L3Harris Aviation Products Technical Publications Catalog
Last update: 2/7/2023
| Product | Type | Pub Part Number | ATA Number | Revision | Revision Date | Title | Subject/Description | Product Part Number |
|---|---|---|---|---|---|---|---|---|
| 612RIU | Installation Manual | AD009A0480 | Orig | 2/1/1982 | Installation and Maintenance Manual | Pub# AD009A0480 | 805D0480 | |
| 612RIU | Service Bulletin | SB-28 | Orig | 4/1/1981 | Waypoint Alert output during VOR/LOC operation. | 805D0450, 805D0480 | ||
| 7100 CVDR | Component Maintenance Manual | L3HARRIS7100-25583-00001-00 | 31-34-01 | 007 | 11/15/2021 | Component Maintenance Publication (CMP) | Cockpit Voice and Flight Data Recorder (Dual - Deployable), 7100-0200-00 | 7100-0200-00 |
| 7100 CVDR | Component Maintenance Manual | 165E1747-00 | 23-70-05 | 09 | 5/6/2014 | 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 | 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 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 |
| 7100 CVDR | Component Maintenance Manual | 165E6493-00 (OBS) | OBS | 2/11/2020 | 7100 Cockpit Voice and Data Recorder CMM (Obs) | See L3HARRIS7100-25583-00001-00 | 7100-0200-00 | |
| 7100 CVDR | Component Maintenance Manual | 0040-28002-01 | 23-70-75 | 03 | 6/20/2022 | 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 | Installation Manual | 0040-28001-07 | 23-70-79 | 00 | 11/16/2020 | Installation and Operation Manual | Cockpit Voice and Flight Data Recorder (SRVIVR25) CVDR, 7104-3700-00 | 7104-3700-00 |
| 7100 CVDR | Installation Manual | 0040-28001-02 | 23-70-77 | 00 | 6/20/2022 | Installation and Operation Manual | Cockpit Voice and Flight Data Recorder (SRVIVR25) CVDR, 7100-3900-00 | 7100-3900-00 |
| 7100 CVDR | Installation Manual | 0040-28002-20 | 23-70-80 | 00 | 6/20/2022 | Installation and Operation Manual | Cockpit Voice and Flight Data Recorder (SRVIVR25) CVDR, 7104-3000-00 | 7104-3000-00 |
| 7100 CVDR | Instruction Manual | 905-E6493-22 | 01 | 11/30/2021 | Instruction Manual | Accident Investigation Procedure | 7100-0200-00 | |
| 7100 CVDR | Instruction Manual | 0040-28003-01 | 04 | 6/20/2022 | Accident Investigation Procedure | SRVIVR25 Accident Investigation Procedure | 7100-3000-00 7100-3900-00 7102-3900-00 7104-3000-00 7104-3700-00 7100-1000-00 7100-1000-12 7100-1000-30 7100-1000-31 7100-1000-70 7100-1100-00 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 7100-2400-00 7100-2400-12 7100-2400-20 7100-2700-00 7100-2700-20 7100-2700-30 7100-4400-00 7100-4400-70 | |
| 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 | 00 | 6/20/2022 | Software 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 | Software | 840-E4519-05 | 8.4 | 8/14/2019 | 840-E4519-05 | SMP V8.4 6627 FDP V3.8 24AD | 2100- | |
| 7100 CVDR | Software | 840-E4519-08 | 9.0 | 8/14/2019 | 840-E4519-08 | SMP 9.0 3156 FDP 4.1 6605 | 2100- | |
| 7100 CVDR | Supplemental Type Certificate | ST04559CH | c | 1/5/2023 | DE HAVILLAND DHC-8-100/300 | STC for DE HAVILLAND DHC-8-100/300 Rev C: Add TCCA approval certificate | 7100- | |
| 7100 CVR | Component Maintenance Manual | 0040-28002-02 | 23-70-70 | 09 | 11/21/2022 | 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 CVDR | Component Maintenance Manual | 165E1747-00 | 23-70-05 | 09 | 5/6/2014 | 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 | 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 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 |
| 7100 CVR | Installation Manual | 0040-28001-18 | 23-70-89 | 00 | 6/20/2022 | 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 | 00 | 6/20/2022 | Installation and Operation Manual | Cockpit Voice Recorder (SRVIVR25) CVR, 7104-1900-00 | 7104-1900-00 |
| 7100 CVR | Installation Manual | 0040-28001-19 | 23-70-90 | 03 | 10/6/2022 | SRVIVR25 (7100) Installation and Operation Manual | Cockpit Voice Recorder (SRVIVR25) CVR, 7102-1000-00 | 7102-1000-00 |
| 7100 CVR | Installation Manual | 0040-28001-06 | 23-70-73 | 00 | 10/27/2020 | Installation and Operation Manual | Cockpit Voice Recorder (SRVIVR25) CVR, 7100-1000-70 | 7100-1000-70 |
| 7100 CVR | Installation Manual | 0040-28001-13 | 23-70-86 | 03 | 2/28/2022 | 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 | 0040-28001-04 | 23-70-71 | 01 | 2/3/2021 | 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 | 01 | 2/3/2021 | Installation and Operation Manual | Cockpit Voice Recorder (SRVIVR25) CVR | 7100-1900-30, 7100-1900-31 |
| 7100 CVR | Installation Manual | 0040-28001-12 | 23-70-85 | 00 | 9/25/2020 | Installation and Operation Manual | Cockpit Voice Recorder (SRVIVR25) CVR, 7102-1900-30 | 7102-1900-30 |
| 7100 CVR | Installation Manual | 0040-28001-15 | 23-70-87 | 00 | 11/16/2020 | Installation and Operation Manual | Cockpit Voice Recorder (SRVIVR25) CVR, 7100-1000-12 | 7100-1000-12 |
| 7100 CVDR | Instruction Manual | 0040-28003-01 | 04 | 6/20/2022 | Accident Investigation Procedure | SRVIVR25 Accident Investigation Procedure | 7100-3000-00 7100-3900-00 7102-3900-00 7104-3000-00 7104-3700-00 7100-1000-00 7100-1000-12 7100-1000-30 7100-1000-31 7100-1000-70 7100-1100-00 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 7100-2400-00 7100-2400-12 7100-2400-20 7100-2700-00 7100-2700-20 7100-2700-30 7100-4400-00 7100-4400-70 | |
| 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 | 00 | 3/31/2022 | 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 | 00 | 4/13/2022 | 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 1.5 | Software Release 1.5 | 7102-1000-00 |
| 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 | Supplemental Type Certificate | ST04559CH | c | 1/5/2023 | DE HAVILLAND DHC-8-100/300 | STC for DE HAVILLAND DHC-8-100/300 Rev C: Add TCCA approval certificate | 7100- | |
| 7100 CVDR | Component Maintenance Manual | 165E1747-00 | 23-70-05 | 09 | 5/6/2014 | 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 | 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 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 |
| 7100 FDR | Component Maintenance Manual | 0040-28002-03 | 31-30-70 | 03 | 6/20/2022 | 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 | 0040-28001-17 | 31-30-76 | 00 | 6/20/2022 | Installation and Operation Manual | Flight Data Recorder (SRVIVR25) FDR, 7100-2400-20, 7100-2700-20 | 7100-2400-20, 7100-2700-20 |
| 7100 FDR | Installation Manual | 0040-28001-09 | 31-30-72 | 02 | 6/20/2022 | 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 | 02 | 6/20/2022 | Installation and Operation Manual | Cockpit Voice and Flight Data Recorder (SRVIVR25) FDR, 7100-3000-00 | 7100-3000-00 |
| 7100 FDR | Installation Manual | 0040-28001-08 | 31-30-71 | 01 | 6/20/2022 | Installation and Instruction Manual | Flight Data Recorder (SRVIVR25) FDR, 7100-2400-00 7100-2700-00 | 7100-2400-00, 7100-2700-00 |
| 7100 FDR | Installation Manual | 0040-28001-11 | 31-30-74 | 00 | 9/25/2020 | Installation and Operation Manual | Flight Data Recorder (SRVIVR25) FDR | 7100-3700-30 |
| 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 | 00 | 10/27/2020 | Installation and Instruction Manual | Flight Data Recorder (SRVIVR25) FDR, 7100-4400-70 Specific, ARINC 747 Variant, no RIPS | 7100-4400-70 |
| 7100 CVDR | Instruction Manual | 0040-28003-01 | 04 | 6/20/2022 | Accident Investigation Procedure | SRVIVR25 Accident Investigation Procedure | 7100-3000-00 7100-3900-00 7102-3900-00 7104-3000-00 7104-3700-00 7100-1000-00 7100-1000-12 7100-1000-30 7100-1000-31 7100-1000-70 7100-1100-00 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 7100-2400-00 7100-2400-12 7100-2400-20 7100-2700-00 7100-2700-20 7100-2700-30 7100-4400-00 7100-4400-70 | |
| 7100 FDR | Service Bulletin | SB002-SVR7100FDR | 00 | 2/28/2022 | Software Releae 1.4 | Software Release 1.4 | 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 | 00 | 3/31/2022 | AMDT A – New Aircraft Interface CCA | AMDT A – New Aircraft Interface CCA | 7100-2700-30, SVR7100FDR-31-0002 | |
| 7100 FDR | Service Bulletin | SB003-SVR7100FDR | SVR7100FDR-31-6001 | 00 | 6/20/2022 | Software 1.5 | Software Release 1.5 | 7100-2400-00, 7100-2700-00, 7100-4400-00 |
| 7100 CVDR | Supplemental Type Certificate | ST04559CH | c | 1/5/2023 | DE HAVILLAND DHC-8-100/300 | STC for DE HAVILLAND DHC-8-100/300 Rev C: Add TCCA approval certificate | 7100- | |
| 7200 RIU | 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 | |
| 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 | 165E010100 (No DL) | 23-70-01 | 3 | 3/4/2004 | A100 / A100A CVR CMM | A100 / A100A CVR CMM by special request only. Contact Avionics.TechPubs@L3Harris.com | 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 | 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 (No DL) | 23-70-02 | 03 | 7/1/2005 | A100S Component Maintenance Manual | A100S CMM by special request only. Contact Avionics.TechPubs@L3Harris.com | 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 |
| 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 | |
| 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 | 165E1233-00 (No DL) | 23-70-03 | 5 | 3/1/2005 | A200S Component Maintenance Manual | A200S CMM by special request only. Contact Avionics.TechPubs@L3Harris.com | S200–0012–00, S200–0003–00, S200–0003–90, S200–0012–91, S200–0003–91 |
| A200S | Service Letter | A200S SSCVR 003 | 01 | 8/23/2006 | NOTIFICATION OF OBSOLESCENCE | NOTIFICATION OF OBSOLESCENCE | 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 | S200-xxxx-xx | |
| AC | Service Bulletin | SB501-1661-11 | A | 3/14/2008 | REPLACEMENT OF SWITCH ON COMPUTER PCB | REPLACEMENT OF SWITCH ON COMPUTER PCB | 501-1661-03, 501-1661-04, 501-1661-05 | |
| AC | Service Bulletin | SB501-1482-1 | Orig | 11/1/1990 | To reduce "Dim" Annunciator light brightness. | To reduce "Dim" Annunciator light brightness. | 501-1482-01 | |
| AC | Service Bulletin | SB501-1679-5 | Orig | 5/15/2002 | Provide a replacement for a part that is no longer procurable. | Provide a replacement for a part that is no longer procurable. | 501-1679-01, 501-1679-02, 501-1679-03 | |
| AC | 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 | |
| AC-111 | Installation Manual | TP-425 | 22-10-15 | Orig | 6/15/1989 | Installation Manual | Pub# TP-425 | 501-1482-01 |
| 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 | 17A717-03-00 |
| Accelerometer | Installation Manual | 165E4878-00 | 05 | 8/12/2014 | Multi-Axial Accelerometer Installation and Operation Manual w/IPC | Multi-Axial Accelerometer | 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 | 17A542-03-01, ARINC 542 / TRI AXIS, Multi-Axial Accelerometer (High Sensitivity) | |
| AD611 | Service Bulletin | SB-47 | Orig | 8/1/1985 | Modification to DME Range Block Adapter to permit module to operate throughout an input range. | 804B0001 | ||
| AD611 | Service Bulletin | SB-51 | Orig | 8/1/1985 | Modification to DME Range Block Adapter Module to increase A+ voltage range. | 804B0116 | ||
| AD611 | Service Bulletin | SB-52 | Orig | 11/1/1985 | Modification to Range Block Adapter Module to permit operation throughtout voltage range. | 804B0116 | ||
| ADC-3000 | Installation Manual | TP-530 | L | 6/15/2016 | Installation and Operation Manual | Pub# TP-530 | 501-1797-23, 501-1797-24, 501-1797-71, 501-1803-145, 501-1803-31C, 501-1803-32B, 501-1826-01, 501-1851-01, 501-1851-2402, 501-1851-2405 | |
| ADC-3000 | Installation Manual | TP-531 | C | 5/27/2009 | Installation and Operation Manual | Pub# TP-531 | 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-( ) | |
| ADC-3000 | Installation Manual | TP-579 | E | 5/1/2018 | Installation and Operation Manual | Pub# TP-579 | 501-1741-2104, 501-1741-2105, 501-1741-2204, 501-1741-2304, 501-1741-2404, 501-1741-2504, 501-1741-2604, 501-1741-2704, 501-1741-2804, 501-1826-01, 501-1881-01 | |
| ADC-3000 | Installation Manual | TP-593 | E | 12/18/2013 | Installation and Operation Manual | Pub# TP-593 | 501-1797-( ), 501-1803-( ), 501-1826-01, 501-1851-2403, 501-1851-2404 | |
| ADC-3000 | Service Bulletin | SB501-1890-1 | Orig | 2/12/2003 | Eliminates erratic altitude display. | 501-1890-( ) | ||
| 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 | SB501-1797-3 | 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 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-177 | C | 5/13/2004 | Repair station only.... air data anomalies | To inform flight line technicians about air data anomalies they may observe on the GH-3000 Electronic Standby Instrument System display and instructions to correct the air data invalidities. | 501-1741-( ), 501-1797-( ) | |
| 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-3000 | Service Letter | SL-190 | Orig | 9/15/2004 | Missing electro magnetic intererence (EMI) filter seal. | Missing electro magnetic intererence (EMI) filter seal. | 501-1797-( ), 501-1881-( ), 501-1890-( ) | |
| 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-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 | 0040-30001-01 | 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 | 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 | |||
| 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-4000 | Service Letter | SL-255 | A | 12/22/2015 | ADC-4000 Satus Indicator | To provide operational information on ADC-4000 Status Indicator (LED) | 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 | |
| ADI-330 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 1 | 11/28/2022 | 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 | 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 | 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-330 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 1 | 11/28/2022 | 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 | A C5 | 11/11/2013 | Component Maintenance Manual | Pub# TP-438 | 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-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-330 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 1 | 11/28/2022 | 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 | 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 | 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-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-333 | Component Maintenance Manual | TP-446 | 34-20-37 | 2 | 8/13/2018 | Component Maintenance Manual | Pub# TP-446 | 501-1657-01 |
| ADI-330 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 1 | 11/28/2022 | 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 | 34-20-62 | 501-1657-02 |
| ADI-333 | Installation Manual | TP-445 | 34-20-67 | A | 12/23/2005 | Installation and Operation Manual | Pub# TP-445 | 501-1657-01, 501-1657-02 |
| ADI-333 | Intermediate Maintenance Manual | 24-20-76 | A | 7/16/2012 | ADI-333B IMM | 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-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-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-330 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 1 | 11/28/2022 | 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-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-330 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 1 | 11/28/2022 | 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-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-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-350 | Component Maintenance Manual | TP-545 | A C1 | 9/3/2002 | Maintenance Manual with IPL | Pub# TP-545 | 501-1742-01 | |
| ADI-350 | Component Maintenance Manual | TP-442 | 34-20-34 | 2 | 6/27/2018 | Component Maintenance Manual | Pub# TP-442 | 406-375-220-101, 501-1617-01 |
| ADI-350 | Component Maintenance Manual | TP-403 | 34-20-22 | Orig | 9/1/1986 | Intermediate Maintenance Manual | Pub# TP-403 | 501-1442-01 |
| ADI-350 | Component Maintenance Manual | TP-390 | 34-20-10 | Orig | 12/1/1983 | Maintenance Manual with IPL | 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 | 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-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- | |
| ADLP - software | Instruction Manual | 165E3596-03 | 01 | 7/15/2021 | ADLP Software v3.6 Operator's Manual | Operator's Manual for ADLP software version 3.6 | 17TES0436 | |
| AFIRS 228S - Iridium | Component Maintenance Manual | 165E5733-10 | 23-28-01 | 08 | 4/26/2022 | AFIRS 228S Iridium CMM | Level 1 Maintenance | 228E5733-00, 228E5733-01, 418E5733-00, 418E5733-01 |
| AFIRS 228S - Iridium | Installation Manual | 165E5733-02 | C | 4/30/2022 | 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 | 05 | 4/26/2022 | 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 | Iridium-SB001 | 00 | 7/11/2016 | Software Revision 17 | Software Revision 17 | 228E5733-00 | |
| AFIRS 228S - Iridium | Service Bulletin | Iridium-SB002 | 07 | 5/11/2018 | MOD 1. fix several field issues | MOD 1 | 228E5733-00 | |
| AFIRS 228S - Iridium | Service Bulletin | Iridium-SB003 | 00 | 9/23/2019 | Software (OFP) 840E5733-18 | Software Revision 18 | 228E5733-00 | |
| AFIRS 228S - Iridium | Service Bulletin | Iridium-SB004 | 00 | 8/20/2019 | SDU functionality | ADMT 4 To increase SDU functionality by adding simultaneous transmission of voice and data. | 228E5733-00 | |
| AFIRS 228S - Iridium | Service Bulletin | SB009-Iridium | SDU228-23-0004 | 01 | 9/6/2022 | SDU Part Number Conversion to 228E5733-01 ADMT A | SDU Part Number Conversion to 228E5733-01 ADMT A | 228E5733-00, 228E5733-01 |
| AFIRS 228S - Iridium | Service Bulletin | SB008-Iridium | SDU228-23-0001 | 04 | 12/13/2022 | 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) | 228E5733-00, 228E5733-01, 228E5733-01 AMDT A, |
| AFIRS 228S - Iridium | Service Bulletin | SB006-Iridium | 02 | 9/26/2022 | Software (OFP) 840E5733-20 | Customer notification of Software 20. | 228E5733-00, 228E5733-01, 228E5733-01 AMDT A | |
| AFIRS 228S - Iridium | Service Bulletin | SB005-Iridium | SDU-23-0000 | 00 | 9/30/2020 | Remove and Replace Data Modem Instructions | Remove and Replace Data Modem Instructions. | 228E5733-00, L3 Aviation Products Repair Station and Authorized Repair Centers Only |
| 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 |
| ADI-330 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 1 | 11/28/2022 | 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-480 | 34-20-54 | A | 4/3/2018 | Installation and Operation Manual | Pub# TP-480 | 501-1568-29, 501-1568-44 |
| 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 | Pilot Guide | TP-573 | D | 2/5/2018 | Pilot's Guide | Pub# TP-573 | 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 | SB501-1568-1 | 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 | SB501-1657-1 | A | 1/22/2003 | To prevent switch damage and shaft separation. | To prevent switch damage and shaft separation. | 501-1657-01 | |
| AI-330 | Service 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-() | ||
| 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-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 |
| ADI-330 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 1 | 11/28/2022 | 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-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 | ||
| 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-330 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 1 | 11/28/2022 | 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 | A1 | 6/7/2018 | Maintenance Manual | Pub#TP-674 | 501-1817-01, 501-1817-02 | |
| 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-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 | SB501-1856-01 | A | 1/23/2012 | Reduce the possibility of bearing damaging sphere housing. | 501-1856-01 | ||
| 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 | SB501-1817-3 | 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 | SB501-1757-1 | 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 | SB501-1745-1 | 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 | SB501-1817-1 | 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 | ||
| 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-330 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 1 | 11/28/2022 | 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-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 | Pub#TP-625 | 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-() | |
| 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- | |
| 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 | |
| ADI-330 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 1 | 11/28/2022 | 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-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-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-439 | 34-20-31 | 1 | 2/8/2016 | Maintenance Manual | Pub# TP-439 | 501-1647-01 |
| 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-803 | Installation Manual | TP-537 | C | 2/4/2016 | Installation and Operation Manual | Pub# TP-537 | 501-1804-01 | |
| AI-803 | Installation Manual | TP-516 | 35-20-66 | 7/26/2005 | Installation and Operation Manual | Pub# TP-516 | 501-1820-01 | |
| AI-803 | Installation Manual | TP-675 | D | 2/4/2016 | AI-803DJ Install Manual | AI-803DJ Install Manual | 501-1907-01 | |
| AI-803 | Installation Manual | TP-590 | C | 2/4/2016 | Installation and Operation Manual | Pub# TP-590 | 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 | SB501-1832-1 | 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 | SB501-1857-2 | 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 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 | SB501-1821-2 | Orig | 5/1/2001 | Improve reliability of erection system. | 501-1821-01 | ||
| 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 | SB501-1857-1 | Orig | 4/17/2002 | Reliability improvement. New part has strengthened locking tang. | 501-1857-01 | ||
| AI-803 | Service Bulletin | SB501-1710-1 | Orig | 12/3/1999 | Removal of external label from unit. | 501-1710-01 | ||
| 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- | |
| AI-803 | Service Letter | SL-162 | Orig | 6/10/1999 | To establish authorization to remove lead seal and replace with safety wire. | |||
| 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-555 | 34-20-01A | B | 6/29/2016 | Component Maintenance Manual | This Revision corrects major volumes of text | 501-1197-20 |
| ADI-330 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 1 | 11/28/2022 | 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 | 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-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-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-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 | Installation Manual | TP-599 | C | 2/4/2016 | Installation and Operation | Pub# TP-599 | 501-1748-01 | |
| AI-804 | Instruction Manual | TP-630 | A | 2/12/2009 | AI-804 Instruction Manual | AI-804 IMM | 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 | SB501-1197-1 | 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 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 | SB501-1748-1 | 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 | SB501-1848-1 | 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 | SB501-1811-1 | 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 | SB501-1798-1 | 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 | SB501-1748-2 | 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 | SB501-1412-1 | 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 | SB501-1296-1 | 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 Letter | SL-77 | Orig | 5/1/1984 | To provide information regarding updated procedures for Model AI-804 Attitude Indicator rotor housing assembly overhaul and repair. | |||
| 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. | |||
| 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- | |
| AI-804 | Service Letter | SL-12 | E | 4/23/2010 | To provide Attitude Indicator operation information. | |||
| AI-804 | Service Letter | SL-281 | A | 10/18/2012 | TP-218 Manual Corrections | |||
| ADI-330 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 1 | 11/28/2022 | 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-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 | |
| 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- | |
| AI-903 | Service Letter | SL-184 | Orig | 12/5/2003 | Proper Operation of Caging Knob | |||
| ADI-330 | Component Maintenance Manual | TP-508 | 34-21-01 | C, Chg 1 | 11/28/2022 | 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-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-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 | 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 | SB501-1170-1 | 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 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. | 501-1078-( ) | ||
| 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 Letter | SL-54 | B | 3/4/1991 | To provide gyro overhaul service centers with information regarding updated procedures for model AI-904 Attitude Indicator rotor housing assembly overhaul and repair. | |||
| 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- | |
| AI-804 | Service Letter | SL-12 | E | 4/23/2010 | To provide Attitude Indicator operation information. | |||
| 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 | |
| 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- | |
| AP General Files | Drawings / SPEC | AutoPilot Service | D | 3/9/2017 | Change location of DN-104 repairs | Change location of DN-104 repairs | 501- | |
| 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 | |
