# British Aerospace BAE 146 SERIES 200A

- Type: Aircraft model (FAA registry)
- Registry code: 1500266
- Manufacturer (registry): BRITISH AEROSPACE
- Model: BAE 146 SERIES 200A
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 4 · Turbo-fan
- Seats: 109
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Data sheet: [TCDS A49EU](https://openairdocs.org/tcds/A49EU) (OpenAirDocs)
- Holder: BAE Systems (Operations) Limited
- Registered aircraft: 8
- Page: https://openairdocs.org/model/british-aerospace-bae-146-series-200a

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2010-09-11 R1](https://openairdocs.org/ad/2010-09-11-R1): Wings · BAE Systems BAe 146-100A, BAe 146-200A, BAe 146-300A and 3 more. Effective Aug 5, 2025
- [AD 2024-17-06](https://openairdocs.org/ad/2024-17-06): Fuselage · BAE Systems BAe 146-100A, BAe 146-200A, BAe 146-300A and 3 more. Effective Nov 4, 2024
- [AD 2024-06-10](https://openairdocs.org/ad/2024-06-10): Landing gear · BAE Systems BAe 146-100A, BAe 146-300A, BAe 146-200A and 3 more. Effective May 22, 2024
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2023-02-10](https://openairdocs.org/ad/2023-02-10): Fuselage · BAE Systems BAe 146-100A, BAe 146-200A, BAe 146-300A and 3 more. Effective Mar 17, 2023
- [AD 2022-23-07](https://openairdocs.org/ad/2022-23-07): Auto-Flight · BAE Systems BAe 146-100A, BAe 146-200A and BAe 146-300A. Effective Jan 4, 2023
- [AD 2022-14-13](https://openairdocs.org/ad/2022-14-13): Fuselage · BAE Systems BAe 146-100A, BAe 146-200A, BAe 146-300A and 3 more. Effective Aug 25, 2022
- [AD 2022-06-14](https://openairdocs.org/ad/2022-06-14): Time Limits/Maintenance Checks · BAE Systems BAe 146-100A, BAe 146-200A, BAe 146-300A and 3 more. Effective May 19, 2022
- [AD 2021-10-27](https://openairdocs.org/ad/2021-10-27): Lights · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Jun 17, 2021
- [AD 2018-23-12](https://openairdocs.org/ad/2018-23-12): Equipment/furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 180 more. Effective Dec 28, 2018
- [AD 2017-04-04](https://openairdocs.org/ad/2017-04-04): Air Conditioning · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Mar 29, 2017
- [AD 2016-16-11](https://openairdocs.org/ad/2016-16-11): Wings · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Sep 16, 2016
- [AD 2016-07-06](https://openairdocs.org/ad/2016-07-06): Time Limits/Maintenance Checks · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective May 5, 2016
- [AD 2014-16-18](https://openairdocs.org/ad/2014-16-18): Landing Gear · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Oct 2, 2014
- [AD 2014-01-04](https://openairdocs.org/ad/2014-01-04): Fire protection · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Mar 14, 2014
- [AD 2013-22-08](https://openairdocs.org/ad/2013-22-08): Wings · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Dec 5, 2013
- [AD 2013-04-13](https://openairdocs.org/ad/2013-04-13): Electrical Power · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Apr 11, 2013
- [AD 2013-02-09](https://openairdocs.org/ad/2013-02-09): Ice and rain protection · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Mar 8, 2013
- [AD 2012-21-16](https://openairdocs.org/ad/2012-21-16): Hydraulic power · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Dec 5, 2012
- [AD 2012-12-22](https://openairdocs.org/ad/2012-12-22): Fuselage · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Jul 30, 2012
- [AD 2012-12-13](https://openairdocs.org/ad/2012-12-13): Fire Protection · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Jul 30, 2012
- [AD 2011-20-02](https://openairdocs.org/ad/2011-20-02): Landing gear · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Oct 28, 2011
- [AD 2011-11-06](https://openairdocs.org/ad/2011-11-06): Landing Gear · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Jul 6, 2011
- [AD 2011-08-11](https://openairdocs.org/ad/2011-08-11): Fuselage · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective May 26, 2011
- [AD 2010-21-10](https://openairdocs.org/ad/2010-21-10): Wings · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Nov 18, 2010
- [AD 2010-18-10](https://openairdocs.org/ad/2010-18-10): Flight controls · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Oct 7, 2010
- [AD 2010-16-10](https://openairdocs.org/ad/2010-16-10): Wings · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Sep 17, 2010
- [AD 2010-16-09](https://openairdocs.org/ad/2010-16-09): Flight Controls · BAE Systems BAe 146-100A and BAe 146-200A. Effective Sep 17, 2010
- [AD 2010-02-11](https://openairdocs.org/ad/2010-02-11): Fuselage · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Mar 4, 2010
- [AD 2009-17-03](https://openairdocs.org/ad/2009-17-03): Fuselage · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Sep 22, 2009
- [AD 2009-15-19](https://openairdocs.org/ad/2009-15-19): Stabilizers · BAE Systems BAe 146-100A and BAe 146-200A. Effective Sep 2, 2009
- [AD 2009-15-08](https://openairdocs.org/ad/2009-15-08): Fuselage. · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Aug 25, 2009
- [AD 2009-12-10](https://openairdocs.org/ad/2009-12-10): Fuselage · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Jul 24, 2009
- [AD 2009-02-09](https://openairdocs.org/ad/2009-02-09): Aft wing links · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Apr 2, 2009
- [AD 2008-23-14](https://openairdocs.org/ad/2008-23-14): Bolts · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Dec 26, 2008
- [AD 2008-10-05](https://openairdocs.org/ad/2008-10-05): Leading edge high lift devices. · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Jun 10, 2008
- [AD 2008-06-08](https://openairdocs.org/ad/2008-06-08): Centre fuselage top aft longeron · BAE Systems BAe 146-100A, BAe 146-200A and BAe 146-300A. Effective Apr 16, 2008
- [AD 2008-04-16](https://openairdocs.org/ad/2008-04-16): APU (auxiliary power unit) · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Apr 3, 2008
- [AD 2007-26-18](https://openairdocs.org/ad/2007-26-18): Accumulator cylinder · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Feb 11, 2008
- [AD 2007-13-06](https://openairdocs.org/ad/2007-13-06): Flight deck side consoles · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Jul 25, 2007
- [AD 2007-04-04](https://openairdocs.org/ad/2007-04-04): Wing top skin under the rib 0 joint strap · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Mar 21, 2007
- [AD 2007-01-01](https://openairdocs.org/ad/2007-01-01): Lift spoiler actuators/jacks · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Feb 13, 2007
- [AD 2006-25-10](https://openairdocs.org/ad/2006-25-10): Lift spoiler jack · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Jan 16, 2007
- [AD 2006-23-16](https://openairdocs.org/ad/2006-23-16): Nose wheel assembly · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Dec 21, 2006
- [AD 2006-23-13](https://openairdocs.org/ad/2006-23-13): Three-phase circuit breaker panels · BAE Systems BAe 146-100A, BAe 146-200A and BAe 146-300A. Effective Dec 18, 2006
- [AD 2006-23-12](https://openairdocs.org/ad/2006-23-12): Hydraulic accumulators · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Dec 18, 2006
- [AD 2006-20-05](https://openairdocs.org/ad/2006-20-05): Inspect chafing in skin of wing-to-fuselage fairing · BAE Systems BAe 146-100A, BAe 146-200A and BAe 146-300A. Effective Nov 2, 2006
- [AD 2006-11-08](https://openairdocs.org/ad/2006-11-08): Flap structure and machined ribs · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Jun 29, 2006
- [AD 2006-10-12](https://openairdocs.org/ad/2006-10-12): Elevator servo tab bearings · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Jun 21, 2006

