power Conditioning | Component Maintenance Manual | GEK-14802 | Orig | 8/15/1969 | Overhaul Instructions | Pub# GEK-14802 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-14803 | 24-30-05 | Orig | 11/1/1969 | Overhaul Manual with IPL | Pub# GEK-14803 | 3S2060DC169A1 |
| GE - Power Conditioning | Component Maintenance Manual | GEK-14807 | 1 | 10/15/1971 | Component Maintenance Manual | Pub# GEK-14807 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-14817 | 24-30-02 | 1 | 6/1/1973 | Overhaul Manual with IPL | Pub# GEK-14817 | |
| GE - Power Conditioning | Component Maintenance Manual | GEK-14820B | B | 8/7/1969 | Depot Maintenance and Parts Breakdown | Pub# GEK-14820B | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-14823 | 2 | 7/11/1990 | Maintenance and Overhaul Manual | Pub# GEK-14823 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-14825A | A | 8/7/1969 | Depot Maintenance and Parts Breakdown | Pub# GEK-14825A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-14826 | 24-30-01 | Orig | 8/28/1968 | Overhaul Manual with IPL | Pub# GEK-14826 | 3S2060DC168A1 |
| GE - Power Conditioning | Component Maintenance Manual | GEK-14828 | Orig | 11/15/1968 | Maintenance and Overhaul Manual | Pub# GEK-14828 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-14829 | Orig | 9/11/1968 | Instructions | Pub# GEK-14829 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-230 | 7/26/2005 | Instructions | Pub# GEK-230 | |||
| GE - Power Conditioning | Component Maintenance Manual | GEK-276 | Orig | 7/26/2005 | Overhaul Instructions with Parts Breakdown | Pub# GEK-276 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-343A | 2 | 1/1/1980 | Overhaul Instructions with Parts Breakdown | Pub# GEK-343A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-34425 | Orig | 11/15/1971 | Overhaul Manual with IPL | Pub# GEK-34425 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-34440 | 24-32-20 | 3 | 7/1/1979 | Overhaul Manual With IPL | Pub# GEK-34440 | |
| GE - Power Conditioning | Component Maintenance Manual | GEK-34442 | 24-30-18 | 1 | 2/15/1975 | Overhaul Manual with IPL | Pub# GEK-34442 | |
| GE - Power Conditioning | Component Maintenance Manual | GEK-34443 | Orig | 2/15/1972 | Overhaul Manual with IPL | Pub# GEK-34443 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-34450 | 24-30-17 | 3 | 12/23/1997 | Component Maintenance Manual | Pub# GEK-34450 | |
| GE - Power Conditioning | Component Maintenance Manual | GEK-34458 | 24-30-14 | Orig | 11/15/1974 | Overhaul Manual with IPL | Pub# GEK-34458 | |
| GE - Power Conditioning | Component Maintenance Manual | GEK-34459 | 24-30-15 | 1 | 7/15/1980 | Overhaul Manual with IPL | GEK-34459 | 3S2060DC168C1B |
| GE - Power Conditioning | Component Maintenance Manual | GEK-344B | 2 | 1/1/1980 | Maintenance and Overhaul Manual | Pub# GEK-344B | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-345 | Orig | 9/1/1968 | Instructions with IPL | Pub# GEK-345 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-4639A | Orig | 9/1/1966 | Maintenance and Overhaul Manual | Pub# GEK-4639A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-4666 | 1 | 10/1/1982 | Instructions with IPL | Pub# GEK-4666 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-4667A | A | 12/15/1966 | Maintenance and Overhaul Manual | Pub# GEK-4667A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-4676 | 1 | 6/1/1973 | Instructions with Parts Breakdown | Pub# GEK-4676 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-4704 | 24-30-11 | 1 | 4/10/1977 | Overhaul Manual with IPL | Pub# GEK-4704 | |
| GE - Power Conditioning | Component Maintenance Manual | GEK-4715 | Orig | 11/1/1965 | Field Maintenance Manual | Pub# GEK-4715 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-4717 | Orig | 12/1/1966 | Field Maintenance Manual | Pub# GEK-4717 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-4781 | C3 | 3/1/1966 | Field Maintenance | Pub# GEK-4781 | 697201-J | |
| GE - Power Conditioning | Component Maintenance Manual | GEK-4782 | C2 | 2/24/1981 | Overhaul | Pub# GEK-4782 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-4783 | Orig | 3/1/1966 | Illustrated Parts Breakdown | Pub# GEK-4783 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-4791 | Orig | 4/15/1966 | Operating and Maintenance Instructions with IPL | Pub# GEK-4791 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-4796 | Orig | 5/1/1966 | Maintenance and Overhaul manaul | Pub# GEK-4796 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-9119 | Orig | 6/1/1966 | Field Maintenance Manual | Pub# GEK-9119 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-93200 | Orig | 1/1/1958 | Instructions | Pub# GEI-93200 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-4704 Supplement A | 24-30-11 | 2/1/1966 | Supplement A to Overhaul Manual | Pub# GEK-4704 Supplement A | ||
| GE - Power Conditioning | Component Maintenance Manual | GEK-4704 Supplement B | 24-30-11 | 2/1/1966 | Overhaul Manual with IPL | Pub# GEK-4704 Supplement B | 3S2060DM118C1 | |
| GE - Power Conditioning | Component Maintenance Manual | GEI-67394 | 1 | 11/1/1958 | Overhaul Instructions with Parts Breakdown | Pub# GEI-67394 | ||
| GE - Power Conditioning | Component Maintenance Manual | GEI-98281B | Orig | 6/1/1965 | Instructions | Pub# GEI-98281B | ||
| GE - Power Conditioning | Installation Manual | GEI-36528B | B | 10/1/1969 | Instructions | Pub# GEI-36528B | ||
| GE - Power Conditioning | Installation Manual | GEI-72518 | Orig | 9/1/1958 | Operating and Maintenance Instructions | Pub# GEI-72518 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC126B1-SB01 | Orig | 5/3/1990 | Provides the procedures for modifying the speed sensing circuit to operate correctly with the replacement components. | 3S2060DC126B1 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC126B1-SB02B | Orig | 8/1/1990 | This document provides additional information for Service Bulletin 3S2060DC126B1-SB01. | 3S2060DC126B1 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC126B1-SB03 | Orig | 8/1/1990 | This document provides additional information for Service Bulletin 3S2060DC126B1-SB01. | 3S2060DC126B1 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC126B1-SB04 | Orig | 5/17/1991 | Provides additional circuit modifications which are required to reduce nuisance tripping of replacement parts for SCS 5 and SCS 6. The modification reduces the noise and temperature sensitivity of the circuit. | 3S2060DC126B1 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC135A1-24-17 | Orig | 2/15/1968 | First modification to replace CR3 and F1 and stamping an "M" after the serial number. Second modification to replace CR14, 15 and 16, changing wires 15-1 and 41 from #22 AWG to #18 AWG and changing "M" to "M1". | 3S2060DC135A1 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC164B1B,B2-24-01 | Orig | 6/16/1977 | Provides availability for a B2-24-01 adjustable resistor and diagnostic and troubleshooting procedures. | 3S2060DC164B1B, 3S2060DC164B1B2 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC168A1-24-01 | Orig | 12/20/1976 | This service bulletin provides instructions for locating and identifying capacitors suspected of leakage. | 3S2060DC168A1 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC168A1-24-02 | Orig | 6/16/1977 | Issued as a product improvement notification to advise operators of the availability of an adjustable resistor having improved service life and reliability. This bulletin also provides diagnostic and troubleshooting procedures to aid in resolving genera | 3S2060DC168A1 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC168A2, A3-24-01 | Orig | 3/1/1977 | This service bulletin provides instructions for locating and identifying capacitors suspected of leakage. | 3S2060DC168A2, 3S2060DC168A3 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC168A2A-24-01 | Orig | 4/4/1977 | This service bulletin provides instructions for locating and identifying capacitors suspected of leakage. | 3S2060DC168A2A | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC168A2A-24-02 | Orig | 6/16/1977 | Issued as a product improvement notification to advise operators of the availability of an adjustable resistor having improved service life and reliability. This bulletin also provides diagnostic and troubleshooting procedures to aid in resolving generat | 3S2060DC168A2A | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC168A2A-24-03 | Orig | 5/31/1990 | This bulletin provides the procedures for modifying the generator control unit to improve the noise rejection characteristics of the over voltage protection circuit. | 3S2060DC168A2A | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC168B1-24-04 | 1 | 3/10/1997 | This bulletin identifies a replacement A2 circuit board which isolates the over voltage protection circuit from capacitor C5 to eliminate this potential problem. | 3S2060DC168B1 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC168C1B-24-01 | Orig | 12/20/1976 | This Service Bulletin provides instructions for locating and identifying capacitors suspected of leakage. | 3S2060DC168C1B | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC168C1B-24-02 | Orig | 6/16/1977 | Issued as a product improvement notification to advise operators of the availability of an adjustable resistor having improved service life and reliability. This bulletin also provides diagnostic and troubleshooting procedures to aid in resolving generat | 3S2060DC168C1B | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC168D1-24-01 | 1 | 3/11/1977 | This Service Bulletin provides instructions for locating and identifying capacitors suspected of leakage. | 3S2060DC168D1 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC168D1-24-02 | 1 | 1/15/1981 | Issued as a product improvement notification to advise operators of the availability of an adjustable resistor having improved service life and reliability. This bulletin also provides diagnostic and troubleshooting procedures to aid in resolving generat | 3S2060DC168D1 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC168D1-24-03 | Orig | 12/1/1993 | This bulletin identifies a replacement A2 circuit board which isolates the over voltage protection circuit from capacitor C5 to eliminate this potential problem. | 3S2060DC168D1 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC168E1-24-01 | Orig | 3/11/1977 | This service bulletin provides instructions for locating and identifying capacitors suspected of leakage. | 3S2060DC168E1 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC168E1-24-02 | Orig | 6/16/1977 | Issued as a product improvement notification to advise operators of the availability of an adjustable resistor having improved service life and reliability. This bulletin also provides diagnostic and troubleshooting procedures to aid in resolving generat | 3S2060DC168E1 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC169A1-24-01 | Orig | 6/16/1977 | Issued as a product improvement notification to advise operators of the availability of an adjustable resistor having improved service life and reliability. This bulletin also provides diagnostic and troubleshooting procedures to aid in resolving generat | 3S2060DC169A1 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DM138A1 | Orig | 2/15/1968 | The revised trip point setting will improve starting characteristics. This readjustment is being offered to insure transfer from the starter mode to the generator mode at idle speed | 3S2060DM138A1 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DR132A1A-24-16 | 2/15/1968 | To improve reliability, a transfer circuit was designed to replace the SCR's associated with the turn-off circuit. | 3S2060DR132A1A | |||
| GE - Power Conditioning | Service Bulletin | SB3S2060DR132C1C-24-01 | Orig | 12/20/1976 | This service bulletin provides instructions for locating and identifying capacitors suspected of leakage. | 3S2060DR132C1C | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DR149A1A-24-01 | 1 | 5/30/1984 | Issued as product improvement modification. | 3S2060DR149A1A | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DC137A1-24-18 | Orig | 9/1/1968 | Modification to circuitry. | 3S2060DC137A1 | ||
| GE - Power Conditioning | Service Bulletin | SB3S2060DR149A1A-24-01-1 | Orig | 5/30/1984 | Revision notice to Service Bulletin SB3S2060DR149A1A-24-01. | 3S2060DR149A1A | ||
| GE - Power Conditioning | Service Letter | SL-121 | B | 5/5/2009 | To provide information necessary to repair units and improve unit reliability. | 3S2060DM169A1, 3S2060DM169A3 | ||
| GH-3000 | Installation Manual | TP-579 | E | 5/1/2018 | Installation and Operation Manual, GH-3000, Rel. 4.x and 5. | Electronic Standby Instrument System Manual includes installation information for DCM-3000 Detachable Configuration Module, ADC-3000 Air Data Computer, ADC-3001 Air Data Computer, ADC-4000 Air Data Computer, and MAG-3000 Magnetometer. | 501-1741-2104, 501-1741-2204, 501-1741-2304, 501-1741-2404, 501-1741-2504, 501-1741-2604, 501-1741-2704, 501-1741-2804, 501-1741-2105. 501-1826-01, 501-1881-01 | |
| GH-3000 | Installation Manual | TP-546 | T | 3/30/2017 | Installation and Operation Manual, GH-3000, Rel. 3.x | Electronic Standby Indicator | 501-1741-0103, 501-1741-0203, 501-1741-0303, 501-1741-0403, 501-1741-0503, 501-1741-0603, 501-1741-0703, 501-1741-0803, 501-1741-2103, 501-1741-2203, 501-1741-2303, 501-1741-2403, 501-1741-2503, 501-1741-2603, 501-1741-2703, 501-1741-2803, 501-1741-3293, 501-1741-4103, 501-1741-4203, 501-1741-4303, 501-1741-4403, 501-1741-4503, 501-1741-4603, 501-1741-4703, 501-1741-4803 | |
| GH-3000 | Installation Manual | TP-531 | C | 5/27/2009 | Installation and Operation Manual, GH-3000, Rel. 2.x | Electronic Standby Instrument System Manual includes installation information for the DCM-3000, ADC-3000, and MAG-3000. | 501-1741-0102, 501-1741-0202, 501-1741-0302, 501-1741-0402, 501-1741-0502, 501-1741-0602, 501-1741-0702, 501-1741-0802, 501-1741-2102, 501-1741-2202, 501-1741-2302, 501-1741-2402, 501-1741-2502, 501-1741-2602, 501-1741-2702, 501-1741-2802, 501-1797-( ), 501-1803-( ), 501-1826-( ) | |
| GH-3000 | Installation Manual | TP-503 | 34-20-57 | A | 5/27/2009 | Installation and Operation Manual, GH-3000, Rel. 1.x | Electronic Standby Indicator | 501-1741-01, 501-1741-02, 501-1741-03, 501-1741-04, 501-1741-05, 501-1741-06, 501-1741-07, 501-1741-08 |
| GH-3000 | Pilot Guide | TP-571 | A | 9/5/2001 | Pilot's Guide, GH-3000, Rel. C27J.2 | Pilot's Guide Electronic Standby Indicator | 501-1741-3293 | |
| GH-3000 | Pilot Guide | TP-547 | H | 7/22/2009 | Pilot's Guide, GH-3000, Rel 3.x | Pilot's Guide | 501-1741-0103 501-1741-0203 501-1741-0303 501-1741-0403 501-1741-0503 501-1741-0603 501-1741-0703 501-1741-0803 501-1741-2103 501-1741-2203 501-1741-2303 501-1741-2403 501-1741-2503 501-1741-2603 501-1741-2703 501-1741-2803 501-1741-3293 501-1741-4103 | |
| GH-3000 | Pilot Guide | TP-577 | B | 8/12/2008 | Pilot's Guide, GH-3000, Rel 4.x | Pilot's Guide | 501-1741-2104 | |
| GH-3000 | Pilot Guide | TP-626 | B | 4/16/2009 | Pilot's Guide, GH-3000, Rel. 5.x | Pilot's Guide Electronic Standby Indicator | 501-1741-2105 | |
| GH-3000 | Printer Copies | TP-547PC | H | 7/22/2009 | Pilot's Guide | Printer copy GH-3000 PG | 501-1741-() | |
| GH-3000 | Printer Copies | TP-626PC | B | 4/16/2009 | Pilot's Guide | Printer copy GH-3000 PG | 501-1741-2105 | |
| GH-3000 | Service Bulletin | SB501-1741-27 | D | 1/2/2007 | To reduce the possibility of the display blanking or failing at start up. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-28 | A | 2/15/2006 | To reduce the possibility of the display blanking or disruption. | 501-1741-(), 501-1741-01, 501-1741-0102, 501-1741-0103, 501-1741-09, 501-1741-2102, 501-1741-2103, 501-1741-2104, 501-1741-3293, 501-1741-4103 | ||
| GH-3000 | Service Bulletin | SB501-1741-32 | B | 5/7/2012 | SB501-1741-32 | 501-1741-09, 501-1741-2102, 501-1741-2103, 501-1741-2104, 501-1741-2105, 501-1741-2202, 501-1741-2203, 501-1741-2204, 501-1741-2302, 501-1741-2303, 501-1741-2304, 501-1741-2402, 501-1741-2403, 501-1741-2404, 501-1741-2502, 501-1741-2503, 501-1741-2504, 501-1741-2602, 501-1741-2603, 501-1741-2604, 501-1741-2702, 501-1741-2703, 501-1741-2704, 501-1741-2802, 501-1741-2803, 501-1741-2804, 501-1741-3293, 501-1741-4103, 501-1741-4203, 501-1741-4303, 501-1741-4403, 501-1741-4503, 501-1741-4603, 501-1741-4703, 501-1741-4803 | ||
| GH-3000 | Service Bulletin | SB501-1741-29 | D | 11/24/2008 | Provide replacment display due to diminishing source. | 501-1741-, 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-30 | D | 11/25/2008 | Provide replacement display due to diminishing source. | 501-1741-, 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-31 | A | 8/3/2007 | Remove fan failure message | Remove fan failure message | 501-1741-0103, 501-1741-0203, 501-1741-0303, 501-1741-0403, 501-1741-0503, 501-1741-0603, 501-1741-0703, 501-1741-0803, 501-1741-2103, 501-1741-2203, 501-1741-2303, 501-1741-2403, 501-1741-2503, 501-1741-2603, 501-1741-2703, 501-1741-2803, 501-1741-3293, 501-1741-4103, 501-1741-4203, 501-1741-4303, 501-1741-4403, 501-1741-4503, 501-1741-4603, 501-1741-4703, 501-1741-4803 | |
| GH-3000 | Service Bulletin | SB501-1741-1 | Orig | 12/1/1997 | To prevent possible damage to unprotected sensor output pin. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-10 | Orig | 6/1/2000 | Provide recess for nameplates to prevent damage during installation or removal. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-11 | Orig | 6/1/2000 | To incorporate new display glass. | 501-1741-09 | ||
| GH-3000 | Service Bulletin | SB501-1741-12 | Orig | 6/1/2000 | Reduce audio frequency noise susceptibility and provide additional isolation of rate sensors. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-13 | Orig | 6/1/2000 | Increase durability of keyboard assembly by using a pinned knob. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-14 | Orig | 6/1/2000 | Increase isolation of energy storage board and case. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-15 | Orig | 7/19/2002 | Product Improvement | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-16 | A | 2/12/2003 | Utilize more reliable connector on 16-BIT A/D CCA. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-17 | A | 2/12/2003 | New Keyboard assembly that is easier to manufacture and repair. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-18 | Orig | 2/11/2003 | To correct startup errors for level Sensor Self Test. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-19 | B | 11/24/2008 | Provide replacement display due to diminishing source. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-2 | Orig | 12/1/1997 | To improve A2 Sensor Assembly output stability which provides constant calibration characteristics and overall attitude performance. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-20 | Orig | 8/20/2003 | Provide additional screw depth engagement in sensor mounting bracket. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-21 | Orig | 3/25/2004 | Better manufacturing of GH-3000 by replacing energy storage board and cover. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-22 | A | 5/20/2004 | Manufacturing Change. Produce a universal lighting controller. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-23 | Orig | 5/20/2004 | Manufacturing Change. Provide replacement for Pitch Rate Sensor Flex. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-24 | Orig | 5/20/2004 | Manufacturing Change. Provide replacement for Roll Rate Sensor Flex. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-25 | Orig | 5/20/2004 | Manufacturing Change. Provide replacement for Yaw Rate Sensor Flex. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-26 | Orig | 5/20/2004 | Manufacturing Change. Consolidation to a single level sensor. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-3 | Orig | 12/1/1997 | To eliminate possible display vertical scrolling by establishing pseudo synchronization of display operating frequencies. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-4 | Orig | 12/1/1997 | To provide for use of fan with improved reliability. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-5 | Orig | 12/1/1997 | To establish proper circuit filtering which minimizes both roll and pitch level signal changes as seen on the ARINC-429 level output signals. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-6 | Orig | 12/1/1997 | To eliminate possible detrimental effects of reverse bias applied to level sensor filter capacitors. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-7 | Orig | 12/4/1998 | To insure proper interface between keyboard circuit card contacts and keyboard flex finger terminations. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-8 | A | 6/1/2000 | To replace energy storage board with improved version. | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-9 | Orig | 6/1/2000 | Improve EMI performance | 501-1741-( ) | ||
| GH-3000 | Service Bulletin | SB501-1741-33 | A | 2/28/2012 | To improve low light level calibration linearity | 501-1741-3103 | ||
| GH-3000 | Service Bulletin | SB501-1741-34 | B | 3/26/2014 | Rev B corrects effectivity by replacing "serial" with "part" | Rev B corrects effectivity by replacing "serial" with "part" | 501-1741-( ) | |
| GH-3000 | Service Letter | SL-251 | A | 12/3/2009 | Supplemental Operation Instructions | Supplemental Operation Instructions | 501-1741-3103 | |
| GH-3000 | Service Letter | SL-324 | A | 4/5/2017 | End of Production Notice | End of Production Notice | 501-1741, 501-1860 | |
| GH-3000 | Service Letter | SL-226 | A | 5/15/2007 | To provide product upgrade information due to product obsolescene | 501-1741-01, 501-1741-0102, 501-1741-0103, 501-1741-02, 501-1741-0202, 501-1741-0203, 501-1741-03, 501-1741-0302, 501-1741-0303, 501-1741-04, 501-1741-0402, 501-1741-0403, 501-1741-05, 501-1741-0502, 501-1741-0503, 501-1741-06, 501-1741-0602, 501-1741-0603, 501-1741-07, 501-1741-0702, 501-1741-0703, 501-1741-08, 501-1741-0802, 501-1741-0803 | ||
| GH-3000 | Service Letter | SL-185 | Orig | 1/20/2004 | Inform customers of the Cessna Citation Bravo Series Aircraft of Airdata problem. | 501-1741-( ) | ||
| GH-3000 | Troubleshooting Guide | TP-602 | B | 3/12/2009 | GH-3000 Troubleshooting Guide | GH-3000 Troubleshooting Guide | 501-1741- ( ) | |
| GH-3001 | Installation Manual | TP-530 | L | 6/15/2016 | Installation and Operation Manual, GH-3001, Rel. 1.x, 2.x, 5.0 | Electronic Standby Instrument System Manual includes installation information for the DCM-3000, ADC-3000 / ADC-4000, and MAG-3000. | GH-3001. 501-1851-01, 501-1851-2402, 501-1851-2405, 501-1851-3402 501-1797-23, 501-1797-24, 501-1797-71, 501-1803-145, 501-1803-31C, 501-1803-32B, 501-1826-01, | |
| GH-3001 | Installation Manual | TP-593 | E | 12/18/2013 | Installation and Operation Manual, GH-3001, Rel. 3.x, 4.x | Uses GH-3000 platform with Software version 4.x. Manual includes installation information for DCM-3000, ADC-3000, ADC-4000, and MAG-3000. | 501-1851-2403, 501-1851-2404 501-1797-( ), 501-1803-( ), 501-1826-01, | |
| GH-3001 | Pilot Guide | TP-535 | C | 10/27/2010 | Pilot's Guide | Pub# TP-535 | 501-1851-01 | |
| GH-3001 | Service Bulletin | SB501-1851-23 | A | 12/17/2007 | To provide replacement display due to diminishing source | To provide replacement display due to diminishing source | 501-1851- | |
| GH-3001 | Service Bulletin | SB501-1851-22 | A | 2/15/2006 | To reduce the possibility of the display blanking or disruption. | 501-1851-01, 501-1851-2402, 501-1851-2403, 501-1851-2404 | ||
| GH-3001 | Service Bulletin | SB501-1851-18 | A | 2/3/2006 | To provide replacement rate sensor flex. | 501-1851-01, 501-1851-2402, 501-1851-2403, 501-1851-2404 | ||
| GH-3001 | Service Bulletin | SB501-1851-19 | A | 2/3/2006 | To provide replacement rate sensor flex. | 501-1851-01, 501-1851-2402, 501-1851-2403, 501-1851-2404 | ||
| GH-3001 | Service Bulletin | SB501-1851-20 | A | 2/3/2006 | To provide replacement rate sensor flex. | 501-1851-01, 501-1851-2402, 501-1851-2403, 501-1851-2404 | ||
| GH-3001 | Service Bulletin | SB501-1851-21 | C | 12/17/2007 | Superseded by SB-501-1851-23 | 501-1851-01, 501-1851-2402, 501-1851-2403, 501-1851-2404 | ||
| GH-3001 | Service Bulletin | SB501-1851-1 | Orig | 1/1/2000 | Improve performance over temperature range. | 501-1851-01 | ||
| GH-3001 | Service Bulletin | SB501-1851-10 | Orig | 7/19/2002 | Product Improvement | 501-1851-01 | ||
| GH-3001 | Service Bulletin | SB501-1851-11 | A | 3/14/2003 | To provide better EMI protection for the unit. | 501-1851-01 | ||
| GH-3001 | Service Bulletin | SB501-1851-12 | Orig | 2/11/2003 | To correct startup errors for level Sensor Self Test. [Part Number 501-1851-2403, with 3.x software]. | 501-1851-2403 | ||
| GH-3001 | Service Bulletin | SB501-1851-13 | Orig | 3/14/2003 | To provide better EMI protection for the unit. | 501-1851-01, 501-1851-2402, 501-1851-2403 | ||
| GH-3001 | Service Bulletin | SB501-1851-14 | A | 12/17/2007 | Superseeded by SB501-1851-23 | 501-1851-01, 501-1851-2402, 501-1851-2403, 501-1851-2404 | ||
| GH-3001 | Service Bulletin | SB501-1851-15 | Orig | 8/20/2003 | Provide additional screw depth engagement in sensor mounting bracket. | 501-1851-01, 501-1851-2402, 501-1851-2403, 501-1851-2404 | ||
| GH-3001 | Service Bulletin | SB501-1851-16 | Orig | 5/20/2004 | Manufacturing Change. New Energy Storage Board and Cover. | 501-1851-01, 501-1851-2402, 501-1851-2403, 501-1851-2404 | ||
| GH-3001 | Service Bulletin | SB501-1851-17 | Orig | 5/20/2004 | Manufacturing Change. Producing a universal Lighting controller. | 501-1851-01, 501-1851-2402, 501-1851-2403, 501-1851-2404 | ||
| GH-3001 | Service Bulletin | SB501-1851-2 | B | 7/24/2013 | Improve EMI performance. | 501-1851-01 | ||
| GH-3001 | Service Bulletin | SB501-1851-3 | A | 4/17/2012 | To incorporate new display glass. | 501-1851-01, 501-1851-2405 | ||
| GH-3001 | Service Bulletin | SB501-1851-4 | B | 7/24/2013 | Reduce audio frequency noise susceptibility and provide additional isolation of rate sensors. | 501-1851-01 | ||
| GH-3001 | Service Bulletin | SB501-1851-5 | B | 7/24/2013 | Improve durability of keyboard assembly. | 501-1851-01 | ||
| GH-3001 | Service Bulletin | SB501-1851-6 | Orig | 6/1/2000 | Provide recess for nameplates to prevent damage during installation or removal. | 501-1851-01 | ||
| GH-3001 | Service Bulletin | SB501-1851-7 | B | 7/24/2013 | FPGA controlled addressing is required with software release 1.2. | 501-1851-01 | ||
| GH-3001 | Service Bulletin | SB501-1851-8 | A | 12/10/2015 | Increase isolation of energy storage board and case. | Revision A incorporates a new model to the effectivity paragraph | 501-1851-01, 501-1851-2405 | |
| GH-3001 | Service Bulletin | SB501-1851-9 | B | 7/24/2013 | Utilize more reliable connector on 16-Bit A/D CCA | 501-1851-01 | ||
| GH-3001 | Service Bulletin | SB501-1851-24 | B | 12/11/2015 | To provide replacement display due to diminshing source | 501-1851-01, 501-1851-2402, 501-1851-2403, 501-1851-2404, 501-1851-2405 | ||
| GH-3001 | Service Bulletin | SB501-1851-25 | A | 7/30/2012 | This product may have a suspected unapproved part (SUP) installed. | 501-1851- | ||
| GH-3001 | Service Bulletin | SB501-1851-26 | A | 6/12/2019 | To eliminate a failed power up condition on certain units if the unit is off for an extended period of time. | Service Bulletin | 501-1851-2402, 501-1851-2405, 501-1851-3402 | |
| GH-3001 | Service Letter | SL-354 | A | 2/12/2020 | End of Production Notice | Service Letter | 501-1851- | |
| GH-3002 | Component Maintenance Manual | TP-539 | G | 1/18/2019 | Maintenance Guide | Electronic Indicator Work Share Kit | 501-1852-0101, 501-1852-0103, 501-1852-0203, 504-1966-01 | |
| GH-3002 | Service Letter | SL-333 | C | 3/28/2019 | End of Manufacturing Notice | End of Production | 501-1852-0101, 501-1852-0103, 501-1852-0203, 504-1966-01 | |
| GH-3004 | Service Bulletin | SB501-1859-18 | B | 7/12/2010 | To reduce the possibility of the display blanking or failing at start up. | 501-1859-02, 501-1859-0203, 501-1859-2202, 501-1859-2203, 501-1859-2603 | ||
| GH-3004 | Service Bulletin | SB501-1859-19 | A | 7/12/2010 | To reduce the possibility of the display blanking or disruption. | 501-1859-02, 501-1859-0203, 501-1859-2202, 501-1859-2203, 501-1859-2603 | ||
| GH-3004 | Service Bulletin | SB501-1859-20 | A | 7/12/2010 | To remove fan failure warning message | 501-1859-02, 501-1859-0203, 501-1859-2202, 501-1859-2203, 501-1859-2603 | ||