| AP General Files | Miscellaneous | Misc. | n/a | 8/22/2022 | Provide list of publications that provide general information on L3 policy, procedures, etc. | Provide list of publications that provide general information on L3 policy, procedures, etc. | all | |
| AP General Files | Miscellaneous | PS-8xx General Information | - | 5/14/2015 | Lead-Acid Battery - PS-8xx | Lead-Acid Battery - PS-8xx | general | |
| 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 | General Information | x.x | 9/8/2022 | Provide list of publications that provide general informaton on L3 policy, procudures, etc. | list of publications that provide general information | all | |
| AP General Files | Pilot Guide | TP-572 | 34-20-62 | V1.0 | 11/1/2001 | CD-ROM - Attitude Indicator Operation | Pub# TP-572 | 501- |
| AP General Files | Service Letter | SL-295n | C | 9/11/2018 | Repair and Overhaul Information | Replacement for RG-227 Transfer of service to Butler Avionics. Obsolete product. | 501-1033-02, 501-1033-03, 501-1169-01, 501-1169-02 | |
| AP General Files | Service Letter | SL-307 | A | 2/29/2016 | Maintenance Manual Revision Packets | Discontinue issuing of Revision Packets | Multi- | |
| AC | 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-261 | F | 4/5/2021 | Shipping Instructions for International Customers | Shipping Instructions for International Customers | 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-293 | E | 11/28/2017 | Spare Piece Part Sales | Spare Piece Part Sales | General | |
| 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- | |
| 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-141 | N | 3/31/2016 | To provide customers a list of technical manuals available for sale by Aviation Products. | List of technical manuals available for sale by Aviation Products. | general | |
| AP General Files | Service Letter | SL-144 | A | 8/31/1998 | Listings of product model numbers and related ownership, design authority, and service responsibilities. | Listings of product model numbers and related ownership, design authority, and service responsibilities. | 505- | |
| 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-39 | A | 7/15/1981 | diode replacement | To inform BFG product users of suitable replacement parts for hard to procure zener diodes, 1N471A and 1N474. | zener diodes, 1N471A and 1N474. | |
| 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-175 | E | 11/30/2021 | Cross-reference of Avaition Products chemical part numbers to vendor and vendor numbers. | Chemical part numbers cross-reference | general | |
| 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 | SL-353 | A | 2/4/2020 | Discontinued Literature Package Distribution | Discontinued Literature Package Distribution | n/a | |
| 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 | 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-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 | 02 | 11/21/2022 | Support Logistics Services Partner Transition | Support Logistics Services Partner Transition | all | |
| 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 | |
| A200S | Service Letter | A200S SSCVR 004 | Orig | 2/3/2011 | NOTIFICATION OF DISCONTINUED PARTS SUPPORT - A200S | NOTIFICATION OF DISCONTINUED PARTS SUPPORT | S200-xxxx-xx | |
| 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-002 | 00 | 7/1/2020 | Change of manufacturers Cage Code. | Change of manufacturers Cage Code. | general | |
| AP General Files | Service Letter | PI/2-001 | 01 | 6/20/2022 | Notification of discontinued product. | Notification of discontinued product. | 17TES0062, 17TES0065, 17TES0066, 17TES0092 | |
| AP General Files | Service Letter | SIL-006 | 01 | 2/2/2023 | 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 | 01 | 2/2/2023 | 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 | |
| BC-815 | Component Maintenance Manual | TP-354 | 1 C | 1/24/2008 | Maintenance Manual | Pub# TP-354 | 501-1321-01 | |
| BC-815 | Installation Manual | TP-350 | B | 6/28/2010 | Installation Instructions | Pub# TP-350 | 501-1321-01 | |
| BTP-1634 | Installation Manual | 009-10140-001 | C | 6/2/2008 | Instruction Manual | Pub# 009-10140-001 | 805-10045-001 | |
| CA-2001 | Installation Manual | TP-258 | Orig | 8/1/1980 | Instruction Manual, Operation and Installation | Pub# TP-258 | 501-1172-01, 501-1172-02, 501-1172-03, 501-1172-04, 501-1172-05, 501-1172-06, 501-1196-01, 501-1196-02, 501-1199-01, 501-1199-02, 501-1199-03, 501-1199-04, 501-1199-05, 501-1199-06, 501-1200-01, 501-1200-02, 501-1200-03, 501-1200-04, 501-1200-05, 501-1201-01, 501-1201-02, 501-1202-01, 501-1202-02, 501-1207-01, 501-1207-02, 501-1207-03, 501-1207-04, 501-1207-05, 501-1207-06, 501-1207-07, 501-1207-08, 501-1232-02, 501-1232-03, 501-1232-04, 501-1232-05, 501-1232-06, 501-1279-01 | |
| 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 | |
| CA-2001 | Service Letter | SL-29 | Orig | 1/9/1980 | To provide information concerning the installation changes necessary for installing CDU with tactile keyboard. | To provide information concerning the installation changes necessary for installing CDU with tactile keyboard. | 501-1172-01, 501-1172-02 | |
| CA-431 | Component Maintenance Manual | TP-452 | 32-50-02 | A | 6/7/2017 | Component Maintenance Manual | Pub# TP-452 | 501-1661-03 501-1661-04 501-1661-05 |
| CA-431 | Service Bulletin | SB501-1726-5 | A | 3/14/2008 | REPLACEMENT FOR SWITCH AND PRIMARY PROCESSOR BOARD | REPLACEMENT FOR SWITCH AND PRIMARY PROCESSOR BOARD | 501-1726-01 | |
| CA-460 | Service Bulletin | SB501-1708-8 | A | 3/14/2008 | REPLACEMENT FOR SWITCH AND PRIMARY PROCESSOR BOARD | REPLACEMENT FOR SWITCH AND PRIMARY PROCESSOR BOARD | 501-1708-( ), 501-1708-02, 501-1708-03 | |
| CA-460 | Service Bulletin | SB501-1708-5 | A | 5/1/2001 | To provide replacement voltage regulator for device no longer procurable. | 501-1708-02, 501-1708-03 | ||
| CA-460 | Service Bulletin | SB501-1708-7 | Orig | 9/26/2001 | To change Amplifier gain to move rudder pedal force command readings closer to the nominal value within the range. | 501-1708-02, 501-1708-03 | ||
| CA-530 | Service Bulletin | SB501-1553-1 | Orig | 6/1/1990 | To provide for use of a capacitor with improved reliability. | 501-1553-01, 501-1553-02 | ||
| CA-530 | Service Bulletin | SB501-1553-2 | 7/26/2005 | None | 501-1553-01, 501-1553-02 | |||
| CA-530 | Service Bulletin | SB501-1553-3 | Orig | 3/1/1992 | To update CA-530H, part number 501-1553-01, to CA-530K, part number 501-1553-03. | 501-1553-01, 501-1553-03 | ||
| CA-530 | Service Bulletin | SB501-1553-4 | Orig | 3/1/1992 | To update CA-530J, part number 501-1553-02 to CA-530K, part number 501-1553-03. | 501-1553-02 | ||
| CA-530 | Service Letter | SL-116 | A | 7/2/1993 | To provide customers with bench level test procedures for the subject computer amplifiers pending a component maintenance manual generation. | 501-1553-01, 501-1553-02, 501-1553-03 | ||
| 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 | |
| 7200 RIU | 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 | |
| CA-2001 | Installation Manual | TP-258 | Orig | 8/1/1980 | Instruction Manual, Operation and Installation | Pub# TP-258 | 501-1172-01, 501-1172-02, 501-1172-03, 501-1172-04, 501-1172-05, 501-1172-06, 501-1196-01, 501-1196-02, 501-1199-01, 501-1199-02, 501-1199-03, 501-1199-04, 501-1199-05, 501-1199-06, 501-1200-01, 501-1200-02, 501-1200-03, 501-1200-04, 501-1200-05, 501-1201-01, 501-1201-02, 501-1202-01, 501-1202-02, 501-1207-01, 501-1207-02, 501-1207-03, 501-1207-04, 501-1207-05, 501-1207-06, 501-1207-07, 501-1207-08, 501-1232-02, 501-1232-03, 501-1232-04, 501-1232-05, 501-1232-06, 501-1279-01 | |
| 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 | ||
| CA-2001 | Service Letter | SL-29 | Orig | 1/9/1980 | To provide information concerning the installation changes necessary for installing CDU with tactile keyboard. | To provide information concerning the installation changes necessary for installing CDU with tactile keyboard. | 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). | 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 | ||
| 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 |
| 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 |
| CT-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 | ||
| DAC-Digital Airborne Computer | Service Bulletin | SB501-1279-1 | Orig | 4/3/1980 | To remoce IFR certification. | 501-1207-( ), 501-1279-01, 501-1280-01 | ||
| DAC-Digital Airborne Computer | Service Bulletin | SB501-1279-4 | Orig | 6/15/1980 | To reinstate IFR certification. | 501-1207-05, 501-1207-08, 501-1207-09, 501-1279-01, 501-1280-01 | ||
| DAC-Digital Airborne Computer | Service Bulletin | SB501-1280-3 | 7/26/2005 | SB501-1280-3 | ||||
| DAC-Digital Airborne Computer | Service Bulletin | SB501-1207-10 | Orig | 6/1/1980 | To reinstate IFR certification. | 501-1207-05, 501-1207-08, 501-1207-09, 501-1279-01, 501-1280-01 | ||
| DAC-Digital Airborne Computer | Service Bulletin | SB501-1207-2 | Orig | 1/1/1978 | To change memory program circuit card. | 501-1207-( ) | ||
| DAC-Digital Airborne Computer | Service Bulletin | SB501-1207-8 | Orig | 4/1/1980 | To remove IFR certification. | 501-1207-( ), 501-1279-01, 501-1280-01 | ||
| DAC-Digital Airborne Computer | Service Letter | SL-24 | Orig | 4/24/1978 | To provide information on replacement of fuse with bus wire to prevent loss of +28 Vdc due to inadvertent blowing of fuse on DC-2001( ) Digital Computers containing Power Supply Assembly PN 502-1105-01. | |||
| DAC-Digital Airborne Computer | Service Letter | SL-36 | C | 1/8/1981 | To provide RNAV System operation that alleviates problems outlined in ALERT Service Bulletins. | |||
| DAC-Digital Airborne Computer | Service Letter | SL-37 | Orig | 6/15/1980 | To comply with the final requirements necessary for cancellation of RNAV ALERT Service Bulletins. | |||
| DAC-Digital Airborne Computer | Service Letter | SL-50 | B | 3/3/1982 | To improve DeHavilland-7 RNAV operations. | |||
| DAC-Digital Airborne Computer | Service Letter | SL-52 | Orig | 1/18/1982 | To eliminate reading the RMI in Test Stages 2 and 3 of RNAV Self Test. | |||
| DAC-Digital Airborne Computer | Supplemental Type Certificate | SA160GL | Amen | 4/15/1977 | Install a J.E.T. DAC-2000 3-D RNAV system. | Install a J.E.T. DAC-2000 3-D RNAV system. | ||
| DAC-Digital Airborne Computer | Supplemental Type Certificate | SA190GL | Orig | 8/16/1977 | Install a J.E.T. DAC-2000 3-D RNAV system. | Install a J.E.T. DAC-2000 3-D RNAV system. | ||
| DAC-Digital Airborne Computer | Supplemental Type Certificate | SA135GL-FMS | Orig | 10/26/1976 | Install a J.E.T. DAC-2000 3-D RNAV system. | Install a J.E.T. DAC-2000 3-D RNAV system. | ||
| DB-340 | Component Maintenance Manual | TP-413 | 27-30-03 | 2 | 9/30/1992 | Maintenance Manual with IPL | Pub# TP-413 | 501-1421-01, 501-1478-01, 501-1546-01 |
| DB-340 | Component Maintenance Manual | TP-391 | 27-30-02 | 5 | 2/15/1986 | Maintenance Manual | Pub# TP-391 | 501-1419-01, 501-1420-01, 501-1421-01, 93-02-861-002 |
| DB-340 | Component Maintenance Manual | TP-465 | 27-30-04 | Orig | 12/23/1992 | Component Maintenance Manual | Pub# TP-465 | 501-1421-01, 501-1478-02, 501-1546-02 |
| DB-341 | Service Bulletin | SB501-1864-1 | Orig | 5/15/2003 | To improve the consistency of the slip clutch torque setting. | 501-1864-01 | ||
| DB-350 | Component Maintenance Manual | TP-485 | 27-39-04 | A | 2/20/2019 | Component Maintenance Manual | Pub# TP-485 | 501-1505-02 |
| DB-360 | Component Maintenance Manual | TP-466 | 27-30-05 | A C2 | 5/2/2016 | CMM with IPL | 501-1684, 501-1684-01, 501-1684-02, 501-1684-03, 501-1684-04, 501-1685, 501-1685-01, 501-1685-02, 501-1685-03, 501-1685-04, 501-1716, 501-1716-01, 501-1716-02, 501-1716-03, 501-1716-04 | |
| DB-380 | Component Maintenance Manual | TP-499 | 27-30-08 | B | 5/30/2018 | Component Maintenance Manual | Pub# TP-499 | 501-1770-01, 501-1770-02, 501-1771-01, 501-1771-02, 501-1772-01, 501-1772-02 |
| DB-380 | Component Maintenance Manual | TP-538 | 27-30-11 | B | 5/30/2018 | Component Maintenance Manual | Pub# TP-538 | 501-1770-03, 501-1770-04, 501-1771-02, 501-1771-04, 501-1772-03, 501-1772-04 |
| DB-380 | Component Maintenance Manual | TP-556 | 27-30-12 | C | 5/30/2018 | Component Maintenance Manual | Pub# TP-556 | 501-1770-05, 501-1771-05, 501-1772-05 |
| DB-380 | Service Bulletin | SB501-1771-1 | Orig | 5/15/2003 | To provide the consistency of the slip clutch torque setting. | 501-1771-(), 501-1771-01 | ||
| DB-380 | Service Letter | SL-160 | Orig | 5/13/1999 | Establishment of new torque requirement when attaching Capstan to Servo Actuator. | 501-1771-01 | ||
| DB-600 | Component Maintenance Manual | TP-323 | 27-39-01 | E C5 | 10/28/2016 | Component Maintenance Manual | Pub# TP-323 | 501-1247-03, 501-1247-04, 501-1247-05, 501-1258-01, 501-1259-03, 501-1259-04, 501-1259-05 |
| DB-600 | Service Bulletin | SB501-1258-1 | A | 2/6/2003 | To improve stability of slip clutch torque setting. | 501-1258-01 | ||
| DB-600 | Service Bulletin | SB501-1258-2 | Orig | 2/6/2003 | To reduce hysteretic effect and increase clutch slip torque stability over time. | 501-1258-01 | ||
| DB-600 | Service Bulletin | SB501-1258-3 | Orig | 5/15/2003 | To improve the consistency of the slip clutch torque setting. | 501-1258-01 | ||
| DB-600 | Service Bulletin | SB501-1258-5 | A | 10/1/2009 | Improve Fatigue properties | Improve Fatigue properties | 501-1258-01 | |
| DB-600 | Service Bulletin | SB501-1258-4 | A | 1/18/2008 | Prevent contact between drum stop and servo mating part | DB-600 Capstan Assembly | 501-1258-01, 501-1258-02 | |
| 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 | Pub# TP-582 | 501-1826-01, 501-1860-0102, 501-1860-0104, 501-1870-( ) | |
| ADC-3000 | Installation Manual | TP-579 | E | 5/1/2018 | Installation and Operation Manual | Pub# TP-579 | 501-1741-2104, 501-1741-2105, 501-1741-2204, 501-1741-2304, 501-1741-2404, 501-1741-2504, 501-1741-2604, 501-1741-2704, 501-1741-2804, 501-1826-01, 501-1881-01 | |
| ADC-3000 | Installation Manual | TP-593 | E | 12/18/2013 | Installation and Operation Manual | Pub# TP-593 | 501-1797-( ), 501-1803-( ), 501-1826-01, 501-1851-2403, 501-1851-2404 | |
| ADC-3000 | Installation Manual | TP-531 | C | 5/27/2009 | Installation and Operation Manual | Pub# TP-531 | 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-( ) | |
| ADC-3000 | Installation Manual | TP-530 | L | 6/15/2016 | Installation and Operation Manual | Pub# TP-530 | 501-1797-23, 501-1797-24, 501-1797-71, 501-1803-145, 501-1803-31C, 501-1803-32B, 501-1826-01, 501-1851-01, 501-1851-2402, 501-1851-2405 | |
| DCM | Installation Manual | TP-559 | K | 3/30/2017 | Installation and Operation Manual, GH-3100 | 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 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-2001 | Service Bulletin | SB501-1207-1 | 7/26/2005 | SB501-1207-1 | ||||
| DGS-710 | Component Maintenance Manual | TP-474 | 1 | 7/20/1994 | Component Maintenance Manual | Pub# TP-474 | 510-1140-01, 510-1140-02 | |
| 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 |
| DGS-710 | Installation Manual | TP-429 | 34-20-26 | Orig | 12/1/1989 | Installation Manual | Pub# TP-429 | 501-1518-01, 501-1518-02 |
| CT-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 | 805D0570 | ||
| DI681 | Service Bulletin | SB-44 | Orig | 6/1/1984 | To allow the RNC601 to communicate with the DI681 DataBase. | 805D0550 | ||
| DI681 | Service Bulletin | SB-46 | Orit | 9/1/1984 | To eliminate wavering left/right needle and erratic OBS operation. | 805D0550 | ||
| DI681 | Service Bulletin | SB-57 | Orig | 2/1/1988 | To allow DI681 to operate as DI681A with RNC601B. | 805D0570 | ||
| 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 | |
| DME | 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-701 | Component Maintenance Manual | TP-398 | 34-20-20 | 7/26/2005 | Maintenance Manual | Pub# TP-398 | ||
| 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 | C | 7/20/2017 | DU-42 Pilots Guide | Pilots Guide | 9200-38500, 9200-38600 | |
| DU-42 | Printer Copies | 0040-38500-01PC | C | 7/20/2017 | DU-42 Pilots Guide | Printer copy DU-42 PG | ||
| DU-42 | Service Bulletin | SB9200-38500-2 | A | 3/15/2016 | DU-42 MOD B | Incorporation of MOD B | 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 | 9200-38600, 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 | 9200-38500-0201 | ||
| DU-42 | Service Bulletin | SB9200-38600-3 | A | 4/19/2016 | Improve engagement of the rear connector standoffs to Connector J3 | 9200-38600-0201 | ||
| DU-42 | Service Bulletin | SB9200-38600-4 | A | 8/25/2016 | Incorporation of MOD D | MOD D | 9200-38600-0201 | |
| DU-42 | Service Bulletin | SB9200-38500-5 | A | 8/14/2017 | Inspection MOD | 9200-38500-0201 | ||
| DU-42 | Service Bulletin | SB9200-38600-5 | A | 8/14/2017 | Inspection MOD | 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 | SB501-1871-4 | B | 2/12/2009 | Provide replacement display due to diminishing source. | 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 | ||
| EFD-750 | Installation Aircraft Tools | 576-6343-02 | 1.00 | 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 | 576-6343-01 | 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 | 576-6343-03 | 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) | 576-6343-03, 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 | E | 7/14/2021 | EFD-750 / MAG-500 Installation Manual | includes SW1.2 / new part number | 9200-15751-0101, 9200-15753-0101, 9200-15754-0101, 9200-15754-0201, 9200-15500-0101, 9200-15500-0201, 9200-15750-0101, 9200-15751-0201, 9200-15754-0301 | |
| EFD-750 | Pilot Guide | 0040-15750-01 | C | 12/12/2019 | EFD-750 Operation Manual | includes SW1.2 | 9200-15753-0101, 9200-15754-0101, 9200-15754-0201, 9200-15751-0101, 9200-15751-0201, 9200-15750-0101 | |
| EFD-750 | Service Bulletin | SB001-EFD-750 | A | 12/12/2019 | System Software Release 1.2 | System Software Release 1.2 | 9200-15753-0101, 9200-15754-0101, 9200-15754-0201 | |
| EFD-750 | Service Bulletin | SB002-EFD-750 | 01 | 8/18/2021 | The incorporation of MOD A provides improved reliability, especially during operation at cold ambient temperatures of -15 Celsius and below. | MOD A – Operational Improvement in Cold Environments | 9200-15750-0101, 9200-15751-0101, 9200-15751-0201, 9200-15753-0101, 9200-15754-0101, 9200-15754-0201 | |
| EFD-750 | Software | EFD-750 Software 1.1 | 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 | 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 | 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 | E | 1/27/2020 | 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 | EFI-650 Installation and Operation Manual (ATR) | 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 | |
| EHSI-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 | ||
| 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 | ||
| ESI-1000 | Installation Manual | 0040-32001-01 | U | 10/13/2017 | ESI-1000 Installation Manual | Pub# 0040-32001-01 | 9200-32000-0101 | |
| 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 | ||
| ESI-1000 | Service Bulletin | SB9200-32000-1 | A | 5/3/2010 | Revise night lighting color from blue to white | 9200-32000-0301, 9200-32000-0401 | ||
| ESI-1000 | Service Bulletin | SB9200-32000-2 | B | 8/6/2012 | Incorporation of Mod 2 | 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 | 9200-32100-0101, 9200-32100-0201, 9200-32100-1001 | ||
| ESI-1000 | Service Bulletin | SB9200-32100-1 | A | 12/22/2010 | LED Backlight is obsolete | 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 | 9200-32000-0301, 9200-32000-0401, 9200-32000-0701, 9200-32000-0801 | ||
| 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 | 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 | 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 | 9200-32100-0101, 9200-32100-0201, 9200-32100-1001 | ||
| 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 | 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 | 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) | 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 | 9200-32100-0201 | |
| 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 | 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 | Supplemental Type Certificate | SA02738CH | 2/15/2022 | ESI-1000 and ESI-2000 - Permission to Use AML STC | ESI-1000 and ESI-2000 | |||
| 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 | SB9200-32500-2 | 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 | 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 | 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 | SB9200-32500-1 | A | 11/11/2010 | Release of new software | Software 1.12 | 9200-32500-0011, 9200-32500-0021, 9200-32500-0031, 9200-32500-0041 | |
| ESI-2000 | Service Bulletin | SB-9200-32500-4 | A | 9/14/2016 | To prevent rate sensor loopback failure at statrt up | To prevent rate sensor loopback failure at statrt up | 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-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-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-2000 | Service Letter | SL-286 | C | 4/1/2016 | Annual battery maintenance | ESI-2000 Battery Maintenance | 9200-32500, 9200-32501 | |
| 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-1000 | Supplemental Type Certificate | SA02738CH | 2/15/2022 | ESI-1000 and ESI-2000 - Permission to Use AML STC | ESI-1000 and ESI-2000 | |||
| ESI-500 | Installation Manual | 0040-15001-01 | J | 2/9/2021 | ESI-500 /MAG-500 Installation Manual | Electronic Standby Indicator | 9200-15000-0101, 9200-15500-0101 | |
| ESI-500 | Pilot Guide | 0040-15000-01 | F | 10/2/2019 | Pilot Guide | ESI-500 Pilot Guide | 9200-15000-0101, 9200-15500-0101 | |
| ESI-500 | Service Bulletin | SB9200-15000-4 | A | 12/15/2016 | Informs customers of 1.3 Software release | Informs customers of 1.3 Software release | 9200-15000-0101 | |
| ESI-500 | Service Bulletin | SB9200-15000-5 | A | 2/17/2017 | 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 | A | 6/6/2016 | The units airspeed sensor output may shift | 9200-15000-0101 | ||
| ESI-500 | Service Bulletin | SB9200-15000-2 | A | 4/20/2016 | ESI-500 Software 1.2 with ACM Tool | 9200-15000-0101 | ||
| ESI-500 | Service Bulletin | SB9200-15000-1 | A | 12/14/2015 | MOD A | Applies to S/N 1021; 1025; 1029; 1030; &1032 | 9200-15000-0101 | |
| ESI-500 | Service Bulletin | SB9200-15000-6 | A | 2/27/2018 | the vertical speed output from the ESI-500 can potentially exceed the tolerances specified for an air data computer. | 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-305 | A | 12/17/2015 | To Prevent damage to MicroSD Card | To Prevent damage to MicroSD Card | 9200-15000-0101 | |
| ESI-500 | Service Letter | SL-309 | B | 3/29/2018 | ESI-500 Battery Maintenance | ESI-500 Battery Maintenance | 9200-15000-0101 | |
| ESI-500 | Service Letter | SL-323 | A | 2/28/2017 | Setting The Real Time Clock | Setting the Real Time Clock | 9200-15000-0101 | |
| ESI-500 | Service Letter | SL-316 | A | 12/15/2016 | 68DC & 71DC Database Subscription | 68DC & 71DC Database Subscription | 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 1.3 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 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-500-15000-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-R01.01 | 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-R01.03 | 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 | H | 12/7/2022 | Installation Manual | Electronic Standby Instrument System with Touch Screen | 9200-43000-0201 | |
| ESIS-5000 | Intermediate Maintenance Manual | 0040-43003-01 | F | 12/7/2022 | Intermediate Maintenance Manual | Electronic Standby Instrument System Level 1 Maintenance | 9200-43000-0201 | |
| ESIS-5000 | Pilot Guide | 0040-43000-01 | C | 9/8/2021 | ESIS 5000 Pilots Guide | Software Release 1.2 | 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 | 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 | 9200-43000-0201 | |
| ESIS-5000 | Service Bulletin | SB9200-43000-3 | A | 2/27/2017 | Software Release 1.1 | Software Release 1.1 | 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. | 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. | 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. | 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 | 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 | 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 | 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 (No DL) | 31-30-02 | TR6 | 5/12/2017 | F1000 Component Maintenance Manual | F1000 CMM by special request only. Contact Avionics.TechPubs@L3Harris.com | 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 | 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 | |
| AP General Files | Service Letter | PI/2-001 | 01 | 6/20/2022 | Notification of discontinued product. | Notification of discontinued product. | 17TES0062, 17TES0065, 17TES0066, 17TES0092 | |
| F1000 | Service Letter | F1000 SSFDR 007 | Orig | 8/12/2014 | Access to F1000 Publications | Access to F1000 Publications | s603-xxxx-xx, s703-xxxx-xx, s800-xxxx-xx, s903-xxxx-xx | |
| F3849 | Installation Manual | 009A0301 | 1 | 8/1/1988 | Installation Manual | Pub# 009A0301 | 805C0620-( ), 805D0602-( ), 805D0660-( ), 805D0661-( ), 805D0662-( ), 805D0663-( ) | |
| F3849 | Installation Manual | 009A0301 | 1 | 8/1/1988 | Installation Manual | Pub# 009A0301 | 805C0620-( ), 805D0602-( ), 805D0660-( ), 805D0661-( ), 805D0662-( ), 805D0663-( ) | |
| F3849 | Installation Manual | 009A0301 | 1 | 8/1/1988 | Installation Manual | Pub# 009A0301 | 805C0620-( ), 805D0602-( ), 805D0660-( ), 805D0661-( ), 805D0662-( ), 805D0663-( ) | |