Historical (superseded or no longer in force):

- [AD 2022-25-18](https://openairdocs.org/ad/2022-25-18) (historical): Landing gear · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Dec 27, 2022
- [AD 2017-12-08](https://openairdocs.org/ad/2017-12-08) (historical): Periodic Inspections · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Jul 20, 2017
- [AD 2015-07-05](https://openairdocs.org/ad/2015-07-05) (historical): Fuselage · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective May 19, 2015
- [AD 2012-16-08](https://openairdocs.org/ad/2012-16-08) (historical): Air Conditioning · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Sep 18, 2012
- [AD 2011-24-06](https://openairdocs.org/ad/2011-24-06) (historical): Fatigue cracking · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Jan 3, 2012
- [AD 2010-10-22](https://openairdocs.org/ad/2010-10-22) (historical): Fuel system · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Jun 25, 2010
- [AD 2010-10-13](https://openairdocs.org/ad/2010-10-13) (historical): Wings · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Jun 21, 2010
- [AD 2010-09-11](https://openairdocs.org/ad/2010-09-11) (historical): Wings · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Jun 8, 2010
- [AD 2006-12-09](https://openairdocs.org/ad/2006-12-09) (historical): Inner webs and flanges at frames 15, 18, 41, and 43 · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Jul 17, 2006
- [AD 2005-23-12](https://openairdocs.org/ad/2005-23-12) (historical): Airworthiness Limitations Section (ALS) · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Dec 27, 2005
- [AD 2005-13-19](https://openairdocs.org/ad/2005-13-19) (historical): Forward fuselage skin · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Aug 2, 2005
- [AD 2005-06-14](https://openairdocs.org/ad/2005-06-14) (historical): Main landing gear (MLG) · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective May 2, 2005
- [AD 2002-03-10](https://openairdocs.org/ad/2002-03-10) (historical): Oleo Strut · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Mar 21, 2002
- [AD 2000-26-07](https://openairdocs.org/ad/2000-26-07) (historical): Ensure Continued Structural Integrity · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Feb 7, 2001
- [AD 99-25-11](https://openairdocs.org/ad/99-25-11) (historical): Retraction Attachment Boss · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Feb 1, 2000
- [AD 99-17-12](https://openairdocs.org/ad/99-17-12) (historical): Side Stays of MLG · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Sep 27, 1999
- [AD 98-21-06](https://openairdocs.org/ad/98-21-06) (historical): Fuselage Skin · BAE Systems BAe 146-100A, BAe 146-200A and BAe 146-300A. Effective Nov 10, 1998
- [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996
- [AD 96-14-09](https://openairdocs.org/ad/96-14-09) (historical): Ice Protection Switches · BAE Systems BAe 146-100A, BAe 146-200A and BAe 146-300A. Effective Jul 22, 1996
- [AD 93-01-11](https://openairdocs.org/ad/93-01-11) (historical): Wing Structural Integrity · BAE Systems BAe 146-100A, BAe 146-200A and BAe 146-300A. Effective Mar 2, 1993

All 175: https://openairdocs.org/model/british-aerospace-bae-146-series-200a/ads.md

## Information bulletins (advisory) (3)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [SAIB NM-08-43](https://openairdocs.org/saib/NM-08-43): Cabin Equipment/Furnishings - Seats. Issued Sep 3, 2008
- [SAIB NM-06-57](https://openairdocs.org/saib/NM-06-57): Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.. Issued Jul 27, 2006

## Registered aircraft (8)

- [N470NA](https://openairdocs.org/aircraft/N470NA): [Neptune Aviation Services Inc](https://openairdocs.org/faa-owner/NEPTUNE%20AVIATION%20SERVICES%20INC), [Missoula, MT](https://openairdocs.org/faa-place/MT/Missoula), built 1986, S/N E2049
- [N472NA](https://openairdocs.org/aircraft/N472NA): [Neptune Aviation Services Inc](https://openairdocs.org/faa-owner/NEPTUNE%20AVIATION%20SERVICES%20INC), [Missoula, MT](https://openairdocs.org/faa-place/MT/Missoula), built 1989, S/N E2138
- [N473NA](https://openairdocs.org/aircraft/N473NA): [Neptune Aviation Services Inc](https://openairdocs.org/faa-owner/NEPTUNE%20AVIATION%20SERVICES%20INC), [Missoula, MT](https://openairdocs.org/faa-place/MT/Missoula), built 1985, S/N E2045
- [N474NA](https://openairdocs.org/aircraft/N474NA): [Neptune Aviation Services Inc](https://openairdocs.org/faa-owner/NEPTUNE%20AVIATION%20SERVICES%20INC), [Missoula, MT](https://openairdocs.org/faa-place/MT/Missoula), S/N E2084
- [N477NA](https://openairdocs.org/aircraft/N477NA): [Neptune Aviation Services](https://openairdocs.org/faa-owner/NEPTUNE%20AVIATION%20SERVICES), [Missoula, MT](https://openairdocs.org/faa-place/MT/Missoula), built 1988, S/N E2103
- [N478NA](https://openairdocs.org/aircraft/N478NA): [Neptune Aviation Services Inc](https://openairdocs.org/faa-owner/NEPTUNE%20AVIATION%20SERVICES%20INC), [Missoula, MT](https://openairdocs.org/faa-place/MT/Missoula), built 1987, S/N E2074
- [N907AS](https://openairdocs.org/aircraft/N907AS): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 1989, S/N E2156
- [N908AS](https://openairdocs.org/aircraft/N908AS): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), S/N E2082

## NTSB investigations (3)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ENG24LA012](https://openairdocs.org/ntsb/ENG24LA012), Mar 1, 2024: British Aerospace BAE 146 Series 200A (N474NA), Missoula, MT, incident, minor damage. Probable cause: The use of a new long term fire retardant with a chemical composition incompatible with the retardant previously in use for the integration-operational field evaluation without adequate testing and…
- [NTSB CHI00IA037](https://openairdocs.org/ntsb/CHI00IA037), Dec 1, 1999: British Aerospace BAE 146-200A (N606AW), Chicago, IL, incident, minor damage. Probable cause: An undetermined failure in the hydraulic system, which resulted in the airplane's entire braking system becoming temporarily inoperative. A factor associated with the incident was the airport…
- [NTSB FTW97LA070](https://openairdocs.org/ntsb/FTW97LA070), Dec 21, 1996: British Aerospace BAE 146-200A (N606AW), Denver, CO, no damage. Probable cause: an inflight encounter with unreported and unanticipated clear air turbulence during landing descent.