| GH-3004 | Service Bulletin | SB501-1859-21 | A | 7/12/2010 | Provide replacement display due to diminishing source. | 501-1859-02, 501-1859-0203, 501-1859-2202, 501-1859-2203, 501-1859-2603 | ||
| GH-3004 | Service Bulletin | SB501-1859-1 | Orig | 1/17/2002 | Provide a unit cover with a recessed mounting surface for unit Nameplate to prevent damage to Nameplate. | 501-1859-02 | ||
| GH-3004 | Service Bulletin | SB501-1859-10 | Orig | 1/7/2004 | Manufacturing Change. | 501-1859-0203, 501-1859-2203, 501-1859-2603 | ||
| GH-3004 | Service Bulletin | SB501-1859-11 | A | 5/20/2004 | Manufacturing Change. Produce a universal Lighting Controller. | 501-1859-02, 501-1859-0203, 501-1859-2202, 501-1859-2203, 501-1859-2603 | ||
| GH-3004 | Service Bulletin | SB501-1859-12 | Orig | 1/7/2004 | Manufacturing Change. | 501-1859-02, 501-1859-0203, 501-1859-2203, 501-1859-2603 | ||
| GH-3004 | Service Bulletin | SB501-1859-13 | Orig | 5/20/2004 | Manufacturing Change. Provide replacement for Pitch Rate Sensor Flex. | 501-1859-02, 501-1859-0203, 501-1859-2202, 501-1859-2203, 501-1859-2603 | ||
| GH-3004 | Service Bulletin | SB501-1859-14 | Orig | 5/20/2004 | Manufacturing Change. Provide replacement for Roll Rate Sensor Flex. | 501-1859-02, 501-1859-0203, 501-1859-2202, 501-1859-2203, 501-1859-2603 | ||
| GH-3004 | Service Bulletin | SB501-1859-15 | Orig | 5/20/2004 | Manufacturing Change. Provide replacement for Yaw Rate Sensor Flex. | 501-1859-02, 501-1859-0203, 501-1859-2202, 501-1859-2203, 501-1859-2603 | ||
| GH-3004 | Service Bulletin | SB501-1859-16 | B | 1/25/2010 | Consolidate to a single level sensor type. | 501-1859-02, 501-1859-0203, 501-1859-2202, 501-1859-2203, 501-1859-2603 | ||
| GH-3004 | Service Bulletin | SB501-1859-2 | Orig | 1/17/2002 | Reduce audio frequency noise susceptibility and provide additional isolation of rate sensors. | 501-1859-02 | ||
| GH-3004 | Service Bulletin | SB501-1859-3 | Orig | 1/17/2002 | Increase durability of Keyboard. | 501-1859-02 | ||
| GH-3004 | Service Bulletin | SB501-1859-4 | Orig | 1/17/2002 | Isolate Energy Storage Board from Case. | 501-1859-02 | ||
| GH-3004 | Service Bulletin | SB501-1859-5 | A | 2/19/2002 | Utilize more reliable connector on 16-Bit A/D CCA | 501-1859-02, 501-1859-2203 | ||
| GH-3004 | Service Bulletin | SB501-1859-6 | Orig | 7/19/2002 | Product Improvement | 501-1859-02, 501-1859-0203, 501-1859-2203, 501-1859-2603 | ||
| GH-3004 | Service Bulletin | SB501-1859-7 | Orig | 2/11/2003 | To correct startup errors for level Sensor Self Test. [Part Number 501-1859-0203, -2203, -2603 - with 3.x software]. | 501-1859-0203, 501-1859-2203, 501-1859-2603 | ||
| GH-3004 | Service Bulletin | SB501-1859-8 | C | 1/25/2010 | To provide replacement display due to diminishing source. | Superceeded by SB501-1859-17 | 501-1859-02, 501-1859-0203, 501-1859-2203, 501-1859-2603 | |
| GH-3004 | Service Bulletin | SB501-1859-9 | Orig | 8/20/2003 | Provide additional screw depth engagement in sensor mounting bracket. | 501-1859-02, 501-1859-0203, 501-1859-2202, 501-1859-2203, 501-1859-2603 | ||
| GH-3004 | Service Bulletin | SB501-1859-17 | B | 1/25/2010 | Replacement Display due to Diminishing source | 501-1859-02, 501-1859-0203, 501-1859-2202, 501-1859-2203, 501-1859-2603 | ||
| GH-3100 | Installation Manual | TP-582 | G | 3/4/2010 | Installation and Operation Manual, GH-3100, sw 4.0 | Pub# TP-582 | 501-1826-01, 501-1860-0102, 501-1860-0104, 501-1870-( ) | |
| GH-3100 | Installation Manual | TP-559 | K | 3/30/2017 | Installation and Operation Manual, GH-3100, SW 3.0 | This manual contains installation and operating information for the GH Electronic Standby Instrument System. Information in this manual includes the following products: GH-3100 Electronic Standby Indicator (with 1.3, 1.4 or 3.0 software), DCM-3100 Detachable configuration Module, and MAG-3000 / MAG-3100 Magnetometer. This information is supplemented and kept current by revisions, service letters and service bulletins. | 501-1826-01, 501-1826-02, 501-1860-0101, 501-1860-0103, 501-1860-0201, 501-1860-0203, 501-1860-0301, 501-1860-0303, 501-1860-0401, 501-1860-0403, 501-1860-0501, 501-1860-0503, 501-1860-0601, 501-1860-0603, 501-1860-0701, 501-1860-0703, 501-1860-1101, 501-1860-1103, 501-1860-1201, 501-1860-1203, 501-1860-1301, 501-1860-1303, 501-1860-1401, 501-1860-1403, 501-1860-1501, 501-1860-1503, 501-1860-1601, 501-1860-1603, 501-1860-1701, 501-1860-1703, 501-1860-1801, 501-1860-1803, 501-1860-2101, 501-1860-2103, 501-1860-2201, 501-1860-2203, 501-1870-( ) | |
| GH-3100 | Installation Manual | TP-629 | B | 3/4/2010 | GH-3100 Instalation & Operation Manual (-0205) | GH-3100 Instalation & Operation Manual (-0205 & -0605 ) | 501-1860-0205, 501-1860-0605 | |
| GH-3100 | Pilot Guide | TP-560 | F | 7/22/2009 | Pilot's Guide | Pub# TP-560 | 501-1860-() | |
| GH-3100 | Service Bulletin | SB501-1860-20 | C | 3/20/2013 | Planning Information | Software Update | 501-1860- ( ), 501-1860- 0101-0801, 501-1860- 1101-1801, 501-1860- 1101-2101, 501-1860- 1101-2201, 501-1870- ( ) | |
| GH-3100 | Service Bulletin | SB501-1860-18 | A | 6/8/2007 | Planning Information | To improve attitude performance when configured without heading. | 501-1860-( ), 501-1860-0101, 501-1860-0201, 501-1860-0301, 501-1860-0401, 501-1860-0501, 501-1860-0601, 501-1860-0701, 501-1860-0801, 501-1860-1101, 501-1860-1201, 501-1860-1301, 501-1860-1401, 501-1860-1501, 501-1860-1601, 501-1860-1701, 501-1860-1801, 501-1860-2101, 501-1860-2201 | |
| GH-3100 | Service Bulletin | SB501-1860-19 | B | 2/12/2009 | Provide replacement display due to diminishing source | Provide replacement display due to diminishing source | 501-1860-0101, 501-1860-0102, 501-1860-0201, 501-1860-0301, 501-1860-0401, 501-1860-0501, 501-1860-0601, 501-1860-0701, 501-1860-0801, 501-1860-1101, 501-1860-1201, 501-1860-1301, 501-1860-1401, 501-1860-1501, 501-1860-1601, 501-1860-1701, 501-1860-1801, 501-1860-2102, 501-1860-2202 | |
| GH-3100 | Service Bulletin | SB501-1860-14 | C | 6/29/2006 | Improvement | To improve attitude accuracy when configured without heading sources. Remove fan failure warning message. | 501-1860-0101, 501-1860-0201, 501-1860-0301, 501-1860-0401, 501-1860-0501, 501-1860-0601, 501-1860-0701, 501-1860-0801, 501-1860-1101, 501-1860-1201, 501-1860-1301, 501-1860-1401, 501-1860-1501, 501-1860-1601, 501-1860-1701, 501-1860-1801, 501-1860-2101, 501-1860-2201 | |
| GH-3100 | Service Bulletin | SB501-1860-15 | C | 11/24/2008 | Provide replacement display due to diminishing source. | 501-1860-( ), 501-1860-0101, 501-1860-0102, 501-1860-0201, 501-1860-0301, 501-1860-0401, 501-1860-0501, 501-1860-0601, 501-1860-0701, 501-1860-0801, 501-1860-1101, 501-1860-1201, 501-1860-1301, 501-1860-1401, 501-1860-1501, 501-1860-1601, 501-1860-1701, 501-1860-1801, 501-1860-2101, 501-1860-2201 | ||
| GH-3100 | Service Bulletin | SB501-1860-12 | C | 6/29/2006 | To reduce the possibility of the display blanking or failing at start up. | 501-1860-0101, 501-1860-0102, 501-1860-0201, 501-1860-0301, 501-1860-0401, 501-1860-0501, 501-1860-0601, 501-1860-0701, 501-1860-0801, 501-1860-1101, 501-1860-1201, 501-1860-1301, 501-1860-1401, 501-1860-1501, 501-1860-1601, 501-1860-1701, 501-1860-1801 | ||
| GH-3100 | Service Bulletin | SB501-1860-13 | B | 6/29/2006 | To reduce the possibility of the display blanking or disruption. | 501-1860-0101, 501-1860-0102, 501-1860-0201, 501-1860-0301, 501-1860-0401, 501-1860-0501, 501-1860-0601, 501-1860-0701, 501-1860-0801, 501-1860-1101, 501-1860-1201, 501-1860-1301, 501-1860-1401, 501-1860-1501, 501-1860-1601, 501-1860-1701, 501-1860-1801, 501-1860-2101, 501-1860-2201 | ||
| GH-3100 | Service Bulletin | SB501-1860-1 | A | 5/24/2004 | To ease manufacturing and repair of the keyboard assembly. | 501-1860-() | ||
| GH-3100 | Service Bulletin | SB501-1860-10 | A | 3/16/2007 | Release of 2.1 software in support of Gulfstream G450 program. | 501-1860-0102 | ||
| GH-3100 | Service Bulletin | SB501-1860-11 | B | 11/20/2009 | Release Software 1.1. New features include the capability to compensate IAS with DCM-3100 loaded constants K1 and K2. | 501-1860-( ) | ||
| GH-3100 | Service Bulletin | SB501-1860-2 | B | 9/2/2003 | To correct startup errors for Level Sensor Self Test. | 501-1860-() | ||
| GH-3100 | Service Bulletin | SB501-1860-3 | Orig | 3/14/2003 | Provide replacement display due to diminishing source. | 501-1860-() | ||
| GH-3100 | Service Bulletin | SB501-1860-4 | A | 8/20/2003 | Correct insufficient timing margin for 16-BIT A/D High Byte-Low Byte Select Line. | 501-1860-( ) | ||
| GH-3100 | Service Bulletin | SB501-1860-5 | Orig | 8/20/2003 | Provide additional screw depth engagement in sensor mounting bracket. | 501-1860-( ) | ||
| GH-3100 | Service Bulletin | SB501-1860-6 | A | 5/20/2004 | Manufacturing Change. Produce a universal Lighting Controller. | 501-1860-( ) | ||
| GH-3100 | Service Bulletin | SB501-1860-7 | Orig | 5/20/2004 | Manufacturing Change. Provide replacement for Pitch Rate Sensor Flex. | 501-1860-( ) | ||
| GH-3100 | Service Bulletin | SB501-1860-8 | Orig | 5/20/2004 | Manufacturing Change. Provide replacement for Roll Rate Sensor Flex. | 501-1860-( ) | ||
| GH-3100 | Service Bulletin | SB501-1860-9 | Orig | 5/20/2004 | Manufacturing Change. Provide replacement for Yaw Sensor Flex. | 501-1860-( ) | ||
| GH-3100 | Service Bulletin | SB501-1860-22 | A | 5/21/2012 | GH-3100 Quick Disconnect Fittings | GH-3100 Quick Disconnect Fittings | 501-1860-2103 | |
| GH-3100 | Service Bulletin | SB501-1860-21 | A | 1/23/2012 | To inform users of a suspected unapproved part (SUP) and to inform them of an inspection MOD effective at next service, which identifies units that have had this condition corrected. | 501-1860-() | ||
| GH-3100 | Service Bulletin | SB501-1860-23 | C | 6/2/2016 | Corrects part number in the identification procedure | Corrects part number in the identification procedure | 501-1860-( ) | |
| GH-3100 | Service Letter | SL-283 | A | 1/29/2013 | Changes Implemented with 4.0 Software | Changes Implemented with 4.0 Software | 501-1860-0102 | |
| GH-3100 | Service Letter | SL-324 | A | 4/5/2017 | End of Production Notice | End of Production Notice | 501-1741, 501-1860 | |
| GH-3100 | Service Letter | SL-186 | G | 4/9/2015 | The GH-3100 Electronic Standby Indicator is subject to requirments of FAA document 14 CFR FAR Part 91.411 every 2 years | 501-1860-( ) | ||
| GH-3100 | Service Letter | SL-245 | A | 6/30/2009 | GH-3100 YAW Error Correction | GH-3100 YAW Error Correction | 501-1860-XXX1 | |
| GH-3100 | Service Letter | SL-244 | B | 2/17/2010 | Replacement of GH-3100 with SW1.3 with SW 3.X | Replacement of GH-3100 with SW1.3 with SW 3.X | 501-1860-XXX1, 501-1860-XXX3 | |
| GH-3100 | Troubleshooting Guide | TP-603 | C | 4/21/2009 | GH-3100 Troubleshooting Guide | GH-3100 Troubleshooting Guide | 501-1860-( ) | |
| GH-3900 | Installation Aircraft Tools | 576-6159-05 | A | 10/11/2022 | ACM Tool for Software 1.6 (GH-3900) | Release 1.6. The GH-3900 system software (8010-34000-0106, Version R01.06) is compatible with aircraft configuration file version 01.10. | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 9200-34100-0101, 9200-34100-0201 576-6159-05 | |
| GH-3900 | Installation Manual | 0040-34001-01 | AB | 10/15/2024 | GH-3900 (SFIS-3900) Install Manual | GH-3900 /SFIS-3900 Install Manual | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501, 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Instruction Manual | 0040-34002-01 | J | 1/9/2023 | GH-3900, Instruction Manual, ACM Tool, 576-6159-02 & 576-6159-03 | ACM Tool Revision 1.00, Aircraft Config File Version: 01.10 | 576-6159-01 576-6159-02 576-6159-03 576-6159-04 576-6159-05 | |
| GH-3900 | Intermediate Maintenance Manual | 0040-34004-01 | 34-20-77 | C2 | 9/9/2024 | GH-3900 Abbreviated Maintenance Manual, (lvl 1 maint.) | Abbreviated Maintenance Manual, level 1 maintenance | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 9200-34100-0101, 9200-34100-0201 |
| GH-3900 | Pilot Guide | 0040-34000-01 | H | 1/9/2023 | GH-3900 (SFIS-3900) ) Pilot's Guide | Incorporates latest S/W 1.6 | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB576-6159-5 | 00 | 1/9/2023 | Service Bulletin, GH-3900, ACM Tool version 01.10 | Release of 576-6159-05, Revision 1.00, Aircraft Config File Version 01.10., Acron Aviation | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB002-GH-3900 | 00 | 1/9/2023 | Software release 1.6 | System Software Release 1.6 | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB9200-34700-10 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-34700-0101, 9200-34700-0401, 9200-34700-0601 | |
| GH-3900 | Service Bulletin | SB576-6159-4 | A | 6/26/2017 | Service Bulletin, GH-3900, ACM Tool version 01.09, release 1.02 | create aircraft configuration files for the GH-3900, Acron Aviation | 9200-34000, 9200-34100 | |
| GH-3900 | Service Bulletin | SB9200-34000-9 | B | 6/26/2017 | Software Release 1.5 | Software Release 1.5 | 9200-34000 | |
| GH-3900 | Service Bulletin | SB9200-34100-9 | A | 6/26/2017 | Software release 1.5 | , Acron Aviation | 9200-34100 | |
| GH-3900 | Service Bulletin | SB576-6159-3 | B | 6/26/2017 | Service Bulletin, GH-3900, ACM Tool version 01.09, Release 1.01 | , Acron Aviation | 9200-34000, 9200-34100 | |
| GH-3900 | Service Bulletin | SB9200-34700-7 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6, Acron Aviation | 9200-34700-0101, 9200-34700-0201, 9200-34700-0401, 9200-34700-0601 | |
| GH-3900 | Service Bulletin | SB9200-34000-10 | A | 12/4/2017 | Error Correcting RAM | 9200-34000, 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 | ||
| GH-3900 | Service Bulletin | SB9200-34100-10 | A | 12/4/2017 | Error correcting RAM | , Acron Aviation | 9200-34100, 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB9200-34000-11 | A | 12/4/2017 | Display Replacement | Display Replacement. This Service Bulletin and MOD have been superseded by Service Bulletin SB001-GH-3900. | 9200-34000, 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 | |
| GH-3900 | Service Bulletin | SB9200-34100-11 | A | 12/18/2017 | Display Replacement | Display Replacement. This Service Bulletin and MOD have been superseded by Service Bulletin SB001-GH-3900., Acron Aviation | 9200-34100, 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB9200-34000-9 | B | 6/26/2017 | Software release 1.5 | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 | ||
| GH-3900 | Service Bulletin | SB9200-34000-8 | A | 12/9/2016 | Software release 1.4 | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 | ||
| GH-3900 | Service Bulletin | SB9200-34100-8 | A | 12/9/2016 | Software release 1.4 | Software 1.4 | 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB9200-34000-7 | A | 9/14/2016 | Prevent rate sensor loopback failure at start up. | To prevent rate sensor loopback failure at start up. | 9200-34000-0101, 9200-34000-0201 | |
| GH-3900 | Service Bulletin | SB9200-34100-7 | A | 9/14/2016 | Prevent rate sensor loopback failure at start up. | To prevent rate sensor loopback failure at start up., Acron Aviation | 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB9200-34700-8 | B | 7/31/2018 | Error Correcting RAM | Error Correcting RAM, Acron Aviation | 9200-34700-0101, 9200-34700-0201, 9200-34700-0601 | |
| GH-3900 | Service Bulletin | SB9200-34000-4 | A | 12/13/2013 | Software release 1.2 (GH-3900) | SW 1.2 Release, Acron Aviation | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 | |
| GH-3900 | Service Bulletin | SB9200-34000-5 | A | 12/13/2013 | Software release for Bootloader 1.03 (GH-3900) | Bootloader Ver R01.03 | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 | |
| GH-3900 | Service Bulletin | SB9200-34100-4 | A | 12/20/2013 | Software release 1.2 | Release of 1.2 Software , Acron Aviation | 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB9200-34100-5 | A | 12/20/2013 | Software release for Bootloader R01.03 | Bootloader S/W R01.03 For System Software Release 1.2 (version R01.02), Acron Aviation | 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB576-6159-2 | A | 12/13/2013 | Service Bulletin, GH-3900, ACM Tool version 01.07 | ACMT Rev 1.07, Acron Aviation | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 | |
| GH-3900 | Service Bulletin | SB576-6159-1 | B | 5/20/2013 | Service Bulletin, GH-3900, ACM Tool version 01.06 | ACMT REV 1.06, Acron Aviation | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 | |
| GH-3900 | Service Bulletin | SB9200-34000-1 | A | 9/17/2012 | Software Release 1.1 | Release of Software 1.1, Acron Aviation | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 | |
| GH-3900 | Service Bulletin | SB9200-34100-1 | A | 9/17/2012 | Software release 1.1 | Release of Software 1.1, Acron Aviation | 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB004-GH-3900 | 00 | 9/9/2024 | Service Bulletin, HW MOD (Ohmite Resistor change) | Replacement of Ohmite Resistors on A2 I/O Assembly CCA. | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB003-GH-3900 | 00 | 1/5/2024 | Service Bulletin, HW MOD | Notice of Change to A1 EMI Assembly | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB001-GH-3900 | 00 | 7/26/2023 | Service Bulletin, Display Replacement | Due to material obsolescence, the current display assembly is being updated with equivalent materials and will be identified with a new part number for tracking purposes. | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB9200-34000-12 | A | 11/14/2019 | Service Bulletin | Backlight LED Replacement. This Service Bulletin and MOD have been superseded by Service Bulletin SB001-GH-3900. | 9200-34000-( ) | |
| GH-3900 | Service Bulletin | SB9200-34100-12 | A | 11/14/2019 | Service Bulletin | Backlight LED Replacement. This Service Bulletin and MOD have been superseded by Service Bulletin SB001-GH-3900., Acron Aviation | 9200-34100-( ) | |
| GH-3900 | Service Bulletin | SB9200-34000-6 | A | 3/16/2016 | Software release 1.3 (GH-3900) | To inform customers of System Software Release 1.3 (version R01.03) for the GH-3900 Indicator., Acron Aviation | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 | |
| GH-3900 | Service Bulletin | SB9200-34100-6 | A | 3/16/2016 | Software release 1.3 | To inform customers of System Software Release 1.3 (version R01.03) for the GH-3900 Indicator., Acron Aviation | 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB9200-34000-2 | A | 12/5/2012 | GH-3900 - MOD A | To update 5V current-limit setting on power supply CCA for high temperatures. Acron Aviation | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 | |
| GH-3900 | Service Bulletin | SB9200-34000-3 | A | 1/10/2013 | GH-3900 - MOD B | Incorporate EMI shielding on rate sensors to meet 200 V/m requirements. Acron Aviation | 9200-34000-0101, 9200-34000-0201 | |
| GH-3900 | Service Bulletin | SB9200-34100-2 | A | 12/5/2012 | GH-3900 - MOD A | To update 5V current-limit setting on power supply CCA for high temperatures. Acron Aviation | 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB9200-34100-3 | A | 1/10/2013 | GH-3900 - MOD B | Incorporate EMI shielding on rate sensors to meet 200 V/m requirements. Acron Aviation | 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Software | 8010-34400-0109 | 1.9 | 11/28/2023 | GH-3900.2 Software 1.9 | GH-3900.2 Software 1.9 (See 576-6157-09 ACM Tool ) | 9200-34400, 9200-34402, 9200-34410, 9200-34500, 9200-34502, 9200-34600, 9200-34602, 9200-34700, 9200-34702, 9200-34800, 9200-34802, 9200-34900 | |
| GH-3900 | Software | 8010-34400-0108 | 1.8 | 6/22/2021 | GH-3900.2 Software 1.8 | GH-3900.2 Software 1.8 (See 576-6157-08 ACM Tool ) | 9200-34400, 9200-34402, 9200-34410, 9200-34500, 9200-34502, 9200-34600, 9200-34602, 9200-34700, 9200-34702, 9200-34800, 9200-34802, 9200-34900 | |
| GH-3900 | Software | 8010-34000- 0101 | A | 9/17/2012 | System Software 1.1 with ACM Tool (GH-3900) | Release 1.1. The GH-3900 system software (8010-34000-0101, Version R01.01) is compatible with aircraft configuration file version 01.07 (revision 1.06 & 1.07) only. | 576-6159-02, 9200-34000, 9200-34100 | |
| GH-3900 | Software | 8010-34400-xxxx | 1.2 | 6/28/2013 | Software 1.2 W/ACMT, GH-3900.2 | Software 1.2 | 9200-34400, 9200-34500, 9200-34600, 9200-34700 | |
| GH-3900 | Software | 8010-34000-0103 | A | 3/17/2016 | System Software 1.3 with ACM Tool (GH-3900) | Release 1.3. The GH-3900 system software (8010-34000-0103, Version R01.03) is compatible with aircraft configuration file version 01.08 (revision 1.03). To use the new options in Release 1.3, a new config file must be generated with Aircraft Configuration Module Tool (576-6159-03). | 9200-34000, 9200-34000-0101, 9200-34000-0201, 9200-34000-0301, 9200-34000-0501, 9200-34100, 9200-34100-0101, 9200-34100-0201 576-6159-03 | |
| GH-3900 | Software | 1.3 | 5/28/2014 | Software 1.3 W/ACMT | Software 1.3 | 9200-34400, 9200-34500, 9200-34600, 9200-34700, 9200-34800 | ||
| GH-3900 | Software | 1.4 | 2/16/2015 | Software 1.4 W/ACMT | Software 1.4 | 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900 | ||
| GH-3900 | Software | 8010-34000-0100 | A | 3/22/2012 | System Software 1.0 (GH-3900) | Release 1.0. The GH-3900 system software (8010-34000-0100, Version R01.00) is compatible with aircraft configuration file version 01.06 (revision 1.03) only. | 9200-34000, 9200-34100 | |
| GH-3900 | Software | 576-6158-01 | 1.0 | 9/6/2012 | GH Field Loader Software | GH Field Loader Software | 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800 | |
| GH-3900 | Software | 1.5 | 11/4/2016 | GH-3900.2 Software 1.5 W/ACMT | 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900 | |||
| GH-3900 | Software | 8010-34400-0107 | 1.7 | 7/8/2019 | GH-3900.2 Software 1.7 | GH-3900.2 Software 1.7 (See 576-6157-08 ACM Tool ) | 9200-34400, 9200-34402, 9200-34410, 9200-34500, 9200-34502, 9200-34600, 9200-34602, 9200-34700, 9200-34702, 9200-34800, 9200-34802, 9200-34900 | |
| GH-3900 | Software | 8010-34000-0106 | A | 1/6/2023 | System Software 1.6 (GH-3900) | Release 1.6. The GH-3900 system software (8010-34000-0106, Version R01.06) is compatible with aircraft configuration file version 01.10. | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 9200-34100-0101, 9200-34100-0201 576-6159-05 | |
| GH-3900 | Software | GH-3900.2-34400-R01.00 | 1.0 | 7/19/2012 | Software Release 1.0 (R01.00) Includes 576-6185-01 & 576-6157-01 | Software Release 1.0 (R01.00) Includes 576-6185-01 & 576-6157-01 | 576-6157-01, 576-6158-01, 9200-34400, 9200-34500, 9200-34600, 9200-34700, 9200-34800 | |
| GH-3900 | Software | GH-3900.2-34400-R01.02 | 1.2 | 6/28/2013 | Software Release 1.2 (R01.02) | Software Release 1.2 (R01.02) | 9200-34400, 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501, 9200-34500, 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601, 9200-34600, 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401, 9200-34700, 9200-34700-0101, 9200-34700-0201, 9200-34700-0401 | |
| GH-3900 | Software | GH-3900.2-34400-R01.04 | 1.4 | 2/16/2015 | Software Release 1.4 R01.04 (W/ACM tool) | Software Release 1.4 R01.04 (W/ACM tool) | 576-6157-05, 576-6158-02, 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900 | |
| GH-3900 | Software | GH-3900.2-34400-R01.01 | 1.1 | 2/6/2013 | Software Release 1.1 (R01.01) (includes ACM Tool) | Software Release 1.1 (R01.01) (includes ACM Tool) | 576-6157-02, 9200-34400, 9200-34500, 9200-34600, 9200-34700 | |
| GH-3900 | Software | GH-3900.2-34400-R01.06 | 1.6 | 12/8/2017 | GH-3900.2-34400-R01.06 | Software Release 1.6 (R01.06) | 9200-34400, 9200-34402, 9200-34410, 9200-34500, 9200-34502, 9200-34600, 9200-34602, 9200-34700, 9200-34702, 9200-34800, 9200-34802, 9200-34900, 9200-34901 | |
| GH-3900 | Software | GH-3900.2-34400-R01.07 | 1.7 | 7/8/2019 | GH-3900.2-34400-R01.07 | Software Release 1.7 (R01.07) | 9200-34402, 9200-34502, 9200-34602, 9200-34702, 9200-34802, 9200-34901, 9200-34400, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900, 9200-34410 | |
| GH-3900.2 | Aircraft Tool | 576-6157-08 | 1.02 | 9/11/2019 | ACM Tool for Software 1.7 & 1.8 (GH-3900.2) | The aircraft config file version (02.16) is created using ACM Tool 576-6157-08 (revision 1.00 superseded by 1.01 or 1.02). Used with system software 1.7 & 1.8. | 9200-34400, 9200-34402, 9200-34410, 9200-34500, 9200-34502, 9200-34600, 9200-34602, 9200-34700, 9200-34702, 9200-34802, 9200-34900. 576-6157-08 | |
| GH-3900.2 | Aircraft Tool | 576-6157-09 | 1.00 | 10/9/2023 | ACM Tool for Software 1.9 (GH-3900.2) | The aircraft config file version (02.17) is created using ACM Tool 576-6157-09 (revision 1.00). Used with system software 1.9. | 9200-34400, 9200-34402, 9200-34410, 9200-34500, 9200-34502, 9200-34600, 9200-34602, 9200-34700, 9200-34702, 9200-34802, 9200-34900. 576-6157-08 | |
| GH-3900.2 | Installation Aircraft Tools | 576-6236-01 | A | 2/22/2017 | ACM Tool for KC-390 GH-3900.2 | ACMT 576-6236-01 | 576-6236-01, 9200-34702-0601 | |
| GH-3900.2 | Installation Manual | 0040-34701-01 | A | 2/22/2017 | GH-3900.2 Opertion Manaul for KC-390 | GH-3900.2 Install Manaul for KC-390 | 9200-34700-0601 | |
| GH-3900.2 | Installation Manual | 0040-34401-01 | AE | 5/27/2025 | GH-3900.2, Installation Manual | GH-3900.2 Electronic Standby Instrument System with Release 1.0, 1.1, 1.2, 1.3, 1.4, 1.5, 1.6, 1.7 , 1.8 & 1.9. Includes the ADC-4000 Air Data Computer and MAG-3000 or MAG-3100 Magnetometer. Details on Simulator unit’s P/N 9200-34701-( ) and 9200-34901-( ) are also provided. | 9200-34400-( ) 9200-34500-( ) 9200-34600-( ) 9200-34700-( ) 9200-34800-( ) 9200-34900-( ) 9200-34402-( ) 9200-34502-( ) 9200-34602-( ) 9200-34702-( ) 9200-34802-( ) 9200-34410-( ) | |
| GH-3900.2 | Instruction Manual | 0040-34402-02 | A | 2/7/2013 | Instruction Manual, ACM Tool, 576-6157-02, Revision 2.03 | Revision 2.03 Aircraft Config File Ver 02.06 | 576-6157-02 | |
| GH-3900.2 | Instruction Manual | 0040-34402-01 | A | 7/18/2012 | Instruction Manual, ACM Tool, 576-6157-01 | 576-6157-01 | ||
| GH-3900.2 | Instruction Manual | 0040-34402-05 | A | 1/23/2015 | Instruction Manual, ACM Tool, 576-6157-05, Revision 2.11 | Revision 2.11, Aircraft Config File Version: 02.11 | 576-6157-05 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900 | |
| GH-3900.2 | Instruction Manual | 0040-34402-03 | B | 12/18/2013 | Instruction Manual, ACM Tool, 576-6157-03, Revision 2.04 /2.05 | Revision 2.04, Aircraft Config File Version: 02.08 Revision 2.05, Aircraft Config File Version: 02.08 | 576-6157-03 | |
| GH-3900.2 | Instruction Manual | 0040-34402-04 | B | 5/20/2014 | Instruction Manual, ACM Tool, 576-6157-04, Revision 2.07 | Revision 2.07 Aircraft Config File 02.09 | 9200-34400, 9200-34500, 9200-34600, 9200-34700, 9200-34800 | |
| GH-3900.2 | Instruction Manual | 0040-34702-01 | A | 2/22/2017 | ACMT For KC-390 GH-3900.2 | ACMT 576-6236-01 | 576-6236-01, 9200-34700-0601 | |
| GH-3900.2 | Instruction Manual | 0040-34402-07 | B | 12/13/2018 | Instruction Manual, ACM Tool, 576-6157-07 Revision 1.03 | Revision 1.03, Aircraft Config File Version: 02.15 | 576-6157-07 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900, 9200-34400 | |
| GH-3900.2 | Instruction Manual | 0040-34402-06 | E | 12/13/2018 | Instruction Manual, ACM Tool, 576-6157-06, Revision 1.04 | Revision 1.04, Aircraft Config File Version: 02.13 | 576-6157-06 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900 | |
| GH-3900.2 | Instruction Manual | 0040-34402-08 | D | 6/28/2021 | Instruction Manual, ACM Tool, 576-6157-08, Revision 1.02 | Revision 1.02, Aircraft Config File Version: 02.16 | 576-6157-08 9200-34400, 9200-34402, 9200-34410, 9200-34500, 9200-34502, 9200-34600, 9200-34602, 9200-34700, 9200-34702, 9200-34800, 9200-34802, 9200-34900 | |
| GH-3900.2 | Instruction Manual | 0040-34402-09 | 01 | 5/27/2025 | Instruction Manual, ACM Tool, 576-6157-09, Revision 1.00 | Revision 1.00, Aircraft Config File Version: 02.17 | 576-6157-09 9200-34400, 9200-34402, 9200-34410, 9200-34500, 9200-34502, 9200-34600, 9200-34602, 9200-34700, 9200-34702, 9200-34800, 9200-34802, 9200-34900 | |
| GH-3900.2 | Intermediate Maintenance Manual | 0040-34404-01 | 34-20-78 | C | 5/27/2025 | GH-3900.2, Abbreviated Component Maintenance Manual, (lvl 1 maint.) | Abbreviated CMM (level 1 maintenance) | 9200-34400, 9200-34402, 9200-34410, 9200-34500, 9200-34502, 9200-34600, 9200-34602, 9200-34700, 9200-34702, 9200-34800, 9200-34802, 9200-34900, 9200-34901 |
| GH-3900.2 | Pilot Guide | 0040-34700-01 | A | 2/22/2017 | GH-3900.2 Opertion Manaul for KC-390 | GH-3900.2 Opertion Manaul for KC-390 | 9200-34700-0601 | |