| F6555 | Service Bulletin | SB805D0663-200 | A | 2/10/2005 | Removing Rubber boots from switches | 805D0663-31 | ||
| F800 | Component Maintenance Manual | 165E0049-00 (No DL) | 31-30-01 | 2 | 1/31/1994 | F800 Component Maintenance Manual | F800 CMM Paper only. Contact techsupport.cas@L3Harris.com | 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 | Service Letter | F800 DFR007 | Orig | 8/12/2014 | Access to F800 technical publications | Access to F800 technical publications | ||
| FA2100 CVDR | Component Maintenance Manual | 165E1690-00 | 23-70-07 | 07 | 8/16/2019 | FA2100 CVDR CMM | FA2100 CVDR CMM | 2100-3073-00, 2100-3073-51, 2100-3083-00, 2100-3083-10, 2100-3083-50, 2100-3083-51, 2100-3084-00, 2100-3283-10, 2100-3283-50 |
| FA2100 CVDR | Component Maintenance Manual | 165E1690-90 | 23-70-90 | 02 | 9/30/2021 | FA2100 CVDR CMM (ITAR) | FA2100 CVDR Component Maintenance Manual (ITAR) | 2100-3083-51, 2100-3083-93, 2100-3084-93, 2100-5083-51, 2100-5283-51 |
| 7100 CVDR | Component Maintenance Manual | 165E1747-00 | 23-70-05 | 09 | 5/6/2014 | 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 | 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 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 |
| 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 | |
| FA2100 CVDR | Installation Aircraft Tools | 17TES0436 | Orig | 12/14/2020 | Software V3.6 | Software - ADLP V3.6 | 17TES0436 | |
| FA2100 CVDR | Installation Manual | 165E1847-10 | Orig | 5/1/2005 | FA2100 CVDR Install Manual for Embraer | FA2100CVDR Install Manual | 2100-3083-10 | |
| FA2100 CVDR | Installation Manual | 165E1847-01 | 02 | 4/22/2010 | FA2100 CVDR Install Manual | FA2100CVDR Install Manual | 2100‐3083‐50, 2100‐3083‐51, 2100‐3084‐50 | |
| FA2100 CVDR | Instruction Manual | 905E1436-22 | F | 9/16/2015 | Accident Investigation Procedure | Instruction Manual, Accident Investigation Procedure | 2100-, 905-E1436-22 | |
| FA2100 CVDR | Miscellaneous | n/a | - | 9/26/2019 | FA2100 90 day Beacon | FA2100 90 day Beacon | 2100- | |
| AP General Files | Service Letter | PI/2-001 | 01 | 6/20/2022 | Notification of discontinued product. | Notification of discontinued product. | 17TES0062, 17TES0065, 17TES0066, 17TES0092 | |
| FA2100 CVDR | Software | 840-E4519-09 | 9.1 | 8/14/2019 | 840-E4519-09 | SMP V9.1 4E13 FDP V4.2 6E59 | 2100- | |
| FA2100 CVDR | Software | 840-E3555-05 | 7.9 | 8/14/2019 | 840-E3555-05 | SMP v7.9 D478 FDP V3.6 9029 | 2100- | |
| FA2100 CVDR | Software | 840-E3555-06 | 8.6 | 8/14/2019 | 840-E3555-06 | SMP V 8.6 811C FDP V3.6 9029 | 2100- | |
| FA2100 CVDR | Software | 840-E3555-07 | 8.7 | 8/14/2019 | 840-E3555-07 | SMP V8.7 CF25 FDP V4.0 C09A ACP V1.3 2B4D | 2100- | |
| FA2100 CVDR | Software | 840-E4519-06 | 8.7 | 8/14/2019 | 840-E4519-06 | SMP V8.7 3032 FDP V4.0 C09C | 2100- | |
| FA2100 CVDR | Software | 840-E5152-06 | 8.7 | 8/14/2019 | 840-E5152-06 | SMP V8.7 EC2F FDP V4.0 C09A | 2100- | |
| FA2100 CVDR | Software | 840-E4568-10 | V8.9 | 8/13/2019 | 840-E4568-10 | 8D8E FDP V2.3 5E%e | 2100- | |
| FA2100 CVDR | Software | 840-E5152-05 | x.x | 8/14/2019 | 840-E5152-05 | SMP 6156 FDP 24AB | 2100- | |
| FA2100 CVDR | Software | 840-E1662-00 | 5.6 | 8/15/2019 | 840-E1662-00 | Operation software SMP V 5.6 5761 FDP V1.5 3Dff | 2100-3073-00 | |
| FA2100 CVDR | Software | 840-E1662-02 | 6.8 | 8/15/2019 | 840-E1662-02 | SMP V6.8 F387 FDP V2.9 75F1 | 2100-xxxx-xx | |
| FA2100 CVDR | Software | 840-E1662-04 | 7.9 | 8/15/2019 | 840-E1662-04 | SMP V7.9 6263 FDP V3.6 9029 | 2100-xxxx-xx | |
| FA2100 CVDR | Software | 840-E1662-05 | 9.3 | 8/15/2019 | 840-E1662-05 | SMP V7.9 3F1F FDP V3.6 9029 | 2100 | |
| FA2100 CVDR | Software | 840-E1662-06 | 8.7 | 8/15/2019 | 840-E1662-06 | SMP V 8.7 39CB FDP V4.0 C09A | 2100 | |
| FA2100 CVDR | Software | 840-E1662-08 | 9.0 | 8/15/2019 | 840-E1662-08 | SMP V9.0 3AEF FDP V4.1 6605 | 2100 | |
| FA2100 CVDR | Software | 840-E1662-09 | 9.1 | 8/15/2019 | 840-E1662-09 | SMP V9.1 57AC FDP V4.2 6E59 | 2100- | |
| FA2100 CVDR | Software | 840-E2261-02 | 7.0 | 8/15/2019 | 840-E2261-02 | SMP V7.0 BDB FDP V3.3 8F56 | 2100- | |
| FA2100 CVDR | Software | 840-E3565-05 | x.x | 8/22/2019 | 840-E3565-05 | 2100- | ||
| FA2100 CVDR | Software | 840-E3565-07 | x.x | 8/22/2019 | 840-E3565-07 | 2100- | ||
| FA2100 CVDR | Software | 840-E3565-08 | x.x | 8/22/2019 | 840-E3565-08 | 2100- | ||
| FA2100 CVDR | Software | 840-E3565-11 | x.x | 8/22/2019 | 840-E3565-11 | 2100- | ||
| FA2100 CVDR | Software | 840-E2261-04 | 7.8 | 8/22/2019 | 840-E2261-04 | SMP V7.8 2E7A FDP V3.6 902B | 2100- | |
| FA2100 CVDR | Software | 840-E2261-05 | 7.9 | 8/22/2019 | 840-E2261-05 | SMP V7.9 2E7A FDP V3.6 902B | 2100- | |
| FA2100 CVDR | Software | 840-E2261-06 | 8.6 | 8/22/2019 | 840-E2261-06 | Smp 8.6 AEC2 FDP V9.0 C09C | 2100- | |
| FA2100 CVDR | Software | 840-E2261-07 | 8.7 | 8/22/2019 | 840-E2261-07 | SMP V8.7 BC2C FDP V4.0 C09C ACP V1.3 2B4D | 2100- | |
| FA2100 CVDR | Software | 840-E2261-09 | 9.0 | 8/22/2019 | 840-E2261-09 | Smp v9.0 BD50 FDP V4.1 607 | 2100- | |
| FA2100 CVDR | Software | 840-E2261-10 | 9.1 | 8/22/2019 | 840-E2261-10 | SMP V9.1 DA13 FDP V4.2 6E5B | 2100- | |
| FA2100 CVDR | Software | 840E1622-02 | x.x | 2/6/2020 | 840-E1622-02 | 2100 | ||
| FA2100 CVDR | Software | 840-E2261-04 | x.x | 2/6/2020 | 840-E2261-04 | 2100- | ||
| FA2100 CVDR | Software | 840-E2261-05 | original | 2/6/2020 | 840-2261-05 | 2100-xxxxx | ||
| FA2100 CVDR | Software | 840-E2261-06 | x.x | 2/6/2020 | 840-E2261-06 | 2100- | ||
| FA2100 CVDR | Software | 840-E2661-04 | x.x | 2/10/2020 | 840-E2661-04 | FA2100 SSCVDR | 2100- | |
| FA2100 CVDR | Software | 840-E2661-06 | x.x | 2/10/2020 | 840-E2661-06 | FA2100 SSCVDR | 2100- | |
| FA2100 CVDR | Software | 840-E2661-09 | x.x | 2/10/2020 | 840-E2661-09 | FA2100 SSCVDR | 2100- | |
| FA2100 CVDR | Software | 840-E2661-10 | x.x | 2/10/2020 | 840-E2661-10 | FA2100 SSCVDR | 2100- | |
| FA2100 CVDR | Software | 840-E5022-03 | x.x | 2/10/2020 | 840-E5022-03 | FA2100 SSCVR Solid State Cockpit Voice Recorder with Datalink and OMS | 2100- | |
| 7100 CVDR | Component Maintenance Manual | 165E1747-00 | 23-70-05 | 09 | 5/6/2014 | 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 | 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 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 | 21 | 1/15/2023 | FA2100 CVR CMM | FA2100 CVR CMM | 2100-1010-00, 2100-1010-50, 2100-1010-51, 2100-1020-00, 2100-1020-02, 2100-1020-50, 2100-1020-51, 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, 2100-1226-02, 2100-1227-02, 2100-1925-22, 2100-1925-23 |
| FA2100 CVDR | Installation Aircraft Tools | 17TES0436 | Orig | 12/14/2020 | Software V3.6 | Software - ADLP V3.6 | 17TES0436 | |
| 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 | |
| FA2100 CVR | Installation Manual | 165E1846-00 | 23-70-06 | 26 | 10/15/2022 | FA2100CVR Install Manual | FA2100CVR Install Manual | 2100-1010-00, 2100-1020-02, 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 CVDR | Instruction Manual | 905E1436-22 | F | 9/16/2015 | Accident Investigation Procedure | Instruction Manual, Accident Investigation Procedure | 2100-, 905-E1436-22 | |
| FA2100 CVDR | Miscellaneous | n/a | - | 9/26/2019 | FA2100 90 day Beacon | FA2100 90 day Beacon | 2100- | |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB033 | 23-70-04-033 | 03 | 11/15/2022 | INTRODUCTION OF NEW SOFTWARE REVISION 12 FOR UNITS WITH HARDWARE MOD 17 | INTRODUCTION OF NEW SOFTWARE REVISION 12 FOR UNITS WITH HARDWARE MOD 17. | 2100-1925-22 2100-1925-23 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB024 | 03 | 9/20/2022 | MOD DOT 17 INTRODUCTION OF NEW CSMU PART NUMBER | 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-SB009 | orig | 12/15/2005 | INTRODUCTION OF A NEW AUDIO COMPRESSOR PRINTED WIRING ASSEMBLY (PWA), P/N: 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 | 02 | 2/1/2023 | MOD 18. Chassis Assembly Update to incorporate moisture prevention countermeasure. | MOD 18 – Chassis Assembly Update | 2100-1025-02, 2100-1026-02, 2100-1226-02 |
| FA2100 CVR | Service Bulletin | FA2100CVR-SB032 | 23-70-04 | 00 | 7/15/2021 | HARDWARE MOD 20 – INTRODUCTION OF CSMU PART NO. 253-E5675-06 | HARDWARE MOD 20 – INTRODUCTION OF CSMU PART NO. 253-E5675-06 | 2100-1225-24 |
| FA2100 CVR | Service Letter | FA2100CVR 001 | Orig | 3/1/2001 | MODEL FA2100CVR UPGRADE FOR A100/A100A INSTALLATIONS | SIL for Model FA2100CVR Upgrade for A100/A100A Installations | ||
| AP General Files | Service Letter | PI/2-001 | 01 | 6/20/2022 | Notification of discontinued product. | Notification of discontinued product. | 17TES0062, 17TES0065, 17TES0066, 17TES0092 | |
| FA2100 CVDR | Software | 840-E5022-03 | x.x | 2/10/2020 | 840-E5022-03 | FA2100 SSCVR Solid State Cockpit Voice Recorder with Datalink and OMS | 2100- | |
| FA2100 CVR | Software | 840-E1657-09 | 00 | 2/10/2020 | 840-E1657-09 | FA2100 SSCVR | 2100-xxxx | |
| FA2100 CVR | Software | 840-E1664-09 | x.x | 2/14/2020 | 840-E1664-09 | 2100- | ||
| FA2100 CVR | Software | 840-E5634-00 | x.x | 2/14/2020 | 840-E5634-00 | 2100- | ||
| FA2100 CVDR | Software | 840-E5152-05 | x.x | 8/14/2019 | 840-E5152-05 | SMP 6156 FDP 24AB | 2100- | |
| FA2100 CVR | Software | 840-E4568-11 | V9.0 | 8/13/2019 | 840-E4568-11 | SMP V9.0 6118 FDP V2.3 5E5E | 2100- | |
| FA2100 CVR | Software | 840-E4568-12 | 9.1 | 8/13/2019 | 840-E4568-12 | SMP 9.1 7DD5 FDP 2.5 F9F1 | 2100- | |
| FA2100 CVDR | Software | 840-E5152-06 | 8.7 | 8/14/2019 | 840-E5152-06 | SMP V8.7 EC2F FDP V4.0 C09A | 2100- | |
| FA2100 FDR | Component Maintenance Manual | 165E1688-00 | 31-30-03 | 18 | 11/15/2022 | FA2100 FDR CMM | FA2100 FDR CMM | 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, 2100-2242-00, 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, 2100-4243-00, 2100-4245-00, 2100-4245-22, 2100-4945-22 |
| 7100 CVDR | Component Maintenance Manual | 165E1747-00 | 23-70-05 | 09 | 5/6/2014 | 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 | 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 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 | Installation Aircraft Tools | 17TES0436 | Orig | 12/14/2020 | Software V3.6 | Software - ADLP V3.6 | 17TES0436 | |
| 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 | |
| FA2100 FDR | Installation Manual | 165E1845-00 | 15 | 11/21/2022 | FA2100 FDR Install Manual | FA2100 FDR Install Manual | 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 CVDR | Instruction Manual | 905E1436-22 | F | 9/16/2015 | Accident Investigation Procedure | Instruction Manual, Accident Investigation Procedure | 2100-, 905-E1436-22 | |
| FA2100 CVDR | Miscellaneous | n/a | - | 9/26/2019 | FA2100 90 day Beacon | FA2100 90 day Beacon | 2100- | |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB024 | 07 | 10/15/2022 | 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-SB029 | 01 | 7/18/2022 | New Parylene Coated CCA | HW MOD 19. Incorporate moisture prevention countermeasure. | 2100-2045-00 | |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB026 | 02 | 8/15/2022 | 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-SB027 | 02 | 1/9/2019 | 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-SB017 | 31-30-03 | Initial | 9/4/2008 | Installation of Mounting Bracket to Support Storage Capacitor | Service Bulletin 17 for FA2100 FDR. MOD DOT 11. | 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-SB031 | 01 | 8/15/2022 | SOFTWARE MOD 06 | SOFTWARE MOD 06 | 2100-4945-22 | |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB030 | 01 | 9/30/2021 | 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 | REPLACEMENT OF NON−CONFORMING HARDWARE | REPLACEMENT OF NON−CONFORMING HARDWARE | 2100- | |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB028 | 31-30-03-028 | 04 | 2/1/2023 | Hardware MOD 18 – Chassis Assembly Update | HW MOD 18 update to chassis assembly Incorporate moisture prevention countermeasure. | 2100-2045-00, 2100-4043-02, 2100-4044-00, 2100-4245-00 2100-4045-60 |
| FA2100 FDR | Service Bulletin | FA2100FDR-SB025 | 08 | 8/15/2022 | 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-SB032 | 00 | 12/23/2021 | 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 | Software | 840-E3552-04 | x.xx | 2/14/2020 | FA 2100 840-E3552-04 | 2100-- | ||
| FA2100 CVDR | Software | 840-E5152-06 | 8.7 | 8/14/2019 | 840-E5152-06 | SMP V8.7 EC2F FDP V4.0 C09A | 2100- | |
| FA2100 CVDR | Software | 840-E5152-05 | x.x | 8/14/2019 | 840-E5152-05 | SMP 6156 FDP 24AB | 2100- | |
| FA2100 FDR | Software | 840-E3555-09 | 9.0 | 8/14/2019 | 840-E3555-09 | SMP V 9.0 D049 FDP V4.1 6605 | 2100- | |
| FA2100 FDR | Software | 840-E1655-07 | original | 2/14/2020 | 840-E1655-07 | Operation Software | 2100-2043-01 | |
| FA2100 FDR | Software | 840-E3552-04 | x.x | 2/14/2020 | 840-E3552-04 | 2100- | ||
| FA2100 FDR | Software | 840-E2660-07 | x.x | 2/14/2020 | 840-E2660-07 | 2100- | ||
| FA2100 FDR | Software | 840-E3552-06 | 4.2 | 9/9/2019 | 840-E3552-06 | Operation Software SMP 9.1 07DE FDP 4.2 6E80 | 2100-4065-00 | |
| FA2200 MADRAS | Installation Manual | 165E1901-01 | 01 | 7/15/2022 | FA2200 MADRAS/FDR Installation & Operation Manual | FA2200 MADRAS/FDR Install Manual, 2202-1300-xx (Restricted) | 2202−1300−, 2202−1300−( ) | |
| FA2300 MADRAS | Installation Manual | 165E1903-36 | 01 | 8/30/2021 | FA2300 CVDR Installation & Operation Instruction Manual | FA2300 CVDR IOM for Rockwell Collins France | 2312−8500−94 | |
| FA2300 MADRAS | Installation Manual | 165E1903-03 | 05 | 10/15/2011 | Installation and Operation Manual | FA2300 CVDR IOM | 2316-1600-00, S056-0048-00, S261-1130-00 | |
| FA2300 MADRAS | Installation Manual | 165E1903-24 | 31-31-24 | 05 | 5/9/2022 | FA2300 CVDR Installation and Operation Instruction Manual for Augusta Westland 119 | FA2300 CVDR IOM | 2316-8440-00, 2316-8440-01, 2316-8440-02 |
| FA2300 MADRAS | Installation Manual | 165E1903-05 | 04 | 12/15/2010 | FA2300 CVDR Installation and Operation Instruction Manual for King Air 200/300 | FA2300 CVDR IOM | 2306-1800-00 | |
| 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 | 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 | 165E5906-02 | 23-70-43 | 00 | 2/22/2021 | FA5000 MADRAS CVDR CMM | FA5000 MADRAS CVDR CMM | 5311-6143-21 |
| FA5000 CVDR | Component Maintenance Manual | 165E1689-01 | 23-70-31 | 01 | 8/23/2018 | Model FA5000 Cockpit Voice Data Recorder | FA5000 CVDR CMM | 500−4030−000, 5003-6100-00, 5003-6100-50, 5013-6100-50 |
| 7100 CVDR | Component Maintenance Manual | 165E1747-00 | 23-70-05 | 09 | 5/6/2014 | 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 | 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 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 |
| FA5000 CVDR | Installation Aircraft Tools | 883-E5413-06 | 00 | 9/6/2022 | FA5000 LDR Software | FA5000 LDR GSE Software | 5000- | |
| FA5000 CVDR | Installation Manual | 165E5327-01 | 14 | 4/13/2020 | FA5000 CVDR Installation and Operation Instruction Manual | FA5000 CVDR Short Case IOM | 5001-6103-11, 5001-6133-11, 5003-6103-11, 5011-6103-11 | |
| 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 | 165E5327−13 | 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 | Instruction Manual | 905E5389-22 | 1 | 1/25/2015 | ACCIDENT INVESTIGATION PROCEDURE | Instruction Manual, Accident Investigation Procedure | 905-E5389-22, 905E5389-22 | |
| 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 | 5013-6100-01 |
| FA5000 CVDR | Service Bulletin | SB001-FA5000 | FA5000-70-6000 | 03 | 10/18/2021 | 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. | 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 | 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 | 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 | 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 | 5011-6133-11, |
| FA5000 CVDR | Service Bulletin | SB002-FA5000 | 00 | 7/15/2022 | Hardware MOD 03 and 04 | Hardware MOD 03 and 04 | 5001-6103-11, 5001-6133-11, 5003-3100-01, 5003-3103-11, 5003-5000-00, 5003-5001-50, 5003-6100-00, 5003-6100-50, 5013-3100-00, 5013-5001-50, 5013-6100-50 | |
| AP General Files | Service Letter | PI/2-001 | 01 | 6/20/2022 | Notification of discontinued product. | Notification of discontinued product. | 17TES0062, 17TES0065, 17TES0066, 17TES0092 | |
| FA5000 CVDR | Software | 840-E2661-01 | 8 | 2/10/2019 | 840-E2661-01 | FA2100 SSCVDR | 2100- | |
| 7100 CVDR | Component Maintenance Manual | 165E1747-00 | 23-70-05 | 09 | 5/6/2014 | 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 | 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 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 |
| FA5000 CVR | Component Maintenance Manual | 165E1689-02 | 23-70-30 | 05 | 11/30/2022 | Model 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 | Component Maintenance Manual | 165E5398-00 | 23-70-40 | 10 | 9/30/2022 | 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 | 02 | 8/30/2022 | Model FA5000 Cockpit Voice Recorder CMM | FA5000 CVR CMM | 5001-5003-11, 5003-5003-11, 5033-5003-11, 5053-5003-11 |
| FA5000 CVDR | Installation Aircraft Tools | 883-E5413-06 | 00 | 9/6/2022 | FA5000 LDR Software | FA5000 LDR GSE Software | 5000- | |
| FA5000 CVR | Installation Manual | 165E5327-11 | 07 | 5/30/2022 | FA5000 CVR Installation & Operation Manual | FA5000 CVR | 5001-5003-11, 5003-5003-11, 500-4030-000, 5053-5003-11 | |
| FA5000 CVR | Installation Manual | 165E5327-00 | 04 | 11/30/2022 | FA5000 Cockpit Voice Recorder 1/2 ATR Short Case IOM | FA5000 Short Case IOM | 500-4030-000, 5001-6103-11, 5003-5000-00, 5003-5000-01, 5011-6103-11 | |
| 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 CVDR | Instruction Manual | 905E5389-22 | 1 | 1/25/2015 | ACCIDENT INVESTIGATION PROCEDURE | Instruction Manual, Accident Investigation Procedure | 905-E5389-22, 905E5389-22 | |
| FA5000 CVR | Service Bulletin | FA5000-SB004 | 02 | 3/16/2015 | Introduction of 90 Day ULB | Introduction of 90 Day ULB | 5000- | |
| 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 | 5003-5003-11, 5053-5003-11, FA5000, FA5003, FA5053 |
| FA5000 CVDR | Service Bulletin | SB002-FA5000 | 00 | 7/15/2022 | Hardware MOD 03 and 04 | Hardware MOD 03 and 04 | 5001-6103-11, 5001-6133-11, 5003-3100-01, 5003-3103-11, 5003-5000-00, 5003-5001-50, 5003-6100-00, 5003-6100-50, 5013-3100-00, 5013-5001-50, 5013-6100-50 | |
| 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 | 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 | 23-70-35, 5001-5003-11, 5003-5003-11 |
| FA5000 CVDR | Service Bulletin | SB001-FA5000 | FA5000-70-6000 | 03 | 10/18/2021 | 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. | 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 | 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 | 5003-5000-01 |
| AP General Files | Service Letter | PI/2-001 | 01 | 6/20/2022 | Notification of discontinued product. | Notification of discontinued product. | 17TES0062, 17TES0065, 17TES0066, 17TES0092 | |
| FA5000 FDR | Component Maintenance Manual | 165E1689-03 | 31-30-30 | 03 | 11/15/2022 | FA5003 Flight Data Recorder CMM | FA5003 FDR CMM | 5003-3100-00, 5003-3100-01, 5013-3100-00, 5013-3100-30 |
| 7100 CVDR | Component Maintenance Manual | 165E1747-00 | 23-70-05 | 09 | 5/6/2014 | 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 | 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 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 |
| FA5000 CVDR | Installation Aircraft Tools | 883-E5413-06 | 00 | 9/6/2022 | FA5000 LDR Software | FA5000 LDR GSE Software | 5000- | |
| FA5000 FDR | Installation Manual | 165E5326-00 | 03 | 11/3/2016 | FA5003 Flight Data Recorder Installation & Operation Manual | FA5003 Flight Data Recorder Installation & Operation Manual | 5003-3100-00, 5003-3100-01, 5013-3100-00 | |
| FA5000 FDR | Installation Manual | 165E5850-02 | INT | 5/26/2016 | FA5013 FDR IOM | FA5013 FDR IOM | 5013-3100-30 | |
| FA5000 CVDR | Instruction Manual | 905E5389-22 | 1 | 1/25/2015 | ACCIDENT INVESTIGATION PROCEDURE | Instruction Manual, Accident Investigation Procedure | 905-E5389-22, 905E5389-22 | |
| FA5000 CVDR | Service Bulletin | SB002-FA5000 | 00 | 7/15/2022 | Hardware MOD 03 and 04 | Hardware MOD 03 and 04 | 5001-6103-11, 5001-6133-11, 5003-3100-01, 5003-3103-11, 5003-5000-00, 5003-5001-50, 5003-6100-00, 5003-6100-50, 5013-3100-00, 5013-5001-50, 5013-6100-50 | |
| FA5000 CVDR | Service Bulletin | SB001-FA5000 | FA5000-70-6000 | 03 | 10/18/2021 | 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. | 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 | 5003-3100-01 |
| FA5000 FDR | Service Bulletin | SB001-FA5013 | FA5013-31-0000 | 01 | 6/15/2021 | Instructions for the installation of Firmware Part No. 840-E5479-04. | Service Bulletin | 5013-6100-01 |
| 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 MADRAS | Installation Manual | 165E5906-01 | 03 | 8/30/2021 | Installation and Operation Instruction Manual | FA5000 MADRAS | 5311-6143-21 | |
| 7100 CVDR | Component Maintenance Manual | 165E1747-00 | 23-70-05 | 09 | 5/6/2014 | 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 | 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 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 |
| 7100 CVDR | Component Maintenance Manual | 165E1747-00 | 23-70-05 | 09 | 5/6/2014 | 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 | 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 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 |
| CA-2001 | Installation Manual | TP-258 | Orig | 8/1/1980 | Instruction Manual, Operation and Installation | Pub# TP-258 | 501-1172-01, 501-1172-02, 501-1172-03, 501-1172-04, 501-1172-05, 501-1172-06, 501-1196-01, 501-1196-02, 501-1199-01, 501-1199-02, 501-1199-03, 501-1199-04, 501-1199-05, 501-1199-06, 501-1200-01, 501-1200-02, 501-1200-03, 501-1200-04, 501-1200-05, 501-1201-01, 501-1201-02, 501-1202-01, 501-1202-02, 501-1207-01, 501-1207-02, 501-1207-03, 501-1207-04, 501-1207-05, 501-1207-06, 501-1207-07, 501-1207-08, 501-1232-02, 501-1232-03, 501-1232-04, 501-1232-05, 501-1232-06, 501-1279-01 | |
| FU-372A | Component Maintenance Manual | TP-263 | C | 8/28/2017 | Field Check | Pub# TP-263 | 509-1005-01 | |
| FU-500 | Instruction Manual | TP-344 | 22-00-01 | C1 | 11/4/2010 | Maintenance Manual with IPL | If unit fails it MUST BE REPLACED | 501-1123-03, 501-1123-04 |
| 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 | Component Maintenance Manual | TP-636 | 24-30-24 | A | 2/7/2011 | Component Maintenance Manual | TP-636 | 24E508294G01 |
| 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-15193 | 24-30-06 | 4 | 12/6/2017 | Component Maintenance Manual | Pub# GEK-15193 | 3S2060DC168B1 |
| 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-34439 | 24-32-50 | 1 | 10/15/1976 | Overhaul Manual With IPL | Pub# GEK-34439 | 3S2060DC168D1 |
| 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 | 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 | TP-495 | 24-34-07 | A | 7/17/2017 | Component Maintenance Manual | Pub# TP-495 | 3S2060DM169A1, 3S2060DM169A3 |
| 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 | ||
| ADC-3000 | Installation Manual | TP-579 | E | 5/1/2018 | Installation and Operation Manual | Pub# TP-579 | 501-1741-2104, 501-1741-2105, 501-1741-2204, 501-1741-2304, 501-1741-2404, 501-1741-2504, 501-1741-2604, 501-1741-2704, 501-1741-2804, 501-1826-01, 501-1881-01 | |
| GH-3000 | Installation Manual | TP-546 | T | 3/30/2017 | Installation and Operation Manual | Removes install information for ADC-4000 and refers to ADC Install Manual 0040-30001-01 | 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 | |
| ADC-3000 | Installation Manual | TP-531 | C | 5/27/2009 | Installation and Operation Manual | Pub# TP-531 | 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-511 | 34-20-60 | 4/29/1996 | Installation and Operation | Pub# TP-511 | 501-1741-04 | |
| GH-3000 | Installation Manual | TP-503 | 34-20-57 | A | 5/27/2009 | Installation and Operations Manual | Pub# TP-503 | 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 | Pub# TP-571 | 501-1741-( ) | |
| GH-3000 | Pilot Guide | TP-547 | H | 7/22/2009 | Pilot's Guide | Pub# TP-547 | 501-1741-( )03, 501-1741-() | |
| GH-3000 | Pilot Guide | TP-502 | 34-20-56 | 02 | 9/11/1998 | Pilot's Guide | Pub# TP-502 | 501-1741-() |
| GH-3000 | Pilot Guide | TP-577 | B | 8/12/2008 | Pilot's Guide | Pub# TP-577 | 501-1741-2104 | |
| GH-3000 | Pilot Guide | TP-626 | B | 4/16/2009 | GH-3000 REL 5.X | GH-3000 REL 5.X | 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 | SB501-1741-1 | 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 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 | SB501-1741-31 | 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 | SB501-1741-29 | 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 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-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-189 | B | 12/7/2004 | 1. Import / Export control issues. 2. Modification status of models GH-3000, GH-3004, and GH-3100. | 501-1741-( ), 501-1859-( ), 501-1860-( ) | ||
| ADC-3000 | Service Letter | SL-177 | C | 5/13/2004 | Repair station only.... air data anomalies | To inform flight line technicians about air data anomalies they may observe on the GH-3000 Electronic Standby Instrument System display and instructions to correct the air data invalidities. | 501-1741-( ), 501-1797-( ) | |
| GH-3000 | Service Letter | SL-179 | A | 4/28/2004 | To provide information concerning fan failures during power ON self-testing. | 501-1741-( ), 501-1860-( ) | ||