## FAA accident and incident reports (31)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19990219015449I](https://openairdocs.org/incident/19990219015449I), Feb 19, 1999: Bag BAE146200A (N292UE), Peoria, IL. (-5)At approximately 800 feet, on departure from runway 31, at Peoria Illinois airport (pia), February 19, 1999, air Wisconsin airlines d.b.a. united express,…
- [Incident 19980707030599I](https://openairdocs.org/incident/19980707030599I), Jul 7, 1998: Bag BAE146200A (N292UE), Rapid City, SD. Fire damaged suitcase was recovered from class d cargo compartment. Following scheduled flight. Suitcase contained tightly-packed clothing and a 3 peice baby…
- [Incident 19980311007009I](https://openairdocs.org/incident/19980311007009I), Mar 11, 1998: Bag BAE146200A (N607AW), Aspen, CO, Minor damage. Narrative: on March 11, 1998 at 1552 hrs local, a BAE-146-200 operated by air Wisconsin airlines ran off the runway at Aspen, Colorado. The aircraft (N607AW)…
- [Incident 19971203043829I](https://openairdocs.org/incident/19971203043829I), Dec 3, 1997: Bag BAE146200A (N183US), Appleton, WI. Narrative: the no. 3 turbine blade failed during cruise. Inspection of the failed component is not completed at this time.
- [Incident 19971203043379I](https://openairdocs.org/incident/19971203043379I), Dec 3, 1997: Bag BAE146200A (N181US), Lincoln, NE. Narrative: on Wednesday, December 3, 1997, N181US, a british aerospace, BAE-146-200A, operated by air Wisconsin airline as flight 601, experienced an…
- [Accident 19961220047279A](https://openairdocs.org/incident/19961220047279A), Dec 20, 1996: N606AW, Denver, CO, No damage. (-16) Two flight attendants injured due to in-flight turbulence.
- [Incident 19961207041789I](https://openairdocs.org/incident/19961207041789I), Dec 7, 1996: Bag BAE146200A (N179US), Springfield, MO. On climbout low oil pressure NR3 engine. Shutdown. Returned sgf. Unable cause. Ferried. Clogged line. Worn gearbox.
- [Incident 19940802047679I](https://openairdocs.org/incident/19940802047679I), Aug 2, 1994: Bag BAE146200A (N606AW), Milwaukee, WI. Fire light NR2 engine on climbout. Used bottles. Returned. Engine fire caused by cracked fuel manifold.
- [Incident 19940204006869I](https://openairdocs.org/incident/19940204006869I), Feb 4, 1994: Bag BAE146200A (N606AW), Rifle, CO, Minor damage. Narrative: after landing at Rifle, Colorado, the aircraft ran off the west end of the runway. Two (2) pilot reports, approximately one (1) hour prior to…
- [Incident 19940106001329I](https://openairdocs.org/incident/19940106001329I), Jan 6, 1994: Bag BAE146200A (N606AW), Aspen, CO, Minor damage. Narrative: the flight was normal until touchdown. Shortly after the nose wheels were on the ground the aircraft began moving to the right of runway centerline.…
- [Incident 19920820037369I](https://openairdocs.org/incident/19920820037369I), Aug 20, 1992: Bag BAE146200A (N607AW), Chicago, IL. Fumes in cabin while taxiing for takeoff. Found a cracked hydraulic pressure supply line.
- [Incident 19920131017489I](https://openairdocs.org/incident/19920131017489I), Jan 31, 1992: Bag BAE146200A (N294UE), Bellingham, WA. Aborted takeoff due to difference between airspeed indicators. Departed end of runway onto grass area.
- [Incident 19920106001959I](https://openairdocs.org/incident/19920106001959I), Jan 6, 1992: Bag BAE146200A (N290UE), Reno, NV. NR1 engine oil pressure fluctuating en route. Shut down before landing. Found oil pump had failed.
- [Incident 19911018056609I](https://openairdocs.org/incident/19911018056609I), Oct 18, 1991: Bag BAE146200A (N606AW), Fort Wayne, IN, Minor damage. NR2 engine fire warning. Fired bottle. Diverted and landed. Turbine failed,tailpipe separated from engine.
- [Incident 19910130010869I](https://openairdocs.org/incident/19910130010869I), Jan 30, 1991: Bac 146200A (N295UE), Fresno, CA. NR3 engine vibration and automatic shutdown. Diverted and landed. Reduction gear carrier assembly failed.
- [Incident 19900928059069I](https://openairdocs.org/incident/19900928059069I), Sep 28, 1990: Bac 146200A (N607AW), Champaign-Urban, IL. First officer had a seizure and passed out. Diverted for landing.
- [Incident 19900730040879I](https://openairdocs.org/incident/19900730040879I), Jul 30, 1990: Bac 146200A (N606AW), Huntsville, AL. Unable to get an up gear indication. Returned. Found a leak in the hydraulic system.
- [Incident 19900718056589I](https://openairdocs.org/incident/19900718056589I), Jul 18, 1990: Bag BAE146100A (N292UE), Reno, NV, Minor damage. Tug rolled into aircraft when driver left tug in neutral. He got out with brakes set to help connect tow bar.
- [Incident 19900715040499I](https://openairdocs.org/incident/19900715040499I), Jul 15, 1990: Bac 146200A (N181US), San Diego, CA. Cargo door warning light on after takeoff. Returned. Baggage strap found caught in door.
- [Incident 19900628033589I](https://openairdocs.org/incident/19900628033589I), Jun 28, 1990: Bac 146200A (N607AW), Chicago, IL, Minor damage. Flight attendant advised pilot of engine fire. No cockpit warning. Returned. Manifold was leaking fuel.
- [Incident 19900529028159I](https://openairdocs.org/incident/19900529028159I), May 29, 1990: Bac 146200A (N607AW), Lexington, KY. Emergency landing due to passenger medical problem. Removed to hospital and resumed flight.
- [Incident 19891006062909I](https://openairdocs.org/incident/19891006062909I), Oct 6, 1989: Bac 146200A (N290UE), Burbank, CA. Smoke from right engine on approach. Landed safely. Vapor trail caused by airflow disruption over broken tailpipe.
- [Incident 19890601037719I](https://openairdocs.org/incident/19890601037719I), Jun 1, 1989: Bag BAE146300A (N403XV), West Palm Beach, FL, Minor damage. While taxiing under marshalling, NR2 engine contacted jetway. Minor damage.
- [Incident 19881102061619I](https://openairdocs.org/incident/19881102061619I), Nov 2, 1988: Bac 146200A (N408XV), Albany, NY. Fire warning. Engine shut down. Returned. Landed without incident. Cause for warning not given.
- [Incident 19881007059069I](https://openairdocs.org/incident/19881007059069I), Oct 7, 1988: Bac 146200A (N606AW), Fort Wayne, IN. Received bird strike to leading edge of left wing during takeoff. Continued flight. No damage to wing.
- [Incident 19880725057989I](https://openairdocs.org/incident/19880725057989I), Jul 25, 1988: Bag JETSTREAM200 (N187US), Monterey, CA. Auto pilot did not capture altitude and aircraft descended below assigned altitude. Replaced altimeter.
- [Incident 19880708067379I](https://openairdocs.org/incident/19880708067379I), Jul 8, 1988: Bac 146200A (N183US), Burbank, CA, Minor damage. Collided with a cement truck while taxiing to the gate. Minor damage. No injuries.
- [Incident 19880422066369I](https://openairdocs.org/incident/19880422066369I), Apr 22, 1988: Bac 146200A (N174US), Big Sur, CA. ATC equipment showed plane below assigned altitude. Pilot verified correct altitude. Radar readout sometimes fautly
- [Incident 19871203074599I](https://openairdocs.org/incident/19871203074599I), Dec 3, 1987: Bac 146200A (N177US), Los Angeles, CA, Substantial damage. Brakes and nosewheel steering failed during maintenance taxi. Aircraft struck a parked aircraft.
- [Incident 19870730052399I](https://openairdocs.org/incident/19870730052399I), Jul 30, 1987: Bac 146200A (N403XV), Washington, DC. On preflight, starter was found loose. Metal from the adapter caused main bearing failures.
- [Incident 19861024079642I](https://openairdocs.org/incident/19861024079642I), Oct 24, 1986: Bac 146200A (N607AW), Chicago, IL, Substantial damage. While holding for departure, aircraft vertical stabilizer was struck by taxiing N4718U.