| GH-3900.2 | Pilot Guide | 0040-34400-01 | U | 5/27/2025 | GH-3900.2, Pilots Guide | Software 1.0. 1.1. 1.2, 1.3, 1.4, 1.5, 1.6, 1.7, 1.8, 1.9 | 9200-34400, 9200-34402, 9200-34410, 9200-34500, 9200-34502, 9200-34600, 9200-34602, 9200-34700, 9200-34702, 9200-34800, 9200-34802, 9200-34900 | |
| GH-3900.2 | Printer Copies | 0040-34400-01PC | U | 5/27/2025 | GH-3900.2, Pilots Guide, (printer copy) | Printer copy GH-3900.2 PG | 9200-34x00-xx | |
| GH-3900.2 | Service Bulletin | SB003-GH-3900.2 | 00 | 11/8/2023 | System Software Release 1.9 | Software Release 1.9 | 9200-34400-( ), 9200-34410-( ) 9200-34500-( ), 9200-34600-( ) 9200-34700-( ), 9200-34800-( ) 9200-34900-( ), 9200-34402-( ) 9200-34502-( ), 9200-34602-( ) 9200-34702-( ), 9200-34802-( ) | |
| GH-3900.2 | Service Bulletin | SB9200-34400-2 | A | 12/5/2012 | GH-3900.2 - MOD A | To update 5V current-limit setting on power supply CCA for high temperatures. Acron Aviation | 9200-34400-0201, 9200-34400-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34410-7 | A | 4/26/2019 | GH-3900.2 - MOD D | Backlight LED Replacement. Acron Aviation | 9200-34400-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34500-2 | A | 12/5/2012 | GH-3900.2 MOD A | Updates the 5V current limit setting, Acron Aviation | 9200-34502-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34700-2 | A | 12/5/2012 | GH-3900.2 MOD A | Updates the 5V current limit setting, Acron Aviation | 9200-34502-0401 | |
| GH-3900.2 | Service Bulletin | SB002-GH-3900.2 | 00 | 2/20/2023 | A9 Display Assembly Replacement | A9 Display Assembly Replacement | 9200-34400-0101 9200-34400-0201 9200-34400-0401 9200-34400-0501 9200-34402-0501 9200-34410-0501 9200-34500-0101 9200-34500-0201 9200-34500-0401 9200-34500-0601 9200-34502-0101 9200-34502-0401 9200-34502-0601 9200-34600-0101 9200-34600-0201 9200-34600-0301 9200-34600-0401 9200-34600-0501 9200-34602-0401 9200-34800-0401 9200-34700-0101 9200-34700-0201 9200-34700-0401 9200-34700-0601 9200-34701-0101 9200-34701-0201 9200-34701-0401 9200-34702-0401 9200-34800-0101 9200-34800-0601 9200-34802-0401 9200-34900-0101 9200-34901-0101 | |
| GH-3900.2 | Service Bulletin | SB9200-34400-11 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34400 | |
| GH-3900.2 | Service Bulletin | SB9200-34500-11 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7, Acron Aviation | 9200-34500 | |
| GH-3900.2 | Service Bulletin | SB9200-34600-10 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7, Acron Aviation | 9200-34600 | |
| GH-3900.2 | Service Bulletin | SB9200-34700-9 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7, Acron Aviation | 9200-34700 | |
| GH-3900.2 | Service Bulletin | SB9200-34800-8 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7, Acron Aviation | 9200-34800 | |
| GH-3900.2 | Service Bulletin | SB9200-34900-7 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7, Acron Aviation | 9200-34900 | |
| GH-3900.2 | Service Bulletin | SB9200-34410-6 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7, Acron Aviation | 9200-34410 | |
| GH-3900.2 | Service Bulletin | SB9200-34402-5 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7, Acron Aviation | SB9200-34402 | |
| GH-3900.2 | Service Bulletin | SB9200-34502-6 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7, Acron Aviation | SB9200-34502 | |
| GH-3900.2 | Service Bulletin | SB9200-34602-5 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7, Acron Aviation | 9200-34602 | |
| GH-3900.2 | Service Bulletin | SB9200-34702-3 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7, Acron Aviation | SB9200-34702 | |
| GH-3900.2 | Service Bulletin | SB9200-34802-5 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7, Acron Aviation | SB9200-34802 | |
| GH-3900.2 | Service Bulletin | SB9200-34700-10 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-34700-0101, 9200-34700-0401, 9200-34700-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34800-9 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-34800-0101, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34502-7 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-34502-0101, 9200-34502-0401, 9200-34502-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34702-4 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-34702-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34802-6 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-34802-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34602-6 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-34602-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34701-3 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-34701-0101, 9200-34701-0201, 9200-34701-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34402-6 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-34402-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34900-8 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-34900-0101 | |
| GH-3900.2 | Service Bulletin | SB9200-34901-6 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-34901-0101 | |
| GH-3900.2 | Service Bulletin | SB9200-34400-12 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-34400-0101, 9200-34400-0201, 9200-34400-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34500-12 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-34500-0101, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34600-11 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-34600-0101, 9200-34600-0201, 9200-34600-0401 | |
| GH-3900.2 | Service Bulletin | SB576-6157-4 | A | 10/30/2019 | Aircraft Configuration Module Tool (rev 1.02) | ACMT Rev 1.02, Aircraft Configuration File Version 02.16, Acron Aviation | 576-6157-08, 9200-34400-, 9200-34402-, 9200-34410-, 9200-34500-, 9200-34502-, 9200-34600-, 9200-34602-, 9200-34700-, 9200-34702-, 9200-34800-, 9200-34802-, 9200-34900- | |
| GH-3900.2 | Service Bulletin | SB576-6157-3 | A | 9/11/2019 | Aircraft Configuration Module Tool (rev 1.01). | ACMT Rev 1.01, Aircraft Configuration File Version 02.16, Acron Aviation | 9200-34400-, 9200-34402-, 9200-34410-, 9200-34500-, 9200-34502-, 9200-34600-, 9200-34602-, 9200-34700-, 9200-34702-, 9200-34800-, 9200-34802-, 9200-34900- 576-6157-08 | |
| GH-3900.2 | Service Bulletin | SB001-GH-3900.2 | 00 | 6/28/2021 | System Software Release 1.8 | Software Release 1.8 | 9200-34400-( ), 9200-34410-( ) 9200-34500-( ), 9200-34600-( ) 9200-34700-( ), 9200-34800-( ) 9200-34900-( ), 9200-34402-( ) 9200-34502-( ), 9200-34602-( ) 9200-34702-( ), 9200-34802-( ) | |
| GH-3900.2 | Service Bulletin | SB9200-34400-7 | A | 11/3/2016 | System Software Release 1.5 | Software 1.5, Acron Aviation | 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34410-2 | A | 11/3/2016 | System Software Release 1.5 | Software 1.5, Acron Aviation | 9200-34410-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34500-7 | A | 11/3/2016 | System Software Release 1.5 | Software 1.5, Acron Aviation | 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34600-6 | A | 11/3/2016 | System Software Release 1.5 | Software 1.5, Acron Aviation | 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34700-6 | A | 11/3/2016 | Software 1.5 Upgrade | Software 1.5, Acron Aviation | 9200-34700-0101, 9200-34700-0201, 9200-34700-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34800-4 | A | 11/3/2016 | System Software Release 1.5 | Software 1.5, Acron Aviation | 9200-34800-0101, 9200-34800-0201, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34900-3 | A | 11/3/2016 | System Software Release 1.5 | Software 1.5, Acron Aviation | 9200-34900-0101 | |
| GH-3900.2 | Service Bulletin | SB9200-34400-6 | A | 9/14/2016 | To prevent rate sensor loopback failure at start up. | To prevent rate sensor loopback failure at start up., Acron Aviation | 9200-34400-0101, 9200-34400-0201, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34410-1 | A | 9/14/2016 | To prevent rate sensor loopback failure at start up. | To prevent rate sensor loopback failure at start up., Acron Aviation | 9200-34410-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34500-6 | A | 9/14/2016 | To prevent rate sensor loopback failure at start up. | To prevent rate sensor loopback failure at start up., Acron Aviation | 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34600-5 | A | 9/14/2016 | To prevent rate sensor loopback failure at start up. | To prevent rate sensor loopback failure at start up., Acron Aviation | 9200-34600-0101, 9200-34600-0201, 9200-34600-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34800-3 | A | 9/14/2016 | To prevent rate sensor loopback failure at start up. | To prevent rate sensor loopback failure at start up., Acron Aviation | 9200-34800-0101, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34900-2 | A | 9/14/2016 | To prevent rate sensor loopback failure at start up. | To prevent rate sensor loopback failure at start up., Acron Aviation | 9200-34900-0101 | |
| GH-3900.2 | Service Bulletin | SB9200-34901-1 | A | 9/14/2016 | To prevent rate sensor loopback failure at start up. | To prevent rate sensor loopback failure at start up., Acron Aviation | 9200-34901-0101 | |
| GH-3900.2 | Service Bulletin | SB9200-34400-9 | A | 12/8/2017 | System Software Release 1.6 | Software Release 1.6, Acron Aviation | 9200-34400, 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34402-4 | A | 12/8/2017 | System Software Release 1.6 | , Acron Aviation | 9200-34402-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34410-4 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6, Acron Aviation | 9200-34410-4 | |
| GH-3900.2 | Service Bulletin | SB9200-34500-9 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6, Acron Aviation | 9200-34500-0101, 9200-34500-0201, 9200-34500-0301, 9200-34500-0401, 9200-34500-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34502-5 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6, Acron Aviation | 9200-34502-0101, 9200-34502-0401, 9200-34502-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34600-8 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6, Acron Aviation | 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34602-4 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6, Acron Aviation | 9200-34602-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34700-7 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6, Acron Aviation | 9200-34700-0101, 9200-34700-0201, 9200-34700-0401, 9200-34700-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34702-2 | A | 12/8/2017 | System Software Release 1.6 | System Software Release 1.6, Acron Aviation | 9200-34702-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34800-6 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6, Acron Aviation | 9200-34800-0101, 9200-34800-0201, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34802-4 | A | 12/8/2017 | System Software Release 1.6 | , Acron Aviation | 9200-34802-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34900-5 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6, Acron Aviation | 9200-34900-0101 | |
| GH-3900.2 | Service Bulletin | SB9200-34901-3 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6, Acron Aviation | 9200-34901-3 | |
| GH-3900.2 | Service Bulletin | SB9200-34402-1 | B | 7/18/2018 | Convert P/N 9200-34400-0501 to P/N 9200-34402-0501 | Convert P/N 9200-34400-0501 to P/N 9200-34402-0501, Acron Aviation | 9200-34400-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34402-2 | A | 6/20/2017 | To prevent rate sensor loopback failure at startup. | To prevent rate sensor loopback failure at startup., Acron Aviation | 9200-34402-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34702-1 | A | 5/3/2017 | To prevent memory corruptions | To prevent memory corruptions, Acron Aviation | 9200-34700-0401, 9200-34702-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34502-1 | B | 5/3/2017 | To prevent Memory Corruptions | , Acron Aviation | 9200-34500, 9200-34502 | |
| GH-3900.2 | Service Bulletin | SB9200-34502-2 | B | 5/3/2017 | To prevent rate sensor loopback failure at start up. | To prevent rate sensor loopback failure at start up., Acron Aviation | 9200-34502 | |
| GH-3900.2 | Service Bulletin | SB9200-34502-3 | A | 2/21/2017 | Updates the 5V current limit setting | Updates the 5V current limit setting, Acron Aviation | 9200-34502-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34602-1 | B | 7/18/2018 | To prevent Memory coruptions | To prevent Memory coruptions, Acron Aviation | 9200-34600-0401, 9200-34602-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34802-1 | B | 7/18/2018 | To prevent Memory Corruptions | To prevent Memory Corruptions, Acron Aviation | 9200-34800-0401, 9200-34802-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34802-2 | A | 2/21/2017 | To prevent rate sensor loopback failure at start up. | To prevent rate sensor loopback failure at start up., Acron Aviation | 9200-34802-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34700-8 | B | 7/31/2018 | Error Correcting RAM | Error Correcting RAM, Acron Aviation | 9200-34700-0101, 9200-34700-0201, 9200-34700-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34400-8 | A | 1/25/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement, Acron Aviation | 9200-34400, 9200-34400-0101, 9200-34400-0201, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34900-4 | A | 1/25/2018 | Display Rate and Sensor CCM Replacement | Display Rate and Sensor CCM Replacement, Acron Aviation | 9200-34900-0101 | |
| GH-3900.2 | Service Bulletin | SB9200-34402-3 | A | 1/25/2018 | Display and Rate Sensor CCM Replacement | Display and Rate Sensor CCM Replacement, Acron Aviation | 9200-34402-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34410-3 | A | 1/25/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement, Acron Aviation | 9200-34410-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34500-8 | B | 3/8/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement, Acron Aviation | 9200-34500-0101, 9200-34500-0201, 9200-34500-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34502-4 | B | 3/8/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement, Acron Aviation | 9200-34502-0101, 9200-34502-0401, 9200-34502-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34802-3 | A | 1/25/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement, Acron Aviation | 9200-34802-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34901-2 | A | 1/25/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement, Acron Aviation | 9200-34901-0101 | |
| GH-3900.2 | Service Bulletin | SB9200-34400-10 | C | 10/11/2018 | Error Correcting RAM | Error Correcting RAM, Acron Aviation | 9200-34400-0101, 9200-34400-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34600-7 | A | 3/8/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM Replacement, Acron Aviation | 9200-34600-0101, 9200-34600-0201, 9200-34600-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34602-3 | A | 3/8/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement, Acron Aviation | 9200-34602-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34800-5 | A | 3/8/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement, Acron Aviation | 9200-34800-0101, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34900-6 | A | 4/4/2018 | Error Correcting RAM | Error Correcting RAM, Acron Aviation | 9200-34900-0101 | |
| GH-3900.2 | Service Bulletin | SB9200-34901-4 | A | 4/4/2018 | Error Correcting RAM | Error Correcting RAM, Acron Aviation | 9200-34901-0101 | |
| GH-3900.2 | Service Bulletin | SB9200-34410-5 | A | 7/31/2018 | Error Correcting RAM (MOD C) | Error Correcting RAM, Acron Aviation | 9200-34500-0201 | |
| GH-3900.2 | Service Bulletin | SB9200-34500-10 | A | 7/31/2018 | Error Correcting RAM | Error Correcting RAM, Acron Aviation | 9200-34500-0201 | |
| GH-3900.2 | Service Bulletin | SB9200-34600-9 | A | 7/31/2018 | Error Correcting RAM | Error Correcting RAM, Acron Aviation | 9200-34600-0101, 9200-34600-0201 | |
| GH-3900.2 | Service Bulletin | SB9200-34701-1 | A | 7/31/2018 | Error Correcting RAM | Error Correcting RAM, Acron Aviation | 9200-34701-0201, 9200-34701-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34800-7 | A | 7/31/2018 | Error Correcting RAM | Error Correcting RAM, Acron Aviation | 9200-34800-0101, 9200-34800-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34400-1 | B | 6/2/2016 | System Software Release 1.1 | Software Revision 1.1, Acron Aviation | 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34500-1 | B | 6/2/2016 | System Software Release 1.1 | Release of Software Ver 1.1, Acron Aviation | 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34600-1 | B | 6/2/2016 | System Software Release 1.1 | Release of Software Version 1.1, Acron Aviation | 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34700-1 | B | 6/2/2016 | Release of Software Version 1.1 | Release of Software Version 1.1, Acron Aviation | 9200-34700-0101, 9200-34700-0201, 9200-34700-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34400-4 | A | 5/28/2014 | System Software Release 1.3 | Software Release 1.3, Acron Aviation | 9200-34400, 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34500-4 | A | 5/28/2014 | System Software Release 1.3 | Software 1.3, Acron Aviation | 9200-34500, 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34600-3 | A | 5/28/2014 | System Software Release 1.3 | Software 1.3, Acron Aviation | 9200-34600, 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34700-4 | A | 5/28/2014 | Software 1.3 | Software 1.3, Acron Aviation | 9200-34700, 9200-34700-0101, 9200-34700-0201, 9200-34700-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34800-1 | A | 5/28/2014 | System Software Release 1.3 | Software 1.3, Acron Aviation | 9200-34800, 9200-34800-0101, 9200-34800-0201, 9200-34800-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34400-5 | B | 2/18/2015 | Corrects software version called out on page 8 step j | Corrects software version called out on page 8 step j , Acron Aviation | 9200-34400, 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34500-5 | A | 1/29/2015 | System Software Release 1.4 | GH-3900.2 System Software Release 1.4, Acron Aviation | 9200-34500, 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34600-4 | A | 1/29/2015 | System Software Release 1.4 | GH-3900.2 System Software Release 1.4, Acron Aviation | 9200-34600, 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34700-5 | A | 1/29/2015 | GH-3900.2 System Software Release 1.4 | GH-3900.2 System Software Release 1.4, Acron Aviation | 9200-34700 | |
| GH-3900.2 | Service Bulletin | SB9200-34800-2 | A | 1/29/2015 | System Software Release 1.4 | GH-3900.2 System Software Release 1.4, Acron Aviation | 9200-34800, 9200-34800-0101, 9200-34800-0201, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34900-1 | A | 1/29/2015 | System Software Release 1.4 | GH-3900.2 System Software Release 1.4, Acron Aviation | 9200-34900, 9200-34900-0101 | |
| GH-3900.2 | Service Bulletin | SB576-6157-2 | A | 12/18/2013 | Aircraft Configuration Module Tool (rev 2.05) | ACMT Rev 2.05, Acron Aviation | 9200-34400-, 9200-34500-, 9200-34600-, 9200-34700-, 9200-34800- | |
| GH-3900.2 | Service Bulletin | SB576-6157-1 | B | 5/24/2013 | Aircraft Configuration Module Tool (rev 2.03) | ACMT REV 2.03.0, Acron Aviation | 9200-34400-, 9200-34500-, 9200-34600-, 9200-34700-, 9200-34800- | |
| GH-3900.2 | Service Bulletin | SB9200-34400-3 | D | 1/29/2014 | System software Release 1.2 (Version R01.02) | Software Version 1.2, Acron Aviation | 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34500-3 | D | 1/29/2014 | System software Release 1.2 (Version R01.02) | Software Version 1.2 , Acron Aviation | 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900.2 | Service Bulletin | SB9200-34600-2 | D | 1/29/2014 | System software Release 1.2 (Version R01.02) | Software Version 1.2 , Acron Aviation | 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900.2 | Service Bulletin | SB9200-34700-3 | D | 1/29/2014 | System Software Release 1.2 (Version R01.02) | Release of 1.2 Software , Acron Aviation | 9200-34700-0101, 9200-34700-0201, 9200-34700-0401 | |
| GH-3900.2 | Software | 8010-34400-xxxx | 1.2 | 6/28/2013 | Software 1.2 W/ACMT, GH-3900.2 | Software 1.2 | 9200-34400, 9200-34500, 9200-34600, 9200-34700 | |
| GH-3900.2 | Software | 1.4 | 2/16/2015 | Software 1.4 W/ACMT | Software 1.4 | 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900 | ||
| GH-3900.2 | Software | 1.3 | 5/28/2014 | Software 1.3 W/ACMT | Software 1.3 | 9200-34400, 9200-34500, 9200-34600, 9200-34700, 9200-34800 | ||
| GH-3900.2 | Software | 8010-34400-0100 | 1.00 | 7/19/2012 | GH-3900.2 S/W 1.00 | GH-3900.2 S/W 1.00 | 9200-34400-xx | |
| GH-3900.2 | Software | 8010-34400-0101 | A | 2/6/2013 | GH3900.2 S/W 1.1 | Software File | 9200-34400, 9200-34500, 9200-34600, 9200-34700 | |
| GH-3900.2 | Software | 576-6158-01 | 1.0 | 9/6/2012 | GH Field Loader Software | GH Field Loader Software | 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800 | |
| GH-3900.2 | Software | 1.5 | 11/4/2016 | GH-3900.2 Software 1.5 W/ACMT | 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900 | |||
| GH-3900.2 | Software | 8010-34400-0107 | 1.7 | 7/8/2019 | GH-3900.2 Software 1.7 | GH-3900.2 Software 1.7 (See 576-6157-08 ACM Tool ) | 9200-34400, 9200-34402, 9200-34410, 9200-34500, 9200-34502, 9200-34600, 9200-34602, 9200-34700, 9200-34702, 9200-34800, 9200-34802, 9200-34900 | |
| GH-3900.2 | Software | 8010-34400-0109 | 1.9 | 11/28/2023 | GH-3900.2 Software 1.9 | GH-3900.2 Software 1.9 (See 576-6157-09 ACM Tool ) | 9200-34400, 9200-34402, 9200-34410, 9200-34500, 9200-34502, 9200-34600, 9200-34602, 9200-34700, 9200-34702, 9200-34800, 9200-34802, 9200-34900 | |
| GH-3900.2 | Software | 8010-34400-0108 | 1.8 | 6/22/2021 | GH-3900.2 Software 1.8 | GH-3900.2 Software 1.8 (See 576-6157-08 ACM Tool ) | 9200-34400, 9200-34402, 9200-34410, 9200-34500, 9200-34502, 9200-34600, 9200-34602, 9200-34700, 9200-34702, 9200-34800, 9200-34802, 9200-34900 | |
| GH-3900.2 | Software | GH-3900.2-34400-R01.07 | 1.7 | 7/8/2019 | GH-3900.2-34400-R01.07 | Software Release 1.7 (R01.07) | 9200-34402, 9200-34502, 9200-34602, 9200-34702, 9200-34802, 9200-34901, 9200-34400, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900, 9200-34410 | |
| GH-3900.2 | Software | GH-3900.2-34400-R01.00 | 1.0 | 7/19/2012 | Software Release 1.0 (R01.00) Includes 576-6185-01 & 576-6157-01 | Software Release 1.0 (R01.00) Includes 576-6185-01 & 576-6157-01 | 576-6157-01, 576-6158-01, 9200-34400, 9200-34500, 9200-34600, 9200-34700, 9200-34800 | |
| GH-3900.2 | Software | GH-3900.2-34400-R01.02 | 1.2 | 6/28/2013 | Software Release 1.2 (R01.02) | Software Release 1.2 (R01.02) | 9200-34400, 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501, 9200-34500, 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601, 9200-34600, 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401, 9200-34700, 9200-34700-0101, 9200-34700-0201, 9200-34700-0401 | |
| GH-3900.2 | Software | GH-3900.2-34400-R01.01 | 1.1 | 2/6/2013 | Software Release 1.1 (R01.01) (includes ACM Tool) | Software Release 1.1 (R01.01) (includes ACM Tool) | 576-6157-02, 9200-34400, 9200-34500, 9200-34600, 9200-34700 | |
| GH-3900.2 | Software | GH-3900.2-34400-R01.04 | 1.4 | 2/16/2015 | Software Release 1.4 R01.04 (W/ACM tool) | Software Release 1.4 R01.04 (W/ACM tool) | 576-6157-05, 576-6158-02, 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900 | |
| GH-3900.2 | Software | GH-3900.2-34400-R01.06 | 1.6 | 12/8/2017 | GH-3900.2-34400-R01.06 | Software Release 1.6 (R01.06) | 9200-34400, 9200-34402, 9200-34410, 9200-34500, 9200-34502, 9200-34600, 9200-34602, 9200-34700, 9200-34702, 9200-34800, 9200-34802, 9200-34900, 9200-34901 | |
| GH-3900RSU | Component Maintenance Manual | 0040-38003-01 | B | 10/18/2016 | GH-3900RSU CMM | GH-3900RSU CMM | 9200-38000-0101, 9200-38100-0101 | |
| GH-3900RSU | Installation Manual | 0040-38001-01 | D | 6/2/2016 | GH-3900RSU Install Manual | Add Software 1.1 add dual display connect | 9200-38000-0101, 9200-38100-0101 | |
| GH-3900RSU | Instruction Manual | 0040-38002-01 | A | 8/14/2013 | Aircraft Configuration Tool | GH-3900RSU Rev 1.01 Config File 03.00 | 9200-38000-xx 9200-38100-xx | |
| GH-3900RSU | Instruction Manual | 0040-38002-02 | B | 9/21/2015 | Aircraft Configuration Tool | GH-3900.2RSU SW1.1 | 576-6207-02 | |
| GH-3900RSU | Service Bulletin | SB9200-38000-2 | A | 9/14/2016 | To prevent rate sensor loopback failure at start up. | To prevent rate sensor loopback failure at start up., Acron Aviation | 9200-38000-0101 | |
| GH-3900RSU | Service Bulletin | SB9200-38100-2 | A | 9/14/2016 | To prevent rate sensor loopback failure at start up. | To prevent rate sensor loopback failure at start up., Acron Aviation | SB9200-38100-0101 | |
| GH-3900RSU | Service Bulletin | SB576-6193-1 | A | 9/24/2015 | AHRS Installation Tool – Rev 1.54 | AHRS Installation Tool – Rev 1.54, Acron Aviation | 9200-38500-0201 9200-38600-0201 | |
| GH-3900RSU | Service Bulletin | SB576-6207-1 | A | 9/24/2015 | Aircraft Configuration Module Tool – Revision 1.01 | Aircraft Configuration Module Tool – Revision 1.01, Acron Aviation | 9200-38000-0101, 9200-38100-0101 | |
| GH-3900RSU | Service Bulletin | SB9200-38100-1 | A | 3/2/2015 | Software release 1.1 | To inform customers of System software Revision 1.1 (version R01.01) for the GH-3900.2RSU, Acron Aviation | 9200-38100- | |
| GH-3900RSU | Service Bulletin | SB9200-38000-1 | A | 3/2/2015 | Software Release 1.1 | To inform customers of System software Revision 1.1 (version R01.01) for the GH-3900.2RSU, Acron Aviation | 9200-38000- | |
| GH-3900RSU | Software | 8010-34000-0101 | 1.1 | 4/15/2015 | Software 1.1 With ACMT | Release 1.1. The GH-3900 system software (8010-34000-0101, Version R01.01) is compatible with aircraft configuration file version 01.07 (revision 1.06 & 1.07) only. | 9200-38000, 9200-38100 | |
| GH-3900RSU | Software | n/a | 1.0 | 8/13/2013 | GH-3900 RSU Software | GH-3900 RSU Software | 576-6193-01, 576-6207-01, 576-6209 | |
| GH-3900RSU | Software | 576-6158-01 | 1.0 | 9/6/2012 | GH Field Loader Software | GH Field Loader Software | 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800 | |
| GH-3900RSU | Software | 576-6193-01 | F | 6/20/2017 | GH-3900RSU AHRS Installation Tool | GH-3900RSU AHRS Installation Tool | 9200-38000-0101, 9200-38100-0101 | |
| GH-3900RSU | Software | GH-3900RSU-38000-R01.01 | 1.1 | 4/14/2015 | GH-3900 RSU software 1.1 | GH-3900 RSU software 1.1 | 9200-38000, 9200-38100 | |
| GH-3900RSU | Software | GH-3900RSU-38000-R01.00 | 1.0 | 8/21/2013 | Software Rel. 01.00 with ACMT | Software Rel. 01.00 with ACMT | 576-6193-01, 576-6207-01, 576-6209, 9200-38000-0101, 9200-38100-0101 | |
| GH-3900RSU | Software | 576-6193-01 | F | 6/20/2017 | AHRS Installation Tool, GH-3900.2RSU | Aircraft AHRS Installation Tool (P/N 576-6193-01) is used to enter angles data, MAG angles/wing flex, and perform the MAG swing. | 9200-38000-0101, 9200-38100-0101 | |
| GH-4001 | Installation Aircraft Tools | 576-6158-03 | A | 3/29/2016 | Tool | Field Loader Tool (altenate to 576-6158-02) | ||
| GH-4001 | Installation Aircraft Tools | 576-6245-04 | B | 2/25/2020 | ACM Tool for Software 1.3 (GH-4001) | Aircraft Configuration Module Tool for SW 1.3 ACM Tool Revision 1.02, Aircraft Config File Version: 05.06 | 9200-45000-( ) 9200-45201-( ) 9200-45300-( ) 9200-45400-( ) | |
| GH-4001 | Installation Aircraft Tools | 576-6245-02 | C | 2/4/2019 | ACM Tool for Software 1.1 (GH-4001) | This software is designed to operate with the GH-4001 Electronic Standby Instrument System, Release 1.1. | 9200-45000-( ) 9200-45201-( ) 9200-45300-( ) 9200-45400-( ) | |
| GH-4001 | Installation Manual | 0040-45001-01 | P | 6/17/2024 | GH-4001 Install Manual | Electronic file not available. Contact L3 for secure copy. International customers will need to obtain a export license. | 576-6158-02, 576-6158-03, 9200-45000-0101, 9200-45000-0301, 9200-45000-0401, 9200-45201-0101, 9200-45201-5101, 9200-45300-0101, 9200-45300-0201, 9200-45400-0301, 9200-45400-0501 9200-45900-0301, 9200-45800-0401, 9200-45900-0401 | |
| GH-4001 | Installation Manual | 0040-45101-01 | A | 3/23/2017 | GH-4001 Installation & Operation Manual | 2.x Specific To T-50 A/C | 9200-45100-0101 | |
| GH-4001 | Instruction Manual | 0040-45102-01 | A | 3/27/2017 | ACM Tool Instruction Manual | ACMT A/C Config File 05.02 | 576-6278-01, 9200-45100-0101 | |
| GH-4001 | Instruction Manual | 0040-45002-02 | A | 5/13/2016 | Aircraft Configuration Module Tool | ACM Tool For SW 1.1 | 576-6245-02, 9200-45000-0101, 9200-45000-0301, 9200-45000-0401, 9200-45201-0101, 9200-45300-0101 | |
| GH-4001 | Instruction Manual | 0040-45002-01 | B | 12/17/2015 | Airctaft Configuration Module tool | ACMT Rev 1.00 AC Config file 05.01 | ||