| ADC-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 | Service Letter | SL-161 | Orig | 6/4/1999 | To establish product knowledge and availability of new GH-3000 with Release 2.0 Software. | |||
| GH-3000 | Service Letter | SL-165 | B | 11/15/2010 | Electronic Standby Indicator System (ESIS) Attitude Operation | 501-1741-( ), 501-1741-( )01, 501-1741-( )02, 501-1741-( )03 | ||
| GH-3000 | Service Letter | SL-169 | E | 5/15/2002 | To advise customers of differences among GH-3000 part numbers, and upgrade policies and procedures. | 501-1741-( ) | ||
| GH-3000 | Troubleshooting Guide | TP-602 | B | 3/12/2009 | GH-3000 Troubleshooting Guide | GH-3000 Troubleshooting Guide | 501-1741- ( ) | |
| ADC-3000 | Installation Manual | TP-593 | E | 12/18/2013 | Installation and Operation Manual | Pub# TP-593 | 501-1797-( ), 501-1803-( ), 501-1826-01, 501-1851-2403, 501-1851-2404 | |
| ADC-3000 | Installation Manual | TP-530 | L | 6/15/2016 | Installation and Operation Manual | Pub# TP-530 | 501-1797-23, 501-1797-24, 501-1797-71, 501-1803-145, 501-1803-31C, 501-1803-32B, 501-1826-01, 501-1851-01, 501-1851-2402, 501-1851-2405 | |
| 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 | SB501-1851-24 | 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 | SB501-1851-22 | 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 | SB501-1851-25 | 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 | Pub# TP-539 | 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 | SB501-1859-17 | 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-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-3000 | Service Letter | SL-189 | B | 12/7/2004 | 1. Import / Export control issues. 2. Modification status of models GH-3000, GH-3004, and GH-3100. | 501-1741-( ), 501-1859-( ), 501-1860-( ) | ||
| DCM | Installation Manual | TP-559 | K | 3/30/2017 | Installation and Operation Manual, GH-3100 | 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 | Installation Manual | TP-582 | G | 3/4/2010 | Installation and Operation Manual | Pub# TP-582 | 501-1826-01, 501-1860-0102, 501-1860-0104, 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 | SB501-1860-12 | 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 | SB501-1860-20 | 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 | SB501-1860-15 | 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 | SB501-1860-14 | 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 | SB501-1860-22 | 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-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-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-189 | B | 12/7/2004 | 1. Import / Export control issues. 2. Modification status of models GH-3000, GH-3004, and GH-3100. | 501-1741-( ), 501-1859-( ), 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-3000 | Service Letter | SL-179 | A | 4/28/2004 | To provide information concerning fan failures during power ON self-testing. | 501-1741-( ), 501-1860-( ) | ||
| GH-3100 | Troubleshooting Guide | TP-603 | C | 4/21/2009 | GH-3100 Troubleshooting Guide | GH-3100 Troubleshooting Guide | 501-1860-( ) | |
| GH-3900 | Component Maintenance Manual | 0040-38003-01 | B | 10/18/2016 | GH-3900RSU CMM | GH-3900RSU CMM | 9200-38000-0101, 9200-38100-0101 | |
| GH-3900 | Component Maintenance Manual | 0040-34003-01 | 34-20-74 | C | 5/15/2017 | GH-3900 CMM | GH-3900 CMM | 9200-34000, 9200-34100 |
| GH-3900 | Installation Aircraft Tools | 576-6157-08 | 1.01 | 9/11/2019 | ACM Tool for GH-3900.2 | ACMT 576-6157-08 (revision 1.01) | 576-6157-08, 9200-34400, 9200-34402, 9200-34410, 9200-34500, 9200-34502, 9200-34600, 9200-34602, 9200-34700, 9200-34702, 9200-34802, 9200-34900 | |
| GH-3900 | 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 | 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 | 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-3900 | Installation Manual | 0040-34001-01 | R | 6/26/2017 | 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 | 0040-34402-02 | A | 2/7/2013 | Revision 2.03 Aircraft Config File Ver 02.06 | Revision 2.03 Aircraft Config File Ver 02.06 | 576-6157-02 | |
| GH-3900 | Instruction Manual | 0040-34402-01 | A | 7/18/2012 | Aircraft Configuration Module Tool | 576-6157-01 | ||
| GH-3900 | Instruction Manual | 0040-34002-01 | H | 6/26/2017 | GH-3900 Aircraft Configuration Module Tool | Aircraft Configuration Module Tool VER 01.09 | 576-6159-03 | |
| GH-3900 | Instruction Manual | 0040-38002-01 | A | 8/14/2013 | Aircraft Configuration Tool | GH-3900RSU Rev 1.01 Config File 03.00 | ||
| GH-3900 | Instruction Manual | 0040-34402-04 | B | 5/20/2014 | ACMT | Revision 2.07 Aircraft Config File 02.09 | 9200-34400, 9200-34500, 9200-34600, 9200-34700, 9200-34800 | |
| GH-3900 | Instruction Manual | 0040-38002-02 | B | 9/21/2015 | Aircraft Configuration Tool | GH-3900.2RSU SW1.1 | 576-6207-02 | |
| GH-3900 | Instruction Manual | 0040-34402-03 | B | 12/18/2013 | Revision 2.04 /2.05 A/C config file 02.08 | Revision 2.04 /2.05 A/C config file 02.08 | ||
| GH-3900 | Instruction Manual | 0040-34402-05 | A | 1/23/2015 | ACMT | 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900 | ||
| GH-3900 | 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 | Instruction Manual | 0040-34402-06 | E | 12/13/2018 | Aircraft Configuration Module Tool | ACMT Instruction Manual | 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900 | |
| GH-3900 | Instruction Manual | 0040-34402-08 | D | 6/28/2021 | Aircraft Configuration Module Tool Rev 1.02, Version 02.16 | Aircraft Configuration Module Tool. (Rev 1.02) | 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 | Instruction Manual | 0040-34402-07 | B | 12/13/2018 | Aircraft Configuration Module Tool 1.03 | Aircraft Configuration Module Tool | 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900, 9200-34400 | |
| GH-3900 | Intermediate Maintenance Manual | 34-20-77 | B | 5/15/2017 | GH-3900 Abbreviated Maintenance Manual | GH-3900 Abbreviated Maintenance Manual | 9200-34000, 9200-34100 | |
| GH-3900 | 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 | Pilot Guide | 0040-34000-01 | G | 6/26/2017 | GH-3900 (SFIS-3900) ) Pilot's Guide | Incorporates S/W 1.4 | ||
| GH-3900 | Pilot Guide | 0040-34400-01 | P | 6/28/2021 | GH-3900.2 Pilots Guide | Software 1.0;1.1; 1.2, 1.3, 1.4, 1.5, 1.6, 1.7, 1.8 | 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 | Printer Copies | 0040-34400-01PC | P | 6/28/2021 | GH-3900.2 Pilots Guide | Printer copy GH-3900.2 PG | ||
| GH-3900 | Service Bulletin | SB9200-34400-1 | B | 6/2/2016 | Release of Software Revision 1.1 | Software Revision 1.1 | 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900 | Service Bulletin | SB9200-34000-1 | A | 9/17/2012 | Release of Software 1.1 | Release of Software 1.1 | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 | |
| GH-3900 | Service Bulletin | SB9200-34100-1 | A | 9/17/2012 | Release of Software 1.1 | Release of Software 1.1 | 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB576-6159-1 | B | 5/20/2013 | ACMT REV 1.06 | ACMT REV 1.06 | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 | |
| GH-3900 | Service Bulletin | SB576-6157-1 | B | 5/24/2013 | ACMT REV 2.03.1 Planning information | ACMT REV 2.03.0 | 9200-34400-, 9200-34500-, 9200-34600-, 9200-34700-, 9200-34800- | |
| GH-3900 | Service Bulletin | SB9200-34700-1 | B | 6/2/2016 | Release of Software Version 1.1 | Release of Software Version 1.1 | 9200-34700-0101, 9200-34700-0201, 9200-34700-0401 | |
| GH-3900 | Service Bulletin | SB9200-34500-1 | B | 6/2/2016 | Release of Software Ver 1.1 | Release of Software Ver 1.1 | 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900 | Service Bulletin | SB9200-34600-1 | B | 6/2/2016 | Release of Software Version 1.1 | Release of Software Version 1.1 | 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900 | Service Bulletin | SB9200-34400-4 | A | 5/28/2014 | Software Release 1.3 | Software Release 1.3 | 9200-34400, 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900 | Service Bulletin | SB9200-34500-4 | A | 5/28/2014 | Software 1.3 | Software 1.3 | 9200-34500, 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900 | Service Bulletin | SB9200-34600-3 | A | 5/28/2014 | Software 1.3 | Software 1.3 | 9200-34600, 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900 | Service Bulletin | SB9200-34700-4 | A | 5/28/2014 | Software 1.3 | Software 1.3 | 9200-34700, 9200-34700-0101, 9200-34700-0201, 9200-34700-0401 | |
| GH-3900 | Service Bulletin | SB9200-34800-1 | A | 5/28/2014 | Software 1.3 | Software 1.3 | 9200-34800, 9200-34800-0101, 9200-34800-0201, 9200-34800-0401 | |
| GH-3900 | 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 | 9200-34400, 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900 | Service Bulletin | SB9200-34500-5 | A | 1/29/2015 | GH-3900.2 System Software Release 1.4 | GH-3900.2 System Software Release 1.4 | 9200-34500, 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900 | Service Bulletin | SB9200-34600-4 | A | 1/29/2015 | GH-3900.2 System Software Release 1.4 | GH-3900.2 System Software Release 1.4 | 9200-34600, 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900 | 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 | 9200-34700 | |
| GH-3900 | Service Bulletin | SB9200-34800-2 | A | 1/29/2015 | GH-3900.2 System Software Release 1.4 | GH-3900.2 System Software Release 1.4 | 9200-34800, 9200-34800-0101, 9200-34800-0201, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900 | Service Bulletin | SB9200-34900-1 | A | 1/29/2015 | GH-3900.2 System Software Release 1.4 | GH-3900.2 System Software Release 1.4 | 9200-34900, 9200-34900-0101 | |
| GH-3900 | Service Bulletin | SB9200-34400-3 | D | 1/29/2014 | GH-3900.2 System software Release 1.2 (Version R01.02) | Software Version 1.2 | 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900 | Service Bulletin | SB9200-34500-3 | D | 1/29/2014 | GH-3900.2 System software Release 1.2 (Version R01.02) | Software Version 1.2 | 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900 | Service Bulletin | SB9200-34600-2 | D | 1/29/2014 | GH-3900.2 System software Release 1.2 (Version R01.02) | Software Version 1.2 | 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900 | Service Bulletin | SB9200-34700-3 | D | 1/29/2014 | GH-3900.2 System Software Release 1.2 (Version R01.02) | Release of 1.2 Software | 9200-34700-0101, 9200-34700-0201, 9200-34700-0401 | |
| GH-3900 | Service Bulletin | SB576-6157-2 | A | 12/18/2013 | ACMT Rev 2.05 | ACMT Rev 2.05 | 9200-34400-, 9200-34500-, 9200-34600-, 9200-34700-, 9200-34800- | |
| GH-3900 | Service Bulletin | SB9200-34000-4 | A | 12/13/2013 | GH-3900 S/W 1.2 | SW 1.2 Release | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 | |
| GH-3900 | Service Bulletin | SB9200-34000-5 | A | 12/13/2013 | GH-3900 Bootloader 1.03 | 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 | Release of 1.2 Software | Release of 1.2 Software | 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB9200-34100-5 | A | 12/20/2013 | GH-3900 Bootloader Software | Bootloader S/W R01.03 | 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB576-6159-2 | A | 12/13/2013 | GH-3900 ACMT | ACMT Rev 1.07 | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 | |
| GH-3900 | Service Bulletin | SB9200-34702-1 | A | 5/3/2017 | To prevent memory corruptions | To prevent memory corruptions | 9200-34700-0401, 9200-34702-0401 | |
| 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 1.5 | 9200-34100 | ||
| GH-3900 | Service Bulletin | SB576-6159-3 | B | 6/26/2017 | Aircraft Configuration Module Tool – Revision 1.09 | 9200-34000, 9200-34100 | ||
| GH-3900 | 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 | 9200-34400-0501 | |
| GH-3900 | 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. | 9200-34402-0501 | |
| GH-3900 | 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. | 9200-34502 | |
| GH-3900 | Service Bulletin | SB9200-34502-3 | A | 2/21/2017 | Updates the 5V current limit setting | Updates the 5V current limit setting | 9200-34502-0401 | |
| GH-3900 | Service Bulletin | SB9200-34602-1 | B | 7/18/2018 | To prevent Memory coruptions | To prevent Memory coruptions | 9200-34600-0401, 9200-34602-0401 | |
| GH-3900 | Service Bulletin | SB9200-34802-1 | B | 7/18/2018 | To prevent Memory Corruptions | To prevent Memory Corruptions | 9200-34800-0401, 9200-34802-0401 | |
| GH-3900 | 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. | 9200-34802-0401 | |
| GH-3900 | Service Bulletin | SB576-6159-4 | A | 6/26/2017 | create aircraft configuration files for the GH-3900 | create aircraft configuration files for the GH-3900 | 9200-34000, 9200-34100 | |
| 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 | 9200-34100, 9200-34100-0101, 9200-34100-0201 | ||
| GH-3900 | Service Bulletin | SB9200-34000-11 | A | 12/4/2017 | Display Replacement | Display Replacement | 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 | 9200-34100, 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Service Bulletin | SB9200-34000-9 | B | 6/26/2017 | System Software Release 1.5 | 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34000-0501 | ||
| GH-3900 | Service Bulletin | SB9200-34400-9 | A | 12/8/2017 | Software Release 1.6 | Software Release 1.6 | 9200-34400, 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900 | Service Bulletin | SB9200-34502-1 | B | 5/3/2017 | To prevent Memory Corruptions | 9200-34500, 9200-34502 | ||
| GH-3900 | Service Bulletin | SB9200-34000-8 | A | 12/9/2016 | GH-3900 SW 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 | SB9200-34800-4 | A | 11/3/2016 | Software 1.5 upgrade | Software 1.5 | 9200-34800-0101, 9200-34800-0201, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900 | Service Bulletin | SB9200-34900-3 | A | 11/3/2016 | Software 1.5 upgrade | Software 1.5 | 9200-34900-0101 | |
| GH-3900 | 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. | SB9200-38100-0101 | |
| GH-3900 | Service Bulletin | SB9200-34400-7 | A | 11/3/2016 | Software 1.5 upgrade | Software 1.5 | 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900 | Service Bulletin | SB9200-34410-2 | A | 11/3/2016 | Software 1.5 upgrade | Software 1.5 | 9200-34410-0501 | |
| GH-3900 | Service Bulletin | SB9200-34500-7 | A | 11/3/2016 | Software 1.5 upgrade | Software 1.5 | 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900 | Service Bulletin | SB9200-34600-6 | A | 11/3/2016 | Software 1.5 upgrade | Software 1.5 | 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900 | Service Bulletin | SB9200-34700-6 | A | 11/3/2016 | Software 1.5 Upgrade | Software 1.5 | 9200-34700-0101, 9200-34700-0201, 9200-34700-0401 | |
| GH-3900 | Service Bulletin | SB576-6207-1 | A | 9/24/2015 | Aircraft Configuration Module Tool – Revision 1.01 | Aircraft Configuration Module Tool – Revision 1.01 | 9200-38000-0101, 9200-38100-0101 | |
| GH-3900 | Service Bulletin | SB9200-34000-7 | A | 9/14/2016 | To 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 | To prevent rate sensor loopback failure at start up. | To prevent rate sensor loopback failure at start up. | 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | 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. | 9200-34400-0101, 9200-34400-0201, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900 | 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. | 9200-34410-0501 | |
| GH-3900 | 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. | 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900 | 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. | 9200-34600-0101, 9200-34600-0201, 9200-34600-0401 | |
| GH-3900 | 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. | 9200-34800-0101, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900 | 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. | 9200-34900-0101 | |
| GH-3900 | 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. | 9200-34901-0101 | |
| GH-3900 | 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. | 9200-38000-0101 | |
| GH-3900 | Service Bulletin | SB9200-34800-7 | A | 7/31/2018 | Error Correcting RAM | Error Correcting RAM | 9200-34800-0101, 9200-34800-0601 | |
| GH-3900 | Service Bulletin | SB9200-34400-12 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34400-0101, 9200-34400-0201, 9200-34400-0501 | |
| GH-3900 | Service Bulletin | SB9200-34500-12 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34500-0101, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900 | Service Bulletin | SB9200-34600-11 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34600-0101, 9200-34600-0201, 9200-34600-0401 | |
| GH-3900 | Service Bulletin | SB9200-34700-10 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34700-0101, 9200-34700-0401, 9200-34700-0601 | |
| GH-3900 | Service Bulletin | SB9200-34800-9 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34800-0101, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900 | Service Bulletin | SB9200-34502-7 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34502-0101, 9200-34502-0401, 9200-34502-0601 | |
| GH-3900 | Service Bulletin | SB9200-34702-4 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34702-0401 | |
| GH-3900 | Service Bulletin | SB9200-34802-6 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34802-0401 | |
| GH-3900 | Service Bulletin | SB9200-34602-6 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34602-0401 | |
| GH-3900 | Service Bulletin | SB9200-34402-4 | A | 12/8/2017 | System Software 1.6 | 9200-34402-0501 | ||
| GH-3900 | Service Bulletin | SB9200-34410-4 | A | 12/8/2017 | System Software 1.6 | System Software 1.6 | 9200-34410-4 | |
| GH-3900 | Service Bulletin | SB9200-34500-9 | A | 12/8/2017 | System Software 1.6 | System Software 1.6 | 9200-34500-0101, 9200-34500-0201, 9200-34500-0301, 9200-34500-0401, 9200-34500-0501 | |
| GH-3900 | Service Bulletin | SB9200-34502-5 | A | 12/8/2017 | System Software 1.6 | System Software 1.6 | 9200-34502-0101, 9200-34502-0401, 9200-34502-0601 | |
| GH-3900 | Service Bulletin | SB9200-34600-8 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6 | 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900 | Service Bulletin | SB9200-34602-4 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6 | 9200-34602-0401 | |
| GH-3900 | Service Bulletin | SB9200-34700-7 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6 | 9200-34700-0101, 9200-34700-0201, 9200-34700-0401, 9200-34700-0601 | |
| GH-3900 | Service Bulletin | SB9200-34700-8 | B | 7/31/2018 | Error Correcting RAM | Error Correcting RAM | 9200-34700-0101, 9200-34700-0201, 9200-34700-0601 | |
| GH-3900 | Service Bulletin | SB9200-34400-8 | A | 1/25/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement | 9200-34400, 9200-34400-0101, 9200-34400-0201, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900 | Service Bulletin | SB9200-34900-4 | A | 1/25/2018 | Display Rate and Sensor CCM Replacement | Display Rate and Sensor CCM Replacement | 9200-34900-0101 | |
| GH-3900 | Service Bulletin | SB9200-34402-3 | A | 1/25/2018 | Display and Rate Sensor CCM Replacement | Display and Rate Sensor CCM Replacement | 9200-34402-0501 | |
| GH-3900 | Service Bulletin | SB9200-34800-6 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6 | 9200-34800-0101, 9200-34800-0201, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900 | Service Bulletin | SB9200-34802-4 | A | 12/8/2017 | System Software Release 1.6 | 9200-34802-0401 | ||
| GH-3900 | Service Bulletin | SB9200-34900-5 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6 | 9200-34900-0101 | |
| GH-3900 | Service Bulletin | SB9200-34901-3 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6 | 9200-34901-3 | |
| GH-3900 | Service Bulletin | SB9200-34901-2 | A | 1/25/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement | 9200-34901-0101 | |
| GH-3900 | Service Bulletin | SB9200-34600-7 | A | 3/8/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM Replacement | 9200-34600-0101, 9200-34600-0201, 9200-34600-0401 | |
| GH-3900 | Service Bulletin | SB9200-34602-3 | A | 3/8/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement | 9200-34602-0401 | |
| GH-3900 | Service Bulletin | SB9200-34410-3 | A | 1/25/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement | 9200-34410-0501 | |
| GH-3900 | Service Bulletin | SB9200-34500-8 | B | 3/8/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement | 9200-34500-0101, 9200-34500-0201, 9200-34500-0601 | |
| GH-3900 | Service Bulletin | SB9200-34502-4 | B | 3/8/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement | 9200-34502-0101, 9200-34502-0401, 9200-34502-0601 | |
| GH-3900 | Service Bulletin | SB9200-34802-3 | A | 1/25/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement | 9200-34802-0401 | |
| GH-3900 | Service Bulletin | SB9200-34400-10 | C | 10/11/2018 | Error Correcting RAM | Error Correcting RAM | 9200-34400-0101, 9200-34400-0401 | |
| GH-3900 | Service Bulletin | SB9200-34800-5 | A | 3/8/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement | 9200-34800-0101, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900 | Service Bulletin | SB9200-34900-6 | A | 4/4/2018 | Error Correcting RAM | Error Correcting RAM | 9200-34900-0101 | |
| GH-3900 | Service Bulletin | SB9200-34901-4 | A | 4/4/2018 | Error Correcting RAM | Error Correcting RAM | 9200-34901-0101 | |
| GH-3900 | Service Bulletin | SB9200-34500-10 | A | 7/31/2018 | Error Correcting RAM | Error Correcting RAM | 9200-34500-0201 | |
| GH-3900 | Service Bulletin | SB9200-34600-9 | A | 7/31/2018 | Error Correcting RAM | Error Correcting RAM | 9200-34600-0101, 9200-34600-0201 | |
| GH-3900 | Service Bulletin | SB9200-34701-1 | A | 7/31/2018 | Error Correcting RAM | Error Correcting RAM | 9200-34701-0201, 9200-34701-0401 | |
| GH-3900 | Service Bulletin | SB576-6157-4 | A | 10/30/2019 | To inform customers of an update to Aircraft Configuration Module Tool (rev 1.02). | ACMT Rev 1.02, Aircraft Configuration 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 | Service Bulletin | SB576-6157-3 | A | 9/11/2019 | To inform customers of an update to Aircraft Configuration Module Tool (rev 1.01). | ACMT Rev 1.01, Aircraft Configuration 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 | Service Bulletin | SB9200-34502-6 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | SB9200-34502 | |
| GH-3900 | Service Bulletin | SB9200-34602-5 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34602 | |
| GH-3900 | Service Bulletin | SB9200-34702-3 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | SB9200-34702 | |
| GH-3900 | Service Bulletin | SB9200-34802-5 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | SB9200-34802 | |
| GH-3900 | Service Bulletin | SB9200-34900-8 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34900-0101 | |
| GH-3900 | Service Bulletin | SB9200-34701-3 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34701-0101, 9200-34701-0201, 9200-34701-0401 | |
| GH-3900 | Service Bulletin | SB9200-34402-6 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34402-0501 | |
| GH-3900 | Service Bulletin | SB9200-34901-6 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34901-0101 | |
| GH-3900 | Service Bulletin | SB9200-34400-11 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34400 | |
| GH-3900 | Service Bulletin | SB9200-34500-11 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34500 | |
| GH-3900 | Service Bulletin | SB9200-34600-10 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34600 | |
| GH-3900 | Service Bulletin | SB9200-34700-9 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34700 | |
| GH-3900 | Service Bulletin | SB9200-34800-8 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34800 | |
| GH-3900 | Service Bulletin | SB9200-34900-7 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34900 | |
| GH-3900 | Service Bulletin | SB9200-34410-6 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34410 | |
| GH-3900 | Service Bulletin | SB9200-34402-5 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | SB9200-34402 | |
| GH-3900 | Service Bulletin | SB001-GH-3900.2 | 00 | 6/28/2021 | Software Release 1.8 | Software Release 1.8 | ||
| GH-3900 | 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-3900 | Software | 1.1 | 4/15/2015 | Software 1.1 With ACMT | Software 1.1 With ACMT | 9200-38000, 9200-38100 | ||
| GH-3900 | Software | 1.0 | 8/13/2013 | GH-3900 RSU Software | GH-3900 RSU Software | 576-6193-01, 576-6207-01, 576-6209 | ||
| GH-3900 | Software | 1.3 | 3/17/2016 | GH-3900 Software 1.3 W/MPC Tool | GH-3900 Software W/MPC 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 | ||
| 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 | 1.2 | 6/28/2013 | Software 1.2 W/ACMT | Software 1.2 | 9200-34400, 9200-34500, 9200-34600, 9200-34700 | ||
| 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 | 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 | 1.1 | 2/6/2013 | GH3900.2 S/W 1.1 | Software File | 9200-34400, 9200-34500, 9200-34600, 9200-34700 | ||
| GH-3900 | Software | Software 1.1 With ACMT | 1.1 | 9/17/2012 | GH-3900 AMCT S/W 1.1 | 576-6159-02, 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 | 1.0 | 3/22/2012 | GH-3900 S/W 1.0 | Software file | 9200-34000, 9200-34100 | ||
| 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 | 576-6193-01 | F | 6/20/2017 | AHRS Installation tool | 9200-38000-0101, 9200-38100-0101 | ||
| 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 | Software | GH-3900-34000-R01.00 | 1.0 | 3/22/2012 | SW Version 1.0 R01.00 | SW Version 1.0 R01.00 | 9200-34000-( ) 9200-34100-( ) | |