## Service difficulty reports (954, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR NI6R202508200065](https://openairdocs.org/sdr/NI6R202508200065), Aug 20, 2025: SEAL. LEAKING. ENROUTE TO THE BEULAH INCIDENT, APPROXIMATELY 30 MILES EAST OF HIF, THE PYLON 3 OVHT LIGHT ILLUMINATED ON THE MWP. THE ENGINES WERE SET TO CLIMB THRUST OF 800 T
- [SDR NI6R202505150060](https://openairdocs.org/sdr/NI6R202505150060), May 15, 2025: WHEEL. CRACKED. AFTER AIRCRAFT DEPARTURE FROM GATEWAY AIRTANKER BASE, MESA, AZ, GROUND PERSONNEL FOUND A PIECE OF AIRCRAFT WHEEL LIP ON THE GROUND. THE SUSPECT AIRCRAFT WAS ENR
- [SDR CA071108007](https://openairdocs.org/sdr/CA071108007), Nov 7, 2007: LINK. UNSERVICEABLE. (CAN) IT HAS BEEN DISCOVERED DURING INSPECTION OF THE ABOVE MENTIONED PART THAT IT IS IN AN UNSERVICEABLE CONDITION. WHILE ON JACKS THE COMPONENT WAS INSPECTED 
- [SDR A6WA200560021](https://openairdocs.org/sdr/A6WA200560021), Mar 6, 2006: FLAP SYSTEM. MALFUNCTIONED. WHEN DEPARTING, FLAPS FAIL AT 18 DEGREES. BOTH FLAP INOP LIGHT AND FLAP FAULT LIGHT ILLUMINATED, FOLLOW ALL QRH CHECKLIST LANDING. ECU FAULT LED NR 4 SHOWING C/
- [SDR AU510002070](https://openairdocs.org/sdr/AU510002070), Dec 12, 2005: ANTI-SKID SYS. FAULTY. FOLLOWING TWO BURST TIRES ON NR 1 MAIN WHEEL, MAINTENANCE CHANGED THE GREEN SYSTEM ANTI-SKID VALVE FOR NR 1 WHEEL POSITION. INVESTIGATION CONTINUING.
- [SDR A6WA200560020](https://openairdocs.org/sdr/A6WA200560020), Dec 3, 2005: SEAL. LEAKING. RT ZONE HI TEMP CAPTAIN ILLUMINATED ENROUTE IN ICING CONDITIONS. REPLACED SEALS AT NR 4 PYLON LEADING EDGE AND LEAK CHECKED WING ANTI-ICE. OPS CHECKED GOOD. (K)
- [SDR A6WA200560017](https://openairdocs.org/sdr/A6WA200560017), Jul 30, 2005: APU. BIRD INGESTION. SMOKE IN CABIN WHEN TURNING ON PACKS. MAINTNANCE C/W EO, BOTH AC PACKS. FOUND BIRD AND OIL IN APU INTAKE. REMOVED AND REPLACED APU, BOTH AC PACKS, JET PUMPS AND
- [SDR A6WA200560016](https://openairdocs.org/sdr/A6WA200560016), Jul 14, 2005: FUEL CONTROL. UNSERVICEABLE. CLIMBING THRU 9000 FT NR 1 ENGINE STARTED TO WIND DOWN. BOTH N1 AND N2 WERE DROPPING, TGT APPEARED TO BE RISING. SECURED ENGINE, PERFORMED IMMEDIATE ACTION CHEC
- [SDR A6WA200460055](https://openairdocs.org/sdr/A6WA200460055), Nov 11, 2004: ACM. MALFUNCTIONED. NR PACK TEMP IS UNCONTROLLABLE IN EITHER MANUAL OR AUTO WHEN USING APU AIR. WILL RUN FULL HOT AND SMOKES CABIN. NOTE: CONTROLLABLE IN (MAN) MODE WITH ENGINE AIR
- [SDR A6WA200460040](https://openairdocs.org/sdr/A6WA200460040), Sep 21, 2004: STRUCTURE. CRACKED. AIRBRAKE STRUCTURE AFT OF FRAME 50 VERTICAL STIFFENER HAS A CRACK RADIATING FROM RIVET. REPAIR IN PROGRESS. (M)
- [SDR A6WA200460036](https://openairdocs.org/sdr/A6WA200460036), Sep 3, 2004: FRAME. CRACKED. FOUND CRACK JUST AFT OF FRAME 29 RIGHT EMANATING FROM A RIVET. MAINTENANCE REQUESTED A REPAIR FROM BAE SYSTEMS REF AVMAX 656-2015002. (M)
- [SDR A6WA200460035](https://openairdocs.org/sdr/A6WA200460035), Sep 3, 2004: SKIN. CRACKED. FOUND CRACK JUST AFT OF FRAME 39 LEFT EMANATING FROM A RIVET. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 656-2015001. (M)
- [SDR A6WA20046002](https://openairdocs.org/sdr/A6WA20046002), Jun 13, 2004: ECU. MALFUNCTIONED. WHEN FLAPS SELECTED FOR 24-33 DEGREES ON TO ASE, FLAP FAULTS AND INOPERATIVE LIGHTS ILLUMINATED FLAPS STUCK AT 24 DEGREES AIRCRAFT RETURNED TO DEN. MAINTENANCE 
- [SDR AUS20040414](https://openairdocs.org/sdr/AUS20040414), May 15, 2004: SEAL. LEAKING. (AUS) RT MAIN LANDING GEAR ACTUATOR RESTRICTOR SEAL LEAKING.
- [SDR A6WA200460015](https://openairdocs.org/sdr/A6WA200460015), May 12, 2004: FLAP TRACK. WORN. NR 2 FLAP TRACK, WEAR FOUND ON NR 2 LT LOWER ROLLER THAT MEASURES .033 INCHES DEEP. REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 607-1907002. MAINTENANCE REM