| GH-4001 | Instruction Manual | 0040-45002-03 | A | 2/12/2019 | Aircraft Configuration Module Tool | ACM Tool for SW 1.2 | 9200-45000-0101, 9200-45000-0301, 9200-45000-0401, 9200-45201-0101, 9200-45201-0501, 9200-45400-0301, 576-6245-03, 9200-45300-0101, 9200-45300-0201 | |
| GH-4001 | Instruction Manual | 0040-45002-04 | B | 2/19/2020 | Aircraft Configuration Module Tool | ACM Tool for SW 1.3 | 9200-45000-( ), 9200-45300-( ), 9200-45400-( ), 576-6245-04, 9200-45201-( ) | |
| GH-4001 | Instruction Manual | 0040-45002-05 | 00 | 6/17/2024 | Aircraft Configuration Module Tool | ACM Tool for SW 1.4 | 9200-45000-( ), 9200-45300-( ), 9200-45400-( ), 576-6245-04, 9200-45201-( ) 9200-45900-0301, 9200-45800-0401, 9200-45900-0401 | |
| GH-4001 | Service Bulletin | SB004-GH-4001 | 00 | 6/17/2024 | System Software Release 1.4 (version R01.04) | System Software Release 1.4 (SW Version R01.04) | 9200-45000-( ), 9200-45201-( ), 9200-45300-( ), 9200-45400-( ) 9200-45900-0301, 9200-45800-0401, 9200-45900-0401 | |
| GH-4001 | Service Bulletin | SB003-GH-4001 | 00 | 1/29/2024 | Hardware MOD - Display Assembly Replacement | To provide alternate A1 Display Assembly when replacement becomes necessary. | 9200-45000-0101, 9200-45000-0301, 9200-45001-0101, 9200-45100-0201, 9200-45100-0701, 9200-45201-0401, 9200-45300-0101, 9200-45300-0201, 9200-45300-0301, 9200-45400-0501 | |
| GH-4001 | Service Bulletin | SB9200-45000-5 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-45000-0101, 9200-45000-0401 | |
| GH-4001 | Service Bulletin | SB9200-45300-3 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-45300-0201, 9200-45300-0301 | |
| GH-4001 | Service Bulletin | SB9200-45201-4 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-45201-0101, 9200-45201-5101 | |
| GH-4001 | Service Bulletin | SB9200-45400-1 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement, Acron Aviation | 9200-45400-0301 | |
| GH-4001 | Service Bulletin | SB576-6245-1 | A | 2/19/2020 | ACM Tool | ACM Tool, Acron Aviation | 9200-45000-, 9200-45001-, 9200-45100-, 9200-45201-, 9200-45300-, 9200-45400- | |
| GH-4001 | Service Bulletin | SB001-GH-4001 | A | 9/18/2019 | System Software Release 1.3 (version R01.03) | GH-4001 - System Software Release 1.3 (SW Version R01.03) | 9200-45000-( ), 9200-45201-( ), 9200-45300-( ), 9200-45400-( ) | |
| GH-4001 | Service Bulletin | SB002-GH-4001 | 00 | 8/12/2020 | Hardware MOD - Alternate Rate Sensor | To provide alternate U1 Rate Sensor when replacement becomes necessary. | 9200-45000-0101, 9200-45000-0401, 9200-45000-3010, 9200-45201-0101, 9200-45201-5101, 9200-45400-0301, 9200-45400-0501 | |
| GH-4001 | Service Bulletin | SB9200-45000-3 | A | 12/18/2017 | Update EESeal to support pin injection waveform 3 conditions. | , Acron Aviation | 9200-45000-0401 | |
| GH-4001 | Service Bulletin | SB9200-45000-4 | A | 2/12/2019 | System Software Release 1.2 (version R01.02) | GH-4001 - System Software Release 1.2, Acron Aviation | 9200-45000-0101, 9200-45000-0301, 9200-45000-0401 | |
| GH-4001 | Service Bulletin | SB9200-45201-1 | A | 6/10/2015 | Eliminate sticking of knob. | , Acron Aviation | 9200-45201-0101 | |
| GH-4001 | Service Bulletin | SB9200-45201-3 | A | 2/12/2019 | System Software Release 1.2 (version R01.02) | GH-4001 - System Software Release 1.2 (SW Version R01.02), Acron Aviation | 9200-45201-0101, 9200-45201-0501 | |
| GH-4001 | Service Bulletin | SB9200-45300-1 | A | 12/18/2017 | Update EESeal to support pin injection waveform 3 conditions. | , Acron Aviation | 9200-45300-0201 | |
| GH-4001 | Service Bulletin | SB9200-45300-2 | A | 2/12/2019 | System Software Release 1.2 (version R01.02) | GH-4001 - System Software Release 1.2 (SW Version R01.02), Acron Aviation | 9200-45300-0101, 9200-45300-0201 | |
| GH-4001 | Service Bulletin | SB9200-45000-2 | A | 8/17/2016 | Incorporation of MOD A | Incorporation of MOD A, Acron Aviation | 9200-45000-0401 | |
| GH-4001 | Service Bulletin | SB9200-45000-1 | A | 5/13/2016 | System Software Release 1.1 | , Acron Aviation | 9200-45000, 9200-45000-0101, 9200-45000-0301, 9200-45000-0401 | |
| GH-4001 | Service Bulletin | SB9200-45201-2 | A | 5/13/2016 | System Software Release 1.1 | , Acron Aviation | 9200-45201, 9200-45201-0101 | |
| GH-4001 | Software | 8010-45000-0103. | orig | 8/29/2019 | GH-4001_Pub-Notice_SW1.3 | GH-4001_Pub-Notice_SW1.3 | 9200-45000-( ) | |
| GH-4200 | Installation Manual | 0040-42000-01 | F | 2/28/2022 | Installation and Operation Manual | Electronic Standby Instrument System | 9200-42000-0201 | |
| GH-4200 | Service Bulletin | SB9200-42000-7 | A | 3/16/2015 | Software Release 1.2 | Software Release 1.2, Acron Aviation | 9200-42000-0201 | |
| GH-4200 | Service Bulletin | SB9200-42000-6 | A | 4/9/2014 | MOD E - Improve Reliability | Improve Reliability of the 5VDC Power Supply, Acron Aviation | 9200-42000-0201 | |
| GH-4200 | Service Bulletin | SB9200-42000-9 | 00 | 2/28/2022 | MOD G – New Rate Sensor | Service Bulletin, Acron Aviation | GH-4200 | |
| GH-4200 | Service Bulletin | SB9200-42000-10 | 00 | 2/28/2022 | MOD H – New Display Backlight CCA | Service Bulletin, Acron Aviation | Gh-4200 | |
| GH-4200 | Service Bulletin | SB9200-42000-11 | 00 | 2/28/2022 | MOD J – New Display Assembly | Service Bulletin, Acron Aviation | 9200-42000-0201 | |
| GH-4200 | Service Bulletin | SB9200-42000-1 | A | 11/7/2012 | MOD A - NVIS display filters | Incorporate NVIS display with IR / Diffusion filter pack sealed to prevent moisture entry between filters. | 9200-42000-0201 | |
| GH-4200 | Service Bulletin | SB9200-42000-2 | A | 11/13/2012 | MOD B - Hardware Update | Incorporate of this modification does the following: • Replace resistors on EMI CCA with Lightning/ESD resistant type resistors. • Replace shims on Keyboard Assembly with fungus inert shims. • Ensure display mounts correctly by replacing align ring. • Incorporate new reliable rate sensor. | 9200-42000-0201 | |
| GH-4200 | Service Bulletin | SB9200-42000-3 | A | 5/23/2013 | MOD C - Replace glass ring | Incorporate MOD C by replacing glass align ring (557-1920-01) with new glass align ring (557-1920-02). | 9200-42000-0201 | |
| GH-4200 | Service Bulletin | SB9200-42000-4 | A | 10/10/2013 | MOD D - Flash Memory | Flash memory with 2010 and earlier date codes can become corrupted during boot which causes a startup failure. | 9200-42000-0201 | |
| GH-4200 | Service Bulletin | SB9200-42000-5 | A | 11/20/2013 | Software Release 1.1 | To inform customers of System Software Release 1.1 (version R01.01) for the GH-4200 Indicator. | 9200-42000-0201 | |
| GH-4200 | Service Bulletin | SB9200-42000-8 | A | 1/22/2015 | MOD F- improve rate sensor | To implement an improved rate sensor that eliminates EEPROM corruption. | 9200-42000-0201 | |
| GH-4200 | Service Bulletin | SB9200-42000-12 | 00 | 5/14/2024 | Future release | To inform customers of System Software Release 1.3 (version R01.03) for the GH-4200 Indicator. | 9200-42000-0201 | |
| GHR-4000 | Installation Manual | 0040-42001-01 | F | 2/28/2022 | Installation and Operation Manual | Manual is ITAR and not availible | 9200-42600-0201 | |
| GHR-4000 | Service Bulletin | SB9200-42600-1 | A | 11/7/2012 | MOD A - NVIS display filters | Incorporate NVIS display with IR / Diffusion filter pack sealed to prevent moisture entry between filters. | 9200-42600-0201 | |
| GHR-4000 | Service Bulletin | SB9200-42600-2 | A | 11/13/2012 | MOD B - Hardware Update | Incorporate of this modification does the following: • Replace resistors on EMI CCA with Lightning/ESD resistant type resistors. • Replace shims on Keyboard Assembly with fungus inert shims. • Ensure display mounts correctly by replacing align ring. • Incorporate new reliable rate sensor. | 9200-42600-0201 | |
| GHR-4000 | Service Bulletin | SB9200-42600-3 | A | 5/23/2013 | MOD C - Replace glass ring | Incorporate MOD C by replacing glass align ring (557-1920-01) with new glass align ring (557-1920-02). | 9200-42600-0201 | |
| GHR-4000 | Service Bulletin | SB9200-42600-4 | A | 10/10/2013 | MOD D - Flash Memory | Flash memory with 2010 and earlier date codes can become corrupted during boot which causes a startup failure. | 9200-42600-0201 | |
| GHR-4000 | Service Bulletin | SB9200-42600-5 | A | 11/20/2013 | Software 1.1 | To inform customers of System Software Release 1.1 (version R01.01) for the GHR-4200 Repeater. | 9200-42600-0201 | |
| GHR-4000 | Service Bulletin | SB9200-42600-6 | A | 3/9/2014 | MOD E - Improve Reliability | Improve Reliability of the 5VDC Power Supply, Acron Aviation | 9200-42600-0201 | |
| GHR-4000 | Service Bulletin | SB9200-42600-9 | A | 5/14/2024 | Future release | To inform customers of System Software Release 1.3 (version R01.03) for the GHR-4000 Repeater. | 9200-42600-0201 | |
| GHR-4000 | Service Bulletin | SB9200-42600-8 | 00 | 2/28/2022 | MOD F - New Display Backlight CCA / MOD G – New Display Assembly | New Display Backlight CCA / MOD G – New Display Assembly | 9200-42600-0201 | |
| GHR-4000 | Service Bulletin | SB9200-42600-7 | A | 3/16/2015 | Software 1.2 | To inform customers of System Software Release 1.2 (version R01.02) for the GHR-4200 Repeater., Acron Aviation | 9200-42600-0201 | |
| GS/2 | Service Bulletin | SB001-ROC7 | 00 | 11/12/2024 | Service Bulletin, MOD 1 | Incorporation of MOD 1 updates the ROC/7 to function with the CICC/3. | 17TES0700 253-E5728-00 17TES0075 | |
| GS/2 | Service Bulletin | SB002-ROC7 | 00 | 11/12/2024 | Service Bulletin, MOD 2 | Incorporation of MOD 2 updates the ROC/7 from Windows 7 to Windows 10 functionality. | 17TES0700 253-E5728-00 | |
| GS/2 | Service Bulletin | SB003-ROC7 | 00 | 12/3/2024 | Service Bulletin, MOD 3 | To provide notification of MOD 3 changes to the ROC/7 Read Out Center. | 17TES0700 253-E5728-00 | |
| GSE | Installation Aircraft Tools | 17TES0436 | Orig | 12/14/2020 | ADLP Software V3.6 | Software - ADLP V3.6 | 17TES0436 | |
| GSE | Instruction Manual | 165E1696-04 | 02 | 11/30/2022 | Operator's Manual, (ROSE) SW Version 4.7 and later | Operations Manual, Read-Out Support Equipment / Recorder Interface, 4.7 or later (ROSE) | 17TES00321, 17TES0060ROSE, 17TES0063, 17TES0700, 883E1894−01 | |
| GSE | Instruction Manual | 165E1696-03 | Initial | 4/8/2010 | Read‐Out Support Equipment/Recorder Interface (ROSE/RI) Software v4 or Higher | GSE, ROSE, SW | 17TES0300, 17TES0400, 17TES0055, 17TES0060, 17TES0063, 17TES0321, 883E1894-01 | |
| GSE | Service Bulletin | ROSE SB012 | 02 | 8/24/2022 | SOFTWARE VERSION 4.10 UPGRADE | Read-Out Support Equipment (ROSE) ROSE V4.10 is intended for new installation on Windows 10 computers, Acron Aviation | 17TES0321 | |
| GSE | Service Bulletin | SB570-8552-5 | A | 4/3/2012 | DCM version 3.0 | To add DCM version 3.0 test capabilities to the JT-147A | 570-8552-01 | |
| GSE | Service Bulletin | SB570-8552-4 | A | 3/27/2006 | DCM version 2.0 test capabilities | To add DCM version 2.0 test capabilities to the JT-147A. | 501-8552-01 | |
| GSE | Software | 17TES0321 | 4.10 | 8/28/2019 | Rose S/W 1.4 | Rose S/W 4.10 | 17TES0321 | |
| GSE | Software | 17TES0321 | 4.10 | 8/28/2019 | Rose S/W 4.10 | Rose S/W 4.10 | 17TES0321 | |
| GSE - Recorder | Miscellaneous | 165E2658–00 | original | 6/1/2001 | Test Equipment Manual, Model A860 CVR Test Panel | For Use With: Cockpit Voice Recorders Models: A100, A100A, GA100, A113, A100S, A200S, FA2100CVR & FA2100CVDR Control Units Models: A151, A151B, A152, A152B, S151, S152, S251, S161, S162 & S262 Microphone Preamplifier Models: A150, S150 & S160 PN: 165E2658–00 | See notes | |
| HI-601 | Component Maintenance Manual | TP-417 | 34-20-24 | 1 | 8/19/1993 | Maintenance Manual | Pub# TP-417 | 501-1537-01 |
| HI-601 | Component Maintenance Manual | TP-462 | 34-20-43 | Chg1 | 1/8/2007 | Component Maintenance Manual | Pub# TP-462 | 501-1652-01 |
| HI-601 | Service Letter | SL-350 | A | 12/17/2019 | End of Manufacturing Notice | End of Manufacturing Notice | 501-1537-01, 501-1652-01 | |
| HI-601 | Service Letter | SL-288 | A | 7/17/2013 | Corrections to Manual | Corrections to TP-462 | 501-1652-01 | |
| HSI-3000 | Installation Manual | TP-600 | C | 8/2/2011 | Installation and Operation Manual | Pub# TP-600 | 501-1899-01 | |
| HSI-3000 | Installation Manual | TP-570 | F | 7/17/2017 | Installation and Operation Manual | This manual contains operation and installation instructions and recommended flightline maintenance information for the HSI 3000 Electronic Horizontal Situation Indicator using 2.x, 3.x, 4.x, & 5.x software. | 501-1847-01, 501-1847-02, 501-1847-03, 501-1847-04, 501-1847-05 | |
| HSI-3000 | Installation Manual | TP-597 | 0 | 3/17/2004 | Installation and Operation Manual | Pub# TP-597 | ||
| HSI-3000 | Service Bulletin | SB501-1899-3 | A | 3/15/2006 | To correct knob action at start up. | 501-1899-01 | ||
| HSI-3000 | Service Bulletin | SB501-1899-2 | A | 3/15/2006 | To correct color and knob operation. | 501-1899-01 | ||
| HSI-3000 | Service Bulletin | SB501-1847-5 | C | 4/8/2010 | To reduce the possibility of the display blanking or failing at start up. | 501-1847-04, 501-1847-05 | ||
| HSI-3000 | Service Bulletin | SB501-1899-1 | C | 1/3/2007 | To reduce the possibility of the display blanking or failing at start up. | 501-1899-01 | ||
| HSI-3000 | Service Bulletin | SB501-1899-7 | A | 6/26/2009 | To provide replacement display due to diminishing source. | To provide replacement display due to diminishing source. | 501-1899-01 | |
| HSI-3000 | Service Bulletin | SB501-1899-6 | B | 6/25/2009 | To provide replacement display due to diminishing source. | MOD 6 superseded by MOD 7 | 501-1899-01 | |
| HSI-3000 | Service Bulletin | SB501-1899-7 | A | 6/25/2009 | To provide replacement display due to diminishing source. | To provide replacement display due to diminishing source. | 501-1899-01 | |
| HSI-3000 | Service Bulletin | SB501-1847-6 | B | 4/8/2010 | Provide replacement display due to diminishing source. | 501-1847-( ) | ||
| HSI-3000 | Service Bulletin | SB501-1847-7 | D | 5/5/2011 | To correct deficiencies in hardware and software resulting in lost data during power interruptions. | To correct deficiencies in hardware and software resulting in lost data during power interruptions. | 501-1847-( ) | |
| HSI-3000 | Service Bulletin | SB501-1847-1 | D | 4/8/2010 | Provide replacement display due to diminishing source. | 501-1847-01, 501-1847-02, 501-1847-04 | ||
| HSI-3000 | Service Bulletin | SB501-1847-2 | E | 12/14/2010 | Eliminate encoder out-of-range faults. | 501-1847-01, 501-1847-02, 501-1847-04 | ||
| HSI-3000 | Service Bulletin | SB501-1847-3 | C | 4/8/2010 | Prevent Acceptance Test Procedure [ATP] failures by ensuring Transformers [A12-T3] and [A12-T4] on the Transformer CCA (P/N 542-2779-02) are matched. | 501-1847-01, 501-1847-02, 501-1847-04 | ||
| HSI-3000 | Service Bulletin | SB501-1847-4 | C | 4/8/2010 | Eliminate encoder out-of-range faults. | 501-1847-01, 501-1847-02, 501-1847-04 | ||
| HSI-3000 | Service Bulletin | SB501-1847-9 | A | 6/12/2012 | SUP Inspection | 501-1847, 501-1847-01, 501-1847-02, 501-1847-03, 501-1847-04, 501-1847-05 | ||
| HSI-3000 | Service Bulletin | SB501-1847-8 | A | 4/8/2010 | Provide replacement display due to diminishing source. | 501-1847-01, 501-1847-04, 501-1847-05 | ||
| HSI-3000 | Service Letter | SL-289 | A | 8/19/2013 | Error code 32 & 38 | Error code 32 & 38 | 501-1847-04, 501-1847-05 | |
| HSI-3000 | Service Letter | SL-287 | A | 6/20/2013 | Fault Code Identification | HSI-3000 Fault Codes | 501-1847-04, 501-1847-05 | |
| ID-1481A | Pilot Guide | TP-307 | C | 2/4/2016 | Pilot's Guide | Pub# TP-307 | 501-1022-01, 501-1032-01, 501-1049-51, 501-1086-01, 501-1098-01, 501-1101-01, 501-1101-02, 501-1131-01, 501-1131-02 | |
| ID-1712/A | Pilot Guide | TP-306 | A | 2/1/2005 | Pilot's Guide | Pub# TP-306 | 501-1077-01, 501-1152-01, 501-1153-01, 501-1154-01, 501-1190-01, 501-1190-02 | |
| ID-2472 | Pilot Guide | 009-10029-001 | B | 11/23/1998 | Pilot's Guide | Pub# 009-10029-001 | 805C0620-( ) | |
| ID-2472 | Pilot Guide | 009-10029-001 | D | 8/21/2012 | Pilot's Guide, ID-2472 | DME/TACAN Indicator Models IN602, IN602+, IN602MD, IN605, ID-2472 and ID-2502 | 9200-35500-( ), 805C0620-( ) | |
| ID-2502 | Pilot Guide | 009-10029-001 | B | 11/23/1998 | Pilot's Guide | Pub# 009-10029-001 | 805C0620-( ) | |
| i-linc | Installation Manual | 0040-19000-01 | J | 2/3/2009 | Installation Manual | Pub# 0040-19000-01 | 9200-19000-01, 9200-19000-02, 9200-19000-03, 9200-19020-01, 9200-19020-02, 9200-19020-03, 9200-19050-01, 9200-19050-02, 9200-19050-03, 9200-19050-11, 9200-19050-12, 9200-19050-13, 9200-19070-01, 9200-19070-02, 9200-19070-03, 9200-19070-11, 9200-19070-12, 9200-19070-13 | |
| i-linc | Pilot Guide | 0040-19001-01 | H | 5/10/2005 | Pilot's Guide | Pub# 0040-19001-01 | 9200-19000-01, 9200-19000-02, 9200-19000-03, 9200-19020-01, 9200-19020-02, 9200-19020-03, 9200-19050-01, 9200-19050-02, 9200-19050-03, 9200-19050-11, 9200-19050-12, 9200-19050-13, 9200-19070-01, 9200-19070-02, 9200-19070-03, 9200-19070-11, 9200-19070-12, 9200-19070-13 | |
| i-linc | Pilot Guide | 0040-19100-01 | B | 8/20/2003 | ChartView Starter Guide | Pub# 0040-19100-01 | 9200-19000-01, 9200-19000-02, 9200-19000-03, 9200-19020-01, 9200-19020-02, 9200-19020-03, 9200-19050-01, 9200-19050-02, 9200-19050-03, 9200-19050-11, 9200-19050-12, 9200-19050-13, 9200-19070-01, 9200-19070-02, 9200-19070-03, 9200-19070-11, 9200-19070-12, 9200-19070-13 | |
| i-linc | Service Bulletin | SB9200-19000-1 | A | 5/13/2005 | Inform customers of 5.2, 5.3 & 5.5 software upgrade. | Inform customers of 5.2, 5.3 & 5.5 software upgrade | 9200-19000-( ) | |
| i-linc | Service Bulletin | SB9200-19020-1 | A | 5/13/2005 | Inform customers of 5.2, 5.3 & 5.5 software upgrade. | 9200-19020-( ) | ||
| i-linc | Service Bulletin | SB9200-19050-1 | A | 5/13/2005 | Inform customers of 5.2, 5.3 & 5.5 software upgrade. | 9200-19050-( ) | ||
| i-linc | Service Bulletin | SB9200-19070-1 | A | 5/13/2005 | Inform customers of 5.2, 5.3 & 5.5 software upgrade. | 9200-19070-( ) | ||
| i-linc | Service Bulletin | SB9200-19000-3 | A | 3/21/2006 | Software Version 5.7 Upgrade | Software Version 5.7 Upgrade | 9200-19000-( ) | |
| i-linc | Service Bulletin | SB9200-19020-3 | A | 3/21/2006 | Software Version 5.7 Upgrade | Software Version 5.7 Upgrade | 9200-19020 | |
| i-linc | Service Bulletin | SB9200-19050-3 | A | 3/21/2006 | Software Version 5.7 Upgrade | Software Version 5.7 Upgrade | 9200-19050-( ) | |
| i-linc | Service Bulletin | SB9200-19070-3 | A | 3/21/2006 | Software Version 5.7 Upgrade | Software Version 5.7 Upgrade | 9200-19070-( ) | |
| i-linc | Service Bulletin | SB9200-19000-2 | A | 7/27/2005 | Inform customers of 5.6 software upgrade. | 9200-19000-( ) | ||
| i-linc | Service Bulletin | SB9200-19020-2 | A | 7/27/2005 | Inform customers of 5.6 software upgrade. | 9200-19020-xx | ||
| i-linc | Service Bulletin | SB9200-19050-2 | A | 7/27/2005 | Inform customers of 5.6 software upgrade. | 9200-19050-( ) | ||
| i-linc | Service Bulletin | SB9200-19070-2 | A | 7/27/2005 | Inform customers of 5.6 software upgrade. | Inform customers of 5.6 software upgrade. | 9200-19070-( ) | |
| i-linc | Service Bulletin | SB-123 | 1 | 9/8/2003 | Inform customers of 5.1 software upgrade. | Inform customers of 5.1 software upgrade. | 9200-19000-( ), 9200-19050-( ) | |
| i-linc | Service Letter | SL-265 | A | 3/11/2011 | Discontinued Support for i-linc MFD | 9200-19000-, 9200-19020-, 9200-19050-, 9200-19070- | ||
| IN602 | Installation Manual | 009A0301 | 1 | 8/1/1988 | Installation Manual | Pub# 009A0301 | 805C0620-( ), 805D0602-( ), 805D0660-( ), 805D0661-( ), 805D0662-( ), 805D0663-( ) | |
| IN602 | Pilot Guide | 009-10029-001 | B | 11/23/1998 | Pilot's Guide | Pub# 009-10029-001 | 805C0620-( ) | |
| IN602 | Pilot Guide | 009-10029-001 | D | 8/21/2012 | Pilot's Guide, ID-2472 | DME/TACAN Indicator Models IN602, IN602+, IN602MD, IN605, ID-2472 and ID-2502 | 9200-35500-( ), 805C0620-( ) | |
| IN602 | Service Bulletin | SB-53 | 11/1/1985 | Mod A, Factory mod only for S/N 170 and lower | ||||
| IN602 | Service Letter | SL-330 | B | 10/2/2018 | Replacement Information for the IN-602 | Replacement Information for the IN-602 | 805C0620, 9200-35500 | |
| IN605 | Pilot Guide | 009-10029-001 | D | 8/21/2012 | Pilot's Guide, ID-2472 | DME/TACAN Indicator Models IN602, IN602+, IN602MD, IN605, ID-2472 and ID-2502 | 9200-35500-( ), 805C0620-( ) | |
| IN605 | Pilot Guide | 009-10029-001 | B | 11/23/1998 | Pilot's Guide | Pub# 009-10029-001 | 805C0620-( ) | |
| JF- Test Set | Installation Manual | TP-409 | Original | 7/26/2005 | Installation Manual | Pub# TP-409 JT-113 | 570-2466-01 | |
| JF- Test Set | Instruction Manual | TP-290 | original | 7/26/2005 | Instruction Manual | Pub# TP-290. Obsolete | 570-1473-05 | |
| JT- Test Set | Instruction Manual | TP-283 | 1 | 4/1/1974 | Instruction Manual and Test Procedures | JT-10 | 570-1428-01 | |
| JT- Test Set | Instruction Manual | TP-623 | B | 3/30/2017 | Instruction Manual | Calibration Test Set | 570-8552-01 | |
| JT- Test Set | Pilot Guide | TP-574 | E | 8/13/2018 | Quick Reference Card | MAG-3000 Calibration Tester Cal Card is placed with the test set. | 570-8552-01 | |
| JT- Test Set | Service Bulletin | SB570-8552-1 | A | 10/12/2001 | To correct an error within the software. | To correct an error within the software. | 570-8552-01 | |
| JT- Test Set | Service Bulletin | SB570-8552-2 | Orig | 10/15/2001 | To correct an error within the software. | To correct an error within the software. | 570-8552-01 | |
| JT- Test Set | Service Bulletin | SB570-8552-3 | A | 3/29/2011 | To add GH-3100 test capabilities to the JT-147A. | To add GH-3100 test capabilities to the JT-147A. | 570-8552-01 | |
| JT- Test Set | Service Bulletin | SB570-8552-4 | A | 3/27/2006 | DCM version 2.0 test capabilities | To add DCM version 2.0 test capabilities to the JT-147A. | 501-8552-01 | |
| JT- Test Set | Service Bulletin | SB570-8552-5 | A | 4/3/2012 | DCM version 3.0 | To add DCM version 3.0 test capabilities to the JT-147A | 570-8552-01 | |
| JT- Test Set | Service Letter | SL-215 | A | 10/4/2006 | JT-147A Calibration Test Set | No periodic calibration or maintenance for the JT-147A Calibration Test Set is required. | 570-8552-01 | |
| LDR1000 | Component Maintenance Manual | 165E4866-02 | 23-70-20 | 03 | 8/13/2019 | Component Maintenance Manual, LDR1000 | LIGHTWEIGHT DATA RECORDER, Acron Aviation | 1000-1000-00 1000-1210-00 1000-1210-11 1000-1710-00 1000-1710-11 |
| LDR1000 | Installation Manual | 165E4866-05 | 02 | 11/10/2023 | Installation and Operation Manual, LDR 1010-3211-11 | LIGHTWEIGHT DATA RECORDER | 1010-3211-11 | |
| LDR1000 | Installation Manual | 165E4866-00TR | TR15 | 3/6/2025 | Installation and Operation Manual, LDR1000TR | LIGHTWEIGHT DATA RECORDER | 1000-1000-00, 1000-1210-00, 1000-1210-11, 1000-1710-00, 1000-1710-11 | |
| LDR1000 | Installation Manual | 165E4866-00 | 14 | 7/13/2020 | Installation and Operation Manual, LDR1000 | LIGHTWEIGHT DATA RECORDER, Acron Aviation | 1000-1000-00, 1000-1210-00, 1000-1210-11, 1000-1710-00, 1000-1710-11 | |
| LDR1000 | Instruction Manual | 165E4866-10 | 23-70-20 | 01 | 10/8/2021 | Coin Battery Replacement Procedure (Restricted), LDR1000 | LDR1000 Coin Battery Replacement Procedure (Restricted) | 1000-1000-00, 1000-1210-00, 1000-1210-11, 1000-1710-00, 1000-1710-11 |
| LDR1000 | Service Bulletin | SB002-LDR1000 | 23-70-20-02 | 00 | 4/17/2023 | Service Bulletin, LDR1000, MOD 1 | MOD 1 – Correct Color Distortion in Recorded Video, Acron Aviation | 1000-1710-11 |
| LNS6000 | Installation Manual | 009A0652 | 2 | 10/9/1995 | Installation Manual | DB683 Airborne Navigation Data Storage system | 805D0651-02, 805D0651-04 | |
| LNS6000 | Installation Manual | 009-10001-001 | B | 3/10/1997 | Installation Manual | Pub# 009-10001-001 | 805-10008-() | |
| LNS6000 | Pilot Guide | 009-10010-001 | Orig | 11/1/1992 | Pilot's Guide | Pub# 009-10010-001 | 805-10008-() | |
| LNS6000 | Pilot Guide | 009-10121-001 | A C1 | 1/3/2000 | Pilot's Guide with GPS Approach | Pub# 009-10121-001 | 805-10008-1( ), 805-10008-101, 805-10008-102, 805-10008-103, 805-10008-104, 805-10008-105, 805-10008-106, 805-10008-107, 805-10008-108, 805-10008-109, 805-10008-110, 805-10008-111, 805-10008-112, 805-10008-113, 805-10008-114, 805-10008-115, 805-10008-116, 805-10008-117, 805-10008-118, 805-10008-119, 805-10008-120 | |
| LNS6000 | Service Bulletin | SB-60 | Orig | 3/1/1987 | To correct an intermittent search problem. | To correct an intermittent search problem., Acron Aviation | 805D0500 | |
| LNS6000 | Service Bulletin | SB-52 | Orig | 11/1/1985 | Modification to Range Block Adapter Module to permit operation throughtout voltage range. | , Acron Aviation | 804B0116 | |
| LNS6000 | Service Bulletin | SB-51 | Orig | 8/1/1985 | Modification to DME Range Block Adapter Module to increase A+ voltage range. | , Acron Aviation | 804B0116 | |
| LNS6000 | Service Bulletin | SB-47 | Orig | 8/1/1985 | Modification to DME Range Block Adapter to permit module to operate throughout an input range. | , Acron Aviation | 804B0001 | |
| LNS6000 | Service Bulletin | SB-40 | Orig | 11/1/1983 | Improve transient response and ripple rejection of LR651 power supply. | , Acron Aviation | 805D0500 | |
| LNS6000 | Service Bulletin | SB-41 | Orig | 11/1/1983 | To reduce RF emissions for the LR651 receiver. | To reduce RF emissions for the LR651 receiver., Acron Aviation | 805D0500 | |
| LNS6000 | Service Bulletin | SB-48 | Orig | 10/1/1984 | To optimize LR651 | To optimize LR651 performance and improve operation in areas that have weak signals with low noise., Acron Aviation | 805D0500 | |
| LNS6000 | Supplemental Type Certificate | SA00810CH | Reis | 2/17/2004 | Installation of BFGoodrich LNS6000 navigation system with RNC6000A remote navigation computer | BFGoodrich LNS6000/ 6000A STC | ||
| LNS6000 | Supplemental Type Certificate | SA00810CH-FMS | Reis | 2/17/2004 | Installation of BFGoodrich LNS6000 navigation system with RNC6000A remote navigation computer | BFGoodrich LNS6000 FMS | ||
| Loran Nav System | Installation Manual | 12710138B | B | 3/1/1987 | Installation Manual | Pub# 12710138B | 30410035-( ) 12710138A 12710138B | |
| Loran Nav System | Installation Manual | 009A0631A | 4 | 4/1/1989 | Installation Manual | Pub# 009A0631A | 009A0631A | |
| Loran Nav System | Installation Manual | 009A0652 | 2 | 10/9/1995 | Installation Manual | DB683 Airborne Navigation Data Storage system | 805D0651-02, 805D0651-04 | |
| Loran Nav System | Pilot Guide | 002A0653 | 2 | 11/21/1995 | Pilot's Guide | Pub# 002A0653 | 805D0651-02, 805D0651-04 | |
| Loran Nav System | Pilot Guide | 002A0550 | 1 | 5/1/1984 | Pilot's Guide | Pub# 002A0550 | 002A0550, 805D0500, 805D0550, 805D0550-01, 805D0550-02, 805D0550-03, 805D0550-04, 805D0550-11, 805D0550-12, 805D0550-13, 805D0550-14, 805D0550-21, 805D0550-22, 805D0550-23, 805D0550-24, 805D0570, 805D0570-01 | |
| Loran Nav System | Pilot Guide | 002A0559 | Orig | 1/1/1987 | Pilot's Guide | Pub# 002A0559 | 002A0559 | |
| Loran Nav System | Pilot Guide | 002A0631C | C | 6/29/1989 | Operations Manual | Pub# 002A0631C | 002A0631C | |
| Loran Nav System | Pilot Guide | 002A0635 | Orig | 12/22/1987 | Operations Manual | Pub# 002A0635 | xxxxx | |
| Loran Nav System | Pilot Guide | 002A0640A | Orig | 6/1/1991 | Pilot's Guide | Pub# 002A0640A | 002A0640A | |
| Loran Nav System | Pilot Guide | 12710139-1 | C1 | 10/7/1993 | Operation Manual | Pub# 12710139-1 | 30410035-( ) | |
| Loran Nav System | Service Bulletin | SB-55 | Orig | 5/1/1986 | LRN500 faceplate bonding modification. | LRN500 faceplate bonding modification., Acron Aviation | 805D0630 | |
| MAG-3000 | Installation Manual | TP-582 | G | 3/4/2010 | Installation and Operation Manual, GH-3100, sw 4.0 | Pub# TP-582 | 501-1826-01, 501-1860-0102, 501-1860-0104, 501-1870-( ) | |
| MAG-3000 | Installation Manual | TP-633 | M | 8/21/2019 | MAG-3000 Installation Manual | Magnetometer | 501-1826-( ), 501-1826-01, 501-1826-03, 501-1826-04, 501-1826-05 | |
| MAG-3000 | Installation Manual | 0040-34401-01 | AE | 5/27/2025 | GH-3900.2, Installation Manual | GH-3900.2 Electronic Standby Instrument System with Release 1.0, 1.1, 1.2, 1.3, 1.4, 1.5, 1.6, 1.7 , 1.8 & 1.9. Includes the ADC-4000 Air Data Computer and MAG-3000 or MAG-3100 Magnetometer. Details on Simulator unit’s P/N 9200-34701-( ) and 9200-34901-( ) are also provided. | 9200-34400-( ) 9200-34500-( ) 9200-34600-( ) 9200-34700-( ) 9200-34800-( ) 9200-34900-( ) 9200-34402-( ) 9200-34502-( ) 9200-34602-( ) 9200-34702-( ) 9200-34802-( ) 9200-34410-( ) | |