| 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-R01.01 | 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-R01.02 | 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-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-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-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-3900 | Software | GH-3900.2-34400-R01.05 | 1.5 | 11/3/2016 | Software Release 1.5 R01.05 (W/ACM Tool) | Software Release 1.5 R01.05 (W/ACM Tool) | 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900 | |
| GH-3900 | Software | GH-3900-34000-R01.03 | 1.3 | 3/17/2016 | SW Version 1.0 R01.00 | SW Version 1.0 R01.00 | 576-6159-03, 9200-34000, 9200-34000-0101, 9200-34000-0201, 9200-34000-0401, 9200-34100, 9200-34100-0101, 9200-34100-0201 | |
| GH-3900 | Installation Aircraft Tools | 576-6157-08 | 1.01 | 9/11/2019 | ACM Tool for GH-3900.2 | ACMT 576-6157-08 (revision 1.01) | 576-6157-08, 9200-34400, 9200-34402, 9200-34410, 9200-34500, 9200-34502, 9200-34600, 9200-34602, 9200-34700, 9200-34702, 9200-34802, 9200-34900 | |
| GH-3900 | 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 | 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 | Y | 1/26/2022 | Installation Manual, GH-3900.2 | This manual contains installation instructions and recommended flightline maintenance information for the 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. The system may include the ADC-4000 Air Data Computer and MAG3000 or MAG-3100 Magnetometer. This information is supplemented and kept current by revisions, service letters and service bulletins. 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 | Instruction Manual | 0040-34402-01 | A | 7/18/2012 | Aircraft Configuration Module Tool | 576-6157-01 | ||
| GH-3900 | Instruction Manual | 0040-34402-02 | A | 2/7/2013 | Revision 2.03 Aircraft Config File Ver 02.06 | Revision 2.03 Aircraft Config File Ver 02.06 | 576-6157-02 | |
| GH-3900 | 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 | Instruction Manual | 0040-34402-06 | E | 12/13/2018 | Aircraft Configuration Module Tool | ACMT Instruction Manual | 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900 | |
| GH-3900 | Instruction Manual | 0040-34402-05 | A | 1/23/2015 | ACMT | 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900 | ||
| GH-3900 | Instruction Manual | 0040-34402-03 | B | 12/18/2013 | Revision 2.04 /2.05 A/C config file 02.08 | Revision 2.04 /2.05 A/C config file 02.08 | ||
| GH-3900 | Instruction Manual | 0040-34402-04 | B | 5/20/2014 | ACMT | Revision 2.07 Aircraft Config File 02.09 | 9200-34400, 9200-34500, 9200-34600, 9200-34700, 9200-34800 | |
| GH-3900 | Instruction Manual | 0040-34402-08 | D | 6/28/2021 | Aircraft Configuration Module Tool Rev 1.02, Version 02.16 | Aircraft Configuration Module Tool. (Rev 1.02) | 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 | Instruction Manual | 0040-34402-07 | B | 12/13/2018 | Aircraft Configuration Module Tool 1.03 | Aircraft Configuration Module Tool | 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900, 9200-34400 | |
| GH-3900.2 | Intermediate Maintenance Manual | 0040-34404-01 | 34-20-78 | B | 7/8/2019 | Abbreviated Component Maintenanence Manual | Abbreviated CMM | 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 | 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 | Pilot Guide | 0040-34400-01 | P | 6/28/2021 | GH-3900.2 Pilots Guide | Software 1.0;1.1; 1.2, 1.3, 1.4, 1.5, 1.6, 1.7, 1.8 | 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 | Printer Copies | 0040-34400-01PC | P | 6/28/2021 | GH-3900.2 Pilots Guide | Printer copy GH-3900.2 PG | ||
| GH-3900 | Service Bulletin | SB9200-34400-1 | B | 6/2/2016 | Release of Software Revision 1.1 | Software Revision 1.1 | 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900 | Service Bulletin | SB9200-34600-1 | B | 6/2/2016 | Release of Software Version 1.1 | Release of Software Version 1.1 | 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900 | Service Bulletin | SB9200-34500-1 | B | 6/2/2016 | Release of Software Ver 1.1 | Release of Software Ver 1.1 | 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900 | Service Bulletin | SB9200-34700-1 | B | 6/2/2016 | Release of Software Version 1.1 | Release of Software Version 1.1 | 9200-34700-0101, 9200-34700-0201, 9200-34700-0401 | |
| GH-3900 | Service Bulletin | SB576-6157-1 | B | 5/24/2013 | ACMT REV 2.03.1 Planning information | ACMT REV 2.03.0 | 9200-34400-, 9200-34500-, 9200-34600-, 9200-34700-, 9200-34800- | |
| GH-3900 | Service Bulletin | SB9200-34400-4 | A | 5/28/2014 | Software Release 1.3 | Software Release 1.3 | 9200-34400, 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900 | Service Bulletin | SB9200-34800-1 | A | 5/28/2014 | Software 1.3 | Software 1.3 | 9200-34800, 9200-34800-0101, 9200-34800-0201, 9200-34800-0401 | |
| GH-3900 | Service Bulletin | SB9200-34700-4 | A | 5/28/2014 | Software 1.3 | Software 1.3 | 9200-34700, 9200-34700-0101, 9200-34700-0201, 9200-34700-0401 | |
| GH-3900 | Service Bulletin | SB9200-34600-3 | A | 5/28/2014 | Software 1.3 | Software 1.3 | 9200-34600, 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900 | Service Bulletin | SB9200-34500-4 | A | 5/28/2014 | Software 1.3 | Software 1.3 | 9200-34500, 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900 | Service Bulletin | SB9200-34900-1 | A | 1/29/2015 | GH-3900.2 System Software Release 1.4 | GH-3900.2 System Software Release 1.4 | 9200-34900, 9200-34900-0101 | |
| GH-3900 | Service Bulletin | SB9200-34800-2 | A | 1/29/2015 | GH-3900.2 System Software Release 1.4 | GH-3900.2 System Software Release 1.4 | 9200-34800, 9200-34800-0101, 9200-34800-0201, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900 | 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 | 9200-34700 | |
| GH-3900 | Service Bulletin | SB9200-34600-4 | A | 1/29/2015 | GH-3900.2 System Software Release 1.4 | GH-3900.2 System Software Release 1.4 | 9200-34600, 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900 | Service Bulletin | SB9200-34500-5 | A | 1/29/2015 | GH-3900.2 System Software Release 1.4 | GH-3900.2 System Software Release 1.4 | 9200-34500, 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900 | 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 | 9200-34400, 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900 | Service Bulletin | SB9200-34700-3 | D | 1/29/2014 | GH-3900.2 System Software Release 1.2 (Version R01.02) | Release of 1.2 Software | 9200-34700-0101, 9200-34700-0201, 9200-34700-0401 | |
| GH-3900 | Service Bulletin | SB9200-34600-2 | D | 1/29/2014 | GH-3900.2 System software Release 1.2 (Version R01.02) | Software Version 1.2 | 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900 | Service Bulletin | SB9200-34500-3 | D | 1/29/2014 | GH-3900.2 System software Release 1.2 (Version R01.02) | Software Version 1.2 | 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900 | Service Bulletin | SB9200-34400-3 | D | 1/29/2014 | GH-3900.2 System software Release 1.2 (Version R01.02) | Software Version 1.2 | 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900 | Service Bulletin | SB576-6157-2 | A | 12/18/2013 | ACMT Rev 2.05 | ACMT Rev 2.05 | 9200-34400-, 9200-34500-, 9200-34600-, 9200-34700-, 9200-34800- | |
| GH-3900 | Service Bulletin | SB9200-34400-7 | A | 11/3/2016 | Software 1.5 upgrade | Software 1.5 | 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900 | Service Bulletin | SB9200-34700-6 | A | 11/3/2016 | Software 1.5 Upgrade | Software 1.5 | 9200-34700-0101, 9200-34700-0201, 9200-34700-0401 | |
| GH-3900 | Service Bulletin | SB9200-34600-6 | A | 11/3/2016 | Software 1.5 upgrade | Software 1.5 | 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900 | Service Bulletin | SB9200-34500-7 | A | 11/3/2016 | Software 1.5 upgrade | Software 1.5 | 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900 | Service Bulletin | SB9200-34410-2 | A | 11/3/2016 | Software 1.5 upgrade | Software 1.5 | 9200-34410-0501 | |
| GH-3900 | Service Bulletin | SB9200-34900-3 | A | 11/3/2016 | Software 1.5 upgrade | Software 1.5 | 9200-34900-0101 | |
| GH-3900 | Service Bulletin | SB9200-34800-4 | A | 11/3/2016 | Software 1.5 upgrade | Software 1.5 | 9200-34800-0101, 9200-34800-0201, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900 | Service Bulletin | SB9200-34502-1 | B | 5/3/2017 | To prevent Memory Corruptions | 9200-34500, 9200-34502 | ||
| GH-3900 | Service Bulletin | SB9200-34400-9 | A | 12/8/2017 | Software Release 1.6 | Software Release 1.6 | 9200-34400, 9200-34400-0101, 9200-34400-0201, 9200-34400-0301, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900 | 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. | 9200-34802-0401 | |
| GH-3900 | Service Bulletin | SB9200-34802-1 | B | 7/18/2018 | To prevent Memory Corruptions | To prevent Memory Corruptions | 9200-34800-0401, 9200-34802-0401 | |
| GH-3900 | Service Bulletin | SB9200-34602-1 | B | 7/18/2018 | To prevent Memory coruptions | To prevent Memory coruptions | 9200-34600-0401, 9200-34602-0401 | |
| GH-3900 | Service Bulletin | SB9200-34502-3 | A | 2/21/2017 | Updates the 5V current limit setting | Updates the 5V current limit setting | 9200-34502-0401 | |
| GH-3900 | 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. | 9200-34502 | |
| GH-3900 | 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. | 9200-34402-0501 | |
| GH-3900 | Service Bulletin | SB9200-34702-1 | A | 5/3/2017 | To prevent memory corruptions | To prevent memory corruptions | 9200-34700-0401, 9200-34702-0401 | |
| GH-3900 | 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. | 9200-34901-0101 | |
| GH-3900 | 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. | 9200-34900-0101 | |
| GH-3900 | 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. | 9200-34800-0101, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900 | 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. | 9200-34600-0101, 9200-34600-0201, 9200-34600-0401 | |
| GH-3900 | 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. | 9200-34500-0101, 9200-34500-0201, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900 | 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. | 9200-34410-0501 | |
| GH-3900 | 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. | 9200-34400-0101, 9200-34400-0201, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900.2 | Service Bulletin | SB9200-34410-5 | A | 7/31/2018 | Error Correcting RAM (MOD C) | Error Correcting RAM | 9200-34500-0201 | |
| GH-3900 | Service Bulletin | SB9200-34800-7 | A | 7/31/2018 | Error Correcting RAM | Error Correcting RAM | 9200-34800-0101, 9200-34800-0601 | |
| GH-3900 | Service Bulletin | SB9200-34602-6 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34602-0401 | |
| GH-3900 | Service Bulletin | SB9200-34802-6 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34802-0401 | |
| GH-3900 | Service Bulletin | SB9200-34702-4 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34702-0401 | |
| GH-3900 | Service Bulletin | SB9200-34502-7 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34502-0101, 9200-34502-0401, 9200-34502-0601 | |
| GH-3900 | Service Bulletin | SB9200-34800-9 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34800-0101, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900 | Service Bulletin | SB9200-34700-10 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34700-0101, 9200-34700-0401, 9200-34700-0601 | |
| GH-3900 | Service Bulletin | SB9200-34600-11 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34600-0101, 9200-34600-0201, 9200-34600-0401 | |
| GH-3900 | Service Bulletin | SB9200-34500-12 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34500-0101, 9200-34500-0401, 9200-34500-0601 | |
| GH-3900 | Service Bulletin | SB9200-34400-12 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34400-0101, 9200-34400-0201, 9200-34400-0501 | |
| GH-3900 | Service Bulletin | SB9200-34701-1 | A | 7/31/2018 | Error Correcting RAM | Error Correcting RAM | 9200-34701-0201, 9200-34701-0401 | |
| GH-3900 | Service Bulletin | SB9200-34600-9 | A | 7/31/2018 | Error Correcting RAM | Error Correcting RAM | 9200-34600-0101, 9200-34600-0201 | |
| GH-3900 | Service Bulletin | SB9200-34500-10 | A | 7/31/2018 | Error Correcting RAM | Error Correcting RAM | 9200-34500-0201 | |
| GH-3900 | Service Bulletin | SB9200-34901-4 | A | 4/4/2018 | Error Correcting RAM | Error Correcting RAM | 9200-34901-0101 | |
| GH-3900 | Service Bulletin | SB9200-34900-6 | A | 4/4/2018 | Error Correcting RAM | Error Correcting RAM | 9200-34900-0101 | |
| GH-3900 | Service Bulletin | SB9200-34800-5 | A | 3/8/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement | 9200-34800-0101, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900 | Service Bulletin | SB9200-34400-10 | C | 10/11/2018 | Error Correcting RAM | Error Correcting RAM | 9200-34400-0101, 9200-34400-0401 | |
| GH-3900 | Service Bulletin | SB9200-34802-3 | A | 1/25/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement | 9200-34802-0401 | |
| GH-3900 | Service Bulletin | SB9200-34502-4 | B | 3/8/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement | 9200-34502-0101, 9200-34502-0401, 9200-34502-0601 | |
| GH-3900 | Service Bulletin | SB9200-34500-8 | B | 3/8/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement | 9200-34500-0101, 9200-34500-0201, 9200-34500-0601 | |
| GH-3900 | Service Bulletin | SB9200-34410-3 | A | 1/25/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement | 9200-34410-0501 | |
| GH-3900 | Service Bulletin | SB9200-34602-3 | A | 3/8/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement | 9200-34602-0401 | |
| GH-3900 | Service Bulletin | SB9200-34600-7 | A | 3/8/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM Replacement | 9200-34600-0101, 9200-34600-0201, 9200-34600-0401 | |
| GH-3900 | Service Bulletin | SB9200-34901-2 | A | 1/25/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement | 9200-34901-0101 | |
| GH-3900 | Service Bulletin | SB9200-34901-3 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6 | 9200-34901-3 | |
| GH-3900 | Service Bulletin | SB9200-34900-5 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6 | 9200-34900-0101 | |
| GH-3900 | Service Bulletin | SB9200-34802-4 | A | 12/8/2017 | System Software Release 1.6 | 9200-34802-0401 | ||
| GH-3900 | Service Bulletin | SB9200-34800-6 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6 | 9200-34800-0101, 9200-34800-0201, 9200-34800-0401, 9200-34800-0601 | |
| GH-3900 | Service Bulletin | SB9200-34402-3 | A | 1/25/2018 | Display and Rate Sensor CCM Replacement | Display and Rate Sensor CCM Replacement | 9200-34402-0501 | |
| GH-3900 | Service Bulletin | SB9200-34900-4 | A | 1/25/2018 | Display Rate and Sensor CCM Replacement | Display Rate and Sensor CCM Replacement | 9200-34900-0101 | |
| GH-3900 | Service Bulletin | SB9200-34400-8 | A | 1/25/2018 | Display and Rate Sensor CCM replacement | Display and Rate Sensor CCM replacement | 9200-34400, 9200-34400-0101, 9200-34400-0201, 9200-34400-0401, 9200-34400-0501 | |
| GH-3900 | Service Bulletin | SB9200-34700-8 | B | 7/31/2018 | Error Correcting RAM | Error Correcting RAM | 9200-34700-0101, 9200-34700-0201, 9200-34700-0601 | |
| GH-3900 | Service Bulletin | SB9200-34700-7 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6 | 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 | 9200-34702-0401 | |
| GH-3900 | Service Bulletin | SB9200-34602-4 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6 | 9200-34602-0401 | |
| GH-3900 | Service Bulletin | SB9200-34600-8 | A | 12/8/2017 | System Software Release 1.6 | System Software 1.6 | 9200-34600-0101, 9200-34600-0201, 9200-34600-0301, 9200-34600-0401 | |
| GH-3900 | Service Bulletin | SB9200-34502-5 | A | 12/8/2017 | System Software 1.6 | System Software 1.6 | 9200-34502-0101, 9200-34502-0401, 9200-34502-0601 | |
| GH-3900 | Service Bulletin | SB9200-34500-9 | A | 12/8/2017 | System Software 1.6 | System Software 1.6 | 9200-34500-0101, 9200-34500-0201, 9200-34500-0301, 9200-34500-0401, 9200-34500-0501 | |
| GH-3900 | Service Bulletin | SB9200-34410-4 | A | 12/8/2017 | System Software 1.6 | System Software 1.6 | 9200-34410-4 | |
| GH-3900 | Service Bulletin | SB9200-34402-4 | A | 12/8/2017 | System Software 1.6 | 9200-34402-0501 | ||
| GH-3900 | Service Bulletin | SB001-GH-3900.2 | 00 | 6/28/2021 | Software Release 1.8 | Software Release 1.8 | ||
| GH-3900 | Service Bulletin | SB9200-34402-5 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | SB9200-34402 | |
| GH-3900 | Service Bulletin | SB9200-34410-6 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34410 | |
| GH-3900 | Service Bulletin | SB9200-34900-7 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34900 | |
| GH-3900 | Service Bulletin | SB9200-34800-8 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34800 | |
| GH-3900 | Service Bulletin | SB9200-34700-9 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34700 | |
| GH-3900 | Service Bulletin | SB9200-34600-10 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34600 | |
| GH-3900 | Service Bulletin | SB9200-34500-11 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34500 | |
| GH-3900 | Service Bulletin | SB9200-34400-11 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34400 | |
| GH-3900 | Service Bulletin | SB9200-34901-6 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34901-0101 | |
| GH-3900 | Service Bulletin | SB9200-34402-6 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34402-0501 | |
| GH-3900 | Service Bulletin | SB9200-34701-3 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34701-0101, 9200-34701-0201, 9200-34701-0401 | |
| GH-3900 | Service Bulletin | SB9200-34900-8 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-34900-0101 | |
| GH-3900 | Service Bulletin | SB9200-34802-5 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | SB9200-34802 | |
| GH-3900 | Service Bulletin | SB9200-34702-3 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | SB9200-34702 | |
| GH-3900 | Service Bulletin | SB9200-34602-5 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | 9200-34602 | |
| GH-3900 | Service Bulletin | SB9200-34502-6 | B | 9/11/2019 | Software Release 1.7 | Software Release 1.7 | SB9200-34502 | |
| GH-3900 | Service Bulletin | SB576-6157-3 | A | 9/11/2019 | To inform customers of an update to Aircraft Configuration Module Tool (rev 1.01). | ACMT Rev 1.01, Aircraft Configuration 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 | Service Bulletin | SB576-6157-4 | A | 10/30/2019 | To inform customers of an update to Aircraft Configuration Module Tool (rev 1.02). | ACMT Rev 1.02, Aircraft Configuration 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 | 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 | 1.2 | 6/28/2013 | Software 1.2 W/ACMT | Software 1.2 | 9200-34400, 9200-34500, 9200-34600, 9200-34700 | ||
| 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 | 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 | 3900.2 S/W 1.00 | 3900.2 S/W 1.00 | 9200-34400-xx | |
| GH-3900 | Software | 1.1 | 2/6/2013 | GH3900.2 S/W 1.1 | Software File | 9200-34400, 9200-34500, 9200-34600, 9200-34700 | ||
| 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 | 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 | Software | GH-3900.2-34400-R01.05 | 1.5 | 11/3/2016 | Software Release 1.5 R01.05 (W/ACM Tool) | Software Release 1.5 R01.05 (W/ACM Tool) | 9200-34400, 9200-34410, 9200-34500, 9200-34600, 9200-34700, 9200-34800, 9200-34900 | |
| 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-R01.01 | 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-R01.00 | 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-R01.04 | 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 | Component Maintenance Manual | 0040-38003-01 | B | 10/18/2016 | GH-3900RSU CMM | GH-3900RSU CMM | 9200-38000-0101, 9200-38100-0101 | |
| GH-3900 | 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-3900 | Instruction Manual | 0040-38002-01 | A | 8/14/2013 | Aircraft Configuration Tool | GH-3900RSU Rev 1.01 Config File 03.00 | ||
| 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 | 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 | 9200-38000- | |
| GH-3900 | 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. | SB9200-38100-0101 | |
| GH-3900 | 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. | 9200-38000-0101 | |
| GH-3900RSU | Service Bulletin | SB9200-42600-7 | A | 3/16/2015 | Release of Software 1.2 | To inform customers of System Software Release 1.2 (version R01.02) for the GHR-4200 Repeater. | 9200-042600-0201 | |
| GH-3900 | Service Bulletin | SB576-6207-1 | A | 9/24/2015 | Aircraft Configuration Module Tool – Revision 1.01 | Aircraft Configuration Module Tool – Revision 1.01 | 9200-38000-0101, 9200-38100-0101 | |
| GH-3900RSU | Service Bulletin | SB576-6193-1 | A | 9/24/2015 | AHRS Installation Tool – Rev 1.54 | AHRS Installation Tool – Rev 1.54 | 9200-38500-0201 9200-38600-0201 | |
| GH-3900 | Software | 1.1 | 4/15/2015 | Software 1.1 With ACMT | Software 1.1 With ACMT | 9200-38000, 9200-38100 | ||
| GH-3900 | Software | 1.0 | 8/13/2013 | GH-3900 RSU Software | GH-3900 RSU Software | 576-6193-01, 576-6207-01, 576-6209 | ||
| GH-3900 | 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-3900 | 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-3900 | 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-3900 | Software | 576-6193-01 | F | 6/20/2017 | AHRS Installation tool | 9200-38000-0101, 9200-38100-0101 | ||
| GH-4001 | Installation Aircraft Tools | 576-6245-04 | B | 2/25/2020 | ACM Tool | ACM Tool | ||
| GH-4001 | Installation Aircraft Tools | 576-6158-03 | A | 3/29/2016 | Tool | Field Loader Tool (altenate to 576-6158-02) | ||
| GH-4001 | Installation Manual | 0040-45001-01 | M | 9/26/2022 | GH-4001 Install Manual | Electronic file not available. Call L3 for secure copy. | 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 | |
| GH-4001 | Installation Manual | 0040-45101-01 | A | 3/23/2017 | GH-4001 Installation & Operation Manual | Not Avaialible on Website | 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 | Service Bulletin | SB9200-45000-3 | A | 12/18/2017 | Update EESeal to support pin injection waveform 3 conditions. | 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 | 9200-45000-0101, 9200-45000-0301, 9200-45000-0401 | |
| GH-4001 | Service Bulletin | SB9200-45201-1 | A | 6/10/2015 | Eliminate sticking of knob. | 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) | 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. | 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) | 9200-45300-0101, 9200-45300-0201 | |
| GH-4001 | Service Bulletin | SB9200-45000-1 | A | 5/13/2016 | System Software Release 1.1 | 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 | 9200-45201, 9200-45201-0101 | ||
| GH-4001 | Service Bulletin | SB9200-45000-2 | A | 8/17/2016 | Incorporation of MOD A | Incorporation of MOD A | 9200-45000-0401 | |
| GH-4001 | Service Bulletin | SB576-6245-1 | A | 2/19/2020 | ACM Tool | ACM Tool | 9200-45000-, 9200-45001-, 9200-45100-, 9200-45201-, 9200-45300-, 9200-45400- | |
| GH-4001 | Service Bulletin | SB9200-45000-5 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-45000-0101, 9200-45000-0401 | |
| GH-4001 | Service Bulletin | SB9200-45300-3 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-45300-0201, 9200-45300-0301 | |
| GH-4001 | Service Bulletin | SB9200-45201-4 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-45201-0101, 9200-45201-5101 | |
| GH-4001 | Service Bulletin | SB9200-45400-1 | A | 4/26/2019 | Backlight LED Replacement | Backlight LED Replacement | 9200-45400-0301 | |
| 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 | To provide alternate U1 Rate Sensor when replacement becomes necessary. | GH-4001 - Hardware MOD | 9200-45000-0101, 9200-45000-0401, 9200-45000-3010, 9200-45201-0101, 9200-45201-5101, 9200-45400-0301, 9200-45400-0501 | |
| GH-4001 | Software | GH-4001-Pub-Notice-SW1.3 | orig | 8/29/2019 | GH-4001_Pub-Notice_SW1.3 | GH-4001_Pub-Notice_SW1.3 | 9200-45000-( ) | |
| GH-4200 | Installation Manual | 0040-42001-01 | F | 2/28/2022 | Installation and Operation Manual | Manual is ITAR and not availible | ||
| 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 | 9200-42000-0201 | |
| GH-4200 | Service Bulletin | SB9200-42000-6 | A | 4/9/2014 | Improve Reliablity of the 5VDC Power Supply | Improve Reliablity of the 5VDC Power Supply | 9200-42000-0201 | |
| GH-4200 | Service Bulletin | SB9200-42000-9 | 00 | 2/28/2022 | MOD G – New Rate Sensor | Service Bulletin | ||
| GH-4200 | Service Bulletin | SB9200-42000-10 | 00 | 2/28/2022 | MOD H – New Display Backlight CCA | Service Bulletin | ||
| GH-4200 | Service Bulletin | SB9200-42000-11 | 00 | 2/28/2022 | MOD J – New Display Assembly | Service Bulletin | 9200-42000-0201 | |
| GH-4200 | Installation Manual | 0040-42001-01 | F | 2/28/2022 | Installation and Operation Manual | Manual is ITAR and not availible | ||
| GHR-4000 | Service Bulletin | SB9200-42600-8 | 00 | 2/28/2022 | MOD F – New Display Backlight CCA / MOD G – New Display Assembly | Service Bulletin | 9200-42600-0201 | |
| FA2100 CVDR | Installation Aircraft Tools | 17TES0436 | Orig | 12/14/2020 | 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 | 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 | |
| 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 | Component Maintenance Manual | TP-417 | 34-20-24 | 1 | 8/19/1993 | Maintenance Manual | Pub# TP-417 | 501-1537-01 |