- [SDR A6WA200460010](https://openairdocs.org/sdr/A6WA200460010), Mar 22, 2004: SHAFT SEAL. LEAKING. STRONG ODOR IN COCKPIT, EYES BURNING WITH AC PACKS ON. MAINTENANCE PERFORMED PACK BURN OUT PROCEDURE. REMOVED AND REPLACED APU ASSEMBLY. (M)
- [SDR A6WA200460006](https://openairdocs.org/sdr/A6WA200460006), Mar 10, 2004: TURBINE WHEEL. DAMAGED. NR 4 ENGINE, 4TH TURBINE WHEEL LOST HEAD OF RIVET WHICH HOLDS BLADE IN PLACE, CAUSING IMPACT DAMAGE TO 4TH NOZZLE CONTAINMENT RIGHT. MAINTENANCE REMOVED AND REP
- [SDR A6WA200360069](https://openairdocs.org/sdr/A6WA200360069), Dec 9, 2003: SKIN. DAMAGED. FOUND CRACKS ON THE LEFT AND RIGHT FUSELAGE ABOVE STRINGER 13 JUST AFT OF FRAME 29 EMANATING FROM THE RIVIT LOCATIONS. MAINTENANCE CUT OUT DAMAGE TO SKIN IAW BA
- [SDR A6WA200360067](https://openairdocs.org/sdr/A6WA200360067), Dec 9, 2003: STRUCTURE. DAMAGED. RIGHT FLAP AT THE NR 4 POSITION BETWEEN RIBS 33 AND 34 OVERSIZE BUSHING REQUIRED. BUSHING LOCALLY MANUFACTURED AT AAO AND CAD PLATED IAW BAE FAX BARA/AVR/6605/0
- [SDR A6WA200360066](https://openairdocs.org/sdr/A6WA200360066), Nov 6, 2003: STRUCTURE. DAMAGED. OVERSIZED BUSHING REQUIRED IN TWO PLACES ON RIGHT FLAP P/N HC579L1400-001, S/N 838H52-86. REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1701-692001. (M)
- [SDR A6WA200360063](https://openairdocs.org/sdr/A6WA200360063), Oct 28, 2003: FLAP TRACK. DAMAGED. INSTALL OF FLAP TRACK NR 1 LANDING PLATE FASTENERS. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1698-6910005. (M)
- [SDR A6WA200360061](https://openairdocs.org/sdr/A6WA200360061), Oct 28, 2003: SKIN. DENTED. FOUND DENTS LEFT AND RIGHT ELEVATOR SERVO AND TRIM TABS, LEFT AND RIGHT TRAILING EDGE PANELS RIB 14A TO 15, LEFT WING INBOARD CENTER, OUTBOARD SPOILERS, RT WING
- [SDR A6WA200360059](https://openairdocs.org/sdr/A6WA200360059), Oct 22, 2003: TAB. DAMAGED. RIGHT OUTBOARD FLAP TAB TRAILING EDGE DAMAGED. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS RED AVMAX FAX 1698-6910001. (M)
- [SDR A6WA200360057](https://openairdocs.org/sdr/A6WA200360057), Oct 20, 2003: SKIN. DENTED. LEFT AND RIGHT WING DENTED, SPOILERS AND T/E PANEL'S, MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1693-6830005. (M)
- [SDR A6WA200360058](https://openairdocs.org/sdr/A6WA200360058), Oct 18, 2003: WIRE. LOOSE. DURING SLIDE DEPLOYMENT FOR FUNCTION TEST LIGHTS CAME ON AND THEN OFF AFTER FULL DEPLOYMENT, INSPECTION FOUND WIRES PULLED OUT OF BATTERY CONNECTORS. MAINTENANC
- [SDR A6WA200360055](https://openairdocs.org/sdr/A6WA200360055), Oct 15, 2003: RIVET. DAMAGED. RT MLG DOOR RIVETS, MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1693-6830003. (M)
- [SDR A6WA200360053](https://openairdocs.org/sdr/A6WA200360053), Oct 7, 2003: PAN. DAMAGED. AFT BAGGAGE DOOR INTERFACE DAMAGE TO THE FORWAD EDGE OF THE AFT BAGGAGE DOOR PAN, LOCATED NEXT TO THE LOWE SHOOT BOLT GUIDE. MAINTENANCE REQUESTED REPAIR FROM B
- [SDR A6WA200360046](https://openairdocs.org/sdr/A6WA200360046), Oct 6, 2003: SKIN. DENTED. DENTS ON THE LEFT AND RIGHT HORIZONTAL STAB MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS RED AMAX FAX 1683-6810002. (M)
- [SDR A6WA200360045](https://openairdocs.org/sdr/A6WA200360045), Oct 6, 2003: SKIN. DELAMINATED. DENTS ON THE LEFT AND RIGHT WING NOW SHOWING SIGNS OF DELAMINATION. MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1683-6810001. (M)
- [SDR A6WA200360051](https://openairdocs.org/sdr/A6WA200360051), Oct 4, 2003: SKIN. DENTED. FOUND DENTS FORWARD OF CARGO DOOR. MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX CAX 1683-6810007. (M)
- [SDR A6WA200360048](https://openairdocs.org/sdr/A6WA200360048), Oct 4, 2003: SKIN. DELAMINATED. DENTS LEFT AND RIGHT ELEVATORS MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1683-6810004. (M)
- [SDR A6WA200360033](https://openairdocs.org/sdr/A6WA200360033), Aug 31, 2003: SPRING. BROKEN. NLG RIGHT WHEEL BRAKE, SPRING BROKEN. MAINTENANCE REMOVED AND REPLACED BROKENS SPRING GUIDE TUBE, SPRING AND REPAIRED DAMAGE TO THE CEILING OVER NLG BAY. (M)