| MAG-3000 | Pilot Guide | TP-574 | E | 8/13/2018 | Quick Reference Card | MAG-3000 Calibration Tester Cal Card is placed with the test set. | 570-8552-01 | |
| MAG-3000 | Service Bulletin | SB501-1826-1 | A | 4/15/2004 | To provide strain relief for end of cable as it exits the unit. | 501-1826-01 | ||
| MAG-3000 | Service Bulletin | SB501-1826-2 | A | 1/4/2005 | Reduce corrosion effects inside MAG-3000. | 501-1826-01, 501-1826-02 | ||
| MAG-3000 | Service Bulletin | SB501-1826-3 | Orig | 6/10/2004 | To prevent magnetization of unit during shipping, handling, installation, or re-packaging. | 501-1826-01, 501-1826-02 | ||
| MAG-3000 | Service Bulletin | SB501-1826-4 | C | 3/1/2007 | Product improvement. To reduce possibility of damage if aircraft installation location environmental conditions exceed RTCA DO-160B section 1.0 Category W (drip-proof). | 501-1826-01, 501-1826-02 | ||
| MAG-3000 | Service Bulletin | SB501-1826-6 | A | 9/19/2011 | MAG-3000 Product Improvement | 501-1826-02 | ||
| MAG-3000 | Service Letter | SL-272 | B | 9/20/2011 | MAG Install Software Update 1.05 | Update of MAG software To inform customers of software updates for the MAG Install Software. | 501-1826- 9200-21200-01 | |
| MAG-3000 | Service Letter | SL-291 | B | 9/24/2013 | MAG-3000 Extreme Temperature Fault | Extreme Temperature Fault | 501-1826, 501-1826-01, 501-1826-02, 501-1826-03, 501-1826-04, 501-1826-05, 501-1826-06, 501-1826-07, 9200-21200 | |
| MAG-3000 | Service Letter | SL-225 | A | 5/15/2007 | To provide customers with a procedure to check and calibrate the MAG-3000 magnetometer. | 501-1826-(), 501-1826-01, 501-1826-02, 501-1826-03 | ||
| MAG-3000 | Service Letter | SL-256 | A | 2/15/2010 | MAG-3000 Interchangeability | MAG-3000 Interchangeability | 501-1826-01, 501-1826-03, 501-1826-04 | |
| MAG-3000 | Service Letter | SL-183 | Orig | 11/14/2003 | Rejections in field due to visual inspections and mishandling of product. | 501-1826-01 | ||
| MAG-3100 | Installation Manual | TP-559 | K | 3/30/2017 | Installation and Operation Manual, GH-3100, SW 3.0 | This manual contains installation and operating information for the GH Electronic Standby Instrument System. Information in this manual includes the following products: GH-3100 Electronic Standby Indicator (with 1.3, 1.4 or 3.0 software), DCM-3100 Detachable configuration Module, and MAG-3000 / MAG-3100 Magnetometer. This information is supplemented and kept current by revisions, service letters and service bulletins. | 501-1826-01, 501-1826-02, 501-1860-0101, 501-1860-0103, 501-1860-0201, 501-1860-0203, 501-1860-0301, 501-1860-0303, 501-1860-0401, 501-1860-0403, 501-1860-0501, 501-1860-0503, 501-1860-0601, 501-1860-0603, 501-1860-0701, 501-1860-0703, 501-1860-1101, 501-1860-1103, 501-1860-1201, 501-1860-1203, 501-1860-1301, 501-1860-1303, 501-1860-1401, 501-1860-1403, 501-1860-1501, 501-1860-1503, 501-1860-1601, 501-1860-1603, 501-1860-1701, 501-1860-1703, 501-1860-1801, 501-1860-1803, 501-1860-2101, 501-1860-2103, 501-1860-2201, 501-1860-2203, 501-1870-( ) | |
| MAG-3100 | Installation Manual | 0040-34401-01 | AE | 5/27/2025 | GH-3900.2, Installation Manual | GH-3900.2 Electronic Standby Instrument System with Release 1.0, 1.1, 1.2, 1.3, 1.4, 1.5, 1.6, 1.7 , 1.8 & 1.9. Includes the ADC-4000 Air Data Computer and MAG-3000 or MAG-3100 Magnetometer. Details on Simulator unit’s P/N 9200-34701-( ) and 9200-34901-( ) are also provided. | 9200-34400-( ) 9200-34500-( ) 9200-34600-( ) 9200-34700-( ) 9200-34800-( ) 9200-34900-( ) 9200-34402-( ) 9200-34502-( ) 9200-34602-( ) 9200-34702-( ) 9200-34802-( ) 9200-34410-( ) | |
| MAG-3100 | Installation Manual | 0040-21200-01 | J | 9/5/2017 | MAG-3100 Installation Manual | MAG-3100 Install Manual | 9200-21200-( ), 9200-21200-01 | |
| MAG-3100 | Instruction Manual | TP-637 | E | 9/5/2013 | TP-637 | MAG INSTALL SOFTWARE | 576-6137, 9200-21200, 9200-21200-01 | |
| MAG-3100 | Service Bulletin | SB9200-21200-1 | A | 5/1/2014 | Incorporate new cable | Incorporate new cable , Acron Aviation | MAG-3100 | |
| MAG-3100 | Service Letter | SL-291 | B | 9/24/2013 | MAG-3000 Extreme Temperature Fault | Extreme Temperature Fault | 501-1826, 501-1826-01, 501-1826-02, 501-1826-03, 501-1826-04, 501-1826-05, 501-1826-06, 501-1826-07, 9200-21200 | |
| MAG-3100 | Service Letter | SL-272 | B | 9/20/2011 | MAG Install Software Update 1.05 | Update of MAG software To inform customers of software updates for the MAG Install Software. | 501-1826- 9200-21200-01 | |
| MAG-3100 | Software | MAG-3100 | 1.05 | 9/27/2011 | Mag Install Software | Mag Install Software | 576-6137 | |
| MAG-500 | Installation Manual | 0040-15001-01 | K | 4/29/2025 | ESI-500 /MAG-500 Installation Manual | Electronic Standby Indicator | 9200-15000-0101, 9200-15500-0101 | |
| MAG-500 | Installation Manual | 0040-15751-01 | G | 4/14/2025 | Installation Manual, EFD-750 / MAG-500 | Electronic Flight Display System EFD-750 Electronic Flight Display MAG-500 Magnetometer | 9200-15751-0101, 9200-15753-0101, 9200-15754-0101, 9200-15754-0201, 9200-15750-0101, 9200-15751-0201, 9200-15754-0301, 9200-15756-0301. 9200-15500-0101, 9200-15500-0201 | |
| MAG-500 | Pilot Guide | 0040-15750-01 | E | 4/14/2025 | Operation Manual, EFD-750 | Electronic Flight Display System | 9200-15753-0101, 9200-15754-0101, 9200-15754-0201, 9200-15751-0101, 9200-15751-0201, 9200-15750-0101, 9200-15756-0301. | |
| MAG-500 | Pilot Guide | 0040-15000-01 | G | 4/28/2025 | Pilot Guide, ESI-500 | Electronic Standby Instrument System, Acron Aviation | 9200-15000-0101, 9200-15500-0101 | |
| MAG-500 | Pilot Guide | 0040-15000-01 Printcopy | G | 4/28/2025 | Pilot Guide, ESI-500 Print copy | Electronic Standby Instrument System, Acron Aviation | 9200-15000-0101, 9200-15500-0101 | |
| MAG-500 | Supplemental Type Certificate | SA04046CH | D | 9/2/2020 | AML STC for ESI-500 | ESI-500 AML STC Package with ICA & AFMS (part 23) | 9200-15000-0101, 9200-15500-0101 | |
| MAG-500 | Supplemental Type Certificate | SR2487AK | 0 | 11/12/2016 | ESI-500 RW STC (part 27) | ESI-500 RW STC (part 27) | 9200-15000-01 | |
| MAT-3100 | Service Bulletin | SB9200-21250-1 | A | 5/1/2014 | New Cable Assembly | New Cable Assembly, Acron Aviation | 9200-21250-01 | |
| MW-701 | Component Maintenance Manual | TP-211 | 4/25/2018 | Multi Function Warning | Multi Function Warning | |||
| MW-701 | Service Bulletin | SB8-1000-1 | 7/26/2005 | SB8-1000-1 | ||||
| NACWS | Instruction Manual | 009-10084-001 | original | 9/16/1994 | Instruction Manual, SCD526 | Serial Communications Device. part of the Naval Aircraft Collision Warning System | 825-10023-001 | |
| NACWS | Miscellaneous | NACWS - N/A | x.x | 1/1/2023 | Information on NACWS | Traffic Alert and Collision Avoidance System (NACWS) NASWS 991 | 009-10042-001 009-10043-001 | |
| NACWS | Pilot Guide | 009-10033-001 | 2 | 5/22/1995 | Operator's Manual | Pub# 009-10033-001 | ||
| NACWS | Pilot Guide | 009-10132-001 | A | 1/28/2000 | Pilot's Guide | Pub# 009-10132-001 | ||
| NACWS | Service Bulletin | SB-95 | Orig | 8/27/2001 | NACWS Low PRF Radar Database update Version RD01M20D. The radar database has been updated with FAA published data for 2001 and with information developed from radar data collection flights by Goodrich Avionics Systems. The database now includes data for t | 805-10012-003, 805-10012-013 | ||
| NACWS | Service Bulletin | SB-94 | B | 8/19/2005 | NACWS Low PRF Radar Database update Version RD01M20D. The radar database has been updated with FAA published data for 2001 and with information developed from radar data collection flights by Goodrich Avionics Systems. The database now includes data for t | 805-10012-003, 805-10012-013 | ||
| NACWS | Service Bulletin | SB-93 | original | 8/19/2005 | Software 1.7 notice for NACWS | T-34 NACWS TRC691 Software Version 1.7 upgrade. Improve NACWS coverage by processing data from the new low PRF Secondary Surveillance Radar Equipment. | 805-10012-003 | |
| NY151 | Installation Manual | 009A0551B | 0 | 11/1/1983 | Installation Manual | Pub# 009A0551B | 805D0500, 805D0520, 805D0530, 805D0550-01, 805D0550-02, 805D0550-03, 805D0550-04 | |
| NY156 | Service Bulletin | SB-74 | C | 5/1/1997 | Modify the NY156 Antenna by installing the protective boot. | 805-10003-001 | ||
| NY156 | Service Letter | SL-139 | Orig | 9/17/1997 | To provide information on the limitations for warranty consideration. | 800-10254-002, 805-10003-001 | ||
| NY156 | Service Letter | SL-206 | B | 5/16/2018 | Remove tape holding O-RING in place before installing antenna on aircraft. | 805-10003-001, 805-10890-001 | ||
| NY162 | Miscellaneous | n/a | x.x | 4/14/2023 | NY162 L-Band Omnidirectional Antenna, information | NY162 L-Band Omnidirectional Antenna P/N 805-10033-( ) The L-band omni-directional antenna is a vertically polarized antenna certified for installation on aircraft with True Air Speed (TAS) up to 400 knots. The system can accommodate one or two L-band antennas, with connection to the TRC2634 Transceiver being made through a single TNC connector. contact fieldservice.avionics@L3harris.com for more in information. | 805-10033-001, 805-10033-002 | |
| NY163 | Miscellaneous | NY162-Reference | x.x | 4/14/2023 | NY162 L-Band Omnidirectional Antenna, information | See SL-346 Repair and service of the is transferred to Extant Aerospace. | 805-10930-001 805-10930-002 | |
| NY164 | Miscellaneous | n/a-1 | x.x | 1/1/2023 | Information on NY164 | See TCAS791 Installation Manual, P/N 009-10013-001 Also Lynx products. | 805-10890-001 | |
| NY164 | Service Letter | SL-206 | B | 5/16/2018 | Remove tape holding O-RING in place before installing antenna on aircraft. | 805-10003-001, 805-10890-001 | ||
| PA-377 | Component Maintenance Manual | TP-206 | Orig | 3/1/1970 | Instruction Manual | Pub# TP-206 | 501-1085-01, 501-1085-02 | |
| PB-1003 | Component Maintenance Manual | TP-348 | 24-50-01 | 1 | 6/5/2018 | Maintenance Manual with IPL | Pub# TP-348 | 501-1262-01, 501-1326-01 |
| PI/1 | Instruction Manual | 165E1630-00 | 07 | 9/30/2021 | PI/1 Operation Manual | PI/1 Operation Manual GSE Test Equipment | 17TES0043, 17TES0051, 17TES0052, 17TES0054, 17TES0074 | |
| PI/1 | Service Bulletin | PI/1 SB001 | Initial | 7/21/2003 | PI/1 MD 01-04, Optional Modification for Remote Playback | PI/1 MOD DOT 01, 02, 03, and 04, Acron Aviation | 17TES0043 17TES0143. | |
| PI/1 | Service Bulletin | PI/1 SB002 | Initial | 9/16/2003 | PI/1 MD 05, Modification for Cable Assembly | PI/1 MOD DOT 05, Acron Aviation | 17TES0043 17TES0143 | |
| PI/1 | Service Bulletin | PI/1 SB003 | Initial | 1/26/2010 | PI/1 MD 07, Compatibility with Data Link SSCVR | PI/1 MOD DOT 07, Acron Aviation | 17TES0043 17TES0143 | |
| PI/1 | Service Bulletin | PI/1 SB004 | Initial | 12/8/2009 | PI/1 MD 08, Replace Obsolete Parts & Software Upgrade | PI/1 MOD DOT 08, Acron Aviation | 17TES0043 17TES0143 | |
| PI/1 | Service Bulletin | PI/1 SB005 | 02 | 10/28/2015 | PI/1 MD 09, Modification Required for NAND Recorders | PI/1 MOD DOT 09, Acron Aviation | 17TES0043 17TES0143 | |
| PI/1 | Service Bulletin | PI/1 SB006 | Initial | 5/10/2018 | PI/1 MD 10, Introduction of Firmware v1.10 | PI/1 MOD DOT 10, Acron Aviation | 17TES0043 17TES0143 | |
| PI/1 | Service Bulletin | SB007-PI | 01 | 6/23/2022 | This service bulletin implements hardware modifications due to obsolete cable assembly. | MOD 11. To replace obsolete cable with new external interconnect cable assembly, Acron Aviation | 17TES0043 | |
| PI/1 | Service Letter | SIL-001-L3AP | 00 | 5/27/2021 | CVR audio data. | If synchronized CVR audio data is required, the .CVR format must be downloaded from the recorder. The .CVR format will produce synchronized audio between all channels | n/A | |
| PI/1 | Service Letter | SIL-001-PI1 | 01 | 7/11/2024 | Service Information Letter, PI-1 | Product and repair of Portable Interface Unit PI/1 used with Flight Recorders. | 17TES0043 | |
| PI/2 | Service Letter | SIL-001-L3AP | 00 | 5/27/2021 | CVR audio data. | If synchronized CVR audio data is required, the .CVR format must be downloaded from the recorder. The .CVR format will produce synchronized audio between all channels | n/A | |
| PI/2 | Service Letter | PI/2-001 | 03 | 2/12/2024 | Notification of discontinued product. | Notification of discontinued product. | 17TES0062, 17TES0065, 17TES0066, 17TES0092 | |
| PS-801 | Component Maintenance Manual | TP-205 | chg2 | 4/1/1974 | PS-801 Maintenance Manual | PS-801 Maintenance Manual | 16-1010-01, 16-1010-02 | |
| PS-801 | Service Letter | SL-4 | original | 2/22/1972 | Service Letter, Battery Maintenance | Battery Maintenance for PS-800 and PS-801 To provide information on PS-800/PS-801 battery maintenance. (Contact Learjet for parts and service). | 16-1010-01 16-1010-02 | |
| PS-828 | Component Maintenance Manual | TP-220 | 34-20-11 | Orig | 5/22/1985 | Operation, Installation, and Maintenance Manual | Pub# TP-220 | 501-1243-01, 501-1458-01 |
| QAR (uQAR) | Component Maintenance Manual | 165E2810-30 | 31-30-20 | 02 | 6/30/2023 | Component Maintenance Manual, MicroQAR | MicroQuick Access Recorder, Acron Aviation | QAR100-02-00, QAR100-03-00, QAR100-03-01, QAR100-04-00, QAR100-23-00, QAR100-34-00, QAR101-33-00, QAR110-35-00, QAR200-01-00, QAR200-02-00, QAR200-02-01, QAR200-02-03, QAR200-03-00, QAR200-03-01, QAR200-03-02, QAR200-03-04, QAR200-04-04, QAR200-05-04, QAR200-05-06, QAR200-25-00, QAR200-30-04, QAR200-33-00, QAR200-34-00, QAR200-35-04, QAR201-00-00, QAR201-02-00, QAR201-04-04, QAR201-05-14, QAR201-30-04, QAR201-33-00, QAR201-35-04, QAR201-65-11, QAR201-65-12, QAR201-65-13, QAR201-65-14, QAR210-05-00, QAR210-35-00, QAR210-35-04, QAR210-75-16, QAR210-75-17, QAR210-75-18 |
| QAR (uQAR) | Installation Aircraft Tools | 17TES0100 | V1.1 | 3/27/2018 | uQAR Application SW | App SW and Device Driver | 17TES0100 | |
| QAR (uQAR) | Installation Manual | 165E2810-00 | 31-30-21 | 11 | 12/15/2023 | Installation & Operation Manual, MicroQAR | MicroQuick Access Recorder QAR100-xx-xx, QAR101-xx-xx, QAR200-xx-xx, QAR201-xx-xx, QAR210-xx-xx, Acron Aviation | QAR100-02-00 QAR100-03-00 QAR100-03-01 QAR100-04-00 QAR100-23-00 QAR100-34-00 QAR101-33-00 QAR110-35-00 QAR200-01-00 QAR200-02-00 QAR200-02-01 QAR200-02-03 QAR200-03-00 QAR200-03-01 QAR200-03-02 QAR200-03-04 QAR200-04-04 QAR200-05-04 QAR200-05-06 QAR200-25-00 QAR200-30-04 QAR200-33-00 QAR200-34-00 QAR200-35-04 QAR201-00-00 QAR201-02-00 QAR201-04-04 QAR201-05-14 QAR201-30-04 QAR201-33-00 QAR201-35-04 QAR201-65-11 QAR201-65-12 QAR201-65-13 QAR201-65-14 QAR210-05-00 QAR210-35-00 QAR210-35-04 |
| QAR (uQAR) | Installation Manual | 165E2810-01 | 31-30-20 | 02 | 5/15/2018 | Installation and Operation Instruction Manual, QAR210-75-16 | microQAR QUICK ACCESS RECORDER, Acron Aviation | QAR210-75-16 |
| QAR (uQAR) | Installation Manual | 165E2810-03 | 31-30-20 | 02 | 5/15/2018 | Installation and Operation Instruction Manual, QAR210-75-17 | microQAR QUICK ACCESS RECORDER, Acron Aviation | QAR210-75-17 |
| QAR (uQAR) | Installation Manual | 165E2810-04 | 31-30-20 | 02 | 5/15/2018 | Installation and Operation Instruction Manual, QAR210-75-18 | microQAR QUICK ACCESS RECORDER, Acron Aviation | QAR210-75-18 |
| QAR (uQAR) | Service Bulletin | QAR210-75-16 SB001 | original | 5/15/2018 | SB001, Service Bulletin for SW 1 | QAR210‐75‐16‐001 SW 1: INTRODUCTION OF SOFTWARE UPDATE REVISION (Version 429) | QAR210-75-16 | |
| QAR (uQAR) | Service Bulletin | QAR210-75-17 SB001 | original | 5/15/2018 | SB001, Service Bulletin for SW 1 | QAR210‐75‐17‐001 SW 1: INTRODUCTION OF SOFTWARE UPDATE REVISION (Version 429) | QAR210-75-17 | |
| QAR (uQAR) | Service Bulletin | QAR210-75-18 SB001 | original | 5/15/2018 | SB001, Service Bulletin for SW 1 | QAR210‐75‐18‐001 SW 1: INTRODUCTION OF SOFTWARE UPDATE REVISION (Version 429) | QAR210-75-18 | |
| QAR (uQAR) | Service Bulletin | UQAR-SB001 | 31-30-20-001 | 03 | 12/1/2008 | SB001, MOD 1 and SW03 | HARDWARE MODIFICATION 1 OF THE uQAR, AND SOFTWARE REVISION R3 | QAR100-xx-xx, QAR20X-xx-xx |
| QAR (uQAR) | Service Bulletin | UQAR-SB002 | 31-30-20-002 | 03 | 5/5/2018 | SB002, SW04 | INTRODUCTION OF SOFTWARE UPDATE REVISION 04 OF THE uQAR | QAR100-xx-xx, QAR200-xx-xx, QAR201-xx-xx |
| QAR (uQAR) | Service Bulletin | UQAR-SB003 | 31-30-20-003 | 03 | 6/23/2010 | SB003, New Memory Card | INTRODUCTION OF 25304000-05 MEMORY CARD. Due to controlled obsolescence, memory cards of less than 512 MB capacity are no longer available for the uQAR. | QAR10X-xx-xx, QAR20X-xx-xx |
| QAR (uQAR) | Service Bulletin | UQAR-SB004 | 31-30-20-004 | original | 6/23/2010 | SB004, SW05 | Quick Access Recorder INTRODUCTION OF SOFTWARE UPDATE REVISION 05 | QAR100-xx-xx, QAR200-xx-xx, QAR201-xx-xx |
| QAR (uQAR) | Service Bulletin | UQAR-SB005 | 31-30-20-005 | original | 9/9/2010 | SB005, New Memory card | INTRODUCTION OF 2530400006 MEMORY CARD AND uQAR SOFTWARE CHANGE 2530400006 Memory Card | QAR100-xx-xx, QAR200-xx-xx, QAR201-xx-xx |
| QAR (uQAR) | Service Bulletin | UQAR-SB006 | 31-30-20-006 | original | 6/1/2020 | SB006, MOD 3 | INTRODUCTION OF MOD DOT 3. For future firmware updates, the capacity of U006 increased from 8K to 16K. | QAR100-xx-xx, QAR200-xx-xx, QAR201-xx-xx |
| QAR (uQAR) | Service Bulletin | UQAR-SB007 | 31-30-20-07 | original | 5/15/2018 | SB007, software update | INTRODUCTION OF SOFTWARE UPDATE REVISION This Software Revision introduces prepping of the memory card at power on. This ensures that the microQAR is ready when 429 data begins, and that all valid data is written. | QAR201−65−11, QAR201−65−12, QAR201−65−13 |
| QAR (uQAR) | Service Bulletin | UQAR-SB008 | original | 5/15/2018 | SB008, update software | INTRODUCTION OF SOFTWARE UPDATE REVISION SanDisk Extreme III memory cards previously used with these microQARs are no longer available. This Software Revision allows the use of newer SanDisk Ultra memory cards. | QAR201−65−11, QAR201−65−12, QAR201−65−13 | |
| QAR (uQAR) | Service Bulletin | UQAR-SB009 | 31-30-20 | 00 | 4/22/2020 | SB009-MD04-Inspection and Replacement of SanDisk Compact Flash Card | SB009-MD04-Inspection and Replacement of SanDisk Compact Flash Card | QAR100-03-01 QAR100-34-00 QAR101-33-00 QAR110-35-00 |
| QAR (uQAR) | Service Letter | SIL002-QAR | Orig | 11/15/2005 | FLASH CARD REPLACEMENT | USERS OF THE MICRO QUICK ACCESS RECORDER, MODELS QAR200, ALL PART NUMBERS | QAR200–00–XX 253-04-0001 253-04-0002 253-04-0003 253-04-0004 | |
| QAR (uQAR) | Supplemental Type Certificate | ST02706AT | A | 10/12/2021 | Supplemental Type Certificate, ST02706AT, QAR, | Installation of micro Quick Access recorder (QAR) | QAR100-( ) QAR101-( ) QAR200-( ) QAR201-( ) | |
| QAR (uQAR) | Supplemental Type Certificate | ST03560AT | A | 1/20/2022 | Supplemental Type Certificate | Micro QAR in MD-80 Series Aircraft | 905E7008-20 | |
| RAU | Installation Manual | 165E4049-00 | 01 | 10/25/2007 | CICC/3 Installation Sheet | Installation Instructions for using CICC3 The CICC/3 requires Rose 3.8 or higher on a PC running Windows XP SP2. | 17TES0075 | |
| RAU | Instruction Manual | 165E1696-04 | 02 | 11/30/2022 | Operator's Manual, (ROSE) SW Version 4.7 and later | Operations Manual, Read-Out Support Equipment / Recorder Interface, 4.7 or later (ROSE) | 17TES00321, 17TES0060ROSE, 17TES0063, 17TES0700, 883E1894−01 | |
| RAU | Instruction Manual | 165E1696-02 | 03 | 3/1/2007 | Operator's Manual, SW Version 3.0 | Read-Out Support Equipment / Recorder Interface, 3.0 | 17TES0055, 17TES0060, 17TES0063, 17TES0300, 17TES0321, 17TES0400, 883E1894−01 | |
| RAU | Miscellaneous | ROSE Analysis Unit (RAU) | x.x | 1/1/2023 | Information on RAU | ROSE Analysis Unit (RAU) | 17TES0055 17TES0060 17TES0063 17TES0068 17TES0700 17TES0060 17TES0063 17TES0321 883E1894-01 | |
| RAU | Service Letter | SIL-001-RAU | 00 | 1/14/2021 | Notification of end of production and sale of the ROSE Analysis Unit. | Notification of end of production and sale of the ROSE Analysis Unit. | 17TES0055, 17TES0060, 17TES0063, 17TES0068 | |
| RDI | Installation Aircraft Tools | RDI Software Release 2.x | 2.1 | 11/12/2020 | Recorder Data Interface | Recorder Data Interface | 17TES0823 | |
| RDI | Instruction Manual | 165E6496-00 | 08 | 7/31/2024 | Recorder Data Interface (RDI) Instruction Manual | Recorder Data Interface (V2.1) & (V3.0) | (V2.1) & (V3.0) 17TES0800, 17TES0900 (V2.1 only) 17TES0901, 17TES0950, 17TES0960. Configuration ID: 8010-18001-xxxx, 8010-18003-xxxx | |
| RDI | Miscellaneous | T800-SDS | 0 | 3/28/2024 | RDI-T800 Main Battery SDS | Getac SDS LI01122021006P01 Rechargeable Lithium Ion / Polymer Battery | T800 | |
| RDI | Miscellaneous | T800-UN38.3 | 0 | 3/28/2024 | RDI-T800 Test Summary | GETAC T800 UN38.3 Test summary | T800 | |
| RDI | Service Bulletin | SB002-RDI | 00 | 3/19/2024 | Service Bulletin, RDI - Version 3.0 | RDI - Version 3.0 | 17TES0823 | |
| RDI | Service Bulletin | SB001-RDI | 00 | 10/5/2021 | RDI - Version 2.1 | RDI - Version 2.1 | 17TES0900, 17TES0901, 17TES0950, 17TES0960 | |
| RDI | Service Letter | SIL-001-L3AP | 00 | 5/27/2021 | CVR audio data. | If synchronized CVR audio data is required, the .CVR format must be downloaded from the recorder. The .CVR format will produce synchronized audio between all channels | n/A | |
| Recorder - Accessories | Component Maintenance Manual | 165E1747-00 | 23-70-05 | 11 | 4/23/2024 | ED-56A Control Units Pre Amplifiers & Microphones CMM | ED−56A CONTROL UNITS, PREAMPLIFIER MODULE, AND MICROPHONE MODULES FOR SOLID−STATE COCKPIT VOICE RECORDERS (SSCVR) SCVR CONTROL UNITS MODELS S151/S161, S152/S162, AND S251/S261 SSCVR PREAMPLIFIER MODULE MODEL S150/S160 SSCVR MICROPHONE MODULES MODELS S055, S056 AND S058 CONTROL UNIT MICROPHONE PREAMPLIFIER MODULE REMOTE MICROPHONE MODULES, Acron Aviation | S151−0020−00 S161−0020−00 S162−0020−00 S151−0030−00 S161−0020−10 S162−0030−00 S151−0040−00 S161−0030−00 S162−0040−00 S151−0050−00 S161−0040−00 S251−1120−00 S151−0060−00 S161−0050−00 S251−1130−00 S152−0020−00 S161−0060−00 S251−1170−00 S152−0020−01 S161−0080−00 S261−1120−00 S152−0030−00 S161−0090−00 S261−1130−00 S152−0030−01 S161−0090−02 S261−0050−00 S152−0040−00 S161−1120−10 S261−1121−00 S161−1390−01 S161−1390−02 S161−1390−03 S161−1090−20 S150−0020−00 S160−0020−00 S150−0020−00 S160−0030−00 S055−0030−00 S056−0048−00 S058−0048−00 S055−0065−00 S056−0048−10 S058−0048−01 S055−0066−00 S056−0048−15 S058−0148−10 S055−0067−00 S056−0049−00 S055−0067−01 S056−0050−00 S055−0068−00 S056−0051−00 S056−0030−00 S056−1048−00 S056−0047−00 |
| Recorder - Accessories | Service Bulletin | 23‐70‐05‐001 | 23‐70‐05 | Initial | 8/22/2013 | SB001-Introduction of S152−0020−01 Control Unit | SB001-Introduction of S152−0020−01 Control Unit Used in Boeing NG Aircraft. | S152−0020−01 |
| RG-225 | Service Letter | SL-174 | A | 4/3/2015 | To provide Avionics Systems, Inc service centers and maintenance personnel with storage information for gyro products. [Replaces SL-113, SL-131, SL-168, SA-89]. | Remove references to AIM Series Gyros. | ||
| RGC250 | Installation Manual | 009-11400-001 | A C4 | 7/27/2000 | Installation Manual | Pub# 009-11400-001 | 805-11400-001, 805-11400-002 | |
| RGC250 | Installation Manual | 009-11407-001 | A | 3/14/2002 | Installation Manual | Pub# 009-11407-001 | 805-11400-003, 805-11400-004 | |
| RGC250 | Pilot Guide | 009-11401-001 | A | 10/9/1998 | Pilot's Guide | Pub# 009-11401-001 | 805-11400-00X | |
| RGC250 | Service Bulletin | SB-91 | Orig | 1/26/2001 | To provide additional protection against damge to the RGC connectors when disengaging the mating connector assembly for the RGC. | 805-11400-001, 805-11400-002 | ||
| RGC250 | Supplemental Type Certificate | SA01034CH | Reis | 2/17/2004 | Installation of RGC250 radar graphics computer. | Installation of RGC250 radar graphics computer. | ||
| RGC250 | Supplemental Type Certificate | SA01034CH-FMS | Reis | 2/17/2004 | Installation of RGC250 radar graphics computer. | Installation of RGC250 radar graphics computer. | ||
| RGC250 | Supplemental Type Certificate | SA01034CH | Reis | 2/17/2004 | Installation of RGC250 radar graphics computer. | Installation of RGC250 radar graphics computer. | ||
| RGC250 | Supplemental Type Certificate | SA01034CH-FMS | Reis | 2/17/2004 | Installation of RGC250 radar graphics computer. | Installation of RGC250 radar graphics computer. | ||
| RGC250 | Supplemental Type Certificate | SA01034CH | Reis | 2/17/2004 | Installation of RGC250 radar graphics computer. | Installation of RGC250 radar graphics computer. | ||
| RGC350 | Installation Manual | 009-12400-001 | A | 6/25/2002 | Installation Manual | Pub# 009-12400-001 | 805-12400-001, 805-12400-002 | |
| RGC350 | Pilot Guide | 009-12401-001 | B | 8/26/2003 | Pilot's Guide | 805-12400-001, 805-12400-002 | ||
| RGC350 | Service Bulletin | SB-128 | Orig | 1/22/2004 | Software upgrade to the RGC350 firmware. Corrects possible RGC350 failure when connected to an L-3 TAWS8000 and a Honeywell Primus Weather Radar Indicator. | 805-12400-( ) | ||
| RGC350 | Service Letter | SL220 | A | 4/26/2007 | Permission to use STC | Permission to use STC | 805-12400-( ), 805-12400-001, 805-12400-002 | |
| RGC350 | Supplemental Type Certificate | SA01034CH | Reis | 2/17/2004 | Installation of RGC250 radar graphics computer. | Installation of RGC250 radar graphics computer. | ||
| RGC350 | Supplemental Type Certificate | SA01034CH-FMS | Reis | 2/17/2004 | Installation of RGC250 radar graphics computer. | Installation of RGC250 radar graphics computer. | ||
| RGC350 | Supplemental Type Certificate | SA01034CH | Reis | 2/17/2004 | Installation of RGC250 radar graphics computer. | Installation of RGC250 radar graphics computer. | ||
| RGC350 | Supplemental Type Certificate | SA01034CH-FMS | Reis | 2/17/2004 | Installation of RGC250 radar graphics computer. | Installation of RGC250 radar graphics computer. | ||
| RGC350 | Supplemental Type Certificate | SA01034CH | Reis | 2/17/2004 | Installation of RGC250 radar graphics computer. | Installation of RGC250 radar graphics computer. | ||
| RGC350 | Supplemental Type Certificate | SA01034CH-FMS | Reis | 2/17/2004 | Installation of RGC250 radar graphics computer. | Installation of RGC250 radar graphics computer. | ||
| RGC350 | Supplemental Type Certificate | SA01034CH-FMS | Reis | 2/17/2004 | Installation of RGC250 radar graphics computer. | Installation of RGC250 radar graphics computer. | ||
| RGC350 | Supplemental Type Certificate | SA01034CH | Reis | 2/17/2004 | Installation of RGC350 radar graphics computer. | Installation of RGC350 radar graphics computer. | ||
| RIPS | Component Maintenance Manual | 165E5398-01 | 23-70-35 | 05 | 1/30/2025 | FA5000 Cockpit Voice Recorder CMM | FA5000 CVR CMM RIPS | 5001-5003-11, 5003-5003-11, 5033-5003-11, 5053-5003-11. 500−4030−000 |
| RIPS | Installation Manual | 165E5327-04 | 02 | 4/30/2024 | Installation and Operation Instruction Manual, FA5000 CVDR | COCKPIT VOICE AND DATA RECORDER MODEL FA5000 CVDR ARINC 757 | 5003−6100−00 RIPS Part Number: 500−4030−000 | |
| RNAV | Pilot Guide | 002A0449A | A | 2/1/1982 | Pilot's Guide | Pub# 002A0449A | 805D0450 | |
| RNAV | Pilot Guide | 002A0490 | Orig | 7/26/2005 | Pilot's Guide | Pub# 002A0490 | 805D0450 | |
| RNAV | Service Bulletin | SB-52 | Orig | 11/1/1985 | Modification to Range Block Adapter Module to permit operation throughtout voltage range. | , Acron Aviation | 804B0116 | |
| RNAV | Service Bulletin | SB-51 | Orig | 8/1/1985 | Modification to DME Range Block Adapter Module to increase A+ voltage range. | , Acron Aviation | 804B0116 | |
| RNAV | Service Bulletin | SB-511-B | 10/1/1978 | B | 805D0200 | |||
| RNAV | Service Bulletin | SB-511-C | Orig | 10/1/1978 | To prevent intermittent errors in measured DME Distance resulting in erroneous RNAV computations. | 805D0200 | ||
| RNAV | Service Bulletin | SB-51ASA-1-A | Orig | 10/1/1979 | Allows Range Monitor switch to be accomplished by KDI572 NAV select switch. | 805D0254 | ||
| RNAV | Service Bulletin | SB-51ASA-B | Orig | 6/1/1979 | To allow course softening to be disable as an installer option. | 805D0251 | ||
| RNAV | Service Bulletin | SB-51DSA-A | Orig | 6/1/1980 | Elliminates COMM transmitter RF interference to RNAV511/51DSA, and reduces To/From meter drive current. | 805D0250 | ||
| RNAV | Service Bulletin | SB-51DSA-B | Orig | 6/1/1979 | To reduce the required sink current on the NAV SELECT LINE to permit NAV selection by the KDI-572. | , Acron Aviation | 805D0250 | |
| RNAV | Service Bulletin | SB-31 | Orig | 1/1/1982 | Slow groundspeed response; Autopilot S-turning; false ground on annunciate output lines; loss of present position readout in range monitor mode | , Acron Aviation | 805D0450 | |
| RNAV | Service Bulletin | SB-34 | Orig | 10/1/1982 | Prevent random "auto shutdown" of RNAV612 microprocessor. | , Acron Aviation | 805D0450 | |