| HI-601 | Service Letter | SL-288 | A | 7/17/2013 | Corrections to Manual | Corrections to 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 | |
| HSI-3000 | Installation Manual | TP-570 | F | 7/17/2017 | Installation and Operation Manual | Pub# TP-570 | 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 | Installation Manual | TP-600 | C | 8/2/2011 | Installation and Operation Manual | Pub# TP-600 | 501-1899-01 | |
| 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 | SB501-1847-6 | 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 | SB501-1899-6 | 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 | SB501-1899-7 | A | 6/26/2009 | To provide replacement display due to diminishing source. | To provide replacement display due to diminishing source. | 501-1899-01 | |
| EHSI-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 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 | SB501-1899-1 | C | 1/3/2007 | To reduce the possibility of the display blanking or failing at start up. | 501-1899-01 | ||
| HSI-3000 | Service Bulletin | SB501-1847-5 | 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 | SB501-1847-4 | C | 4/8/2010 | Eliminate encoder out-of-range faults. | 501-1847-01, 501-1847-02, 501-1847-04 | ||
| HSI-3000 | Service Bulletin | SB501-1847-2 | 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 | SB501-1847-1 | D | 4/8/2010 | Provide replacement display due to diminishing source. | 501-1847-01, 501-1847-02, 501-1847-04 | ||
| HSI-3000 | Service Letter | SL-181 | Orig | 4/16/2003 | Update indicators with 1.C3 software to 2.0 software. | 501-1847-01 | ||
| HSI-3000 | Service Letter | SL-287 | A | 6/20/2013 | Fault Code Identification | HSI-3000 Fault Codes | 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 | |
| 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-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 | |
| 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 | 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 | 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 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 | 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 Letter | SL-265 | A | 3/11/2011 | Discontinued Support for i-linc MFD | 9200-19000-, 9200-19020-, 9200-19050-, 9200-19070- | ||
| F3849 | Installation Manual | 009A0301 | 1 | 8/1/1988 | Installation Manual | Pub# 009A0301 | 805C0620-( ), 805D0602-( ), 805D0660-( ), 805D0661-( ), 805D0662-( ), 805D0663-( ) | |
| ID-2472 | Pilot Guide | 009-10029-001 | B | 11/23/1998 | Pilot's Guide | Pub# 009-10029-001 | 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 | |
| ID-2472 | Pilot Guide | 009-10029-001 | B | 11/23/1998 | Pilot's Guide | Pub# 009-10029-001 | 805C0620-( ) | |
| JF- Test Set | Component Maintenance Manual | TP-290 | original | 7/26/2005 | Instruction Manual | Pub# TP-290 | 570-1473-05 | |
| JF- Test Set | Installation Manual | TP-409 | Original | 7/26/2005 | Installation Manual | Pub# TP-409 JT-113 | 570-2466-01 | |
| JT- Test Set | Component Maintenance Manual | TP-278 | 1 | 6/17/1985 | Instruction Manual | Pub# TP-278 | 570-1426-02, 570-1685-01 | |
| JT- Test Set | Component Maintenance Manual | TP-280 | Reis | 4/1/1974 | Instruction Manual and Test Procedures | JT-7 | 570-1433-01 | |
| JT- Test Set | Component Maintenance Manual | TP-283 | 1 | 4/1/1974 | Instruction Manual and Test Procedures | JT-10 | 570-1428-01 | |
| JT- Test Set | Component Maintenance 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 | |
| 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 | |
| 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 | |
| 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 | |
| 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 | Installation Manual | 165E4866-00 | 14 | 7/13/2020 | LDR1000 Installation and Operation Manual | LDR1000 Install Manual | 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 | LDR1000 Coin Battery Replacement Procedure (Restricted) | LDR1000 Coin Battery Replacement Procedure (Restricted) | 1000-1000-00, 1000-1210-00, 1000-1210-11, 1000-1710-00, 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-40 | Orig | 11/1/1983 | Improve transient response and ripple rejection of LR651 power supply. | 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. | 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. | 805D0500 | |
| AD611 | Service Bulletin | SB-47 | Orig | 8/1/1985 | Modification to DME Range Block Adapter to permit module to operate throughout an input range. | 804B0001 | ||
| LNS6000 | Service Bulletin | SB-60 | Orig | 3/1/1987 | To correct an intermittent search problem. | To correct an intermittent search problem. | 805D0500 | |
| AD611 | Service Bulletin | SB-51 | Orig | 8/1/1985 | Modification to DME Range Block Adapter Module to increase A+ voltage range. | 804B0116 | ||
| AD611 | Service Bulletin | SB-52 | Orig | 11/1/1985 | Modification to Range Block Adapter Module to permit operation throughtout voltage range. | 804B0116 | ||
| LNS6000 | Service Letter | SL-154 | Orig | 4/23/1998 | To provide proper configuration setup procedures and replacement of GPS antenna. | 805-10008-( ) | ||
| 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 | 009A0631A | 4 | 4/1/1989 | Installation Manual | Pub# 009A0631A | 009A0631A | |
| LNS6000 | Installation Manual | 009A0652 | 2 | 10/9/1995 | Installation Manual | DB683 Airborne Navigation Data Storage system | 805D0651-02, 805D0651-04 | |
| Loran Nav System | Installation Manual | 12710138B | B | 3/1/1987 | Installation Manual | Pub# 12710138B | 30410035-( ) 12710138A 12710138B | |
| Loran Nav System | Pilot Guide | 12710139-1 | C1 | 10/7/1993 | Operation Manual | Pub# 12710139-1 | 30410035-( ) | |
| 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 | Service Bulletin | SB-55 | Orig | 5/1/1986 | LRN500 faceplate bonding modification. | LRN500 faceplate bonding modification. | 805D0630 | |
| ADC-3000 | Installation Manual | TP-593 | E | 12/18/2013 | Installation and Operation Manual | Pub# TP-593 | 501-1797-( ), 501-1803-( ), 501-1826-01, 501-1851-2403, 501-1851-2404 | |
| DCM | Installation Manual | TP-582 | G | 3/4/2010 | Installation and Operation Manual | Pub# TP-582 | 501-1826-01, 501-1860-0102, 501-1860-0104, 501-1870-( ) | |
| ADC-3000 | Installation Manual | TP-579 | E | 5/1/2018 | Installation and Operation Manual | Pub# TP-579 | 501-1741-2104, 501-1741-2105, 501-1741-2204, 501-1741-2304, 501-1741-2404, 501-1741-2504, 501-1741-2604, 501-1741-2704, 501-1741-2804, 501-1826-01, 501-1881-01 | |
| 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 | |
| ADC-3000 | Installation Manual | TP-530 | L | 6/15/2016 | Installation and Operation Manual | Pub# TP-530 | 501-1797-23, 501-1797-24, 501-1797-71, 501-1803-145, 501-1803-31C, 501-1803-32B, 501-1826-01, 501-1851-01, 501-1851-2402, 501-1851-2405 | |
| ADC-3000 | Installation Manual | TP-531 | C | 5/27/2009 | Installation and Operation Manual | Pub# TP-531 | 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-( ) | |
| 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 | |
| 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-182 | Orig | 4/29/2004 | Exposure of the magnetometer to magnetic fields. | 501-1826-01, 501-1826-02 | ||
| 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 | 0040-21200-01 | J | 9/5/2017 | MAG-3100 Installation Manual | MAG-3100 Install Manual | 9200-21200-( ), 9200-21200-01 | |
| DCM | Installation Manual | TP-559 | K | 3/30/2017 | Installation and Operation Manual, GH-3100 | 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 | 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 | ||
| 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-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 | |
| ESI-500 | Installation Manual | 0040-15001-01 | J | 2/9/2021 | ESI-500 /MAG-500 Installation Manual | Electronic Standby Indicator | 9200-15000-0101, 9200-15500-0101 | |
| EFD-750 | Installation Manual | 0040-15751-01 | E | 7/14/2021 | EFD-750 / MAG-500 Installation Manual | includes SW1.2 / new part number | 9200-15751-0101, 9200-15753-0101, 9200-15754-0101, 9200-15754-0201, 9200-15500-0101, 9200-15500-0201, 9200-15750-0101, 9200-15751-0201, 9200-15754-0301 | |
| EFD-750 | Pilot Guide | 0040-15750-01 | C | 12/12/2019 | EFD-750 Operation Manual | includes SW1.2 | 9200-15753-0101, 9200-15754-0101, 9200-15754-0201, 9200-15751-0101, 9200-15751-0201, 9200-15750-0101 | |
| ESI-500 | Pilot Guide | 0040-15000-01 | F | 10/2/2019 | Pilot Guide | ESI-500 Pilot Guide | 9200-15000-0101, 9200-15500-0101 | |
| 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 | |
| MAT-3100 | Service Bulletin | SB9200-21250-1 | A | 5/1/2014 | New Cable Assembly | New Cable Assembly | 9200-21250-01 | |
| MT-101 | Component Maintenance Manual | TP-237 | 22-20-01 | 8 | 5/30/2018 | Instruction Manual, Operation, Installation, Maintenance | Pub# TP-237 | 501-1132-01, 501-1132-02, 501-1132-04, 501-1132-05 |
| MT-101 | Service Bulletin | SB501-1132-1 | Orig | 11/20/1974 | To extend upper Mach limit. | 501-1132-01, 501-1132-02 | ||
| MT-101 | Service Bulletin | SB501-1132-10 | C | 8/1/1980 | To provide consistent monitor latch reset with out-of-phase F input during ground test. | 501-1132-02 | ||
| MT-101 | Service Bulletin | SB501-1132-11 | A | 8/1/1980 | To increase monitor latch circuit reset time. | 501-1132-02 | ||
| MT-101 | Service Bulletin | SB501-1132-12 | Orig | 1/1/1983 | To update MT-101 to Model E. | 501-1132-01, 501-1132-02, 501-1132-03 | ||
| MT-101 | Service Bulletin | SB501-1132-13 | A | 1/1/1983 | To prevent trim oscillation and improve mach gain circuit temperature characteristics. | 501-1132-04, 501-1132-05 | ||
| MT-101 | Service Bulletin | SB501-1132-14 | B | 6/1/1990 | To prevent fail light from flashing during ground test. | 501-1132-04, 501-1132-05 | ||
| MT-101 | Service Bulletin | SB501-1132-15 | A | 9/21/2006 | To improve short circuit protection on MT-101A,B,D and E. | 501-1132-( ) | ||
| MT-101 | Service Bulletin | SB501-1132-16 | A | 8/1/1983 | To allow manual trim circuit operation with lower logic levels. | 501-1132-01, 501-1132-02 | ||
| MT-101 | Service Bulletin | SB501-1132-17 | A | 11/1/1988 | To use higher reliability diode. | 501-1132-( ) | ||
| MT-101 | Service Bulletin | SB501-1132-18 | Orig | 9/1/1988 | To increase the unit service life by replacing four power supply capacitors with new components. | 501-1132-( ) | ||
| MT-101 | Service Bulletin | SB501-1132-19 | Orig | 8/1/1990 | To prevent possible damage to circuit card due to excessive heat in the event of a power supply failure. | 501-1132-( ) | ||
| MT-101 | Service Bulletin | SB501-1132-2 | Orig | 5/1/1975 | To protect transformer from line shorts. | 501-1132-01 | ||
| MT-101 | Service Bulletin | SB501-1132-3 | Orig | 5/1/1975 | To improve noise immunity. | 501-1139-01 | ||
| MT-101 | Service Bulletin | SB501-1132-4 | Orig | 10/1/1975 | To prevent ground loop. | 501-1132-01 | ||
| MT-101 | Service Bulletin | SB501-1132-5 | Orig | 11/1/1976 | To reduce monitor trip at high mach. | 501-1132-01 | ||
| MT-101 | Service Bulletin | SB501-1132-6 | Orig | 12/1/1977 | To enable self-test circuit to work with all air data sensors. | 501-1132-01 | ||
| MT-101 | Service Bulletin | SB501-1132-7 | Orig | 6/1/1978 | To prevent premature aural warning during manual trim at low temperature. | 501-1132-01 | ||
| MT-101 | Service Bulletin | SB501-1132-8 | Orig | 2/1/1979 | To prevent fail light from illuminating during manual trim condition. | 501-1132-01 | ||
| MT-101 | Service Bulletin | SB501-1132-9 | G | 8/1/1980 | To update MT-101A to MT-101B configuration by adding Mach Trim latching circuit. | 501-1132-01, 501-1132-02 | ||
| MT-101 | Service Letter | SL-45 | Orig | 6/1/1981 | To inform customers of potential problems with 2N5822 CA-200and 2N5195 transistors. | |||
| 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 | Pilot Guide | 009-10132-001 | A | 1/28/2000 | Pilot's Guide | Pub# 009-10132-001 | ||
| NACWS | Pilot Guide | 009-10033-001 | 2 | 5/22/1995 | Operator's Manual | Pub# 009-10033-001 | ||
| 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-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 | ||
| 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 | ||
| NY163 | Service Bulletin | SB805-10930-01 | A | 11/24/2010 | To provide authorized service centers procedures to check antenna anti-static coating properties. | 805-10930-001, 805-10930-002 | ||
| NY163 | Service Bulletin | SB805-10930-02 | A | 11/24/2010 | To improve -Band rejection | 805-10930-001, 805-10930-002 | ||
| 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 | ||
| CA-2001 | Installation Manual | TP-258 | Orig | 8/1/1980 | Instruction Manual, Operation and Installation | Pub# TP-258 | 501-1172-01, 501-1172-02, 501-1172-03, 501-1172-04, 501-1172-05, 501-1172-06, 501-1196-01, 501-1196-02, 501-1199-01, 501-1199-02, 501-1199-03, 501-1199-04, 501-1199-05, 501-1199-06, 501-1200-01, 501-1200-02, 501-1200-03, 501-1200-04, 501-1200-05, 501-1201-01, 501-1201-02, 501-1202-01, 501-1202-02, 501-1207-01, 501-1207-02, 501-1207-03, 501-1207-04, 501-1207-05, 501-1207-06, 501-1207-07, 501-1207-08, 501-1232-02, 501-1232-03, 501-1232-04, 501-1232-05, 501-1232-06, 501-1279-01 | |
| PA-377 | Component Maintenance Manual | TP-206 | Orig | 3/1/1970 | Instruction Manual | Pub# TP-206 | 501-1085-01, 501-1085-02 | |
| PB-1002 | 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 |
| PB-1002 | Service Letter | SL-21 | F | 9/21/1987 | To provide information when installing BFG Static Inverters, Phase Lock Boxes and Parallel Systems in various aircraft. | |||
| PB-1002 | 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 |
| PB-1002 | Service Letter | SL-21 | F | 9/21/1987 | To provide information when installing BFG Static Inverters, Phase Lock Boxes and Parallel Systems in various aircraft. | |||
| PB-1002 | Service Letter | SL-21 | F | 9/21/1987 | To provide information when installing BFG Static Inverters, Phase Lock Boxes and Parallel Systems in various aircraft. | |||
| 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 | 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 | 17TES0043 | |
| PI/1 | Service Letter | SIL-001-L3AP | 00 | 5/27/2021 | 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 | 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-L3AP | 00 | 5/27/2021 | 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 | 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 | |
| AP General Files | Service Letter | PI/2-001 | 01 | 6/20/2022 | Notification of discontinued product. | Notification of discontinued product. | 17TES0062, 17TES0065, 17TES0066, 17TES0092 | |
| PL-100 | Component Maintenance Manual | TP-243 | 24-50-03 | 1 | 5/15/1991 | PL-100 Phase Lock Adapter | PL-100 Phase Lock Adapter | 501-1179-01, 501-1179-02 |
| PL-100 | Service Bulletin | SB501-1179-2 | Orig | 3/1/1992 | To prevent chafing and breakdown between chassis and flex cable caused by flex cable rubbing against CCA mounting hardware. | 501-1179-02 | ||
| PB-1002 | Service Letter | SL-21 | F | 9/21/1987 | To provide information when installing BFG Static Inverters, Phase Lock Boxes and Parallel Systems in various aircraft. | |||
| PL-103 | Component Maintenance Manual | TP-378 | 24-50-02 | 3 | 1/4/2002 | Maintenance Manual with IPL | Pub# TP-378 | 501-1334-01, 501-1334-02, 501-1594-01 |
| PL-103 | Installation Manual | TP-374 | 24-50-04 | Reis | 12/15/1992 | Installation Manual | Pub# TP-374 | 501-1334-01, 501-1334-02 |
| PL-103 | Service Bulletin | SB501-1334-1 | Orig | 10/1/1985 | To insure test requirements of Table 5-2, steps 5, 6 and 7 in TP-378. | 501-1334-01, 501-1334-02 | ||
| PL-103 | Service Bulletin | SB501-1334-2 | Orig | 10/1/1985 | To eliminate possible oscillations to the over/under voltage circuit. | 501-1334-01, 501-1334-02 | ||
| PL-103 | Service Bulletin | SB501-1334-3 | Orig | 7/1/1986 | To assure proper phase lock operation at low temperature; and to correct the gain of the precision rectifier to negative polarity input voltages. | 501-1334-01, 501-1334-02 | ||
| PL-103 | Service Bulletin | SB501-1334-4 | Orig | 5/1/1987 | To replace U2, U5, and U13 and prevent possible oscillations at temperature extremes. | 501-1334-01, 501-1334-02 | ||
| PL-103 | Service Bulletin | SB501-1334-5 | Orig | 5/1/1987 | To improve capture reliability at high temperature. | 501-1334-01, 501-1334-02 | ||
| PL-103 | Service Bulletin | SB501-1334-6 | Orig | 5/1/1987 | To insure proper connector engagement. | 501-1334-01, 501-1334-02 | ||
| PL-103 | Service Bulletin | SB501-1334-7 | Orig | 6/28/2004 | To prevent intermittent energization of bus-tie relay during startup by inhibiting the circuit for a one second delay after energization. | 501-1334-01, 501-1334-03 | ||
| PB-1002 | Service Letter | SL-21 | F | 9/21/1987 | To provide information when installing BFG Static Inverters, Phase Lock Boxes and Parallel Systems in various aircraft. | |||
| PL-103 | Component Maintenance Manual | TP-378 | 24-50-02 | 3 | 1/4/2002 | Maintenance Manual with IPL | Pub# TP-378 | 501-1334-01, 501-1334-02, 501-1594-01 |
| CA-2001 | Installation Manual | TP-258 | Orig | 8/1/1980 | Instruction Manual, Operation and Installation | Pub# TP-258 | 501-1172-01, 501-1172-02, 501-1172-03, 501-1172-04, 501-1172-05, 501-1172-06, 501-1196-01, 501-1196-02, 501-1199-01, 501-1199-02, 501-1199-03, 501-1199-04, 501-1199-05, 501-1199-06, 501-1200-01, 501-1200-02, 501-1200-03, 501-1200-04, 501-1200-05, 501-1201-01, 501-1201-02, 501-1202-01, 501-1202-02, 501-1207-01, 501-1207-02, 501-1207-03, 501-1207-04, 501-1207-05, 501-1207-06, 501-1207-07, 501-1207-08, 501-1232-02, 501-1232-03, 501-1232-04, 501-1232-05, 501-1232-06, 501-1279-01 | |
| PS-800 | Component Maintenance Manual | TP-204 | 4/1/1974 | PS-800 Maintenance Manual | PS-800 Maintenance Manual | 501-1043-01, 501-1043-02 | ||
| PS-800 | Service Letter | SL-4 | A | 2/22/1972 | To provide information on PS-800/PS-801 battery maintenance. (Contact Learjet for parts and service). | |||
| PS-800 | Service Letter | SL-7 | Orig | 1/2/1973 | To provide PS-800 manual correction, JT-5 manual correction, PS-823 manual modification clarification, installation of inductor to reduce effects on PS-823 when keying high capacitance radio and information on gyro handling. | |||
| PS-800 | Service Letter | SL-11 | B | 6/11/1986 | To provide Emergency Power Supply use information. (Contact Learjet for parts and service). | 501-1046-( ), 501-1075-( ) | ||
| PS-801 | Component Maintenance Manual | TP-205 | 4/1/1974 | PS-801 Maintenance Manual | PS-801 Maintenance Manual | 16-1010-01, 16-1010-02 | ||
| PS-800 | Service Letter | SL-11 | B | 6/11/1986 | To provide Emergency Power Supply use information. (Contact Learjet for parts and service). | 501-1046-( ), 501-1075-( ) | ||
| PS-800 | Service Letter | SL-4 | A | 2/22/1972 | To provide information on PS-800/PS-801 battery maintenance. (Contact Learjet for parts and service). | |||
| PS-823 | Component Maintenance Manual | TP-202 | 24-20-03 | B | 8/1/2018 | Component Maintenance Manual | TP-202 | 501-1075-01, 501-1075-02, 501-1075-03, 501-1075-04, 501-1075-05, 501-1075-06, 501-1075-07, 501-1075-08, 501-1075-09, 501-1075-10, 501-1075-11, 501-1075-12, 501-1075-13, 501-1075-14, 501-1075-15, 501-1075-16 |
| PS-823 | Installation Manual | TP-352 | Orig | 6/10/1987 | Installation instructions | Pub# TP-352 | 501-1075-01, 501-1075-02, 501-1075-03, 501-1075-04, 501-1075-05, 501-1075-06, 501-1075-07, 501-1075-08, 501-1075-09, 501-1075-10, 501-1075-11, 501-1075-12, 501-1075-13, 501-1075-14, 501-1075-15, 501-1075-16 | |
| PS-823 | Service Bulletin | SB501-1075-1 | B | 5/15/2002 | To prevent transistor leakage during battery charging. | 501-1075-01, 501-1075-02, 501-1075-05, 501-1075-06, 501-1075-10, 501-1075-13, 501-1075-14 | ||
| PS-823 | Service Bulletin | SB501-1075-10 | A | 5/10/2002 | To correct modification identification. | 501-1075-05, 501-1075-06, 501-1075-07, 501-1075-08, 501-1075-13, 501-1075-14, 501-1075-15, 501-1075-16 | ||
| PS-823 | Service Bulletin | SB501-1075-11 | A | 5/10/2002 | Refer to SB501-1075-8 | |||
| PS-823 | Service Bulletin | SB501-1075-12 | A | 5/10/2002 | To prevent premature turn-off and battery damage due to overcharging. | 501-1075-( ) | ||
| PS-823 | Service Bulletin | SB501-1075-13 | A | 5/10/2002 | To relocate C18 to prevent interference with connector. | 501-1075-( ) | ||
| PS-823 | Service Bulletin | SB501-1075-14 | A | 5/10/2002 | To provide for use of battery without operating inverter. | 501-1075-( ) | ||
| PS-823 | Service Bulletin | SB501-1075-15 | B | 5/10/2002 | To permit by-pass of circuit protection fuse. | 501-1075-( ) | ||
| PS-823 | Service Bulletin | SB501-1075-16 | G | 5/10/2002 | To provide charging resistor and battery input line isolation, and prevent battery damage due to charging circuit failure. | 501-1075-( ) | ||
| PS-823 | Service Bulletin | SB501-1075-17 | A | 7/26/2005 | SB501-1075-17 | 501-1075-( ) | ||
| PS-823 | Service Bulletin | SB501-1075-18 | C | 5/10/2002 | To improve starting without application of AC power at low temperature extremes. | 501-1075-( ) | ||
| PS-823 | Service Bulletin | SB501-1075-19 | A | 5/5/2002 | Rescinded. Part number replacement now identified in SB501-1075-20 and manual TP-202 | 501-1075-( ) | ||
| PS-823 | Service Bulletin | SB501-1075-2 | 7/26/2005 | SB501-1075-2 | 501-1075-( ) | |||
| PS-823 | Service Bulletin | SB501-1075-20 | C | 6/30/2005 | To disseminate information concerning replacement of parts no longer procurable. | 501-1075-( ) | ||
| PS-823 | Service Bulletin | SB501-1075-21 | B | 5/5/2002 | To provide self-locking hardware at selected locations. | 501-1075-( ) | ||
| PS-823 | Service Bulletin | SB501-1075-22 | A | 5/5/2002 | To insure that shifted phase voltage level is maintained after time-out. | 501-1075-01, 501-1075-02, 501-1075-05, 501-1075-06, 501-1075-09, 501-1075-10, 501-1075-13, 501-1075-14 | ||
| PS-823 | Service Bulletin | SB501-1075-23 | E | 2/28/2003 | To provide emergency buss fuse bypass. FACTORY ONLY MODIFICATION | 501-1075-01, 501-1075-02, 501-1075-03, 501-1075-04, 501-1075-05, 501-1075-06, 501-1075-07, 501-1075-08 | ||
| PS-823 | Service Bulletin | SB501-1075-24 | A | 4/30/2002 | Rescinded and superseded by SB501-1075-25. | |||
| PS-823 | Service Bulletin | SB501-1075-25 | A | 4/30/2002 | To improve transistor turn-off time and reduce internal heat rise. | 501-1075-( ) | ||
| PS-823 | Service Bulletin | SB501-1075-26 | A | 4/30/2002 | To reduce transistor heat rise and improve RFI. | 501-1075-( ) | ||
| PS-823 | Service Bulletin | SB501-1075-27 | A | 4/30/2002 | To reduce possibility of circuit damage due to excessive testing or low voltage. | 501-1075-05, 501-1075-06, 501-1075-07, 501-1075-08, 501-1075-13, 501-1075-14, 501-1075-15, 501-1075-16 | ||
| PS-823 | Service Bulletin | SB501-1075-28 | A | 4/30/2002 | To prevent possible electrical damage due to mishandling of cover. | 501-1075-05, 501-1075-06, 501-1075-07, 501-1075-08, 501-1075-13, 501-1075-14, 501-1075-15, 501-1075-16 | ||
| PS-823 | Service Bulletin | SB501-1075-3 | 7/26/2005 | SB501-1075-3 | 501-1075-( ) | |||
| PS-823 | Service Bulletin | SB501-1075-4 | H | 5/15/2002 | To provide battery monitoring test capability. (Return to factory for modification.) | 501-1075-01, 501-1075-02, 501-1075-03, 501-1075-04, 501-1075-09, 501-1075-10, 501-1075-11, 501-1075-12 | ||
| PS-823 | Service Bulletin | SB501-1075-5 | A | 5/15/2002 | To aid starting with capacitive loads. | 501-1075-( ) | ||
| PS-823 | Service Bulletin | SB501-1075-6 | A | 5/10/2002 | To prevent inverter output during battery test. | 501-1075-05, 501-1075-06, 501-1075-07, 501-1075-08, 501-1075-13, 501-1075-14, 501-1075-15, 501-1075-16 | ||
| PS-823 | Service Bulletin | SB501-1075-7 | B | 5/10/2002 | Superceded by SB501-1075-26 | |||
| PS-823 | Service Bulletin | SB501-1075-8 | B | 5/15/2002 | To relocate Q9 to increase heatsink capability. | 501-1075-( ) | ||
| PS-823 | Service Bulletin | SB501-1075-9 | A | 5/10/2002 | To reduce heat rise to improve battery charge. | 501-1075-( ) | ||
| PS-823 | Service Letter | SL-5 | B | 4/15/1983 | To provide information on PS-823 battery cell test & maintenance. | 501-1075-( ) | ||
| PS-823 | Service Letter | SL-48 | A | 7/23/2001 | To provide information on replacement of PS-823 with PS-835 and SI-100 Static Inverter. | 501-1075-( ), 501-1228-( ) | ||
| PS-800 | Service Letter | SL-7 | Orig | 1/2/1973 | To provide PS-800 manual correction, JT-5 manual correction, PS-823 manual modification clarification, installation of inductor to reduce effects on PS-823 when keying high capacitance radio and information on gyro handling. | |||
| PS-823 | Service Letter | SL-79 | Orig | 5/15/1984 | To eliminate vertical freedom of "short" cells in battery packs. | 501-1075-( ) | ||
| PS-823 | Service Letter | SL-8 | U | 6/23/2011 | To provide PS-823 battery pack charging and test information as it appears in Component Maint. Manual TP-202. | Periodic Manitenance for PS-823 | 501-1075-( ), 501-1075-01, 501-1075-02, 501-1075-03, 501-1075-04, 501-1075-05, 501-1075-06, 501-1075-07, 501-1075-08, 501-1075-09, 501-1075-10, 501-1075-11, 501-1075-12, 501-1075-13, 501-1075-14, 501-1075-15, 501-1075-16 | |
| PS-823 | Service Letter | SL-64 | E | 8/19/2010 | To inform customers of the effects of battery out gassing. | Obsolete | ||
| PS-823 | Service Letter | SL-84 | C | 2/24/2011 | To disseminate battery cell/pack availability/non-availability. (Supersedes SL-61) | |||