- [SDR AUS20010916](https://openairdocs.org/sdr/AUS20010916), Aug 21, 2001: BEARING. FAILED. (AUS) NR 2 MAIN WHEEL INNER BEARING DISINTEGRATED CAUSING THE INNER RACE TO FUSE TO THE AXLE.
- [SDR AUS20010763](https://openairdocs.org/sdr/AUS20010763), Jul 15, 2001: ENGINE. LEAKING. (AUS) NR 3 ENGINE HP COMPRESSOR CONTAMINATED WITH OIL. FUMES IN CABIN.
- [SDR CA010830017](https://openairdocs.org/sdr/CA010830017), Jul 13, 2001: WHEEL. CRACKED. (CAN) THE WHEEL HAD BEEN REMOVED DUE TO THE TIRE BEING WORN TO LIMITS. DURING THE CLEANING PROCESS, TWO CRACKS WERE DISCOVERED VISUALLY. THEY RAN FROM THE LIGHT
- [SDR AUS20010793](https://openairdocs.org/sdr/AUS20010793), Jul 10, 2001: PUMP. WORN. (AUS) ENGINE DRIVEN HYDRAULIC PUMP INTERNAL AND EXTERNAL DRIVE SPLINES WORN EXCESSIVELY.
- [SDR AUS20010727](https://openairdocs.org/sdr/AUS20010727), Jul 10, 2001: ENGINE. FAILED. (AUS) NR 3 ENGINE OIL PRESSURE LOSS.
- [SDR AUS20010691](https://openairdocs.org/sdr/AUS20010691), Jul 7, 2001: ENGINE. MALFUNCTIONED. (AUS) NR 2 ENGINE HAD NO OIL PRESSURE. LIMITED INFORMATION PROVIDED.
- [SDR CA010703022](https://openairdocs.org/sdr/CA010703022), Jun 27, 2001: BEARING. MAKING METAL. (CAN) DURING ROUTINE INSPECTION NR 4 ENGINE FULL FLOW CHIP DETECTOR WAS FOUND TO HAVE "CONDITION 2" CONTAMINATION. THE ENGINE WAS REPLACED AND THE AIRCRAFT WAS 
- [SDR CA010723001](https://openairdocs.org/sdr/CA010723001), Jun 21, 2001: COMPUTER. MALFUNCTIONED. (CAN) DURING A MAINTENANCE ENGINE RUN, THE NR 1 ANTI-ICE VALVE CIRCUIT BREAKER POPPED AND WOULD NOT RESET. MAINTENANCE REPLACED THE JUST INSTALLED THRUST MODULA
- [SDR AUS20010622](https://openairdocs.org/sdr/AUS20010622), Jun 16, 2001: SKIN. CRACKED. (AUS) FUSELAGE SKIN CRACKED IN AREA LOCATED IMMEDIATELY AFT OF FRAME 29 BENEATH THE WING ROOT DOUBLER. FOUND DURING INSPECTION IAWISB53-144 AND AD/BAE146/70.
- [SDR CA010625001](https://openairdocs.org/sdr/CA010625001), Jun 13, 2001: PIN. DAMAGED. (CAN) LARGE SECTION OF CHROME MISSING FROM DIAMETER "A" PIN (PARENT METAL CORRODED UNDER AREA OF MISSING CHROME) DEFECT FOUND REMOVAL OF PIN WHEN RETRACTION ACT
- [SDR AUS20010539](https://openairdocs.org/sdr/AUS20010539), May 28, 2001: SKIN. CRACKED. (AUS) FUSELAGE SKIN CRACKED IN THE AREA BETWEEN FR 35 AND FR 36 ATSTRINGER LOCATIONS 2L AND 3L. CRACK LENGTH 558.8MM (22IN).
- [SDR AUS20010538](https://openairdocs.org/sdr/AUS20010538), May 28, 2001: RECORDER. UNSERVICEABLE. (AUS) OPERATIONAL CHECK AND CALIBRATION CHECK OF FLIGHT DATA RECORDER (FDR) NOT CARRIED OUT. PERSONNEL/MAINTENANCE ERROR.
- [SDR AUS20010506](https://openairdocs.org/sdr/AUS20010506), May 20, 2001: FIRE LOOP. WORN. (AUS) NR 1 ENGINE FIRE DETECTOR WIRING LOOM CHAFED.
- [SDR A6WA200100035](https://openairdocs.org/sdr/A6WA200100035), May 20, 2001: ACTUATOR. FAILED. NR 4 ENGINE AUTO SHUTDOWN GROUND PERSONNEL NOTICED FLAMES COMING OUT OF TAIL PIPE PILOT FIRED BOTH FIRE BOTTLES. MAINTENANCE REMOVED AND REPLACED BLEED BAND ACT
- [SDR CA010621041](https://openairdocs.org/sdr/CA010621041), May 11, 2001: CONTROL UNIT. LEAKING. (CAN) INVESTIGATION INTO A HYDRAULIC LEAK RESULTED IN REPLACEMENT OF THE FLAP POWER UNIT WHICH WAS FOUND TO BE LEAKING FROM AN OUTPUT SHAFT CAVITY DRAIN. THIS P
- [SDR CA010522011](https://openairdocs.org/sdr/CA010522011), Apr 29, 2001: PROXIMITY SENSOR. FAILED. (CAN) THE FLIGHT CREW REPORTED THE L/H RED "GEAR UNSAFE" LIGHT ILLUMINATED ACCOMPANIED BY GEAR HORN, STICK SHAKER, AND MANUAL SPOILER FAULT WHILE AT THE GATE AF
- [SDR A6WA200100033](https://openairdocs.org/sdr/A6WA200100033), Apr 26, 2001: FRAME. CRACKED. FUSELAGE FRAME 18 CRACKED. MAINTENANCE REPARED FRAME 18 LT SIDE IAW BAE SYSTEMS FAX REF BARA/AVR/5362/01, BARA/AVR/5360/01, AND RIL HC537H9453.
- [SDR A6WA200100030](https://openairdocs.org/sdr/A6WA200100030), Apr 22, 2001: ELEVATOR. CONTAMINATED. PITCH OSCILLATION OCCURRED ON CLIMBOUT. MAINTENANCE DRAINED WATER FROM ELEVATORS.