| RNAV | Service Bulletin | SB-35 | Orig | 11/1/1982 | Reduces VOR smoothing time constant in approach mode. | , Acron Aviation | 805D0450 | |
| RNAV | Service Bulletin | SB-36 | A | 1/1/1983 | Increase input level range of 51ASA-1 9960Hz input signal. | , Acron Aviation | 805D0254 | |
| RNAV | Service Bulletin | SB-37 | A | 1/1/1983 | Increases input signal range of 51ASA 9960Hz input signal. | , Acron Aviation | 805D0251 | |
| RNAV | Service Bulletin | SB-23 | Orig | 4/1/1981 | Prevent momentary RNAV annunciate output during turn-on | , Acron Aviation | 805D0450 | |
| RNAV | Service Bulletin | SB-24 | Orig | 4/1/1981 | RNAV612 Microprocessor Program Corrections and Improvements. | , Acron Aviation | 805D0450 | |
| RNAV | Service Bulletin | SB-25 | Orig | 4/1/1981 | Momentary VOR Diagnostic for RNAV612 | , Acron Aviation | 805D0450 | |
| RNAV | Service Bulletin | SB-26 | Orig | 4/1/1981 | Com Transmitter RF Interference in 51DSA and 51DSA/C328 | , Acron Aviation | 805D0250 | |
| RNAV | Service Bulletin | SB-27 | Orig | 5/1/1981 | Momentary RNAV annunciate output during turn-on/turn-off and DME Hold diagnostic in VOR/LOC operation. | , Acron Aviation | 805D0450 | |
| RNAV | Service Bulletin | SB-29 | Orig | 5/1/1981 | RNAV612 and 612RIU distance computation error when VNAV541 or VNAV541A has no A+ applied. | , Acron Aviation | 805D0400 | |
| RNAV | Service Bulletin | SB-47 | Orig | 8/1/1985 | Modification to DME Range Block Adapter to permit module to operate throughout an input range. | , Acron Aviation | 804B0001 | |
| RNC6000 | Supplemental Type Certificate | SA00810CH | Reis | 2/17/2004 | Installation of BFGoodrich LNS6000 navigation system with RNC6000A remote navigation computer | BFGoodrich LNS6000/ 6000A STC | ||
| RNC6000 | Supplemental Type Certificate | SA00810CH-FMS | Reis | 2/17/2004 | Installation of BFGoodrich LNS6000 navigation system with RNC6000A remote navigation computer | BFGoodrich LNS6000 FMS | ||
| RNC601 | Component Maintenance Manual | 009A0550 | Orig | 8/1/1985 | Installation and Maintenance Manual | Pub# 009A0550 | 805D0500, 805D0520, 805D0530, 805D0550-( ), 805D0570, 805D0580 | |
| RNC601 | Installation Manual | 009A0551B | 0 | 11/1/1983 | Installation Manual | Pub# 009A0551B | 805D0500, 805D0520, 805D0530, 805D0550-01, 805D0550-02, 805D0550-03, 805D0550-04 | |
| RNC601 | Service Bulletin | SB-46 | Orit | 9/1/1984 | To eliminate wavering left/right needle and erratic OBS operation. | , Acron Aviation | 805D0550 | |
| RNC601 | Service Bulletin | SB-38 | Orig | 11/1/1983 | Provide DC Sine/Cosine RMI Drive provided at RNC601 J1. | , Acron Aviation | 805D0550 | |
| RNC601 | Service Bulletin | SB-39 | Orig | 11/1/1983 | Corrects missing foil run on PC Board and decreases low level flag to 0.7vdc. | , Acron Aviation | 805D0550 | |
| RNC601 | Service Bulletin | SB-44 | Orig | 6/1/1984 | To allow the RNC601 to communicate with the DI681 DataBase. | , Acron Aviation | 805D0550 | |
| RNC601 | Service Bulletin | SB-45 | Orig | 9/1/1984 | Improvement of Automatic Ident Decoding | , Acron Aviation | 805D0550 | |
| RNC601 | Service Bulletin | SB-49 | Orig | 10/1/1984 | Eliminate intermittent display blanking | , Acron Aviation | 805D0550 | |
| RNC601 | Service Bulletin | SB-56 | Oig | 3/1/1987 | To allow the RNC601 and RNC601A to operate with the same functions as the RNC601B. | , Acron Aviation | 805D0550 | |
| RNC601 | Service Bulletin | SB-57 | Orig | 2/1/1988 | To allow DI681 to operate as DI681A with RNC601B. | , Acron Aviation | 805D0570 | |
| RT-1634(V) | Installation Manual | 009-10062-001 | L | 9/26/2018 | Installation Manual, TACAN | AN/ARN-154(V) | 805D0602-46, 805D0602-30, 805D0602-31, 805D0602-32, 805D0602-33, 805D0602-34, 805D0602-35, 805D0602-36, 805D0602-38, 805D0602-39, 805D0602-42, 805D0602-43, 805D0602-44, 805D0602-45, 805D0602-51, 805D0602-52, 805D0602-60 | |
| RT-1634(V) | Pilot Guide | 009-10138-001 | F | 9/1/2009 | Pilot's Guide | Pub# 009-10138-001 | 805D0602-() | |
| RT-1634(V) | Service Bulletin | SB-70 | Orig | 8/1/1996 | Software update to re-enable automatic antenna switching following pilot- initiated self test. | Software update to re-enable automatic antenna switching following pilot- initiated self test. | 805D0602-30, 805D0602-32, 805D0602-34, 805D0602-35, 805D0602-36, 805D0602-50 | |
| RT-1634(V) | Service Bulletin | SB805D0602-200 | A | 11/9/2004 | Software version 2.4 | Software version 2.4 adds label 002 and 0012 to ARINC 429 output bus #2 to Tracking Channel C. It also changes output label 035 bits 14 and 15 to match corresponding bits on input label 035., Acron Aviation | 805D0602-45 | |
| RT-1634(V) | Service Bulletin | SB805D0602-201 | A | 3/10/2005 | Service Bulletin, RT-1634 | Replace C2 on power supply from 100 V to 125 V part., Acron Aviation | 805D0602-39, 805D0602-43, 805D0602-44, 805D0602-45, 805D0602-51 | |
| RT-1634(V) | Service Bulletin | SB-97 | Orig | 2/4/2002 | single-port ARINC-429 RT-1634(V) | To make the single-port ARINC-429 RT-1634(V) TACAN's compatible with the U.S. Army Model A2D (AMCOM DWG P/N 1000484) 1553 to 429 converter. | 805D0602-31, 805D0602-32, 805D0602-35, 805D0602-38, 805D0602-42 | |
| RT-1634(V) | Service Bulletin | SB805D0602-205 | A | 5/17/2006 | Software Upgrade Version 2.5 and 2.6 | Software Upgrade Version 2.5 and 2.6, Acron Aviation | 805D0602-45 | |
| RT-1634(V) | Service Bulletin | SB805D0602-204 | A | 11/17/2005 | Modulator PCB Modification | Modulator PCB Modification, Acron Aviation | 805D0602-43, 805D0602-44, 805D0602-45, 805D0602-51, 805D0602-52 | |
| RT-1634(V) | Service Bulletin | SB805D0602-206 | A | 6/21/2006 | Software Upgrade Version 2.1 | Software Upgrade Version 2.1, Acron Aviation | 805D0602-51 | |
| RT-1634(V) | Service Bulletin | SB805D0602-207 | A | 6/21/2006 | Software Upgrade Revision 2.1 | Software Upgrade Revision 2.1, Acron Aviation | 805D0602-52 | |
| RT-1634(V) | Service Bulletin | SB805D0602-202 | B | 6/15/2006 | Power Supply Inductor Modification | Power Supply Inductor Modification, Acron Aviation | 805D0602-30, 805D0602-31, 805D0602-32, 805D0602-33, 805D0602-34, 805D0602-35, 805D0602-36, 805D0602-38, 805D0602-39, 805D0602-42, 805D0602-43, 805D0602-44, 805D0602-45, 805D0602-50, 805D0602-51, 805D0602-52 | |
| RT-1634(V) | Service Bulletin | SB805D0602-203 | B | 6/15/2006 | Modulator PCB Modification | Change capacitors C502 and C503 on the Modulator PCB from metal film polycarbonate to ceramic., Acron Aviation | 805D0602-( ) | |
| RT-1634(V) | Service Bulletin | SB-98 | Orig | 4/9/2002 | Interface compatibility | Makes interface of RT-1634(V)-43 TACAN compatible with the Wulfsberg Electronics RMS 555 and Honeywell FPD 500 EFIS systems | 805D0602-43 | |
| RT-1634(V) | Service Bulletin | SB-131 | C | 6/15/2006 | TACAN, Low-Pass Filter Modification | Mod adds a low pass filter to the synthesizer PCB Assembly. (Mod will improve the condition of the VCO input signal). | 805D0602( ) | |
| RT-1634(V) | Service Bulletin | SB-126 | Orig | 11/12/2003 | Software version 2.3 | Software version 2.3 has been released. Upgrade synchronizes the regenerated audio ident output from the RT-1634 with the ident transmission from ground stations. | 805D0602-45 | |
| RT-1634(V) | Service Bulletin | SB-118 | Orig | 5/20/2003 | software version 2.6 | This upgrade adds Tracking Channel C (input and output) to ARINC 429 Bus #1. This upgrade will be identified as software version 2.6 on the serial number ID tag. | 805D0602-43 | |
| RT-1634(V) | Service Bulletin | SB-122 | Orig | 8/18/2003 | Software version 2.1 followed by an additional upgrade to version 2.2 has been released. | Software version 2.1 followed by an additional upgrade to version 2.2 has been released. | 805D0602-45 | |
| RT-1634(V) | Service Bulletin | SB-106 | Orig | 10/24/2002 | Correct the "Hold Mode" status of the ARINC-429 echo label. | 805D0602-43 | ||
| SA-500 | Service Letter | SL-102 | Orig | 11/4/1987 | To provide information for the proper method of adjusting the brush block to armature contact and general burn-in requirements. | To provide information for the proper method of adjusting the brush block to armature contact and general burn-in requirements. | 501-1067-( ), 501-1112-( ), 501-1212-( ) | |
| SCD526 | Installation Manual | 009-10084-001 | Orig | 9/16/1994 | Instruction Manual | Pub# 009-10084-001 | 825-10023-001 | |
| SCD526 | Instruction Manual | 009-10084-001 | original | 9/16/1994 | Instruction Manual, SCD526 | Serial Communications Device. part of the Naval Aircraft Collision Warning System | 825-10023-001 | |
| SCR-750 | Component Maintenance Manual | TP-208 | C1 | 12/1/1970 | Instruction Manual | Pub# TP-208 | 2-1005-01, 2-1005-02 | |
| SHSI-3000 | Installation Manual | TP-600 | C | 8/2/2011 | Installation and Operation Manual | Pub# TP-600 | 501-1899-01 | |
| SHSI-3000 | Service Bulletin | SB501-1899-1 | C | 1/3/2007 | To reduce the possibility of the display blanking or failing at start up. | 501-1899-01 | ||
| SHSI-3000 | Service Bulletin | SB501-1899-2 | A | 3/15/2006 | To correct color and knob operation. | 501-1899-01 | ||
| SHSI-3000 | Service Bulletin | SB501-1899-3 | A | 3/15/2006 | To correct knob action at start up. | 501-1899-01 | ||
| SHSI-3000 | Service Bulletin | SB501-1899-7 | A | 6/25/2009 | To provide replacement display due to diminishing source. | To provide replacement display due to diminishing source. | 501-1899-01 | |
| SHSI-3000 | Service Bulletin | SB501-1899-6 | B | 6/25/2009 | To provide replacement display due to diminishing source. | MOD 6 superseded by MOD 7 | 501-1899-01 | |
| SHSI-3000 | Service Bulletin | SB501-1899-7 | A | 6/26/2009 | To provide replacement display due to diminishing source. | To provide replacement display due to diminishing source. | 501-1899-01 | |
| SIM-1000 | Service Bulletin | SB9200-32800-1 | B | 1/29/2013 | SIM-1000 - MOD A | To standardize DSP boards across ESI product line. Acron Aviation | 9200-32800-201 | |
| SIM-1000 | Service Bulletin | SB9200-32800-2 | B | 1/29/2013 | SIM-1000 - MOD B | Improve backlight low end brightness characteristics. Acron Aviation | 9200-32800-201 | |
| SIM-3000 | Service Bulletin | SB501-1827-14 | A | 2/28/2012 | To improve low light level calibration linearity | 501-1827-3103 | ||
| SIM-3000 | Service Bulletin | SB501-1827-16 | B | 4/19/2013 | Inspect for SUP | Inspect for SUP | 501-1827-0103, 501-1827-0203, 501-1827-07, 501-1827-08, 501-1827-09, 501-1827-2103, 501-1827-2104, 501-1827-2105, 501-1827-2193, 501-1827-2203, 501-1827-2293, 501-1827-2405, 501-1827-2503, 501-1827-2603, 501-1827-3103, 501-1827-3293 | |
| SIM-3000 | Service Bulletin | SB501-1827-17 | A | 11/6/2014 | Display Replacement | Display Replacement | 501-1827-0103 | |
| SIM-3000 | Service Bulletin | SB501-1827-13 | A | 3/18/2010 | Planning Information | 501-1827-2104 | ||
| SIM-3000 | Service Bulletin | SB501-1827-11 | B | 12/1/2008 | Provide replacement display due to diminishing source. | Provide replacement display due to diminishing source. | 501-1827-2302, 501-1827-2402 | |
| SIM-3000 | Service Bulletin | SB501-1827-9 | B | 11/24/2008 | Provide replacement display due to diminishing source. | 501-1827-2103, 501-1827-2104, 501-1827-2193, 501-1827-2203, 501-1827-2293, 501-1827-2503, 501-1827-2603 | ||
| SIM-3000 | Service Bulletin | SB501-1827-8 | A | 2/15/2006 | To reduce the possibility of the display blanking or disruption. | 501-1827-0103, 501-1827-0203, 501-1827-0283, 501-1827-07, 501-1827-08, 501-1827-2103, 501-1827-2104, 501-1827-2193, 501-1827-2203, 501-1827-2293, 501-1827-2503, 501-1827-2603 | ||
| SIM-3000 | Service Bulletin | SB501-1827-7 | B | 2/3/2006 | To reduce the possibility of the display blanking or failing at start up. | 501-1827-0103, 501-1827-0203, 501-1827-0283, 501-1827-07, 501-1827-08, 501-1827-2103, 501-1827-2104, 501-1827-2193, 501-1827-2203, 501-1827-2293, 501-1827-2503, 501-1827-2603 | ||
| SIM-3000 | Service Bulletin | SB501-1827-2 | Orig | 3/14/2003 | Improve durability of keyboard assembly. | 501-1827-01, 501-1827-02, 501-1827-03, 501-1827-04, 501-1827-06, 501-1827-2302, 501-1827-2402 | ||
| SIM-3000 | Service Bulletin | SB501-1827-4 | A | 1/3/2007 | Provide replacement display due to diminishing source. | 501-1827-2103, 501-1827-2193, 501-1827-2203, 501-1827-2302, 501-1827-2402, 501-1827-2503, 501-1827-2603 | ||
| SIM-3000 | Service Letter | SL-334 | A | 8/14/2018 | End of Production Notice | Service Letter | 501-1827, 501-1891, 501-1903 | |
| SIM-3001 | Service Bulletin | SB501-1827-16 | B | 4/19/2013 | Inspect for SUP | Inspect for SUP | 501-1827-0103, 501-1827-0203, 501-1827-07, 501-1827-08, 501-1827-09, 501-1827-2103, 501-1827-2104, 501-1827-2105, 501-1827-2193, 501-1827-2203, 501-1827-2293, 501-1827-2405, 501-1827-2503, 501-1827-2603, 501-1827-3103, 501-1827-3293 | |
| SIM-3001 | Service Bulletin | SB501-1827-15 | A | 10/19/2012 | Software Release 2.2 | Software Release 2.2 | 501-1827-07 | |
| SIM-3002 | Service Bulletin | SB501-1827-16 | B | 4/19/2013 | Inspect for SUP | Inspect for SUP | 501-1827-0103, 501-1827-0203, 501-1827-07, 501-1827-08, 501-1827-09, 501-1827-2103, 501-1827-2104, 501-1827-2105, 501-1827-2193, 501-1827-2203, 501-1827-2293, 501-1827-2405, 501-1827-2503, 501-1827-2603, 501-1827-3103, 501-1827-3293 | |
| SIM-3100 | Installation Manual | TP-619 | A | 5/22/2006 | Installation and Operation Manual, for P/N 501-1891-( ) | SIM-3100 - ESIS Simulator | 501-1891-0102 | |
| SIM-3100 | Installation Manual | TP-632 | A | 12/9/2009 | Installation and Operation Manual, for P/N 501-1903-( ) | SIM-3100 - ESIS Simulator | 501-1903-0101, 501-1903-0201, 501-1903-0301, 501-1903-0401, 501-1903-2101, 501-1903-2103, 501-1903-2201 | |
| SIM-3100 | Service Bulletin | SB501-1891-1 | Orig | 5/20/2004 | Manufacturing Change. Producing a universal Lighting controller. | 501-1891-0102 | ||
| SIM-3100 | Service Bulletin | SB501-1891-2 | A | 2/3/2006 | Service bulletin, MOD 2 | To reduce the possibility of the display blanking or failing at start up. | 501-1891-0102 | |
| SIM-3100 | Service Bulletin | SB501-1891-3 | B | 11/24/2008 | Service Bulletin, MOD 3 | Provide replacement display due to diminishing source. | 501-1891-0102 | |
| SIM-3100 | Service Bulletin | SB501-1891-4 | 12/26/2007 | RELEASE OF SOFTWARE 2.1 | RELEASE OF SOFTWARE 2.1 | 501-1891-0102 | ||
| SIM-3100 | Service Bulletin | SB501-1903-1 | A | 12/15/2008 | Replacement of Display due to diminishing source | 501-1903-0101, 501-1903-0201, 501-1903-0301, 501-1903-0401, 501-1903-2101, 501-1903-2201 | ||
| SIM-3100 | Service Bulletin | SB501-1903-2 | A | 12/15/2008 | Replacement of Display due to diminishing source | 501-1903-0501, 501-1903-0601, 501-1903-0701, 501-1903-0801 | ||
| SIM-3100 | Service Bulletin | SB501-1903-3 | A | 12/15/2008 | Release of Software 1.2 | 501-1903-0101, 501-1903-0201, 501-1903-0301, 501-1903-0401, 501-1903-0501, 501-1903-0601, 501-1903-0701, 501-1903-0801, 501-1903-2101, 501-1903-2201 | ||
| SIM-3100 | Service Bulletin | SB501-1903-5 | A | 3/3/2014 | Inspection MOD | Inspection MOD | 501-1903-0101, 501-1903-0201, 501-1903-0205, 501-1903-0301, 501-1903-0401, 501-1903-0501, 501-1903-0601, 501-1903-0701, 501-1903-2101, 501-1903-2103, 501-1903-2201 | |
| SIM-3100 | Service Bulletin | SB501-1891-8 | A | 3/3/2014 | Inspection for Suspected Unapproved Parts | Inspection for Suspected Unapproved Parts | 501-1891-0102 | |
| SIM-3100 | Service Bulletin | SB501-1891-5 | A | 3/6/2008 | Service Bulletin, MOD 5 | Reduce possibility of display Blanking | 501-1981-0102 | |
| SIM-3100 | Service Bulletin | SB501-1891-6 | A | 11/28/2008 | Service Bulletin, MOD 6 | Replacement Display due to Diminishing Source | 501-1891-0102 | |
| SIM-3100 | Service Bulletin | SB501-1891-7 | A | 4/19/2013 | Inspection MOD | Check for SUP | 501-1891-0102 | |
| SIM-3100 | Service Bulletin | SB501-1903-4 | A | 4/19/2013 | INSPECTION MOD | Inspection for SUP | 501-1903-0101, 501-1903-0201, 501-1903-0301, 501-1903-0401, 501-1903-0501, 501-1903-0601, 501-1903-0701, 501-1903-0801, 501-1903-2101, 501-1903-2103, 501-1903-2201 | |
| SIM-3100 | Service Letter | SL-334 | A | 8/14/2018 | End of Production Notice | Service Letter | 501-1827, 501-1891, 501-1903 | |
| SIM-750 | Installation Aircraft Tools | 576-6439-02 | A | 9/23/2020 | ACM Tool | Aircraft Configuration Module Tool, SIM-750 Simulator | ||
| SIM-750 | Installation Manual | 0040-15800-01 | 01 | 4/21/2025 | Installation Manual, SIM-750 | Electronic Flight Display Simulator Model: SIM-750 (Acron Aviation) | 9200-15800-0101 9200-15800-0301 | |
| SRVIVR - LW-Series | Component Maintenance Manual | 6082036 | 31-30-15 | initial change 1 | 6/16/2020 | Component Maintenance Manual | SRVIVR-CVFDR-1553 (QUAD RS-422) | 1493100-3401 |
| SRVIVR - LW-Series | Component Maintenance Manual | 165E6100-00 | 31-30-01 | 01 | 6/9/2025 | Component Maintenance Manual, Commercial | Cockpit Voice and Flight Data Recorder | CVR / 1493100-1100 FDR-717 / 1493100-2100 CVFDR-717 / 1493100-3103 CVFDR-429 / 1493100-3104 CVFDR-429 / 1493100-3105 CVFDR-429 / 1493100-3106 CVFDR-429 / 1493100-3107 |
| SRVIVR - LW-Series | Component Maintenance Manual | 165E6702-00 | 31-30-16 | B2 | 1/21/2025 | Component Maintenance Manual, SRVIVR, CVFDR-1553 | CVFDR-1553 (QUAD RS-422) | 1493100-3402 |
| SRVIVR - LW-Series | Component Maintenance Manual | 6081151 | 31-30-01 | F | 5/6/2025 | Component Maintenance Manual, Commercial | SRVIVR-CVR, SRVIVR-FDR, SRVIVR-FDR-717, SRVIVR-CVFDR-429 | 1493100-1000, 1493100-2000, 1493100-3001, 1493100-3002 |
| SRVIVR - LW-Series | Installation Manual | 0040-29001-01 | 03 | 8/18/2021 | Installation and Operation Manual | SRVIVR-CSMU | 1490002-0010 | |
| SRVIVR - LW-Series | Installation Manual | 165E6903-01 | 00 | 5/24/2021 | Installation and Operation Manual | eSRVIVR-FDR-1553 | 1493200-2000 | |
| SRVIVR - LW-Series | Installation Manual | 165E6748-02 | 01 | 5/10/2024 | Installation Manual | SRVIVR-CVFDR-1553 | 1493100-3410 | |
| SRVIVR - LW-Series | Installation Manual | 0040-14901-01 | 01 | 11/15/2024 | Installation and Operation Manual | SRVIVR® Cockpit Voice and Flight Data Recorder Model: SRVIVR-CVFDR-429 Encrypted SRVIVR | 1493200-3200 | |
| SRVIVR - LW-Series | Installation Manual | 165E6358-01 | A | 6/13/2016 | Installation and Operation Manual | SRVIVR-CVFDR-1553 | 1493100-3400 | |
| SRVIVR - LW-Series | Installation Manual | 165E6379-01 | C | 6/6/2023 | Installation and Operation Manual | SRVIVR-FDR-1553 | 1493100-2403 | |
| SRVIVR - LW-Series | Installation Manual | 6081152 | E | 6/9/2025 | Installation Manual. Commercial | SRVIVR-CVR, SRVIVR-FDR-717, SRVIVR-CVFDR-429, SRVIVR-CVFDR-717 Variants | 1493100-1100, 1493100-2100, 1493100-3103, 1493100-3104 | |
| SRVIVR - LW-Series | Installation Manual | 6082027 | Orig | 2/21/2014 | Installation Manual | SRVIVR-CVFDR-1553 Variant (with ACSMU) | 1493100-3401 | |
| SRVIVR - LW-Series | Installation Manual | 165E6247-01 | - | 6/13/2016 | Installation and Operation Manual | eSRVIVR Encrypted SRVIVR-CVFDR-1553 | 1493200-3000 | |
| SRVIVR - LW-Series | Installation Manual | 6081117 | E | 5/6/2025 | Installation and Operation Manual, Commercial | SRVIVR-CVR, SRVIVR-FDR, SRVIVR-FDR-717, SRVIVR-CVFDR-429 | 1493100-1000, 1493100-2000, 1493100-3001, 1493100-3002 | |
| SRVIVR - LW-Series | Service Bulletin | SB004-SRVIVR | 00 | 5/6/2025 | Software Update (OFP 9010598-0110) | INTRODUCTION OF SOFTWARE UPDATE OPERATIONAL FLIGHT PROGRAM (OFP)- 9010598-0110 | 1493100-1000, 1493100-2000, 1493100-3001, 1493100-3002 | |
| SRVIVR - LW-Series | Service Bulletin | SB005-SRVIVR | 00 | 6/9/2025 | Software Update (OFP 9010598-0110) | INTRODUCTION OF SOFTWARE UPDATE OPERATIONAL FLIGHT PROGRAM (OFP)- 9010598-0110 | 1493100-3103 | |
| SRVIVR - LW-Series | Service Bulletin | SRVIVR SB001 | Orig | 3/22/2013 | MOD E | ISSUE OF AUDIO RECORDER DISTORTION AND REMOVAL OF SWITCH CIRCUITRY TO PREVENT ARINC 429/717 BUS ATTENUATION | 1493100-1000 1493100-2000 1493100-3001 1493100-3002 1493100-1100 1493100-2100 1493100-3103 1493100-3104 1493100-3105 1493100-2200 1493100-2201 | |
| SRVIVR - LW-Series | Service Bulletin | SRVIVR SB002 | orig | 8/18/2017 | Software update. Upgrade ULB from 30 to 90 day [MOD F or G] | INTRODUCTION OF SOFTWARE UPDATE OPERATIONAL FLIGHT PROGRAM (OFP)- 0109 SOFTWARE UPDATE OPERATIONAL FLIGHT PROGRAM (OFP)- 0109; Upgrade ULB from 30 to 90 day [MOD F or G] | 1493100-1100 1493100-2100 1493100-3103 1493100-3104 | |
| SRVIVR - LW-Series | Service Bulletin | SRVIVR SB-2015-003 | 01 | 7/21/2016 | INTRODUCTION OF L-3AR 90-DAY UNDERWATER LOCATOR BEACON | MOD DOT F INTRODUCTION OF L-3AR 90-DAY UNDERWATER LOCATOR BEACON | 1493100-1000 1493100-2000 1493100-3001 1493100-3002 980-xxx-xxx | |
| SRVIVR - LW-Series | Service Letter | SIL-001-SRVIVR | 00 | 9/19/2023 | Service Information Letter | A software error exists that can cause data corruption of previously recorded data within a data partition upon the next application of power when recording. | 1493100-x4xx | |
| TACAN | Installation Manual | 0040-35001-01 | L | 10/16/2023 | Tacan+ Installation Manual | Incorporates 1.11 Software and new part number. License required. | 9200-35000-0101 9200-35000-0201 9200-35000-0301 9200-35000-0401 | |
| TACAN | Service Bulletin | SB001-BTP-1634 | 00 | 4/3/2023 | MOD A: Add TACAN+ Compatibility. | Bench Test Panel for AN/ARN-154 (V) TACAN System MOD A: Add TACAN+ Compatibility to BTP-1634. | 805-10045-001, 805-10045-002, 805-10045-003 | |
| TACAN | Service Bulletin | SB9200-35000-1 | B | 2/4/2019 | To replace components on Transmitter and frequency Generator Circuit Card Assemblies due to part availability. | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102, 9200-35000-0103 | |
| TACAN | Service Bulletin | SB9200-35000-14 | A | 9/13/2017 | To inform customers of Software Version 1.10 for the TRC2634 Transceiver. | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TACAN | Service Bulletin | SB9200-35000-11 | A | 4/14/2016 | To inform customers of Software Version 1.9 for the TRC2634 Transceiver. | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TACAN | Service Bulletin | SB9200-35000-12 | C | 2/4/2019 | Reliability improvement providing reduced likelihood of unit incurring a degraded operational range condition. (MOD E) | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102, 9200-35000-0103 | |
| TACAN | Service Bulletin | SB9200-35000-13 | C | 2/4/2019 | To improve unit power up performance. (MOD F) | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102, 9200-35000-0103 | |
| TACAN | Service Bulletin | SB9200-35000-2 | A | 8/23/2012 | To inform customers of Software Version 1.3 for the TRC2634 Transceiver. | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TACAN | Service Bulletin | SB9200-35000-4 | A | 11/13/2012 | Software Version 1.4 | To inform customers of Software Version 1.4 for the TRC2634 Transceiver. TACAN+ / TRC2634 Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TACAN | Service Bulletin | SB9200-35000-5 | C | 2/4/2019 | Units listed in Table 1 were shipped without tin plating (bare copper) on the ground foil P/N 9000-35027-01 used on RF transmitter. The bare copper ground foil, must be replaced with tin plated copper ground foil to prevent degradation of the transmitter. | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TACAN | Service Bulletin | SB9200-35000-6 | A | 8/19/2013 | Temporary loss of tracking (less than 3 seconds) can occur when two or more tracking channels are tuned to, or un-tuned from, the same frequency. (SW Version 1.5) | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TACAN | Service Bulletin | SB9200-35000-7 | B | 2/4/2019 | To improve reliability and reduce likelihood of premature failure of fielded units. | TACAN+ / TRC2634 | 9200-35000-0101, 9200-35000-0102, 9200-35000-0103 | |
| TACAN+ | Installation Manual | 0040-35001-01 | L | 10/16/2023 | Tacan+ Installation Manual | Incorporates 1.11 Software and new part number. License required. | 9200-35000-0101 9200-35000-0201 9200-35000-0301 9200-35000-0401 | |
| TACAN+ | Pilot Guide | 0040-35000-01 | D | 2/7/2023 | TACAN+ Pilots Guide | Supports 1.6; 1.7, & 1.8 Software | 9200-35000-0101, 9200-35000-0201 | |
| TACAN+ | Service Bulletin | SB9200-35000-7 | B | 2/4/2019 | To improve reliability and reduce likelihood of premature failure of fielded units. | TACAN+ / TRC2634 | 9200-35000-0101, 9200-35000-0102, 9200-35000-0103 | |
| TACAN+ | Service Bulletin | SB9200-35000-6 | A | 8/19/2013 | Temporary loss of tracking (less than 3 seconds) can occur when two or more tracking channels are tuned to, or un-tuned from, the same frequency. (SW Version 1.5) | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TACAN+ | Service Bulletin | SB9200-35000-8 | A | 5/18/2015 | Service Bulletin, Software 1.6 | TACAN+ / TRC2634 Corrects an intermittent mode change issue associated with the MIL-STD-1553B interface (part no. 9200-35000-0101 only), and eliminates a condition where the TRC2634 transceiver may reply to interrogations while in Air-Air Receive-Only mode. SW1.6, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TACAN+ | Service Bulletin | SB9200-35000-9 | A | 6/22/2015 | Service Bulletin, SW 1.7 | TACAN+ / TRC2634 Incorporation of this software implements 1553 interface software v1.3 that will correct intermittent 1553 output data for tracking channels C and D. SW1.7, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TACAN+ | Service Bulletin | SB9200-35000-5 | C | 2/4/2019 | Units listed in Table 1 were shipped without tin plating (bare copper) on the ground foil P/N 9000-35027-01 used on RF transmitter. The bare copper ground foil, must be replaced with tin plated copper ground foil to prevent degradation of the transmitter. | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TACAN+ | Service Bulletin | SB9200-35000-4 | A | 11/13/2012 | Software Version 1.4 | To inform customers of Software Version 1.4 for the TRC2634 Transceiver. TACAN+ / TRC2634 Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TACAN+ | Service Bulletin | SB9200-35000-2 | A | 8/23/2012 | To inform customers of Software Version 1.3 for the TRC2634 Transceiver. | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TACAN+ | Service Bulletin | SB9200-35000-3 | B | 2/4/2019 | Service Bulletin, MOD C | TACAN+ / TRC2634 Implement new Digital PCB assembly's P/N 9220-35008-01; -02., Acron Aviation | 9200-35000-0101, 9200-35000-0102, 9200-35000-0103 | |
| TACAN+ | Service Bulletin | SB9200-35000-13 | C | 2/4/2019 | To improve unit power up performance. (MOD F) | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102, 9200-35000-0103 | |
| TACAN+ | Service Bulletin | SB9200-35000-12 | C | 2/4/2019 | Reliability improvement providing reduced likelihood of unit incurring a degraded operational range condition. (MOD E) | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102, 9200-35000-0103 | |
| TACAN+ | Service Bulletin | SB9200-35000-11 | A | 4/14/2016 | To inform customers of Software Version 1.9 for the TRC2634 Transceiver. | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TACAN+ | Service Bulletin | SB9200-35000-10 | A | 7/6/2015 | Service Bulletin, Release 1.8 | TACAN+ / TRC2634 Adds the capability to detect a lead aircraft that is transmitting in Beacon mode (coarse bearing signals) and, if this air-air bearing signal is not present, to automatically enter a new High Signal Dynamics 20-Meter mode of operation. Release 1.8, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TACAN+ | Service Bulletin | SB9200-35000-14 | A | 9/13/2017 | To inform customers of Software Version 1.10 for the TRC2634 Transceiver. | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TACAN+ | Service Bulletin | SB9200-35000-1 | B | 2/4/2019 | To replace components on Transmitter and frequency Generator Circuit Card Assemblies due to part availability. | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102, 9200-35000-0103 | |
| TAWS8000 | Database | TAWS DataBase | x.x | 1/1/2023 | Information on TAWS Database | Databases are sold as exchanges through Avionics Service. The -001 is a North American Database and the -002 is a Worldwide Database. Please email Avionics.Service@L3Harris.com | TAWS | |
| TAWS8000 | Drawings / SPEC | TAWS Database Notice | n/a | 4/22/2024 | TAWS Database Updates | TAWS8000/8100 DB you need to send the CF card to Grand Rapids Factory. It cannot be updated in the field. Contact avionics service for a price and lead time. DB is updated by L3H every 30 days. Phone: 1-321-674-4900 Email: Avionics.Service@L3Harris.com | 805-18000-001, 805-18200-001, 805-18200-002, 805-18650-001 | |
| TAWS8000 | Installation Manual | 009-18001-001 | J | 6/20/2023 | Installation Manual | Terrain Awareness and Warning System | 805-18000-001 | |