| PS-800 | Service Letter | SL-11 | B | 6/11/1986 | To provide Emergency Power Supply use information. (Contact Learjet for parts and service). | 501-1046-( ), 501-1075-( ) | ||
| PS-823 | Service Letter | SL-109 | A | 8/7/2000 | To inform users and service centers the merits of using BFG inspected of cells. | |||
| PS-823 | Service Letter | SL-270 | C | 10/6/2015 | To provide service facilities with shelf life information for NiCad batteries | Updates the descriptive paragraph | 501-1075-( ) | |
| PS-823 | Service Letter | SL-331 | A | 3/14/2018 | PS-823 Battery Replacement Policy | PS-823 Battery Replacement Policy | 501-1075, 501-1075-01, 501-1075-02, 501-1075-03, 501-1075-04, 501-1075-05, 501-1075-06, 501-1075-08, 501-1075-09, 501-1075-10, 501-1075-11, 501-1075-12, 501-1075-13, 501-1075-14, 501-1075-15, 501-1075-16 | |
| PS-823 | Service Letter | SL-311 | B | 1/9/2017 | Manual Subscription Service Policy | 501-1075, 501-1228, 501-1682, 501-1712, 501-1719 | ||
| PS-823 | Service Letter | SIL-001-PS-823 | 00 | 5/4/2022 | PS-823 - End of Battery Sales Notice | PS-823 - End of Battery Sales Notice | 501-1075-xx | |
| 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 |
| PS-834 | Component Maintenance Manual | TP-475 | 24-30-06 | B | 4/23/2018 | Component Maintenance Manual | TP-475 | 501-1682-01, 501-1682-02 |
| PS-834 | Installation Manual | TP-447 | 24-30-05 | B | 5/8/2006 | Installation and Operation Manual | Pub# TP-447 | 501-1682-01, 501-1682-02 |
| PS-834 | Service Bulletin | SB501-1682-1 | B | 5/8/2006 | To prevent possible internal short circuit within the battery assembly, that may have occurred during assembly, and could result in a loss of battery power. | 501-1682-01 | ||
| PS-834 | Service Bulletin | SB501-1682-2 | A | 7/18/2001 | To provide replacement parts for devices no longer available. | 501-1682-01 | ||
| PS-834 | Service Bulletin | SB501-1682-3 | Orig | 5/1/2001 | Provide replacement part for a device no longer procurable. | 501-1682-01, 501-1682-02 | ||
| PS-834 | Service Bulletin | SB501-1682-4 | Orig | 7/18/2001 | Provide replacement part for a device no longer procurable. | 501-1682-01, 501-1682-02 | ||
| PS-834 | Service Bulletin | SB501-1682-5 | Orig | 5/15/2003 | To add warning instructions for proper care and maintenance of battery pack to prevent voiding warranty. | 501-1682-01, 501-1682-02 | ||
| PS-834 | Service Bulletin | SB501-1682-6 | D | 11/21/2011 | To prevent Q16 from overheating. | To prevent Q16 from overheating. | 501-1682-01, 501-1682-02 | |
| PS-834 | Service Letter | SL-120 | F | 11/30/2009 | To provide a procedure which will permit charging and testing of the PS-834 Emergency Power Supply using a locally generated test set-up, to determine the integrity of the unit prior to installation in an aircraft, or to satisfy the annual charge/discharg | 501-1682-( ), 501-1682-01, 501-1682-02 | ||
| PS-823 | Service Letter | SL-64 | E | 8/19/2010 | To inform customers of the effects of battery out gassing. | Obsolete | ||
| PS-823 | Service Letter | SL-311 | B | 1/9/2017 | Manual Subscription Service Policy | 501-1075, 501-1228, 501-1682, 501-1712, 501-1719 | ||
| PS-834 | Service Letter | SL-337 | B | 3/28/2019 | End of Manufacturing Notice | Service Letter | 501-1682-01, 501-1682-02 | |
| PS-834 | Service Letter | SL-269 | D | 5/11/2017 | To provide service facilities with shelf life information for sealed lead batteries. | Sealed Lead Acid Batteries- Shelf Life | 501-1228( ), 501-1682-(), 501-1712( ), 501-1719( ) | |
| PS-834 | Troubleshooting Guide | TP-608 | C | 6/11/2009 | Troubleshooting Guide, PS-834 | Troubleshooting Guide, PS-834 | 501-1682-02 | |
| PS-835 | Component Maintenance Manual | TP-329 | 24-30-02 | C5 | 3/30/2020 | Component Maintenance Manual | TP-329 | 501-1228-01, 501-1228-02, 501-1228-03, 501-1228-04, 501-1228-05, 501-1228-06, 501-1228-07 |
| PS-835 | Installation Manual | TP-336 | 24-30-04 | R | 9/26/2022 | Installation Manual | several updates: the purpose of the equipment, venting and the verbiage in low and high temperature storage | 501-1228-01, 501-1228-02, 501-1228-03, 501-1228-04, 501-1228-05, 501-1228-06, 501-1228-07 |
| PS-835 | Service Bulletin | SB501-1228-1 | B | 2/28/2004 | To prevent J2 from arcing during testing. | 501-1228, 501-1228-01, 501-1228-02 | ||
| PS-835 | Service Bulletin | SB501-1228-10 | C | 5/15/2004 | To provide emergency buss fuse bypass. | 501-1228-02, 501-1228-04 | ||
| PS-835 | Service Bulletin | SB501-1228-11 | A | 2/28/2004 | To prevent possible inadvertent shorting. | 501-1228-01, 501-1228-03, 501-1228-05 | ||
| PS-835 | Service Bulletin | SB501-1228-12 | A | 11/20/2003 | To prevent shorting the batteries to the case in the event of cover damage in areas of the battery CCA. | 501-1228-() | ||
| PS-835 | Service Bulletin | SB501-1228-13 | A | 2/28/2004 | To provide protection against improper charging. | 501-1228-() | ||
| PS-835 | Service Bulletin | SB501-1228-14 | B | 2/28/2004 | To correct improper battery wire routing that could result in wire insulation cold flow and eventual short circuit condition. | 501-1228-04 | ||
| PS-835 | Service Bulletin | SB501-1228-15 | A | 6/20/2003 | To add warning instructions for proper care and maintenance of battery pack to prevent voiding of warranty. | 501-1228-() | ||
| PS-835 | Service Bulletin | SB501-1228-2 | B | 2/28/2004 | To provide improved thermal resistor to reduce the possibility of shorting. | 501-1228-01, 501-1228-02 | ||
| PS-835 | Service Bulletin | SB501-1228-3 | A | 2/28/2004 | To provide increased insulation between battery cell BT 12 and the chassis. | 501-1228-02 | ||
| PS-835 | Service Bulletin | SB501-1228-4 | B | 2/28/2004 | To prevent the possibility of PWB damage due to loss of battery to chassis isolation. | 501-1228-01, 501-1228-02 | ||
| PS-835 | Service Bulletin | SB501-1228-5 | B | 2/28/2004 | To insure proper installation of PS-835A Mod 3 and PS-835B Mod 4. | 501-1228-01, 501-1228-02 | ||
| PS-835 | Service Bulletin | SB501-1228-6 | D | 2/28/2004 | To install Mod 1 on A2 PC Board to reduce possibility of transistors shorting to ground. | 501-1228-01, 501-1228-02 | ||
| PS-835 | Service Bulletin | SB501-1228-7 | Orig | 5/20/1982 | To provide self-test of power supply output as well as battery output to detect possible fuse failure. | 501-1228-01, 501-1228-02, 501-1228-03, 501-1228-04 | ||
| PS-835 | Service Bulletin | SB501-1228-8 | B | 1/30/2002 | To meet voltage spike test catagory "A" of DO-160A Environmental test requirements. | 501-1228-01, 501-1228-02 | ||
| PS-835 | Service Bulletin | SB501-1228-9 | A | 2/28/2004 | To improve heater enabling circuit. | 501-1228-01, 501-1228-02, 501-1228-03, 501-1228-04 | ||
| PS-834 | Service Letter | SL-269 | D | 5/11/2017 | To provide service facilities with shelf life information for sealed lead batteries. | Sealed Lead Acid Batteries- Shelf Life | 501-1228( ), 501-1682-(), 501-1712( ), 501-1719( ) | |
| PS-835 | Service Letter | SL-264 | E | 1/26/2017 | PS-835 Battery Replacement | Service Letter | 501-1228-( ) | |
| PS-823 | Service Letter | SL-311 | B | 1/9/2017 | Manual Subscription Service Policy | 501-1075, 501-1228, 501-1682, 501-1712, 501-1719 | ||
| PS-835 | Service Letter | SL-322 | A | 1/26/2017 | PS-835 Battery Repalcement Policy | Service Letter | 501-1228, 501-1228-01, 501-1228-02, 501-1228-03, 501-1228-04, 501-1228-05, 501-1228-06, 501-1228-07 | |
| PS-823 | Service Letter | SL-64 | E | 8/19/2010 | To inform customers of the effects of battery out gassing. | Obsolete | ||
| PS-835 | Service Letter | SL-59 | A | 8/14/1982 | To inform Learjet operators of FAA requirements for use of PS-835( ) Emergency Power Supplies. | 501-1228-( ) | ||
| PS-835 | Service Letter | SL-61 | 10/14/1982 | Replaced by SL-84A. | ||||
| PS-835 | Service Letter | SL-80 | AD | 4/11/2018 | PS-835 Battery inspection and maintenance procedures. | PS-835 Battery inspection and maintenance procedures | 501-1228-(), 501-1228-01, 501-1228-02, 501-1228-03, 501-1228-04, 501-1228-05, 501-1228-06, 501-1228-07 | |
| PS-823 | Service Letter | SL-48 | A | 7/23/2001 | To provide information on replacement of PS-823 with PS-835 and SI-100 Static Inverter. | 501-1075-( ), 501-1228-( ) | ||
| PS-823 | Service Letter | SL-84 | C | 2/24/2011 | To disseminate battery cell/pack availability/non-availability. (Supersedes SL-61) | |||
| PS-835 | Service Letter | SL-85 | Orig | 12/14/1984 | To disseminate information about cell tie down straps. | |||
| PS-823 | Service Letter | SL-109 | A | 8/7/2000 | To inform users and service centers the merits of using BFG inspected of cells. | |||
| PS-835 | Service Letter | SL-105 | A | 4/5/1988 | To provide a PS-835 Power Supply self-test procedure for units installed in Cessna Citation Aircraft. | 501-1228-( ) | ||
| PS-835 | Troubleshooting Guide | TP-607 | B | 6/6/2008 | PS-835 Troubleshooting guide | PS-835 Troubleshooting guide | 501-1228-01, 501-1228-02, 501-1228-03, 501-1228-04, 501-1228-05, 501-1228-06 | |
| PS-850 | Component Maintenance Manual | TP-483 | 24-30-08 | C5 | 4/16/2019 | Component Maintenance Manual | TP-483 | 501-1712-01, 501-1712-02, 501-1712-03, 501-1712-04, 501-1719-01, 501-1719-02 |
| PS-850 | Installation Manual | TP-470 | 24-30-07 | K | 8/22/2017 | Installation and Operation Manual | Add Model D to Discharge Test criteria | 501-1712-01, 501-1712-02, 501-1712-03, 501-1712-04, 501-1719-01, 501-1719-02 |
| PS-850 | Service Bulletin | SB501-1719-10 | B | 8/19/2010 | Prevent Short Circuits | Eliminate the potential for short circuits due to insulation failure | 501-1719-( ), 501-1719-01, 501-1719-02 | |
| PS-850 | Service Bulletin | SB501-1712-2 | Orig | 11/1/1993 | To insure proper remote test lamp illumination when other than the BFG recommended installation configuration is used. | 501-1712-( ), 501-1719-( ) | ||
| PS-850 | Service Bulletin | SB501-1719-1 | Orig | 5/1/2001 | To prevent possible internal short circuit within battery which may occur during assembly and could result in loss of battery power. | 501-1719-02 | ||
| PS-850 | Service Bulletin | SB501-1719-2 | Orig | 11/1/1993 | To insure proper remote test lamp illumination when other than the BFG recommended installation configuration is used. | 501-1719-( ) | ||
| PS-850 | Service Bulletin | SB501-1719-3 | Orig | 10/1/1995 | To insure positive battery retention under all component tolerance conditions. | 501-1719-01, 501-1719-02 | ||
| PS-850 | Service Bulletin | SB501-1719-4 | A | 3/2/1998 | To prevent possible low battery capacity indication. Present calibration setting may exhibit low capacity indication with actual capacities in excess of 50%. | 501-1719-01, 501-1719-02 | ||
| PS-850 | Service Bulletin | SB501-1719-5 | Orig | 7/12/2001 | Provide replacement parts for devices no longer available. | 501-1719-01, 501-1719-02 | ||
| PS-850 | Service Bulletin | SB501-1719-6 | Orig | 8/1/2002 | Provide positive stop for battery to prevent movement under sever shock. | 501-1719-01, 501-1719-02 | ||
| PS-850 | Service Bulletin | SB501-1719-7 | B | 12/12/2013 | To reduce susceptibility of the heater circuit to overheating of Q5 and Q6 transistors on the A2 circuit card. | REV B | 501-1719-01, 501-1719-02 | |
| PS-850 | Service Bulletin | SB501-1719-8 | Orig | 5/15/2003 | To add warning instructions for proper care and maintenance of battery pack to prevent voiding warranty. | 501-1719-01, 501-1719-02 | ||
| PS-850 | Service Bulletin | SB501-1719-9 | A | 4/12/2005 | To inform customers of lowered battery storage capacity for specific units installed between November 1, 2004 through March 31, 2005. | 501-1719-01, 501-1719-02 | ||
| PS-850 | Service Letter | SL-170 | K | 7/23/2014 | PS-850/PS-855 Battery Inspection, Storage and Maintenance Procedures. | Updated Discharge Test criteria | 501-1712-(), 501-1712-01, 501-1712-02, 501-1712-03, 501-1712-04, 501-1719-(), 501-1719-01, 501-1719-02 | |
| PS-823 | Service Letter | SL-64 | E | 8/19/2010 | To inform customers of the effects of battery out gassing. | Obsolete | ||
| PS-834 | Service Letter | SL-269 | D | 5/11/2017 | To provide service facilities with shelf life information for sealed lead batteries. | Sealed Lead Acid Batteries- Shelf Life | 501-1228( ), 501-1682-(), 501-1712( ), 501-1719( ) | |
| PS-823 | Service Letter | SL-311 | B | 1/9/2017 | Manual Subscription Service Policy | 501-1075, 501-1228, 501-1682, 501-1712, 501-1719 | ||
| PS-850 | Troubleshooting Guide | TP-609 | B | 6/6/2008 | Troubleshooting Guide, PS-850 and PS-855 | Troubleshooting Guide, PS-850 and PS-855 | ||
| PS-850 | Component Maintenance Manual | TP-483 | 24-30-08 | C5 | 4/16/2019 | Component Maintenance Manual | TP-483 | 501-1712-01, 501-1712-02, 501-1712-03, 501-1712-04, 501-1719-01, 501-1719-02 |
| PS-850 | Installation Manual | TP-470 | 24-30-07 | K | 8/22/2017 | Installation and Operation Manual | Add Model D to Discharge Test criteria | 501-1712-01, 501-1712-02, 501-1712-03, 501-1712-04, 501-1719-01, 501-1719-02 |
| PS-855 | Service Bulletin | SB501-1712-11 | B | 8/19/2010 | PS-855 Prevent Short Circuits | PS-855 Prevent Short Circuits | 501-1712-( ), 501-1712-01, 501-1712-02, 501-1712-03, 501-1712-04 | |
| PS-850 | Service Bulletin | SB501-1712-2 | Orig | 11/1/1993 | To insure proper remote test lamp illumination when other than the BFG recommended installation configuration is used. | 501-1712-( ), 501-1719-( ) | ||
| PS-855 | Service Bulletin | SB501-1712-3 | Orig | 10/26/1995 | To insure positive battery retention under all component tolerance conditions. | 501-1712-01, 501-1712-02 | ||
| PS-855 | Service Bulletin | SB501-1712-4 | A | 8/13/1997 | To prevent possible low battery capacity indication. Present calibration setting may exhibit low capacity indication with actual capacities in excess of 50%. | 501-1712-01, 501-1712-02 | ||
| PS-855 | Service Bulletin | SB501-1712-5 | Orig | 12/1/1997 | To allow unit to meet DO-160C, Section 20, Category Y for 200.0 V/meter. | 501-1712-03 | ||
| PS-855 | Service Bulletin | SB501-1712-6 | Orig | 7/12/2001 | To provide replacement parts for devices that are no longer available. | 501-1712-01, 501-1712-02, 501-1712-03 | ||
| PS-855 | Service Bulletin | SB501-1712-7 | Orig | 8/1/2002 | Provide positive stop for battery to prevent movement under sever shock. | 501-1712-01, 501-1712-02, 501-1712-03 | ||
| PS-855 | Service Bulletin | SB501-1712-8 | B | 12/12/2013 | To reduce susceptibility of the heater circuit to overheating of Q5 and Q6 transistors on the A2 circuit card. | 501-1712-01, 501-1712-02, 501-1712-03 | ||
| PS-855 | Service Bulletin | SB501-1712-9 | Orig | 5/15/2003 | To add warning instructions for proper care and maintenance of battery pack to prevent voiding warranty. | 501-1712-01, 501-1712-02, 501-1712-03 | ||
| PS-855 | Service Bulletin | SB501-1712-1 | Orig | 5/1/2001 | To prevent possible internal short circuit within battery which may occur during assembly and could result in loss of battery power. | 501-1712-02 | ||
| PS-855 | Service Bulletin | SB501-1712-10 | D | 9/9/2011 | To inform customers of lowered battery storage capacity for specific units installed between November 1, 2004 through March 31, 2005. | 501-1712-01, 501-1712-02, 501-1712-03, 501-1712-04 | ||
| PS-823 | Service Letter | SL-64 | E | 8/19/2010 | To inform customers of the effects of battery out gassing. | Obsolete | ||
| PS-850 | Service Letter | SL-170 | K | 7/23/2014 | PS-850/PS-855 Battery Inspection, Storage and Maintenance Procedures. | Updated Discharge Test criteria | 501-1712-(), 501-1712-01, 501-1712-02, 501-1712-03, 501-1712-04, 501-1719-(), 501-1719-01, 501-1719-02 | |
| PS-834 | Service Letter | SL-269 | D | 5/11/2017 | To provide service facilities with shelf life information for sealed lead batteries. | Sealed Lead Acid Batteries- Shelf Life | 501-1228( ), 501-1682-(), 501-1712( ), 501-1719( ) | |
| PS-823 | Service Letter | SL-311 | B | 1/9/2017 | Manual Subscription Service Policy | 501-1075, 501-1228, 501-1682, 501-1712, 501-1719 | ||
| PS-850 | Troubleshooting Guide | TP-609 | B | 6/6/2008 | Troubleshooting Guide, PS-850 and PS-855 | Troubleshooting Guide, PS-850 and PS-855 | ||
| QAR (uQAR) | Component Maintenance Manual | 165E2810-30 | 31-30-20 | 01 | 5/15/2018 | MicroQAR Quick Access Recorder CMM | MicroQAR CMM | 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 | 31-30-20 | 09 | 5/15/2018 | MicroQAR Installation & Operation Manual | MicroQAR IOM | QAR100-xx-xx, QAR101-xx-xx, QAR200-xx-xx, QAR201-xx-xx, QAR210-xx-xx |
| 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 | ST03560AT | A | 1/20/2022 | Supplemental Type Certificate | Micro QAR in MD-80 Series Aircraft | 905E7008-20 | |
| 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-( ) | |
| 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 | |
| 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 | |
| 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 | |
| CA-2001 | Installation Manual | TP-258 | Orig | 8/1/1980 | Instruction Manual, Operation and Installation | Pub# TP-258 | 501-1172-01, 501-1172-02, 501-1172-03, 501-1172-04, 501-1172-05, 501-1172-06, 501-1196-01, 501-1196-02, 501-1199-01, 501-1199-02, 501-1199-03, 501-1199-04, 501-1199-05, 501-1199-06, 501-1200-01, 501-1200-02, 501-1200-03, 501-1200-04, 501-1200-05, 501-1201-01, 501-1201-02, 501-1202-01, 501-1202-02, 501-1207-01, 501-1207-02, 501-1207-03, 501-1207-04, 501-1207-05, 501-1207-06, 501-1207-07, 501-1207-08, 501-1232-02, 501-1232-03, 501-1232-04, 501-1232-05, 501-1232-06, 501-1279-01 | |
| RC-2001 | Service Letter | SL-38 | SL-3 | 9/18/1980 | To provide information concerning Continuity checks between the RC-2001relay mating connector and other RC-2001 Aircraft components. | |||
| 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 | 03 | 9/27/2021 | Recorder Data Interface (RDI) Instruction Manual | Recorder Data Interface | 17TES0800, 17TES0900, 17TES0901, 17TES0950, 17TES0960 | |
| RDI | Service Bulletin | SB001-RDI | 00 | 10/5/2021 | RDI - Version 2.1 | RDI - Version 2.1 | 17TES0900, 17TES0901, 17TES0950, 17TES0960 | |
| PI/1 | Service Letter | SIL-001-L3AP | 00 | 5/27/2021 | 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 | 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 | |
| RDI | Service Letter | SIL-001-RDI | 00 | 10/6/2020 | Introduction of new tablet-based Recorder Data Interface (RDI) | Introduction of new tablet-based Recorder Data Interface (RDI) | 17TES0900 | |
| RDI | Software | RDI Release 2.1 | 2.1 | 4/30/2020 | RDI Software | Recorder Data Interface | 17TES0823 | |
| 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 | |
| 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. | ||
| 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. | ||
| RGC250 | 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. | ||
| RIPS | Installation Manual | 165-E4900-01 | 03 | 3/28/2022 | Installation & Operation Manual | TYPE II / II-A | 100-2010-000, 100-2010-001, 100-2010-100, 100-2010-101 | |
| RIPS | Service Letter | SIL-001-RIPS | 00 | 3/28/2022 | New optional RIPS Maintenance periodic maintenance plan. | New optional RIPS Maintenance periodic maintenance plan. | 100-2010-100, 100-2010-101 | |
| 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 | |
| 612RIU | Service Bulletin | SB-28 | Orig | 4/1/1981 | Waypoint Alert output during VOR/LOC operation. | 805D0450, 805D0480 | ||
| RNAV | Service Bulletin | SB-29 | Orig | 5/1/1981 | RNAV612 and 612RIU distance computation error when VNAV541 or VNAV541A has no A+ applied. | 805D0400 | ||
| RNAV | Service Bulletin | SB-23 | Orig | 4/1/1981 | Prevent momentary RNAV annunciate output during turn-on | 805D0450 | ||
| RNAV | Service Bulletin | SB-24 | Orig | 4/1/1981 | RNAV612 Microprocessor Program Corrections and Improvements. | 805D0450 | ||
| RNAV | Service Bulletin | SB-25 | Orig | 4/1/1981 | Momentary VOR Diagnostic for RNAV612 | 805D0450 | ||
| RNAV | Service Bulletin | SB-26 | Orig | 4/1/1981 | Com Transmitter RF Interference in 51DSA and 51DSA/C328 | 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. | 805D0450 | ||
| AD611 | Service Bulletin | SB-47 | Orig | 8/1/1985 | Modification to DME Range Block Adapter to permit module to operate throughout an input range. | 804B0001 | ||
| 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 | 805D0450 | ||
| RNAV | Service Bulletin | SB-34 | Orig | 10/1/1982 | Prevent random "auto shutdown" of RNAV612 microprocessor. | 805D0450 | ||
| RNAV | Service Bulletin | SB-35 | Orig | 11/1/1982 | Reduces VOR smoothing time constant in approach mode. | 805D0450 | ||
| RNAV | Service Bulletin | SB-36 | A | 1/1/1983 | Increase input level range of 51ASA-1 9960Hz input signal. | 805D0254 | ||
| RNAV | Service Bulletin | SB-37 | A | 1/1/1983 | Increases input signal range of 51ASA 9960Hz input signal. | 805D0251 | ||
| AD611 | Service Bulletin | SB-52 | Orig | 11/1/1985 | Modification to Range Block Adapter Module to permit operation throughtout voltage range. | 804B0116 | ||
| AD611 | Service Bulletin | SB-51 | Orig | 8/1/1985 | Modification to DME Range Block Adapter Module to increase A+ voltage range. | 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. | 805D0250 | ||
| 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 | ||
| DI681 | Component Maintenance Manual | 009A0550 | Orig | 8/1/1985 | Installation and Maintenance Manual | Pub# 009A0550 | 805D0500, 805D0520, 805D0530, 805D0550-( ), 805D0570, 805D0580 | |
| NY151 | 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-38 | Orig | 11/1/1983 | Provide DC Sine/Cosine RMI Drive provided at RNC601 J1. | 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. | 805D0550 | ||
| DI681 | Service Bulletin | SB-46 | Orit | 9/1/1984 | To eliminate wavering left/right needle and erratic OBS operation. | 805D0550 | ||
| DI681 | Service Bulletin | SB-44 | Orig | 6/1/1984 | To allow the RNC601 to communicate with the DI681 DataBase. | 805D0550 | ||
| RNC601 | Service Bulletin | SB-45 | Orig | 9/1/1984 | Improvement of Automatic Ident Decoding | 805D0550 | ||
| RNC601 | Service Bulletin | SB-49 | Orig | 10/1/1984 | Eliminate intermittent display blanking | 805D0550 | ||
| DI681 | Service Bulletin | SB-57 | Orig | 2/1/1988 | To allow DI681 to operate as DI681A with RNC601B. | 805D0570 | ||
| RNC601 | Service Bulletin | SB-56 | Oig | 3/1/1987 | To allow the RNC601 and RNC601A to operate with the same functions as the RNC601B. | 805D0550 | ||
| 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-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 | ||
| 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. | 805D0602-45 | |
| RT-1634(V) | Service Bulletin | SB805D0602-201 | A | 3/10/2005 | Replace C2 on power supply from 100 V to 125 V part. | 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 | 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 | SB805D0602-202 | B | 6/15/2006 | Power Supply Inductor Modification | Power Supply Inductor Modification | 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. | 805D0602-( ) | |
| 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 | 805D0602-45 | |
| RT-1634(V) | Service Bulletin | SB805D0602-204 | A | 11/17/2005 | Modulator PCB Modification | Modulator PCB Modification | 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 | 805D0602-51 | |
| RT-1634(V) | Service Bulletin | SB805D0602-207 | A | 6/21/2006 | Software Upgrade Revision 2.1 | Software Upgrade Revision 2.1 | 805D0602-52 | |
| SA-151 | Component Maintenance Manual | TP-486 | 22-10-19 | Orig | 7/31/1996 | Component Maintenance Manual | Pub# TP-486 | 501-1535-04 |
| SA-151 | Installation Manual | TP-432 | 22-10-17 | Reis | 2/28/1998 | Installation Manual | Pub# TP-432 | 501-1535-04 |
| SA-151 | Service Bulletin | SB501-1535-4 | Orig | 7/1/1997 | To insure proper retention of Pinion Gear to DC Servo Motor shaft. | 501-1535-04 | ||
| SA-151 | Service Letter | SL-99 | A | 2/16/1998 | To provide specific policy concerning lubrication requirements of BFGAS. Servo Actuator products. | 501-1535-01 | ||
| SA-151 | Supplemental Type Certificate | SA1464GL | Amen | 10/15/1996 | Installation of Jet Electronics and Technology, Inc., servo actuator model SA-151A or SA-151D in the Bendix M4 autopilot. | Installation of Jet Electronics and Technology, Inc., servo actuator model SA-151A or SA-151D in the Bendix M4 autopilot. | 501-1535-01, 501-1535-04 | |
| SA-151 | Supplemental Type Certificate | SA1463GL | Amen | 10/15/1996 | Installation of Jet Electronics and Technology, Inc. servo actuator model SA-151A or SA-151D in the Bendix M4 autopilot. | Installation of Jet Electronics and Technology, Inc. servo actuator model SA-151A or SA-151D in the Bendix M4 autopilot. | 501-1535-01, 501-1535-04 | |
| DB-340 | Component Maintenance Manual | TP-391 | 27-30-02 | 5 | 2/15/1986 | Maintenance Manual | Pub# TP-391 | 501-1419-01, 501-1420-01, 501-1421-01, 93-02-861-002 |
| SA-340 | Service Bulletin | SB501-1420-1 | A | 4/1/1993 | To prevent possible erroneous fail light indication. | 501-1420-01 | ||
| SA-340 | Service Bulletin | SB501-1420-2 | Orig | 4/1/1985 | To prevent erroneous fail light indication. | 501-1420-01 | ||
| SA-340 | Service Bulletin | SB501-1420-3 | Orig | 9/1/1985 | To provide transient suppresser diodes (VR1 and VR2) with a higher zener voltage level (74.7V Vs. 33V). | 501-1420-01 | ||
| SA-340 | Service Bulletin | SB501-1420-4 | Orig | 6/1/1991 | To compensate for tolerance shifts resulting in inability to set torque. | 501-1420-01 | ||
| SA-340 | Service Bulletin | SB501-1420-5 | Orig | 3/14/2003 | Sleeve bearing chatters and is noisy when dry. | 501-1420-01 | ||