All 954: https://openairdocs.org/model/british-aerospace-bae-146-series-200a/reports.md

## STCs that may be installed (OpenAirDocs) (58, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC SA3964NM](https://openairdocs.org/stc/SA3964NM): Installation of closet and class divider. Safran Cabin Inc
- [STC SA3414NM](https://openairdocs.org/stc/SA3414NM): Installation of floor proximity emergency escape path marking system. Bruce Aerospace Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST02829LA](https://openairdocs.org/stc/ST02829LA): Conversion of a BAE Systems (Operations) Limited BAe 146-200 passenger configuration to a firefighting airtanker with the installation of a 3000 USG retardant tank system. Airspray USA Ltd
- [STC ST02080CH](https://openairdocs.org/stc/ST02080CH): Installation of VHF-3 Antenna Structural Provisions. Amphenol Cable and Interconnect Technologies Inc
- [STC ST02086CH](https://openairdocs.org/stc/ST02086CH): Installation of a Spectra Lux Dlink Aircraft Communications Addressing and Reporting System (ACARS). Amphenol Cable and Interconnect Technologies Inc
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST04647CH](https://openairdocs.org/stc/ST04647CH): INSTALL SOLID STATE DIGITAL FLIGHT DATA RECORDER (DFDR) SYSTEM. DAN BUZZ & ASSOCIATES LLC
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST02281LA](https://openairdocs.org/stc/ST02281LA): Installation of internal tank, associated systems and support structure for the aerial dispensing of liquids. Neptune Aviation Services
- [STC ST00261DE-D](https://openairdocs.org/stc/ST00261DE-D): Installation of dual AlliedSignal GNS-XLs Flight Management System. Honeywell International Inc
- [STC ST00255DE-D](https://openairdocs.org/stc/ST00255DE-D): Installation of AlliedSignal VHF AFIS. Honeywell International Inc
- [STC ST01805WI](https://openairdocs.org/stc/ST01805WI): Modification of Rockwell Collins TCAS II System Installation with DC powered TCAS Transmitter Receiver Processor. Rockwell Collins Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST02406LA](https://openairdocs.org/stc/ST02406LA): Installation of TCAS version 7.1. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST02793CH](https://openairdocs.org/stc/ST02793CH): Install Aero Medical Products Mfg., Inc. Air Ambulance Stretcher P/N 125 using Installation Kit P/N 805. Paul/ Lanna Egan LLC
- [STC SA7076NM](https://openairdocs.org/stc/SA7076NM): Installation of Stretcher Carrier. Air Medic LLC
- [STC SA2419NM](https://openairdocs.org/stc/SA2419NM): Installation of seating arrangement. American Airlines Inc
- [STC SA2418NM](https://openairdocs.org/stc/SA2418NM): Installation of a Collins ARINC communications addressing and reporting system (ACARS). American Airlines Inc
- [STC SA2453NM](https://openairdocs.org/stc/SA2453NM): Installation of a Collins WXR-700X Weather Radar System with Turbulence Detection Mode. American Airlines Inc
- [STC SA2550SO](https://openairdocs.org/stc/SA2550SO): Installation of mixed seating. American Airlines Inc
- [STC ST02530LA](https://openairdocs.org/stc/ST02530LA): Installation of T2CAS with TCAS version 7.1. Aircraft Communication & Surveillance Systems
- [STC ST02524LA](https://openairdocs.org/stc/ST02524LA): Installation of TCAS version 7.0. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST01202WI-D](https://openairdocs.org/stc/ST01202WI-D): Modification of an existing FAA approved Collins TPR-720, TPR-900 or TPR-901 Mode S transponder installation in Part 25 Aircraft using Collins Drawing Index as listed on AML No. ST01202WI-D, latest FAA approved revision. Rockwell Collins Inc
- [STC ST01256WI-D](https://openairdocs.org/stc/ST01256WI-D): Modification of a Collins TPR-720, TPR-900 or TPR-901 Mode S Transponder System installation with an ATC/TCAS Control Panel to an Elementary Surveillance Compliant Collins TPR-901 Mode S Transponder System installation with a Flight ID/ATC/TCAS Control Panel in accordance with Collins Drawing Index as listed on AML No. ST01256WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [STC ST02248NY](https://openairdocs.org/stc/ST02248NY): Installation of EMS HSD-64, HSD-128, HSD-HCM, and HSD-X. EMS Technologies Canada Ltd
- [STC SA1069GL](https://openairdocs.org/stc/SA1069GL): Installation of Grimes Floor Proximity Lighting System. Honeywell International Inc
- [STC ST00579CH](https://openairdocs.org/stc/ST00579CH): Installation of a GTE Airfone Public Telephone System (Genstar). U.S. Technical Consultants Inc
- [STC ST00844WI-D](https://openairdocs.org/stc/ST00844WI-D): Modification of Collins TCAS II or TCAS-94 (TCAS II) system installation with Collins TTR-920 Change 7.0 Receiver Transmitter to a Collins TCAS II or TCAS-94 OTCAS II) system installation with Collins TTR-921 or Collins TTR-4000 Change 7.0 TCAS Receiver Transmitter. Rockwell Collins Inc
- [STC ST00525WI-D](https://openairdocs.org/stc/ST00525WI-D): Modification of Collins 618M-4 VHF COMM Receiver Transmitter Installation to a 618M-5 VHF COMM Receiver Transmitter installation with either a Gables G7406-02 or Avtech 7522-1-2 VHF COMM Receiver Transmitter Control Series using with Collins Installation Instructions as listed on AML No. ST00525WI-D, or later FAA approved revisions. Rockwell Collins Inc
- [STC ST00626CH](https://openairdocs.org/stc/ST00626CH): Installation of replacement immersion heater. Aircraft Food Service Equipment Repair
- [STC ST01004NY](https://openairdocs.org/stc/ST01004NY): Installation of cargo restraint straps. Airline Container Manufacturing Co Inc. Lists BAe 146 Series
- [STC SA4592NM-D](https://openairdocs.org/stc/SA4592NM-D): Installation of a dual SANS 7000 TACAN system. Learjet Inc
- [STC ST00705LA](https://openairdocs.org/stc/ST00705LA): Installation of Honeywell Traffic Alert and Collision Avoidance System (TCAS II). ACSS (Aviation Communication and Surveillance Syst
- [STC SA1969SO](https://openairdocs.org/stc/SA1969SO): Installation of class E cargo compartment and 9.0g restraint bulkhead. Pemco Aeroplex Inc
- [STC SA1970SO](https://openairdocs.org/stc/SA1970SO): Installation of aft cargo door. Pemco Aeroplex Inc
- [STC SA1971SO](https://openairdocs.org/stc/SA1971SO): Installation of a cargo handling system. Pemco Aeroplex Inc
- [STC ST00075NY](https://openairdocs.org/stc/ST00075NY): Installation of Mode S Transponder and TCAS II System. Navair Limited
- [STC ST09228SC](https://openairdocs.org/stc/ST09228SC): Installation of dual Universal Navigation Model UNS-1M Navigation Management Systems. Advanced Avionics Technologies
- [STC ST00403NY](https://openairdocs.org/stc/ST00403NY): Replacement of cargo bay lining panels. Field Aviation East Limited
- [STC ST00209NY](https://openairdocs.org/stc/ST00209NY): Installation of Interior Trim Panels. PA Aerospace, Ltd
- [STC ST09121SC](https://openairdocs.org/stc/ST09121SC): Installation of a Safeflight Reactive Windshear System Model 6508. Advanced Avionics Technologies
- [STC ST00888AT](https://openairdocs.org/stc/ST00888AT): Installation of 88 passenger seating interior configuration. Atlantic Southeast Airlines
- [STC SA3440NM](https://openairdocs.org/stc/SA3440NM): Installation of floor proximity emergency escape path marking system. Intl Valve Co