| TAWS8000 | Instructions for Continued Airworthiness iCA | ES400-300103-200 | C | 9/8/2003 | Instructions for Continued Airworthiness Supplement | For TAWS 8000 Terrain Awareness Warning System Installed on Raytheon Aircraft Company Beech 400, 400A, 400T Aircraft. | TAWS8000 | |
| TAWS8000 | Pilot Guide | 009-18000-001 | D | 9/2/2003 | Pilot's Guide | Pub# 009-18000-001 | 805-18000-001 | |
| TAWS8000 | Printer Copies | 009-18000-001PC | D | 9/2/2003 | Pilot's Guide | |||
| TAWS8000 | Service Bulletin | SB-108 | Orig | 2/12/2003 | A production change to add patent numbers to the serial number and ID tag. | 805-18000-001 | ||
| TAWS8000 | Service Bulletin | SB-111 | Orig | 3/20/2003 | Correct a problem that may cause a unit to fail factory testing. | 805-18000-001 | ||
| TAWS8000 | Service Bulletin | SB-112 | Orig | 3/14/2003 | Maintenance upgrade. [software version 1.9 upgrade]. | 805-18000-001 | ||
| TAWS8000 | Service Bulletin | SB-133 | Orig | 8/16/2004 | Release of Software version 1.11. Corrects service menu data monitor for the ARINC 429 recievers and descretes. Corrects the intermittent lighting of the "terrain not available" lamp and occurrence of error 17. | 805-18000-001 | ||
| TAWS8000 | Service Bulletin | SB-A127 | Orig | 12/9/2003 | Software upgrade incorporates changes for the GPS position correction when using | 805-18000-001 | ||
| TAWS8000 | Service Bulletin | SB805-18000-200 | A | 3/14/2005 | Software Version 1.12 Upgrade | , Acron Aviation | 805-18000-001 | |
| TAWS8000 | Service Bulletin | SB-A117 | Orig | 7/9/2003 | To prevent degradation of computed altitude that may result when a baro set potentiometer is connected to the TAWS8000 and also connected to an ADC. Refer to SM-134 | 805-18000-001 | ||
| TAWS8000 | Service Bulletin | SB805-18000-202 | A | 1/23/2012 | To inform users of a suspected unapproved part (SUP) and to inform them of an inspection MOD effective at next service, which identifies units that have had this condition corrected. | , Acron Aviation | 805-18000-001 | |
| TAWS8000 | Service Letter | SL-230 | A | 1/23/2008 | Incorrect Elevation Reported for Black Rock Mountain In Canada | TAWS TERRAIN ALERT | 805-18000-001, 805-18650-001 | |
| TAWS8000 | Service Letter | SL-221 | A | 7/19/2007 | Permission to use STC | Permission to use STC | 805-18000-001 | |
| TAWS8000 | Supplemental Type Certificate | ST01881CH-D-FMS | Reis | 9/19/2003 | TAWS8000 (TAWS B) installation. Beechjet 400 | Installation of a Goodrich Avionics Systems LANDMARK Terrain Awarenes and Warning System TAWS8000 (TAWS B) installation. | ||
| TAWS8000 | Supplemental Type Certificate | ST01881CH-D | Reis | 9/19/2003 | Installation of a Goodrich Avionics Systems LANDMARK Terrain Awarenes and Warning System TAWS8000 (TAWS B) installation. | Installation of a Goodrich Avionics Systems LANDMARK Terrain Awarenes and Warning System TAWS8000 (TAWS B) installation. | ||
| TAWS8000 | Supplemental Type Certificate | SA01663CH-D-FMS | Amen | 11/12/2004 | Installation of an L-3 Communications Avionics Systems Terrain Awareness & Warning System TAWS 8000 or TAWS 8100. | Installation of an L-3 Communications Avionics Systems Terrain Awareness & Warning System TAWS 8000 or TAWS 8100. | ||
| TAWS8000 | Supplemental Type Certificate | SA01663CH-D | Reis | 11/12/2004 | Installation of an L-3 Communications Avionics Systems Terrain Awareness & Warning System TAWS 8000 or TAWS 8100. | Installation of an L-3 Communications Avionics Systems Terrain Awareness & Warning System TAWS 8000 or TAWS 8100. | ||
| TAWS8000 | Troubleshooting Guide | TP-611 | C | 6/6/2008 | TAWS8000 Troubleshooting Guide | TAWS8000 Troubleshooting Guide | ||
| TAWS8100 | Database | TAWS DataBase | x.x | 1/1/2023 | Information on TAWS Database | Databases are sold as exchanges through Avionics Service. The -001 is a North American Database and the -002 is a Worldwide Database. Please email Avionics.Service@L3Harris.com | TAWS | |
| TAWS8100 | Drawings / SPEC | TAWS Database Notice | n/a | 4/22/2024 | TAWS Database Updates | TAWS8000/8100 DB you need to send the CF card to Grand Rapids Factory. It cannot be updated in the field. Contact avionics service for a price and lead time. DB is updated by L3H every 30 days. Phone: 1-321-674-4900 Email: Avionics.Service@L3Harris.com | 805-18000-001, 805-18200-001, 805-18200-002, 805-18650-001 | |
| TAWS8100 | Installation Manual | 009-18651-001 | G | 6/20/2023 | Installation Manual | Terrain Awareness and Warning System | 805-18650-001 | |
| TAWS8100 | Pilot Guide | 009-18650-001 | A | 9/1/2004 | Pilot's Guide, TAWS8100 | LandMark. Class B terrain awareness & Warning System | 805-18650-001 | |
| TAWS8100 | Service Bulletin | SB805-18650-201 | A | 5/18/2009 | TAWS 8100 Software Version 2.09 Upgrade | TAWS 8100 Software Version 2.09 Upgrade, Acron Aviation | 805-18650-001 | |
| TAWS8100 | Service Bulletin | SB805-18650-200 | A | 2/10/2005 | Mod A - Add insulator between mouning bracket and PCB of U2 and U3 | , Acron Aviation | 805-18650-001 | |
| TAWS8100 | Service Bulletin | SB805-18650-202 | A | 1/23/2012 | To inform users of a suspected unapproved part (SUP) and to inform them of an inspection MOD effective at next service, which identifies units that have had this condition corrected. | , Acron Aviation | 805-18650-001 | |
| TAWS8100 | Service Letter | SL-342 | A | 4/18/2019 | GPS WAAS 1201 Sensor Issue | GPS WAAS 1201 Sensor Issue | 805-18650-001 | |
| TAWS8100 | Service Letter | SL-222 | A | 4/26/2007 | Permission to use STC | Permission to use STC | 805-18650-001 | |
| TAWS8100 | Service Letter | SL-230 | A | 1/23/2008 | Incorrect Elevation Reported for Black Rock Mountain In Canada | TAWS TERRAIN ALERT | 805-18000-001, 805-18650-001 | |
| TAWS8100 | Service Letter | SL-203 | A | 1/11/2005 | Notify dealers that the TAWS8100 requires an extra pin on the serial cable (pin 7) when using the service menu via laptop. | 805-18650-001 | ||
| TAWS8100 | Service Letter | SL-205 | Orig | 12/8/2004 | Remove caution and limitation of installing a TAWS8100 on an aircraft equipped with SATCOM. | 805-18650-001 | ||
| TAWS8100 | Supplemental Type Certificate | SA01663CH-D | Reis | 11/12/2004 | Installation of an L-3 Communications Avionics Systems Terrain Awareness & Warning System TAWS 8000 or TAWS 8100. | Installation of an L-3 Communications Avionics Systems Terrain Awareness & Warning System TAWS 8000 or TAWS 8100. | ||
| TAWS8100 | Supplemental Type Certificate | SA01663CH-D-FMS | Amen | 11/12/2004 | Installation of an L-3 Communications Avionics Systems Terrain Awareness & Warning System TAWS 8000 or TAWS 8100. | Installation of an L-3 Communications Avionics Systems Terrain Awareness & Warning System TAWS 8000 or TAWS 8100. | ||
| TAWS8100 | Troubleshooting Guide | TP-612 | C | 6/6/2008 | TAWS8100 Troubleshooting Guide | TAWS8100 Troubleshooting Guide | ||
| TCAS791 | Installation Manual | 009-10013-001 | H | 7/18/2013 | Installation Manual | Pub# 009-10013-001 | 805-10001-(), 805-10001-004, 805-10001-005, 805-10001-024, 805-10001-025, 805-10001-026 | |
| TCAS791 | Pilot Guide | 009-10025-001 | G | 6/24/2004 | Pilot's Guide | Pub# 009-10025-001 | 805-10001 | |
| TCAS791 | Service Letter | SL-235 | A | 5/29/2008 | Identify alternate display software drivers available with software v1.5 or higher. | TCAS791 installations using alternate display(s). | TCAS791 | |
| TCAS791 | Supplemental Type Certificate | SA8709SW-FMS | Reis | 2/17/2004 | Installation of a Traffic Alert and Collision Avoidance System I (TCAS I) model TCAS 791/791A. | Installation of a Traffic Alert and Collision Avoidance System I (TCAS I) model TCAS 791/791A. | ||
| TCAS791 | Supplemental Type Certificate | SA8709SW | Reis | 2/17/2004 | Installation of a Traffic Alert and Collision Avoidance System I (TCAS I) model TCAS 791/791A. | Installation of a Traffic Alert and Collision Avoidance System I (TCAS I) model TCAS 791/791A. | ||
| TCAS791 | Supplemental Type Certificate | ST155CH-FMS | Reis | 2/17/2004 | Installation of BF Goodrich Avionics systems TCAS791 traffic alert and collison avoidance system I (TCASI). | Installation of BF Goodrich Avionics systems TCAS791 traffic alert and collison avoidance system I (TCASI). | ||
| TCAS791 | Supplemental Type Certificate | ST155CH | Reis | 3/14/2006 | Installation of BF Goodrich Avionics systems TCAS791 traffic alert and collison avoidance system I (TCASI). | Installation of BF Goodrich Avionics systems TCAS791 traffic alert and collison avoidance system I (TCASI). | ||
| TCAS791 | Supplemental Type Certificate | SA373CH-FMS | Reis | 2/17/2004 | Installation of a BFGoodrich Flight Systems TCAS I | Installation of a BFGoodrich Flight Systems TCAS I | ||
| TCAS791 | Supplemental Type Certificate | SA373CH | Reis | 2/17/2004 | Installation of a BFGoodrich Flight Systems TCAS I. | Installation of a BFGoodrich Flight Systems TCAS I. | ||
| TCAS791 | Supplemental Type Certificate | ST319CH-FMS | Reis | 2/17/2004 | Installation of a TCAS 791 Traffic Alert and Collision Avoidance System (TCAS) I. | Installation of a TCAS 791 Traffic Alert and Collision Avoidance System (TCAS) I. | ||
| TCAS791 | Supplemental Type Certificate | ST319CH | Reis | 2/17/2004 | Installation of a TCAS 791 Traffic Alert and Collision Avoidance System (TCAS) I. | Installation of a TCAS 791 Traffic Alert and Collision Avoidance System (TCAS) I. | ||
| TCAS791 | Supplemental Type Certificate | ST00296WI-FMS | Reis | 2/17/2004 | Installation of a TCAS-791 traffic alert and collision avoidance system (TCAS I). | TCAS-791 (TCAS I). Cessna 650 | ||
| TCAS791 | Supplemental Type Certificate | ST00296WI | Reis | 2/17/2004 | Installation of a TCAS-791 traffic alert and collision avoidance system (TCAS I). | TCAS-791 (TCAS I). on Cessna 650 | ||
| TCAS791 | Supplemental Type Certificate | ST364CH-FMS | Reis | 2/17/2004 | Installation of a TCAS I (Model TCAS791). | Installation of a TCAS I (Model TCAS791). | ||
| TCAS791 | Supplemental Type Certificate | ST364CH | Reis | 2/17/2004 | Installation of a TCAS I (Model TCAS791). | Installation of a TCAS I (Model TCAS791). | ||
| TCAS791 | Supplemental Type Certificate | ST282CH-FMS | Reis | 2/17/2004 | Installation of TCAS-791 traffic alert and collision avoidance system (TCAS I). | Installation of TCAS-791 traffic alert and collision avoidance system (TCAS I). | ||
| TCAS791 | Supplemental Type Certificate | ST282CH | Reis | 2/17/2004 | Installation of TCAS-791 traffic alert and collision avoidance system (TCAS I). | Installation of TCAS-791 traffic alert and collision avoidance system (TCAS I). | ||
| TCAS791 | Supplemental Type Certificate | ST374CH-FMS | Reis | 2/13/2002 | Installation of a TCAS I. | Installation of a TCAS I. | ||
| TCAS791 | Supplemental Type Certificate | ST374CH | Reis | 2/13/2002 | Installation of a TCAS I. | Installation of a TCAS I. | ||
| TCAS791 | Supplemental Type Certificate | ST219CH-FMS | Reis | 2/17/2004 | Installation of BFGoodrich TCAS-791 traffic alert and collision avoidance system (TCAS I). | Installation of BFGoodrich TCAS-791 traffic alert and collision avoidance system (TCAS I). | ||
| TCAS791 | Supplemental Type Certificate | ST219CH | Reis | 2/17/2004 | Installation of BFGoodrich TCAS-791 traffic alert and collision avoidance system (TCAS I). | Installation of BFGoodrich TCAS-791 traffic alert and collision avoidance system (TCAS I). | ||
| TCAS791 | Supplemental Type Certificate | ST238CH-FMS | Reis | 2/17/2004 | Installation of a BFGoodrich Flight Systems TCAS I. | Installation of a BFGoodrich Flight Systems TCAS I. | ||
| TCAS791 | Supplemental Type Certificate | ST238CH | Reis | 2/17/2004 | Installation of BFGoodrich TCAS I. | Installation of BFGoodrich TCAS I. | ||
| TCAS791 | Supplemental Type Certificate | ST328CH-FMS | Reis | 2/17/2004 | Installation of a TCAS-791 traffic alert and collision avoidance system (TCAS I). | TCAS-791 (TCAS I). IAI 1124 | ||
| TCAS791 | Supplemental Type Certificate | ST328CH | Reis | 2/17/2004 | Installation of a TCAS-791 traffic alert and collision avoidance system (TCAS I). | Installation of a TCAS-791 traffic alert and collision avoidance system (TCAS I). | ||
| TCAS791 | Supplemental Type Certificate | SA00929AT | Reis | 2/17/2004 | Installation of a TCAS-791 traffic alert and collision avoidance system (TCAS I). | TCAS-791/A STC Beech 99. | ||
| TCAS791 | Supplemental Type Certificate | ST381CH-FMS | Reis | 2/17/2004 | Installation of a Goodrich Avionics Systems TCAS I. | Installation of a Goodrich Avionics Systems TCAS I. | ||
| TCAS791 | Supplemental Type Certificate | ST381CH | Reis | 2/17/2004 | Installation of a Goodrich Avionics Systems TCAS I. | Installation of a Goodrich Avionics Systems TCAS I. | ||
| TCAS791 | Supplemental Type Certificate | ST00155DE-D-FMS | Reis | 2/17/2004 | Installation of TCAS 791 TCAS I System. | Installation of TCAS 791 TCAS I System. | ||
| TCAS791 | Supplemental Type Certificate | ST00155DE-D | Reis | 2/17/2004 | Installation of TCAS 791 TCAS I System. | Installation of TCAS 791 TCAS I System. | ||
| TCAS791 | Supplemental Type Certificate | SA378CH-FMS | Reis | 2/17/2004 | TRC-791 | Beech 65-90 w/FMS | ||
| TCAS791 | Supplemental Type Certificate | SA378CH | Reis | 2/17/2004 | Installation of TCAS I. | Installation of TCAS I. | ||
| TCAS791 | Supplemental Type Certificate | SA00929AT-FMS | Reis | 2/17/2004 | Installation of a TCAS-791 traffic alert and collision avoidance system (TCAS I). | TCAS-791 FMS for Beech 99 | ||
| TCAS791 | Supplemental Type Certificate | SA92CH | Reis | 2/17/2004 | Installation of a flight systems traffic alert and collision avoidance system,TCAS 1 (Model TCAS791). | Installation of a flight systems traffic alert and collision avoidance system,TCAS 1 (Model TCAS791). | ||
| TCAS791 | Supplemental Type Certificate | SA92CH | Reis | 2/17/2004 | Installation of a flight systems traffic alert and collision avoidance system,TCAS 1 (Model TCAS791). | Installation of a flight systems traffic alert and collision avoidance system,TCAS 1 (Model TCAS791). | ||
| TCAS791 | Supplemental Type Certificate | SA00061DE-FMS | Resi | 2/17/2004 | Installation of Goodrich Model TCAS791/791A traffic alert and collision avoidance system (TCAS) I. | Installation of Goodrich Model TCAS791/791A traffic alert and collision avoidance system (TCAS) I. | ||
| TCAS791 | Supplemental Type Certificate | SA156CH-FMS | Reis | 2/17/2004 | Installation of Goodrich Avionics Systems TCAS791/791A Traffic Alert and Collision System (TCAS I). | Installation of Goodrich Avionics Systems TCAS791/791A Traffic Alert and Collision System (TCAS I). | ||
| TCAS791 | Supplemental Type Certificate | SA156CH | Reis | 2/17/2004 | Installation of Goodrich Avionics Systems TCAS791/791A Traffic Alert and Collision System (TCAS I). | Installation of Goodrich Avionics Systems TCAS791/791A Traffic Alert and Collision System (TCAS I). | ||
| TCAS791 | Supplemental Type Certificate | SA106CH-FMS | Reis | 2/17/2004 | Installation of TCAS 791 Traffic Alert and Collision Avoidance System I (TCAS I). | Installation of TCAS 791 Traffic Alert and Collision Avoidance System I (TCAS I). | ||
| TCAS791 | Supplemental Type Certificate | SA106CH | Reis | 2/17/2004 | Installation of TCAS 791 Traffic Alert and Collision Avoidance System I (TCAS I). | Installation of TCAS 791 Traffic Alert and Collision Avoidance System I (TCAS I). | ||
| TCAS791 | Supplemental Type Certificate | SA8655SW-FMS | Reis | 2/17/2004 | Installation of interfaced provisions only for TCAS791 Traffic Alert and Collision Avoidance System I (TCAS I). | Installation of interfaced provisions only for TCAS791 Traffic Alert and Collision Avoidance System I (TCAS I). | ||
| TCAS791 | Supplemental Type Certificate | SA8655SW | Reis | 2/17/2004 | Installation of interfaced provisions only for TCAS791 Traffic Alert and Collision Avoidance System I (TCAS I). | Installation of interfaced provisions only for TCAS791 Traffic Alert and Collision Avoidance System I (TCAS I). | ||
| TCAS791 | Supplemental Type Certificate | SA306CH | Reis | 2/17/2004 | Installation of Model TCAS 791 TCAS I. | Installation of Model TCAS 791 TCAS I. | ||
| TCAS791 | Supplemental Type Certificate | ST316CH-FMS | Reis | 2/17/2004 | Installation of a TCAS791/791A Traffic alert and collision avoidance system I (TCAS I). | Installation of a TCAS791/791A Traffic alert and collision avoidance system I (TCAS I). | ||
| TCAS791 | Supplemental Type Certificate | ST316CH | Reis | 2/17/2004 | Installation of a TCAS791/791A Traffic alert and collision avoidance system I (TCAS I). | Installation of a TCAS791/791A Traffic alert and collision avoidance system I (TCAS I). | ||
| TCAS791 | Supplemental Type Certificate | ST00029LB-FMS | Reis | 2/17/2004 | Installation of BFGoodrich traffic alert and collision avoidance system(TCAS I). | Installation of BFGoodrich traffic alert and collision avoidance system(TCAS I). | ||
| TCAS791 | Supplemental Type Certificate | ST00029LB | Reis | 2/17/2004 | Installation of BFGoodrich traffic alert and collision avoidance system(TCAS I). | Installation of BFGoodrich traffic alert and collision avoidance system(TCAS I). | ||
| TCAS791 | Supplemental Type Certificate | ST126CH-FMS | Reis | 3/15/2006 | Installation of Traffic Alert and Collision Avoidance System I (TCAS I) system. | Installation of Traffic Alert and Collision Avoidance System I (TCAS I) system. | ||
| TCAS791 | Supplemental Type Certificate | ST126CH | Reis | 2/17/2004 | Installation of Traffic Alert and Collision Avoidance System I (TCAS I) system. | Installation of Traffic Alert and Collision Avoidance System I (TCAS I) system. | ||
| TCAS791 | Supplemental Type Certificate | ST00106WI-FMS | Reis | 2/17/2004 | Installation of a BFGoodrich model TCAS791 traffic alert and collision avoidance system (TCAS) I. | Installation of a BFGoodrich model TCAS791 traffic alert and collision avoidance system (TCAS) I. | ||
| TCAS791 | Supplemental Type Certificate | ST00106WI | Reis | 2/17/2004 | Installation of a BFGoodrich model TCAS791 traffic alert and collision avoidance system (TCAS) I. | Installation of a BFGoodrich model TCAS791 traffic alert and collision avoidance system (TCAS) I. | ||
| TCAS791 | Supplemental Type Certificate | SR268CH-FMS | Reis | 2/17/2004 | BFG FlightSystems TCAS I (Model TCAS-791/A). S-76 | TCAS I (Model TCAS-791/A). on S-76 | ||
| TCAS791 | Supplemental Type Certificate | SR268CH | Reis | 2/17/2004 | Installation of BFG FlightSystems TCAS I (Model TCAS-791/A). | Installation of BFG FlightSystems TCAS I (Model TCAS-791/A). | ||
| TCAS791 | Troubleshooting Guide | 009-10109-001 | 04 | 4/29/2009 | TCAS 791 Troubleshooting guide | TCAS 791 Troubleshooting guide | ||
| TP-100 | Component Maintenance Manual | TP-345 | Orig | 9/2/1980 | Instruction Manual | Pub# TP-345 | 501-1322-01 | |
| TRC2634 | Installation Manual | 0040-35001-01 | L | 10/16/2023 | Tacan+ Installation Manual | Incorporates 1.11 Software and new part number. License required. | 9200-35000-0101 9200-35000-0201 9200-35000-0301 9200-35000-0401 | |
| TRC2634 | Pilot Guide | 0040-35000-01 | D | 2/7/2023 | TACAN+ Pilots Guide | Supports 1.6; 1.7, & 1.8 Software | 9200-35000-0101, 9200-35000-0201 | |
| TRC2634 | Service Bulletin | SB9200-35000-1 | B | 2/4/2019 | To replace components on Transmitter and frequency Generator Circuit Card Assemblies due to part availability. | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102, 9200-35000-0103 | |
| TRC2634 | Service Bulletin | SB9200-35000-14 | A | 9/13/2017 | To inform customers of Software Version 1.10 for the TRC2634 Transceiver. | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TRC2634 | Service Bulletin | SB9200-35000-10 | A | 7/6/2015 | Service Bulletin, Release 1.8 | TACAN+ / TRC2634 Adds the capability to detect a lead aircraft that is transmitting in Beacon mode (coarse bearing signals) and, if this air-air bearing signal is not present, to automatically enter a new High Signal Dynamics 20-Meter mode of operation. Release 1.8, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TRC2634 | Service Bulletin | SB9200-35000-11 | A | 4/14/2016 | To inform customers of Software Version 1.9 for the TRC2634 Transceiver. | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TRC2634 | Service Bulletin | SB9200-35000-12 | C | 2/4/2019 | Reliability improvement providing reduced likelihood of unit incurring a degraded operational range condition. (MOD E) | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102, 9200-35000-0103 | |
| TRC2634 | Service Bulletin | SB9200-35000-13 | C | 2/4/2019 | To improve unit power up performance. (MOD F) | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102, 9200-35000-0103 | |
| TRC2634 | Service Bulletin | SB9200-35000-3 | B | 2/4/2019 | Service Bulletin, MOD C | TACAN+ / TRC2634 Implement new Digital PCB assembly's P/N 9220-35008-01; -02., Acron Aviation | 9200-35000-0101, 9200-35000-0102, 9200-35000-0103 | |
| TRC2634 | Service Bulletin | SB9200-35000-2 | A | 8/23/2012 | To inform customers of Software Version 1.3 for the TRC2634 Transceiver. | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TRC2634 | Service Bulletin | SB9200-35000-4 | A | 11/13/2012 | Software Version 1.4 | To inform customers of Software Version 1.4 for the TRC2634 Transceiver. TACAN+ / TRC2634 Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TRC2634 | Service Bulletin | SB9200-35000-5 | C | 2/4/2019 | Units listed in Table 1 were shipped without tin plating (bare copper) on the ground foil P/N 9000-35027-01 used on RF transmitter. The bare copper ground foil, must be replaced with tin plated copper ground foil to prevent degradation of the transmitter. | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TRC2634 | Service Bulletin | SB9200-35000-9 | A | 6/22/2015 | Service Bulletin, SW 1.7 | TACAN+ / TRC2634 Incorporation of this software implements 1553 interface software v1.3 that will correct intermittent 1553 output data for tracking channels C and D. SW1.7, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TRC2634 | Service Bulletin | SB9200-35000-8 | A | 5/18/2015 | Service Bulletin, Software 1.6 | TACAN+ / TRC2634 Corrects an intermittent mode change issue associated with the MIL-STD-1553B interface (part no. 9200-35000-0101 only), and eliminates a condition where the TRC2634 transceiver may reply to interrogations while in Air-Air Receive-Only mode. SW1.6, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TRC2634 | Service Bulletin | SB9200-35000-6 | A | 8/19/2013 | Temporary loss of tracking (less than 3 seconds) can occur when two or more tracking channels are tuned to, or un-tuned from, the same frequency. (SW Version 1.5) | TACAN+ / TRC2634, Acron Aviation | 9200-35000-0101, 9200-35000-0102 | |
| TRC2634 | Service Bulletin | SB9200-35000-7 | B | 2/4/2019 | To improve reliability and reduce likelihood of premature failure of fielded units. | TACAN+ / TRC2634 | 9200-35000-0101, 9200-35000-0102, 9200-35000-0103 | |
| TRC497 | Service Letter | SL-299 | B | 8/27/2015 | Service Letter - Service transfer of SKYWATCH to Extant Aerospace | Transfer of Service SKY497 and SKY899 | 805-10800-( ) 805-11900-( ) | |
| TRC69 | Service Bulletin | SB-94 | B | 8/19/2005 | NACWS Low PRF Radar Database update Version RD01M20D. The radar database has been updated with FAA published data for 2001 and with information developed from radar data collection flights by Goodrich Avionics Systems. The database now includes data for t | 805-10012-003, 805-10012-013 | ||
| TRC69 | Service Bulletin | SB-95 | Orig | 8/27/2001 | NACWS Low PRF Radar Database update Version RD01M20D. The radar database has been updated with FAA published data for 2001 and with information developed from radar data collection flights by Goodrich Avionics Systems. The database now includes data for t | 805-10012-003, 805-10012-013 | ||
| TRC691 | Service Bulletin | SB-95 | Orig | 8/27/2001 | NACWS Low PRF Radar Database update Version RD01M20D. The radar database has been updated with FAA published data for 2001 and with information developed from radar data collection flights by Goodrich Avionics Systems. The database now includes data for t | 805-10012-003, 805-10012-013 | ||
| TRC691 | Service Bulletin | SB-94 | B | 8/19/2005 | NACWS Low PRF Radar Database update Version RD01M20D. The radar database has been updated with FAA published data for 2001 and with information developed from radar data collection flights by Goodrich Avionics Systems. The database now includes data for t | 805-10012-003, 805-10012-013 | ||
| TRC691 | Service Bulletin | SB-93 | original | 8/19/2005 | Software 1.7 notice for NACWS | T-34 NACWS TRC691 Software Version 1.7 upgrade. Improve NACWS coverage by processing data from the new low PRF Secondary Surveillance Radar Equipment. | 805-10012-003 | |
| TRC791 | Pilot Guide | 009-10025-001 | G | 6/24/2004 | Pilot's Guide | Pub# 009-10025-001 | 805-10001 | |
| TRC791 | Service Bulletin | SB-83 | Orig | 2/1/2000 | Software Upgrade to Ver. 1.5 | 805-10001-004, 805-10001-005, 805-10001-024, 805-10001-025, 805-10001-026 | ||
| TRC791 | Service Bulletin | SB-72 | Orig | 12/1/1996 | Advise problem may arise when connecting to ARNIC 429 Data Bus | 805-10001-( ) | ||
| TRC791 | Service Bulletin | SB-73 | Orig | 2/1/1997 | Mofify mounting tray to elliminate mounting difficulties. | 805-10024-001, 805-10024-002 | ||
| TRC791 | Service Bulletin | SB-66 | 1 | 10/1/1994 | Eliminate connector misalignment and damage. | 805-10024-001, 805-10024-002 | ||
| TRC791 | Service Bulletin | SB-68 | Orig | 1/1/1995 | To improve the reliability of the whisper shout function. | |||
| TRC791 | Service Bulletin | SB805-10001-1 | B | 3/21/2006 | "...change to the RF Receiver PCB Assembly to prevent contact with another PCB assemlby. | , Acron Aviation | 805-10001-004, 805-10001-005, 805-10001-006, 805-10001-007 | |
| TRC791 | Service Letter | SL-140 | Orig | 9/17/1997 | To provide information on the limitations for warranty consideration. | |||
| TRC791 | Service Letter | SL-253 | B | 10/14/2015 | Collision Avoidence- Interference Check | Silver Crown Interference /Remove SkyWatch References | 805-10001-001, 805-10001-002, 805-10001-003, 805-10001-004, 805-10001-005, 805-10001-006, 805-10001-021, 805-10001-022, 805-10001-023, 805-10001-024, 805-10001-025, 805-10001-026 | |
| TRC791 | Supplemental Type Certificate | SA00929AT | Reis | 2/17/2004 | Installation of a TCAS-791 traffic alert and collision avoidance system (TCAS I). | TCAS-791/A STC Beech 99. | ||
| TRC791 | Supplemental Type Certificate | SA00929AT-FMS | Reis | 2/17/2004 | Installation of a TCAS-791 traffic alert and collision avoidance system (TCAS I). | TCAS-791 FMS for Beech 99 | ||
| TSC-1000 | Installation Manual | 0040-44001-01 | F | 10/31/2022 | Installation Manual, TSC-1000 | Touch Screen Controller | 9200-44000-0101 | |
| TSC-1000 | Installation Manual | 0040-44004-01 | B | 9/11/2020 | Remove and Replace Instructions | TSC-1000 (R&R) Remove and Replace Instructions | 0040-44000-0101 | |
| TSC-1000 | Intermediate Maintenance Manual | 0040-44003-01 | 24- | F | 10/25/2022 | Intermediate Maintenance Manual, TSC-1000 | Touch Screen Controller | 9200-44000-0101 |
| TSC-1000 | Service Bulletin | SB9200-44000-2 | A | 4/16/2019 | Service Bulletin, MOD C | To replace obsolete hold up capacitor., Acron Aviation | 9200-44000-0101 | |
| TSC-1000 | Service Bulletin | SB9200-44000-1 | B | 9/7/2022 | Service Bulletin, MOD B | To improve display bonding characteristic., Acron Aviation | 9200-44000-0101 | |
| TSC-1000 | Service Bulletin | SB9200-44000-3 | B | 6/27/2019 | Service Bulletin, MOD A | To correct anomalous behavior on the display under certain temperature conditions and slow ramp rates on the 28VDC input power line., Acron Aviation | 9200-44000-0101 | |
| TSC-1000 | Service Bulletin | SB9200-44000-4 | 01 | 9/7/2022 | Service Bulletin, MOD D | MOD D provides information on new A1 Display Assembly., Acron Aviation | 9200-44000-0101 | |
| TSC-1000 | Service Bulletin | SB9200-44000-5 | 02 | 9/27/2021 | Service Bulletin, MOD E | MOD E provides information on new A2 Main Assembly that will allow unit to power up at faster voltage rise times., Acron Aviation | 9200-44000-0101 | |
| TSC-1000 | Service Bulletin | SB9200-44000-6 | 00 | 3/16/2021 | Service Bulletin, MOD F | Incorporation of MOD ensures that the latest version of the sequencer configuration is loaded on the TSC-1000 using the automated router. [MOD F], Acron Aviation | 9200-44000-0101 | |
| TSC-1000 | Service Bulletin | SB9200-44000-7 | 00 | 3/16/2021 | Service Bulletin, MOD G | Solder defects have been found on a limited number of TSC-1000 Processor CCA’s. [MOD G], Acron Aviation | 9200-44000-0101 | |