| SA-340 | Service Bulletin | SB501-1420-6 | A | 3/12/2010 | Product improvement to eliminate possibility of slip clutch failures. | 501-1420-01 | ||
| SA-340 | Service Letter | SL-246 | AU | 5/4/2022 | Component Replacement List | Component Replacement List | 3S2060DC168A2A, 501-1478-02, 501-1478-03 | |
| DB-340 | Component Maintenance Manual | TP-413 | 27-30-03 | 2 | 9/30/1992 | Maintenance Manual with IPL | Pub# TP-413 | 501-1421-01, 501-1478-01, 501-1546-01 |
| DB-340 | Component Maintenance Manual | TP-465 | 27-30-04 | Orig | 12/23/1992 | Component Maintenance Manual | Pub# TP-465 | 501-1421-01, 501-1478-02, 501-1546-02 |
| SA-341 | Service Bulletin | SB501-1478-11 | B | 5/18/2009 | To Improve rigidity of clutch field anti-rotation stop | To Improve rigidity of clutch field anti-rotation stop | 501-1478-04, 501-1478-05 | |
| SA-341 | Service Bulletin | SB501-1478-12 | A | 5/18/2009 | To Improve rigidity of clutch field anti-rotation stop | To Improve rigidity of clutch field anti-rotation stop | 501-1478-02, 501-1478-03 | |
| SA-341 | Service Bulletin | SB501-1478-9 | A | 7/21/2008 | To ensure the integrity of one circuit board track | To ensure the integrity of one circuit board track | 501-1478-03 | |
| SA-341 | Service Bulletin | SB501-1478-10 | A | 7/21/2008 | To ensure the integrity of one circuit board track | To ensure the integrity of one circuit board track | 501-1478-04, 501-1478-05 | |
| SA-341 | Service Bulletin | SB501-1478-13 | A | 11/8/2012 | -04 MOD 9 -05 MOD5 | 501-1478-04, 501-1478-05 | ||
| SA-341 | Service Bulletin | SB501-1478-1 | Orig | 8/1/1987 | To prevent fail indication caused by difference in torque motor DC values. | 501-1478-01 | ||
| SA-341 | Service Bulletin | SB501-1478-2 | Orig | 9/1/1988 | To prevent possible shorting of Q1 on the A1 CCA to J1 connector mounting hardware. | 501-1478-2 | ||
| SA-341 | Service Bulletin | SB501-1478-3 | A | 11/21/2008 | To allow for wider tolerance motor. | 501-1478-01 | ||
| SA-341 | Service Bulletin | SB501-1478-5 | A | 5/1/1999 | To insure proper retention of servo- motor gear to motor shaft. Refer to SB501-1478-7. | 501-1478-01, 501-1478-03, 501-1478-04 | ||
| SA-341 | Service Bulletin | SB501-1478-6 | A | 2/1/1998 | Product improvement to reduce the effects of vibration | 501-1478-04 | ||
| SA-341 | Service Bulletin | SB501-1478-7 | Orig | 5/1/1999 | To strengthen shaft-gear joint. | 501-1478-01, 501-1478-03, 501-1478-04 | ||
| SA-341 | Service Bulletin | SB501-1478-8 | Orig | 10/1/2000 | To provide a revised method of retaining cover assembly screws. | 501-1478-02, 501-1478-03, 501-1478-04, 501-1478-05 | ||
| SA-341 | Service Bulletin | SB501-1478-4 | Orig | 3/1/1992 | To insure compatibility of threaded parts and prevent possible damage to internal mechanism. | 501-1478-01 | ||
| SA-341 | Service Letter | SL-231 | A | 2/25/2008 | Component Reliability | Notify customers of tracability concern | 501-1259-04, 501-1478-04, 501-1478-05, 501-1684-04, 501-1770-01, 501-1770-03, 501-1770-04, 501-1770-05 | |
| SA-340 | Service Letter | SL-246 | AU | 5/4/2022 | Component Replacement List | Component Replacement List | 3S2060DC168A2A, 501-1478-02, 501-1478-03 | |
| SA-350 | Component Maintenance Manual | TP-460 | 27-39-03 | Orig | 6/1/1992 | Component Maintenance Manual | Pub# TP-460 | 501-1483-02 |
| SA-350 | Component Maintenance Manual | TP-400 | 27-39-02 | 1 | 1/15/1987 | Maintenance Manual with IPL | Pub# TP-400 | 501-1483-01 |
| SA-350 | Service Bulletin | SB501-1483-3 | A | 12/3/2013 | SA-350B MOD 2 | SA-350B MOD 2 | 501-1483-02 | |
| SA-350 | Service Bulletin | SB501-1483-4 | B | 4/27/2016 | SA-350A & B MOD 3 | SA-350A & B MOD 3 | 501-1483-01, 501-1483-02 | |
| SA-350 | Service Bulletin | SB501-1483-1 | A | 5/1/1999 | To prevent A2-Q1 breakdown due to inductive kick from servo motor and improve fail warning system. | 501-1483-01 | ||
| SA-350 | Service Bulletin | SB501-1483-2 | A | 4/27/2016 | To insure proper retention of motor gear to shaft. | 501-1483-01, 501-1483-02 | ||
| SA-151 | Service Letter | SL-99 | A | 2/16/1998 | To provide specific policy concerning lubrication requirements of BFGAS. Servo Actuator products. | 501-1535-01 | ||
| SA-350 | Service Letter | SL-97 | B | 10/15/1987 | Cancellation of periodic scheduled maintenance for the SA-350A Servo Actuator. | |||
| DB-360 | Component Maintenance Manual | TP-466 | 27-30-05 | A C2 | 5/2/2016 | CMM with IPL | 501-1684, 501-1684-01, 501-1684-02, 501-1684-03, 501-1684-04, 501-1685, 501-1685-01, 501-1685-02, 501-1685-03, 501-1685-04, 501-1716, 501-1716-01, 501-1716-02, 501-1716-03, 501-1716-04 | |
| SA-360 | Service Bulletin | SB501-1684-2 | Orig | 5/1/1999 | To strengthen shaft-gear joint. | 501-1684-03, 501-1684-04 | ||
| SA-360 | Service Bulletin | SB501-1684-3 | Orig | 10/2/2000 | To provide an alternate method of retaining cover assembly screws. | 501-1684-03, 501-1684-04 | ||
| SA-360 | Service Bulletin | SB501-1684-4 | A | 11/2/2001 | Improve the dynamic operation by adding filter capacitors to prevent unwanted oscillations from A1U1, A1Q1, and A1Q2. | 501-1684-04 | ||
| SA-360 | Service Bulletin | SB501-1684-5 | Orig | 9/14/2004 | To improve reliability of Switch S1. | 501-1684-04 | ||
| SA-360 | Service Bulletin | SB501-1648-7 | A | 11/8/2012 | Inspect for out of tolerance part | 501-1684-04 | ||
| SA-360 | Service Bulletin | SB501-1684-6 | A | 5/12/2009 | Set Screw Replacement | 501-1864-03, 501-1864-04 | ||
| SA-360 | Service Bulletin | SB501-1684-1 | A | 5/21/1999 | Insure proper retention of pinion gear to DC Servo Motor shaft | Superseeded By MOD 2 see SB501-1684-2 | 501-1684-03 | |
| SA-360 | Service Bulletin | SB501-1684-7 | A | 11/8/2012 | Inspect for out of tolerance part | |||
| SA-341 | Service Letter | SL-231 | A | 2/25/2008 | Component Reliability | Notify customers of tracability concern | 501-1259-04, 501-1478-04, 501-1478-05, 501-1684-04, 501-1770-01, 501-1770-03, 501-1770-04, 501-1770-05 | |
| DB-380 | Component Maintenance Manual | TP-499 | 27-30-08 | B | 5/30/2018 | Component Maintenance Manual | Pub# TP-499 | 501-1770-01, 501-1770-02, 501-1771-01, 501-1771-02, 501-1772-01, 501-1772-02 |
| DB-380 | Component Maintenance Manual | TP-556 | 27-30-12 | C | 5/30/2018 | Component Maintenance Manual | Pub# TP-556 | 501-1770-05, 501-1771-05, 501-1772-05 |
| SA-380 | Service Bulletin | SB501-1770-2 | A | 7/21/2008 | Planning Information | CCA 542-2644 needs track replaced by jumper wire | 501-1770-( ), 501-1770-01, 501-1770-02, 501-1770-03, 501-1770-04, 501-1770-05 | |
| SA-380 | Service Bulletin | SB501-1770-3 | A | 5/6/2009 | To improve rigidity of clutch field anti-rotation stop | 501-1770-01, 501-1770-02, 501-1770-03, 501-1770-04, 501-1770-05 | ||
| SA-380 | Service Bulletin | SB501-1770-4 | A | 11/9/2012 | Inspect for out of tolerance part | 501-1770-01, 501-1770-03, 501-1770-04, 501-1770-05 | ||
| SA-380 | Service Bulletin | SB501-1770-1 | Orig | 10/1/2000 | To provide an alternate method of retaining cover assembly screws. | 501-1770-( ) | ||
| SA-340 | Service Letter | SL-246 | AU | 5/4/2022 | Component Replacement List | Component Replacement List | 3S2060DC168A2A, 501-1478-02, 501-1478-03 | |
| SA-341 | Service Letter | SL-231 | A | 2/25/2008 | Component Reliability | Notify customers of tracability concern | 501-1259-04, 501-1478-04, 501-1478-05, 501-1684-04, 501-1770-01, 501-1770-03, 501-1770-04, 501-1770-05 | |
| SA-401 | Component Maintenance Manual | TP-451 | 32-50-03 | A | 2/20/2019 | Component Maintenance Manual | Pub# TP-451 | 501-1662-01 |
| SA-401 | Service Bulletin | SB501-1662-1 | Orig | 1/31/1992 | To insure proper servo actuator operation when the servo is subjected to temperature extremes. | 501-1662-01 | ||
| SA-401 | Service Bulletin | SB501-1662-10 | Orig | 10/3/2000 | To improve output gear impact strength. | 501-1662-01 | ||
| SA-401 | Service Bulletin | SB501-1662-11 | A | 11/30/2006 | Provide replacement part for a device no longer procurable. | 501-1662-01 | ||
| SA-401 | Service Bulletin | SB501-1662-2 | Orig | 2/20/1992 | To provide rebias for high noise, reduction in friction levels and improve producibility. | 501-1662-01 | ||
| SA-401 | Service Bulletin | SB501-1662-3 | Orig | 3/20/1992 | To incorporate A1 Mod 3 replacing Servo Actuator CCA. | 501-1662-01 | ||
| SA-401 | Service Bulletin | SB501-1662-4 | Orig | 3/20/1992 | To incorporate Mod 4, replacing actuator assembly B1 motor. | 501-1662-01 | ||
| SA-401 | Service Bulletin | SB501-1662-5 | Orig | 3/4/1993 | To insure proper connector bracket retention. | 501-1662-01 | ||
| SA-401 | Service Bulletin | SB501-1662-6 | Orig | 3/4/1993 | To insure that maximum output torque level can be maintained. | 501-1662-01 | ||
| SA-401 | Service Bulletin | SB501-1662-7 | Orig | 1/26/1995 | To improve the reliability of terminal block solder joints on filter circuit card assembly A1A2. | 501-1662-01 | ||
| SA-401 | Service Bulletin | SB501-1662-8 | A | 11/30/2006 | To provide replacement part for part no longer available. | 501-1662-01 | ||
| SA-401 | Service Bulletin | SB501-1662-9 | Orig | 5/1/2000 | Improve axial stability of gear. . | 501-1662-01 | ||
| SA-151 | Service Letter | SL-99 | A | 2/16/1998 | To provide specific policy concerning lubrication requirements of BFGAS. Servo Actuator products. | 501-1535-01 | ||
| SA-401 | Service Letter | SIL-001-SA-401A | 00 | 10/11/2021 | SA-401A - End of Manufacturing Notice | SA-401A - End of Manufacturing Notice | 501-1662-01 | |
| SA-460 | Component Maintenance Manual | TP-467 | 32-50-04 | A | 6/27/2018 | Component Maintenance Manual | Pub# TP-467 | 501-1711-02 |
| SA-460 | Service Bulletin | SB501-1711-1 | Orig | 1/1/1993 | To eliminate possible shorting between heat sink and circuit card tracks. | 501-1711-02 | ||
| SA-460 | Service Bulletin | SB501-1711-2 | Orig | 7/1/1994 | To compensate for changes in P-channel transistors. | 501-1711-02 | ||
| SA-460 | Service Bulletin | SB501-1711-3 | Orig | 7/1/1996 | This modification will prevent possible interference between Torque Control Circuit Card Assembly (mounted on brackets being replaced) and motor housing. | 501-1711-02 | ||
| SA-460 | Service Bulletin | SB501-1711-4 | Orig | 4/1/1998 | To provide replacement part for part no longer available. | 501-1711-02 | ||
| SA-460 | Service Bulletin | SB501-1711-5 | Orig | 5/1/2000 | Improve axial stability of gear. | 501-1711-02 | ||
| SA-460 | Service Bulletin | SB501-1711-6 | Orig | 10/1/2000 | To improve output gear impact strength. | 501-1700-02 | ||
| SA-460 | Service Bulletin | SB501-1711-7 | Orig | 10/16/2001 | Provide replacement part for a device no longer procurable. | 501-1711-02 | ||
| SA-460 | Service Bulletin | SB501-1711-8 | Orig | 5/1/2001 | Provide replacement part for a device no longer procurable. | 501-1711-02 | ||
| SA-460 | Service Bulletin | SB501-1708-6 | Orig | 5/1/2001 | Eliminate possibility of crystal oscillator shorting to via hole, or damaging solder mask. | 501-1708-02, 501-1708-03 | ||
| SA-151 | Service Letter | SL-99 | A | 2/16/1998 | To provide specific policy concerning lubrication requirements of BFGAS. Servo Actuator products. | 501-1535-01 | ||
| SA-460 | Service Letter | SIL-001-SA-460B | 00 | 10/11/2021 | SA-460B - End of Manufacturing Notice | SA-460B - End of Manufacturing Notice | 501-1711-02 | |
| SA-151 | Service Letter | SL-99 | A | 2/16/1998 | To provide specific policy concerning lubrication requirements of BFGAS. Servo Actuator products. | 501-1535-01 | ||
| SA-500 | Service Letter | SL-95 | 1 | 10/25/1988 | To provide information concerning the inspection and overhaul intervals for servo actuators. | |||
| 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-( ) | |
| DB-600 | Component Maintenance Manual | TP-323 | 27-39-01 | E C5 | 10/28/2016 | Component Maintenance Manual | Pub# TP-323 | 501-1247-03, 501-1247-04, 501-1247-05, 501-1258-01, 501-1259-03, 501-1259-04, 501-1259-05 |
| SA-600 | Service Bulletin | SB501-1259-1 | Orig | 10/1/1979 | To prevent possible interference between R1 and Q4. | 501-1259-01 | ||
| SA-600 | Service Bulletin | SB501-1259-10 | Orig | 8/1/1997 | Product improvement to quiet and remove wear of bronze bearing. | 501-1259-( ) | ||
| SA-600 | Service Bulletin | SB501-1259-11 | Orig | 7/1/1997 | Product improvement to eliminate possibility of slip clutch failures. | 501-1259-( ) | ||
| SA-600 | Service Bulletin | SB501-1259-12 | Orig | 12/1/2000 | To change screw retention system. | 501-1259-04 | ||
| SA-600 | Service Bulletin | SB501-1259-2 | Orig | 4/1/1985 | To ensure proper fail lamp operation with revised pilot/copilot release logic. | 501-1259-03 | ||
| SA-600 | Service Bulletin | SB501-1259-3 | A | 7/1/1981 | To ensure that actuator rotor and shaft assembly setscrews are secure. | 501-1259-03, 501-1259-04 | ||
| SA-600 | Service Bulletin | SB501-1259-4 | Orig | 5/1/1982 | To reduce interference between clutch L1 rotor and field. | 501-1259-01, 501-1259-02, 501-1259-03 | ||
| SA-600 | Service Bulletin | SB501-1259-5 | A | 4/1/1985 | To ensure proper fail lamp operation with the use of a transistor with improved leakage characteristics. | 501-1259-03, 501-1259-04 | ||
| SA-600 | Service Bulletin | SB501-1259-6 | A | 4/1/1985 | To provide a more constant output torque on the servo actuator. | 501-1259-03, 501-1259-04 | ||
| SA-600 | Service Bulletin | SB501-1259-7 | A | 4/1/1985 | To prevent erroneous fail light indication. | 501-1259-03, 501-1259-04 | ||
| SA-600 | Service Bulletin | SB501-1259-8 | A | 4/1/1987 | To remove internal G-switch and re-identify the SA-600C (P/N 501-1259-03) to SA-600D (P/N 501-1259-04). | 501-1259-03 | ||
| SA-600 | Service Bulletin | SB501-1259-9 | A | 8/1/1991 | Replacement of Spur Gear to compensate for tolerance shifts resulting in inability to set slip clutch torque. | 501-1259-03, 501-1259-04, 501-1259-05 | ||
| SA-341 | Service Letter | SL-231 | A | 2/25/2008 | Component Reliability | Notify customers of tracability concern | 501-1259-04, 501-1478-04, 501-1478-05, 501-1684-04, 501-1770-01, 501-1770-03, 501-1770-04, 501-1770-05 | |
| SC-400 | Component Maintenance Manual | TP-207 | C1 | 12/1/1970 | Instruction Manual | Pub# TP-207 | 201-1001-001 | |
| SC-400 | Service Bulletin | SB201-1001-1 | Orig | 3/1/1970 | To provide for the selection of the parallel tuned circuit for proper voltage regulation and insure proper short circuit protection. | |||
| SC-400 | Service Bulletin | SB201-1001-2 | A | 11/1/1978 | To provide for proper transistor life. | |||
| SC-841 | Component Maintenance Manual | TP-353 | 24-30-01 | A | 3/12/2018 | Maintenance Manual with IPL | Pub# TP-353 | 501-1318-01 |
| SC-841 | Installation Manual | TP-351 | A | 4/5/2007 | Installation Instructions | Pub# TP-351 | 501-1318-01 | |
| SC-841 | Service Bulletin | SB501-1318-1 | Orig | 12/1/1982 | To modify connector A1J1 mounting to insure positive contact. | 501-1318-01 | ||
| SC-841 | Service Bulletin | SB501-1318-2 | A | 9/1/1987 | To eliminate op amp oscillation and insure proper short circuit current limiting operation. | 501-1318-01 | ||
| SC-841 | Service Bulletin | SB501-1318-3 | Orig | 9/1/1987 | To eliminate op amp oscillation and ensure conduction angle dead band w/resistor tolerance buildup. | 501-1318-01 | ||
| SC-841 | Service Bulletin | SB501-1318-4 | A | 3/30/1992 | To improve current limit circuit signal flow. | 50-1318-01 | ||
| SC-841 | Service Bulletin | SB501-1318-5 | A | 3/31/1992 | To insure proper starting and prevent possible damage under loaded conditions. | 501-1318-01 | ||
| SC-841 | Service Bulletin | SB501-1318-6 | Orig | 4/28/1998 | to insure proper current limit circuit operation while under short circuit conditions. | 501-1318-01 | ||
| SC-841 | Service Bulletin | SB501-1318-7 | A | 10/18/2021 | To reduce susceptiability of insulation breakdown to case. | Service Bulletin | 501-1318-01 | |
| SC-841 | Service Letter | SL-69 | Orig | 5/20/1983 | To provide information allowing wider tolerance at No Load, and Low Input Voltage. | |||
| SCD526 | Installation Manual | 009-10084-001 | Orig | 9/16/1994 | Instruction Manual | Pub# 009-10084-001 | 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 | |
| HSI-3000 | Installation Manual | TP-600 | C | 8/2/2011 | Installation and Operation Manual | Pub# TP-600 | 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 | SB501-1899-3 | A | 3/15/2006 | To correct knob action at start up. | 501-1899-01 | ||
| 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 | 6/25/2009 | To provide replacement display due to diminishing source. | To provide replacement display due to diminishing source. | 501-1899-01 | |
| HSI-3000 | Service Bulletin | SB501-1899-6 | 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 | 6/26/2009 | To provide replacement display due to diminishing source. | To provide replacement display due to diminishing source. | 501-1899-01 | |
| SI-100 | Component Maintenance Manual | TP-338 | 24-20-02 | 2 | 7/31/1993 | Maintenance Manual with IPL | TP-338 | 501-1206-01, 501-1330-01 |
| SI-100 | Component Maintenance Manual | TP-392 | 24-20-10 | 2 | 4/30/1991 | Maintenance Manual with IPL | Pub# TP-392 | 501-1205-01, 501-1205-02, 501-1475-01 |
| SI-100 | Component Maintenance Manual | TP-360 | 24-30-03 | 3 | 10/22/1987 | Maintenance Manual with IPL | Pub# TP-360 | 501-1240-01, 501-1240-02 |
| SI-100 | Installation Manual | TP-346 | A | 4/13/2007 | Installation Instructions | Pub# TP-346 | 501-1240-01, 501-1240-02 | |
| SI-100 | Installation Manual | TP-540 | F | 7/22/2014 | Installation and Operation Manual | Updated to include Inverters previously listed as ITAR and are now EAR | 501-1128- ( ), 501-1148-01, 501-1148-02, 501-1167-01, 501-1167-02, 501-1205-01, 501-1205-02, 501-1206-01, 501-1235-01, 501-1249-01, 501-1265-01, 501-1329-01, 501-1330-01, 501-1475-01, 501-1666-01, 501-1666-02, 501-1724-01 | |
| ESI-1000 | Installation Manual | 0040-32001-01 | U | 10/13/2017 | ESI-1000 Installation Manual | Pub# 0040-32001-01 | 9200-32000-0101 | |
| 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 | ||
| SI-100 | Service Bulletin | SB501-1205-1 | Orig | 3/1/1985 | To provide over voltage adjustment. | To provide over voltage adjustment. | 501-1205-01 | |
| SI-100 | Service Bulletin | SB501-1205-2 | Orig | 3/1/1985 | To insure integrity of circuit card connector interface by staking and soldering connector pins. | To insure integrity of circuit card connector interface by staking and soldering connector pins. | 501-1205-01 | |
| SI-100 | Service Bulletin | SB501-1205-3 | Orig | 3/1/1985 | To provide warning light indication under all shut down conditions. | To provide warning light indication under all shut down conditions. | 501-1205-01 | |
| SI-100 | Service Bulletin | SB501-1205-5 | Orig | 10/1/1989 | To improve frequency stability during stand alone operation. | To improve frequency stability during stand alone operation. | 501-1205-01, 501-1205-02, 501-1475-01 | |
| ESI-1000 | Service Bulletin | SB9200-32000-1 | A | 5/3/2010 | Revise night lighting color from blue to white | 9200-32000-0301, 9200-32000-0401 | ||
| ESI-1000 | Service Bulletin | SB9200-32100-2 | A | 4/4/2011 | Incorporation of Mod B | 9200-32100-0101, 9200-32100-0201, 9200-32100-1001 | ||
| ESI-1000 | Service Bulletin | SB9200-32000-2 | B | 8/6/2012 | Incorporation of Mod 2 | 9200-32000-0101, 9200-32000-0201, 9200-32000-0301, 9200-32000-0401 | ||
| ESI-1000 | Service Bulletin | SB9200-32100-1 | A | 12/22/2010 | LED Backlight is obsolete | 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 | 9200-32000-0301, 9200-32000-0401, 9200-32000-0701, 9200-32000-0801 | ||
| 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 | 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 | 9200-32100-0101, 9200-32100-0201, 9200-32100-1001 | ||
| ESI-1000 | Service Bulletin | SB9200-32000-5 | A | 8/23/2012 | Improve backlight low end brightness characteristics | 9200-32000-0101, 9200-32000-0201, 9200-32000-0301, 9200-32000-0401, 9200-32000-0701, 9200-32000-0801 | ||
| 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 | 9200-32100-0201 | |
| 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) | 9200-32100-1001 | |
| 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 | 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 | 9200-32100-0101, 9200-32100-0201, 9200-32100-1001, 9200-32100-3203 | |
| SI-100 | Service Bulletin | SB501-1205-4 | Orig | 5/1/1989 | To improve frequency stability during stand alone operation. | To improve frequency stability during stand alone operation. | 501-1205-01 | |
| SI-100 | Service Bulletin | SB501-1240-1 | A | 7/1/1985 | To improve AC output characteristics over full input voltage range. | 501-1240-01, 501-1240-02 | ||
| SI-100 | Service Bulletin | SB501-1240-2 | Orig | 7/1/1984 | To insure proper output levels when starting under full load. | 501-1240-01, 501-1240-02 | ||
| SI-100 | Service Bulletin | SB501-1240-3 | A | 12/1/1986 | To prevent improper assembly from causing an inadvertent short of 115 Vac to case. | 501-1240-01, 501-1240-02 | ||
| SI-100 | Service Bulletin | SB501-1240-4 | Orig | 5/1/1985 | To prevent possible fracturing of capacitor leads. | 501-1240-01, 501-1240-02 | ||
| SI-100 | Service Bulletin | SB501-1240-5 | Orig | 12/1/1986 | To insure isolation of the 115 Vac output interconnects. | 501-1240-01, 501-1240-02 | ||
| SI-100 | Service Bulletin | SB501-1475-4 | Orig | 3/1/1992 | To replace wet tantalum capacitors with solid tantalum capacitors. | 501-1475-01 | ||
| SI-100 | Service Bulletin | SB501-1475-2 | 3/1/1992 | To improve frequency stability when the inverter is used as a stand alone. | To improve frequency stability when the inverter is used as a stand alone. | 501-1475-01 | ||
| SI-100 | Service Bulletin | SB501-1475-3 | Orig | 3/1/1992 | To insure proper auxiliary power supply operation under parallel inverter and remote turn-off conditions. | To insure proper auxiliary power supply operation under parallel inverter and remote turn-off conditions. | 501-1475-01 | |
| SI-100 | Service Bulletin | SB501-1475-1 | Orig | 5/1/1989 | To improve frequency stability during "stand alone" operation. | 501-1475-01 | ||
| SI-100 | Service Letter | SL-91 | Orig | 8/19/1985 | To disseminate information concerning the selection of the proper transistors when replacement of the output transistors is necessary. | |||
| SI-100 | Service Letter | SL-90 | Orig | 8/9/1985 | To provide information concerning failure of power transistors during short circuit conditions. | |||
| PB-1002 | Service Letter | SL-21 | F | 9/21/1987 | To provide information when installing BFG Static Inverters, Phase Lock Boxes and Parallel Systems in various aircraft. | |||
| 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 | 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 | Supplemental Type Certificate | SA02738CH | 2/15/2022 | ESI-1000 and ESI-2000 - Permission to Use AML STC | ESI-1000 and ESI-2000 | |||
| SI-100 | Component Maintenance Manual | TP-392 | 24-20-10 | 2 | 4/30/1991 | Maintenance Manual with IPL | Pub# TP-392 | 501-1205-01, 501-1205-02, 501-1475-01 |
| SI-100 | Component Maintenance Manual | TP-338 | 24-20-02 | 2 | 7/31/1993 | Maintenance Manual with IPL | TP-338 | 501-1206-01, 501-1330-01 |
| SI-100 | Installation Manual | TP-540 | F | 7/22/2014 | Installation and Operation Manual | Updated to include Inverters previously listed as ITAR and are now EAR | 501-1128- ( ), 501-1148-01, 501-1148-02, 501-1167-01, 501-1167-02, 501-1205-01, 501-1205-02, 501-1206-01, 501-1235-01, 501-1249-01, 501-1265-01, 501-1329-01, 501-1330-01, 501-1475-01, 501-1666-01, 501-1666-02, 501-1724-01 | |
| ESI-1000 | Installation Manual | 0040-32001-01 | U | 10/13/2017 | ESI-1000 Installation Manual | Pub# 0040-32001-01 | 9200-32000-0101 | |
| 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 | ||
| SI-100 | Service Bulletin | SB501-1205-5 | Orig | 10/1/1989 | To improve frequency stability during stand alone operation. | To improve frequency stability during stand alone operation. | 501-1205-01, 501-1205-02, 501-1475-01 | |
| SI-100 | Service Bulletin | SB501-1205-3 | Orig | 3/1/1985 | To provide warning light indication under all shut down conditions. | To provide warning light indication under all shut down conditions. | 501-1205-01 | |
| SI-100 | Service Bulletin | SB501-1205-2 | Orig | 3/1/1985 | To insure integrity of circuit card connector interface by staking and soldering connector pins. | To insure integrity of circuit card connector interface by staking and soldering connector pins. | 501-1205-01 | |
| SI-100 | Service Bulletin | SB501-1205-1 | Orig | 3/1/1985 | To provide over voltage adjustment. | To provide over voltage adjustment. | 501-1205-01 | |
| ESI-1000 | Service Bulletin | SB9200-32000-5 | A | 8/23/2012 | Improve backlight low end brightness characteristics | 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 | 9200-32100-0101, 9200-32100-0201, 9200-32100-1001 | ||
| ESI-1000 | Service Bulletin | SB9200-32000-4 | A | 4/9/2012 | Replace obsolete LED Backlight assembly | 9200-32000-0101, 9200-32000-0201, 9200-32000-0301, 9200-32000-0401, 9200-32000-0701, 9200-32000-0801 | ||
| 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 | SB9200-32000-6 | A | 12/17/2012 | Incorporation of 1.1 Software | 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 | 9200-32100-0101, 9200-32100-0201, 9200-32100-1001 | ||
| ESI-1000 | Service Bulletin | SB9200-32000-2 | B | 8/6/2012 | Incorporation of Mod 2 | 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 | 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 | 9200-32000-0301, 9200-32000-0401 | ||
| ESI-1000 | Service Bulletin | SB9200-32000-7 | A |