| TSC-1000 | Service Bulletin | SB9200-44000-9 | TSC1000-31-0005 | 00 | 10/31/2022 | Service Bulletin, MOD J | MOD J – Replace Solid State Drive, Acron Aviation | 9200-44000-0101 |
| TSC-1000 | Service Bulletin | SB9200-44000-8 | TSC1000-31-0004 | 00 | 4/28/2021 | Service Bulletin, MOD H | MOD H – Correct Fault Code Failures, Acron Aviation | 9200-44000-0101 |
| TSC-1000 | Service Letter | SIL-001-TSC-1000 | 00 | 10/28/2020 | Touch Screen Controller (TSC) Operation | Touch Screen Controller (TSC) Operation | 9200-44000-0101 | |
| TSC-1000 | Service Letter | SL-352 | C | 6/16/2021 | Screen Discolor at Power Up | Screen Discolor at Power Up | 9200-44000-0101 | |
| TSC-1000 | Service Letter | SIL-002-TSC-1000 | 00 | 6/16/2021 | Touch Screen Controller (TSC) Packaging | Touch Screen Controller (TSC) Packaging | 9200-44000-0101 | |
| ULB | Component Maintenance Manual | Novega 22960-00 | 25-60-00 | 00.3 | 3/3/2025 | GREEN90 ULB Component Maintenance Manual | GREEN90 90 Day ULB Component Maintenance Manual (CMM) for PN 266E6914-00 | 266E6914-00 |
| ULB | Component Maintenance Manual | 165E5542-00 | 25-62-01 | 09 | 6/21/2024 | Component Maintenance Manual for Underwater Locator Beacon (ULB) | Multiple Underwater Locater Beacon (ULB) Conversion kits Battery replacement kits | (Conversion kit part no.) 0686224-00, 068E5542-00, 147E5542-00, 266E5542-00 (ULB part no.) 266E5542-00 266E0305-00 266E0305-01 266E0305-02, 266E6914-00, 9080−10036−01 (Replacement kits part no.) 147E5542-00, 147E0305-00 |
| ULB | Installation Manual | 165E5542-10 | 04 | 6/21/2024 | Installation & Operation Manual for ULB | Multiple Underwater Locater Beacon (ULB) Conversion Kits Battery replacement kits | (Conversion kit part no.) 0686224-00, 068E5542-00, 147E5542-00, 266E5542-00 (ULB part no.) 266E5542-00 266E0305-00 266E0305-01 266E0305-02, 266E6914-00, 9080−10036−01 (Replacement kits part no.) 147E5542-00, 147E0305-00 | |
| ULB | Service Letter | SIL-003-ULB | 02 | 3/6/2025 | Service Information Letter, NTO for ULB | No Technical Objection (NTO) FA2100 and FA5000 Recorder Models for alternate Underwater Locator Beacon (ULB) installation. TSO-C142B Compliant Devices: • P/N 9080-10036-01. DK290-11, Dukane (Non-Restricted Class 9 Lithium Battery) • P/N 266-E6914-00. Green90, Novega P/N: 22960−00 (Lithium Free Battery) | ALL FA2100, FA5000 ULB: 9080-10036-01 ULB: 266-E6914-00 | |
| ULB | Service Letter | SIL-002-ULB | 00 | 9/16/2024 | Battery Information for 90 Day Underwater Locator Beacon (ULB). | Provide Composition Information on Ingredients and Transportation Rules information on 90-day ULB. NOTE: The battery is considered a battery inside a contained product (i.e., ULB). | P/N 266E5542-00 (Dukane DK120/90) P/N 9080-10036-01 (Dukane DK290-11) P/N 266E6914-00 (Novega 22960-00, GREEN90) | |
| ULB | Service Letter | SIL-004-ULB | 00 | 1/23/2025 | Notification of Dukane Seacom Service Information Letter. | Reports of internal battery spring discoloration within the DK120/90 have been reported by service technicians performing field battery replacement activities in accordance with Technical Manual 03-TM-0063 Section V. | P/N 266E5542-00 (Dukane DK120/90) | |
| VG-204 | Component Maintenance Manual | TP-312 | 34-20-14 | 8 | 3/6/2018 | Component Maintenance Manual, VG-204AB, VG-204V, VG-204Z | Pub# TP-312 | 501-1224-01, 501-1224-02, 501-1453-01 |
| VG-204 | Component Maintenance Manual | TP-357 | 34-20-07 | 7 | 3/5/2012 | Instruction Manual | Pub# TP-357 | 501-1255-01 |
| VG-204 | Component Maintenance Manual | TP-230 | R1 C | 2/14/2008 | Instruction Manual | Pub# TP-230, Acron Aviation | 501-1120-01 | |
| VG-204 | Component Maintenance Manual | TP-250 | 34-20-13 | 10 | 6/20/2003 | Maintenance Manual with IPL | Displacement Gyroscope | 501-1160-01 |
| VG-204 | Component Maintenance Manual | TP-251 | 34-20-09 | A4 | 12/11/2024 | Maintenance Manual with IPL | Displacement Gyroscope Model: VG-204D | 501-1113-01 |
| VG-204 | Component Maintenance Manual | TP-252 | 1 C3 | 2/14/2008 | Maintenance Data | Pub# TP-252 | 501-1125-01 | |
| VG-204 | Component Maintenance Manual | TP-414 | 34-20-23 | 7/26/2005 | Maintenance Manual | Pub# TP-414 | 501-1503-01 | |
| VG-204 | Component Maintenance Manual | TP-492 | 34-20-53 | B | 8/28/2017 | Component Maintenance Manual, VG-204AM | Pub# TP-492 | 501-1731-01 |
| VG-204 | Installation Manual | TP-594 | C | 8/22/2019 | Installation Manual | Pub# TP-594 | 501-1113-01, 501-1160-01, 501-1160-02, 501-1494-01 | |
| VG-204 | Installation Manual | TP-363 | 34-20-14 | Reis | 3/10/1986 | Installation instructions, VG-204AB | Displacement Gyroscope | 501-1453-01 |
| VG-204 | Installation Manual | TP-487 | 34-20-47 | Orig | 5/11/1994 | Installation and Operation Manual, VG-204AM | Pub# TP-487 | 501-1731-01 |
| VG-204 | Service Bulletin | SB501-1160-16 | A | 7/13/2005 | Improve reliability by updating units in the field to current. | 501-1160-01 | ||
| VG-204 | Service Bulletin | SB501-1160-1 | B | 5/1/1999 | To reduce audible noise. | 501-1160-01 | ||
| VG-204 | Service Bulletin | SB501-1160-10 | Orig | 1/1/1985 | To install more reliable stator. | 501-1160-01 | ||
| VG-204 | Service Bulletin | SB501-1160-11 | Orig | 6/1/1985 | To improve initial erection timing. | 501-1160-01 | ||
| VG-204 | Service Bulletin | SB501-1160-12 | Orig | 3/1/1992 | To ensure roll erection cut-off circuit operates. | 501-1160-01 | ||
| VG-204 | Service Bulletin | SB501-1160-13 | C | 2/17/2004 | To improve drift performance and eliminate potential of spring on pitch axis from rubbing on shield of bearing. | 501-1160-01 | ||
| VG-204 | Service Bulletin | SB501-1160-14 | Orig | 11/26/2003 | Prevent possible pitch precession by ensuring gimbal freedom. | 501-1160-02 | ||
| VG-204 | Service Bulletin | SB501-1160-15 | Orig | 6/2/2004 | Insure synchro output signals are compatible with application. | 501-1160-02 | ||
| VG-204 | Service Bulletin | SB501-1160-2 | Orig | 9/1/1981 | To eliminate nutation. | 501-1160-01 | ||
| VG-204 | Service Bulletin | SB501-1160-3 | Orig | 9/1/1981 | To improve reliability. | 501-1160-01 | ||
| VG-204 | Service Bulletin | SB501-1160-4 | Orig | 10/1/1983 | To insure roll erection when in the cut-off mode. | 501-1160-01 | ||
| VG-204 | Service Bulletin | SB501-1160-5 | B | 11/1/1984 | To minimize false erection and eliminate shaft looseness. | 501-1160-01 | ||
| VG-204 | Service Bulletin | SB501-1160-6 | Orig | 6/1/1984 | To replace base. | 501-1160-01 | ||
| VG-204 | Service Bulletin | SB501-1160-7 | Orig | 6/1/1984 | To replace cover. | 501-1160-01 | ||
| VG-204 | Service Bulletin | SB501-1160-8 | Orig | 6/1/1984 | To use higher reliability diode. | 501-1160-01 | ||
| VG-204 | Service Bulletin | SB501-1160-9 | Orig | 8/1/1984 | To minimize Synchro modulation. | 501-1160-01 | ||
| VG-204 | Service Bulletin | SB501-1113-1 | A | 4/30/2002 | To reduce audible noise. (Refer to SB501-1113-11) | , Acron Aviation | 501-1113-01 | |
| VG-204 | Service Bulletin | SB501-1113-10 | Orig | 6/1/1985 | To improve initial erection timing. | , Acron Aviation | 501-1113-01 | |
| VG-204 | Service Bulletin | SB501-1113-11 | A | 10/11/2005 | Improve drift and vibration performance and eliminate potential of spring on pitch axis from rubbing on shield of bearing. | , Acron Aviation | 501-1113-01 | |
| VG-204 | Service Bulletin | SB501-1113-2 | Orig | 2/1/1984 | To eliminate nutation. | , Acron Aviation | 501-1113-01 | |
| VG-204 | Service Bulletin | SB501-1113-3 | A | 8/1/1984 | To minimize false erections and eliminate shaft looseness. | , Acron Aviation | 501-1113-01 | |
| VG-204 | Service Bulletin | SB501-1113-4 | A | 9/1/1983 | To insure correct relay is installed upon the 542-1213-01 Frame Circuit Card Assembly. | , Acron Aviation | 501-1113-01 | |
| VG-204 | Service Bulletin | SB501-1113-5 | Orig | 2/1/1984 | To replace cover. | , Acron Aviation | 501-1113-01 | |
| VG-204 | Service Bulletin | SB501-1113-6 | Orig | 2/1/1984 | To replace base. | , Acron Aviation | 501-1113-01 | |
| VG-204 | Service Bulletin | SB501-1113-7 | Orig | 6/1/1984 | To install higher reliability diode. | , Acron Aviation | 501-1113-01 | |
| VG-204 | Service Bulletin | SB501-1113-8 | Orig | 8/1/1984 | To minimize Synchro modulation. | , Acron Aviation | 501-1113-01 | |
| VG-204 | Service Bulletin | SB501-1113-9 | Orig | 1/1/1985 | To install a more reliable stator. | , Acron Aviation | 501-1113-01 | |
| VG-204 | Service Bulletin | SB501-1120-1 | Orig | 11/1/1989 | To provide for variations in transistor configuration. | , Acron Aviation | 501-1120-01 | |
| VG-204 | Service Bulletin | SB501-1453-1 | Orig | 10/1/1988 | To reduce EMI. | 501-1453-01 | ||
| VG-204 | Service Bulletin | SB501-1453-2 | Orig | 11/1/1993 | MOD 2 - To reduce pitch kicks. MOD 3 - To reduce output variations | 501-1453-01 | ||
| VG-204 | Service Bulletin | SB501-1453-3 | A | 9/1/1994 | To reduce environmental effects of vibration and shock. | 501-1453-01 | ||
| VG-204 | Service Bulletin | SB501-1453-4 | C | 2/17/2004 | To improve drift performance and eliminate potential of spring on pitch axis from rubbing on shield of bearing. | 501-1453-01 | ||
| VG-204 | Service Bulletin | SB501-1453-5 | A | 12/1/2000 | Improve reliability of connection. | 501-1453-01 | ||
| VG-204 | Service Bulletin | SB501-1255-1 | A | 5/1/1999 | To reduce audible noise. | 501-1255-01 | ||
| VG-204 | Service Bulletin | SB501-1255-2 | Orig | 8/1/1984 | To install K3 relay on 542-1360-01 Frame Circuit Card Assembly. | 501-1255-01 | ||
| VG-204 | Service Bulletin | SB501-1255-3 | A | 7/1/1985 | To strengthen base assembly and thereby improve reliability. | 501-1255-01 | ||
| VG-204 | Service Bulletin | SB501-1255-4 | Orig | 6/1/1984 | To strengthen cover and thereby improve reliability. | 501-1255-01 | ||
| VG-204 | Service Bulletin | SB501-1255-5 | Orig | 6/1/1984 | To install higher reliability diode. | 501-1255-01 | ||
| VG-204 | Service Bulletin | SB501-1255-6 | Orig | 1/1/1985 | To install a more reliable stator. | 501-1255-01 | ||
| VG-204 | Service Bulletin | SB501-1255-7 | Orig | 2/1/1985 | To install higher reliability diode. | 501-1255-01 | ||
| VG-204 | Service Bulletin | SB501-1255-8 | C | 2/17/2004 | To improve drift performance and eliminate potential of spring on pitch axis from rubbing on shield of bearing. | 501-1255-01 | ||
| VG-204 | Service Bulletin | SB501-1255-9 | Orig | 12/1/2000 | Improve reliability of connection. | 501-1255-01 | ||
| VG-204 | Service Bulletin | SB501-1224-1 | Orig | 12/1/1980 | To reduce audible noise. | 501-1224-01 | ||
| VG-204 | Service Bulletin | SB501-1224-10 | Orig | 1/1/1985 | To install a more reliable stator. | 501-1224-02 | ||
| VG-204 | Service Bulletin | SB501-1224-11 | Orig | 2/1/1985 | To install higher reliability diodes. | 501-1224-01, 501-1224-02 | ||
| VG-204 | Service Bulletin | SB501-1224-12 | Orig | 6/1/1985 | To improve initial erection timing. | 501-1224-01, 501-1224-02 | ||
| VG-204 | Service Bulletin | SB501-1224-13 | C | 11/15/2002 | To reduce gyro signal interference with autopilot by conversion to VG-204AB configuration. [Factory Modification Only] | 501-1224-02 | ||
| VG-204 | Service Bulletin | SB501-1224-14 | A | 2/1/1994 | To reduce environmental effects of vibration and shock. | 501-1224-01, 501-1224-02 | ||
| VG-204 | Service Bulletin | SB501-1224-2 | Orig | 9/1/1981 | To eliminate nutation. | 501-1224-01 | ||
| VG-204 | Service Bulletin | SB501-1224-3 | Orig | 9/1/1981 | To improve reliability. | 501-1224-01 | ||
| VG-204 | Service Bulletin | SB501-1224-4 | A | 8/1/1985 | To retrofit gyro to VG-204Z configuration. | 501-1224-01 | ||
| VG-204 | Service Bulletin | SB501-1224-5 | Orig | 6/1/1984 | To replace base. | 501-1224-01, 501-1224-02 | ||
| VG-204 | Service Bulletin | SB501-1224-6 | Orig | 6/1/1984 | To replace cover. | 501-1224-01, 501-1224-02 | ||
| VG-204 | Service Bulletin | SB501-1224-7 | Orig | 6/1/1984 | To use diodes of higher reliability. | 501-1224-01, 501-1224-02 | ||
| VG-204 | Service Bulletin | SB501-1224-8 | A | 5/1/1985 | To minimize false erections. | 501-1224-01, 501-1224-02 | ||
| VG-204 | Service Bulletin | SB501-1224-9 | Orig | 7/1/1984 | To reduce Synchro modulation by demagnetizing unit. | 501-1224-02 | ||
| VG-204 | Service Letter | SL-33 | A | 8/28/2000 | To provide information on incorporation of Mod No. 20 which reduces pitch Synchro noise | Inactive | 501- | |
| VG-204 | Service Letter | SL-35 | B | 9/13/2000 | To clarify operating procedures and erection indications. | |||
| VG-204 | Service Letter | SL-174 | A | 4/3/2015 | To provide Avionics Systems, Inc service centers and maintenance personnel with storage information for gyro products. [Replaces SL-113, SL-131, SL-168, SA-89]. | Remove references to AIM Series Gyros. | ||
| VG-204 | Service Letter | SL-180 | Orig | 4/17/2003 | To advise authorized service centers on repair of Frame Circuit Card Assemblies. | 501-1255-01, 501-1453-01 | ||
| VG-204 | Service Letter | SL-111 | Orig | 12/1/1989 | To provide gyro service centers with information regarding allowed use of DG-106 alternate solvent for performing gyro leak check. | |||
| VG-204 | Service Letter | SIL-001-VG-204 | 00 | 3/31/2025 | End of Manufacturing Notice. | VG-204 AM - End of Manufacturing Notice | 501-1731-01 | |
| VG-204 | Service Letter | SL-275 | A | 1/26/2012 | To provide official approval for the discontinuation of the need to perform reliability tests that may be called out in maintenanc manuals for products listed in the Effectivity paragraph | |||
| VG-204 | Service Letter | SL-274 | A | 1/4/2012 | To provide offical approval for the use of eqivalent test equipment to test and validate the functionality of vertical gyros manufactured by L-3 Avionics Systems. | |||
| VG-206 | Component Maintenance Manual | TP-322 | 34-20-08 | 6 | 12/17/2024 | Maintenance Manual with IPL | Pub# TP-322 | 501-1204-01 |
| VG-206 | Installation Manual | TP-424 | 34-20-08 | Orig | 6/15/1989 | Installation Manual | Pub# TP-424 | 501-1204-01 |
| VG-206 | Installation Manual | TP-226 | Orig | 11/8/1974 | Installation Instructions | Pub# TP-226, Acron Aviation | 501-1150-01 | |
| VG-206 | Service Bulletin | SB501-1204-1 | A | 2/1/1981 | To reduce audible noise. Refer to SB501-1204-19. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-10 | Orig | 8/1/1984 | To replace base. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-11 | Orig | 8/1/1984 | To replace cover. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-12 | A | 10/1/1984 | To replace old stators with new stator and Terminal Board. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-13 | Orig | 1/1/1985 | To remove components to eliminate DC voltage in pitch switch. Refer to SB501-1204-17. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-14 | B | 12/1/1998 | To reduce pitch acceleration errors and insure adequate flag voltage. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-15 | Orig | 11/1/1988 | To eliminate relay chatter at time out caused by power supply sag when relays energize. Refer to SB501-1204-17. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-16 | Orig | 6/1/1991 | Modification to eliminate harmonic noise generated by two magnet gyroscope rotor assemblies. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-17 | Orig | 7/1/1992 | To provide a replacement for Flex Frame Circuit Card Assembly in the event these circuit card assemblies become non-serviceable. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-18 | Orig | 5/1/1993 | To provide information/instructions for replacement of cutoff switches P/N 561-1504-01 with P/N 561-1602-01 or -02. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-19 | D | 5/19/2005 | To improve gyro performance by replacing double row bearing on pitch axis with single row bearing. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-2 | A | 2/11/2009 | To reduce roll freedom when power is off. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-3 | Orig | 11/1/1983 | To reduce possibility of improper Synchro outputs. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-4 | A | 8/1/1984 | To reduce pitch transient noise. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-5 | Orig | 11/1/1983 | To insure complete cut-off of single wheel monitor circuit when in "OFF" mode. Refer to SB501-1204-17 | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-6 | Orig | 11/1/1983 | To prevent terminal boards from warping. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-7 | Orig | 11/1/1983 | To prevent solenoid shaft from coming loose. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-8 | C | 10/1/1999 | To incorporate transient protection for U1 and improve single wheal operation. To improve reliability of output signals to inner axis terminal board. | 501-1204-01 | ||
| VG-206 | Service Bulletin | SB501-1204-9 | Orig | 11/1/1983 | To improve reliability of radar printed circuit board. | 501-1204-01 | ||
| VG-206 | Service Letter | SL-111 | Orig | 12/1/1989 | To provide gyro service centers with information regarding allowed use of DG-106 alternate solvent for performing gyro leak check. | |||
| VG-206 | Service Letter | SL-174 | A | 4/3/2015 | To provide Avionics Systems, Inc service centers and maintenance personnel with storage information for gyro products. [Replaces SL-113, SL-131, SL-168, SA-89]. | Remove references to AIM Series Gyros. | ||
| VG-206 | Service Letter | SL-35 | B | 9/13/2000 | To clarify operating procedures and erection indications. | |||
| VG-206 | Service Letter | SL-33 | A | 8/28/2000 | To provide information on incorporation of Mod No. 20 which reduces pitch Synchro noise | Inactive | 501- | |
| VG-206 | Service Letter | SL-274 | A | 1/4/2012 | To provide offical approval for the use of eqivalent test equipment to test and validate the functionality of vertical gyros manufactured by L-3 Avionics Systems. | |||
| VG-208 | Component Maintenance Manual | TP-260 | 34-20-12 | 15 | 1/13/2025 | Maintenance Manual with IPL | Displacement Gyroscope | 501-1121-01, 501-1121-02, 501-1209-01, 501-1210-01 |
| VG-208 | Installation Manual | TP-270 | B | 9/4/2012 | Installation Manual | Pub# TP-270 | 501-1121-01, 501-1209-01, 501-1210-01 | |
| VG-208 | Service Bulletin | SB501-1210-11 | A | 9/25/1990 | To improve reliability by replacing stators. | 501-1210-01 | ||
| VG-208 | Service Bulletin | SB501-1209-1 | B | 5/1/1999 | To eliminate the possibility of shorting leads of resisitors R4 and R7. | 501-1209-01 | ||
| VG-208 | Service Bulletin | SB501-1209-10 | Orig | 8/1/1984 | To minimize false erections. | 501-1209-01 | ||
| VG-208 | Service Bulletin | SB501-1209-11 | Orig | 1/1/1985 | To install more reliable stator. | 501-1209-01 | ||
| VG-208 | Service Bulletin | SB501-1209-12 | Orig | 1/1/1985 | To remove components to eliminate DC voltage on pitch switch. | 501-1209-01 | ||
| VG-208 | Service Bulletin | SB501-1209-13 | Orig | 6/1/1992 | To provide use of capacitor with improved reliability characteristics. | 501-1209-01 | ||
| VG-208 | Service Bulletin | SB501-1209-14 | A | 5/1/1999 | Incorporation of this modification will eliminate interference between the unit cover and Resistor A5R4. | 501-1209-01 | ||
| VG-208 | Service Bulletin | SB501-1209-15 | A | 5/1/2001 | To improve drift performance and eliminate potential of spring on pitch axis from rubbing on shield of bearing. | 501-1209-01 | ||
| VG-208 | Service Bulletin | SB501-1209-2 | B | 5/1/1999 | To reduce audible noise. | 501-1209-01 | ||
| VG-208 | Service Bulletin | SB501-1209-3 | A | 9/1/1984 | To improve reliability. | 501-1209-01 | ||
| VG-208 | Service Bulletin | SB501-1209-4 | B | 4/1/1985 | To eliminate nutation. | 501-1209-01 | ||
| VG-208 | Service Bulletin | SB501-1209-5 | Orig | 8/1/1984 | To prevent solenoid shaft from coming loose. | 501-1209-01 | ||
| VG-208 | Service Bulletin | SB501-1209-6 | Orig | 8/1/1984 | To minimize Synchro modulation. | 501-1209-01 | ||
| VG-208 | Service Bulletin | SB501-1209-7 | A | 7/1/1985 | To replace base. | 501-1209-01 | ||
| VG-208 | Service Bulletin | SB501-1209-8 | Orig | 8/1/1984 | To replace cover. | 501-1209-01 | ||
| VG-208 | Service Bulletin | SB501-1209-9 | A | 4/1/1986 | To reduce Synchro modulation and remove mod 19 parts. | 501-1209-01 | ||
| VG-208 | Service Bulletin | SB501-1210-1 | B | 5/1/1999 | To eliminate the possiblity of shorting of resisitors R4 and R7. | 501-1210-01 | ||
| VG-208 | Service Bulletin | SB501-1210-10 | Orig | 8/1/1984 | To minimize false erections. | 501-1210-01 | ||
| VG-208 | Service Bulletin | SB501-1210-12 | Orig | 1/1/1985 | To remove components to eliminate DC voltage on pitch switch. | 501-1210-01 | ||
| VG-208 | Service Bulletin | SB501-1210-13 | Orig | 6/1/1992 | To provide use of a capacitor with improved reliability characteristics. | 501-1210-01 | ||
| VG-208 | Service Bulletin | SB501-1210-14 | B | 8/18/2006 | Incorporation of this modification will eliminate interference between the unit cover and Resistor A5R4. | 501-1210-01 | ||
| VG-208 | Service Bulletin | SB501-1210-15 | A | 5/1/2001 | To improve drift performance and eliminate potential of spring on pitch axis from rubbing on shield of bearing. | 501-1210-01 | ||
| VG-208 | Service Bulletin | SB501-1210-16 | B | 7/4/2003 | Unsecured Pitch Stop can come loose during operation. | 501-1210-01 | ||
| VG-208 | Service Bulletin | SB501-1210-2 | B | 5/1/1999 | To reduce audible noise. | 501-1210-01 | ||
| VG-208 | Service Bulletin | SB501-1210-3 | A | 9/1/1984 | To replace flex circuits with molded Terminal Board. | 501-1210-01 | ||
| VG-208 | Service Bulletin | SB501-1210-4 | B | 4/1/1985 | To eliminate nutation. | 501-1210-01 | ||
| VG-208 | Service Bulletin | SB501-1210-5 | Orig | 8/1/1984 | To prevent solenoid shaft from coming loose. | 501-1210-01 | ||
| VG-208 | Service Bulletin | SB501-1210-6 | Orig | 8/1/1984 | To minimize Synchro modulation. | 501-1210-01 | ||
| VG-208 | Service Bulletin | SB501-1210-7 | A | 7/1/1985 | To replace base. | 501-1210-01 | ||
| VG-208 | Service Bulletin | SB501-1210-8 | Orig | 8/1/1984 | To replace cover. | 501-1210-01 | ||
| VG-208 | Service Bulletin | SB501-1210-9 | A | 4/1/1986 | To reduce Synchro modulation and remove mod 19 parts. | 501-1210-01 | ||
| VG-208 | Service Bulletin | SB501-1121-1 | B | 5/1/1999 | To eliminate the possibility of shorting leads of resistors R4 and R7. Refer to SB501-1121-14A. | , Acron Aviation | 501-1121-01 | |
| VG-208 | Service Bulletin | SB501-1121-10 | Orig | 8/1/1984 | To minimize false erection. | , Acron Aviation | 501-1121-01 | |
| VG-208 | Service Bulletin | SB501-1121-11 | Orig | 1/1/1985 | To install a more reliable stator. | , Acron Aviation | 501-1121-01 | |
| VG-208 | Service Bulletin | SB501-1121-12 | Orig | 1/1/1985 | To remove components to eliminate DC voltage on pitch switch. | , Acron Aviation | 501-1121-01 | |
| VG-208 | Service Bulletin | SB501-1121-13 | Orig | 6/1/1992 | To provide use of a capacitor with improved reliability characteristics. | , Acron Aviation | 501-1121-01 | |
| VG-208 | Service Bulletin | SB501-1121-14 | A | 5/1/1999 | Incorporation of this modification will eliminate interference between the unit cover and Resistor A5R4. | , Acron Aviation | 501-1121-01 | |
| VG-208 | Service Bulletin | SB501-1121-15 | A | 5/1/2001 | To improve drift performance and eliminate potential of spring on pitch axis from rubbing on shield of bearing. | , Acron Aviation | 501-1121-01 | |
| VG-208 | Service Bulletin | SB501-1121-2 | B | 5/1/1999 | To reduce audible noise. | , Acron Aviation | 501-1121-01 | |
| VG-208 | Service Bulletin | SB501-1121-3 | A | 4/1/1985 | To replace flex circuits with molded Terminal Board. | , Acron Aviation | 501-1121-01 | |
| VG-208 | Service Bulletin | SB501-1121-4 | A | 4/1/1985 | To eliminate nutation. | , Acron Aviation | 501-1121-01 | |
| VG-208 | Service Bulletin | SB501-1121-5 | Orig | 8/1/1984 | To prevent solenoid shaft from coming loose. | , Acron Aviation | 501-1121-01 | |
| VG-208 | Service Bulletin | SB501-1121-6 | Orig | 8/1/1984 | To minimize Synchro modulation. | , Acron Aviation | 501-1121-01 | |
| VG-208 | Service Bulletin | SB501-1121-7 | A | 7/1/1985 | To replace base. | , Acron Aviation | 501-1121-01 | |
| VG-208 | Service Bulletin | SB501-1121-8 | Orig | 8/1/1984 | To replace cover. | , Acron Aviation | 501-1121-01 | |
| VG-208 | Service Bulletin | SB501-1121-9 | A | 4/1/1986 | To reduce Synchro modulation and remove mod 19 parts. | , Acron Aviation | 501-1121-01 | |
| VG-208 | Service Letter | SL-33 | A | 8/28/2000 | To provide information on incorporation of Mod No. 20 which reduces pitch Synchro noise | Inactive | 501- | |
| VG-208 | Service Letter | SL-35 | B | 9/13/2000 | To clarify operating procedures and erection indications. | |||
| VG-208 | Service Letter | SL-174 | A | 4/3/2015 | To provide Avionics Systems, Inc service centers and maintenance personnel with storage information for gyro products. [Replaces SL-113, SL-131, SL-168, SA-89]. | Remove references to AIM Series Gyros. | ||
| VG-208 | Service Letter | SL-173 | Orig | 5/2/2001 | Plate and Mod decal replacement | To authorize replacement of Bendix Identification Plate and Modification Decal for service centers with access to TP-260. | 501-1209-01 | |
| VG-208 | Service Letter | SL-111 | Orig | 12/1/1989 | To provide gyro service centers with information regarding allowed use of DG-106 alternate solvent for performing gyro leak check. | |||
| VG-208 | Service Letter | SL-152 | Orig | 1/21/1998 | Provide information on how to replace RCR resistor with an RWR sized resisitor. | 501-1121-01, 501-1209-01, 501-1210-01, 501-1687-01 | ||
| VG-208 | Service Letter | SL-274 | A | 1/4/2012 | To provide offical approval for the use of eqivalent test equipment to test and validate the functionality of vertical gyros manufactured by L-3 Avionics Systems. | |||
| VG-208 | Service Letter | SIL-001-VG-208 | 00 | 3/31/2025 | End of Manufacturing Notice | VG-208 C- End of Manufacturing Notice | 501-1210-01 | |
| VG-401 | Service Letter | SL-274 | A | 1/4/2012 | To provide offical approval for the use of eqivalent test equipment to test and validate the functionality of vertical gyros manufactured by L-3 Avionics Systems. | |||
| VNAV | Service Bulletin | SB-29 | Orig | 5/1/1981 | RNAV612 and 612RIU distance computation error when VNAV541 or VNAV541A has no A+ applied. | , Acron Aviation | 805D0400 | |
| VRS-3000 | Installation Manual | TP-561 | P | 10/18/2016 | Installation Manual | Updated DO-160 Information | 501-1854-1101, 501-1854-1102, 501-1854-1201, 501-1854-1301, 501-1854-1401, 501-1854-1501, 501-1854-1601, 501-1854-2101, 501-1854-2102 | |
| VRS-3000 | Service Bulletin | SB501-1854-1 | B | 11/18/2014 | Add Pulse Width Modulation (PWM) to improve synchro output resolution. | Add Part Number 501-1854-01501 & 501-1854-01601 | 501-1854-1101, 501-1854-1201, 501-1854-1301, 501-1854-1401, 501-1854-1501, 501-1854-1601 | |
| VRS-3000 | Service Bulletin | SB501-1854-2 | B | 11/18/2014 | Prevent the decrease in synchro loopback voltage which could result in ATP or BIT test failure. | ADD P/N 501-1854-1501 & 501-1854-1601 | 501-1854-( ), 501-1854-1101, 501-1854-1201, 501-1854-1301, 501-1854-1401, 501-1854-1501, 501-1854-1601 | |
| VRS-3000 | Service Bulletin | SB501-1854-3 | B | 11/18/2014 | Correct Sensor Calibration. | Add P/N 501-1854-1501 & 501-1854-1601 | 501-1854-1101, 501-1854-1201, 501-1854-1301, 501-1854-1401, 501-1854-1501, 501-1854-1601 | |
| VRS-3000 | Service Bulletin | SB501-1854-4 | A | 10/18/2016 | Software 1.2 | Incorporates Software 1.2 | 501-1854-1101, 501-1854-1201, 501-1854-1301, 501-1854-1401, 501-1854-1501, 501-1854-1601, 501-1854-2101 | |
| VRS-3010 | Installation Manual | TP-592 | F | 10/28/2016 | Installation Manual | Pub# TP-592 | 501-1877-01, 501-1877-02 | |
| VRS-3010 | Service Bulletin | SB501-1877-1 | B | 4/4/2011 | Correct sensor calibration. | 501-1877-01 | ||
| VRS-3010 | Service Bulletin | SB501-1877-3 | A | 10/31/2016 | Software 1.2 | Software 1.2 | 501-1877-01, 501-1877-02 | |
| VRS-3010 | Service Bulletin | SB501-1877-2 | B | 10/28/2016 | Convert VRS-3010 to VRS-3020 (P/N 501-1877-02) to provide access to existing digital outputs | 501-1877-01 | ||
| VRS-3020 | Installation Manual | TP-592 | F | 10/28/2016 | Installation Manual | Pub# TP-592 | 501-1877-01, 501-1877-02 | |
| VRS-3020 | Service Bulletin | SB501-1877-3 | A | 10/31/2016 | Software 1.2 | Software 1.2 | 501-1877-01, 501-1877-02 | |
| VRS-4000 | Installation Manual | TP-598 | E | 4/28/2015 | Installation Manual | Add part number 501-1892-1201 | 501-1892-1101, 501-1892-1201 |