All 58: https://openairdocs.org/model/british-aerospace-bae-146-series-200a/stcs.md

## PMA parts (OpenAirDocs) (747, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [S9413-008WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121945012520261009134003.0001): Packing, Preform - Fluorocarbon. Wencor, LLC · PMA PQ1370NM · Replaces S9413-008 · Oct 1, 2026
- [AF300P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183022610920260717175325.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026
- [AF302](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172030289420260717175327.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026
- [AF300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100475321920260717175323.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026
- [858885-3WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156222213420260107202051.0001): Diaphragm-Air. Wencor, LLC · PMA PQ1370NM · Replaces 858885-3 · Oct 30, 2025
- [650-0100-05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170633596620250603134030.0001): Cellular Module, avCM LTE. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [400-21149G-3-305, 400-21149G-3-315, 400-21149G-3-405, 400-21149G-3-415, 400-21149G-3-505, 400-21149G-3-515, 400-21149G-3-605, 400-21149G-3-615, 400-21149G-3-915](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158343515320250603134041.0001): Assy, LRU Adapter (avRDC or MAX). Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [21149GK-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148671001820250612143624.0001): Installation Kit, miniQAR / avRDC QAR. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [804-1250-32](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141557572720250612143633.0001): avRDC MAX QAR. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [804-1250-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138833256520250612143629.0001): avRDC QAR. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [650-0100-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119871943820250603134026.0001): Cellular Module (avCM 4G), GSM / GRPS 4G, Quad Band, SMA. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [804-1201, 804-1205, 804-1205-03, 804-1212, 804-1216](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110154462520250612143620.0001): miniQAR MKIII. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [400-21149G-3-101, 400-21149G-3-103, 400-21149G-3-105, 400-21149G-3-111, 400-21149G-3-113, 400-21149G-3-115, 400-21149G-3-205, 400-21149G-3-215, 400-21149G-3-715, 400-21149G-3-815](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102270356720250603134037.0001): Assy, LRU Adapter (miniQAR MKIII). Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [802-0100-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100939741320250603134033.0001): Kit, avCM 4G Adapter. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [PT-RL-50035](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107874573720250114193040.0001): Relay, 28 VDC. B/E Aerospace Inc · PMA PQ3417CE · Replaces RL-50035 · Nov 25, 2024
- [447883LA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133324749420241107175401.0001): Valve, Safety Assy. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 447883 · Nov 5, 2024
- [858888-3WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194660406220250506130830.0001): Plate, Diaphragm Retaining. Wencor, LLC · PMA PQ1370NM · Replaces 858888-3 · Sep 29, 2024
- [858887-4WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127785023720250506130825.0001): Plate, Diaphragm-Backing. Wencor, LLC · PMA PQ1370NM · Replaces 858887-4 · Sep 29, 2024
- [LA555153](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192294215920240904014312.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555153 · Aug 28, 2024
- [LA412505](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185742199920240904014204.0001): Sleeve. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 412505 · Aug 28, 2024
- [LA555015](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177623628120240904014245.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555015 · Aug 28, 2024
- [LA01000X200A20B6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167775333620241016174854.0001): O-Ring. LanAir Research and Development Inc · PMA PQ1031NE · Replaces R01000X200A20B6 · Aug 28, 2024
- [LA553044](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164223761720240904014230.0001): Valve. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 553044 · Aug 28, 2024
- [LA3460X240A20B6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162102154120240904014157.0001): O-Ring. LanAir Research and Development Inc · PMA PQ1031NE · Replaces R03460X240A20B6 · Aug 28, 2024
- [LA490X190A5005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161699516820240904014210.0001): O-Ring. LanAir Research and Development Inc · PMA PQ1031NE · Replaces R00490X190A50D5 · Aug 28, 2024
- [LA555070](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151269729420240904014305.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555070 · Aug 28, 2024
- [LA553008](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145917844920240904014224.0001): Gasket. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 553008 · Aug 28, 2024
- [LA555016](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141320259420240904014251.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555016 · Aug 28, 2024
- [LA220X160A20B6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134244263720240904014150.0001): O-Ring. LanAir Research and Development Inc · PMA PQ1031NE · Replaces R00220X160A20B6 · Aug 28, 2024
- [LA449039](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133844028820241016174948.0001): Mask Lock. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 449039 · Aug 28, 2024
- [LA559018](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128621373520240904014320.0001): Dilution Screen. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 559018 · Aug 28, 2024
- [LA555012](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120890724220240904014238.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555012 · Aug 28, 2024
- [LA555033](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112465035020240904014258.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555033 · Aug 28, 2024
- [LA495357](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106084472820240904014217.0001): Sleeve. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 495357 · Aug 28, 2024
- [422B340LA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130612083020240724143346.0001): Overhaul Kit. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 422B340 · Jul 3, 2024
- [PM-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157066921120240807154255.0001): Radome Mask. PM Research, Inc. · PMA PQ10049NE · Replaces N/A · Jun 24, 2024
- [3163811-7WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102142794820240919140157.0001): Valve - Poppet. Wencor, LLC · PMA PQ1370NM · Replaces 3163811-7 · Jan 30, 2024
- [APM62-0132-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148159608920240301165924.0001): Float Assy, Vent Valve. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces 62-0132-1 · Dec 14, 2023
- [APM62-0132-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159063916020231212163837.0001): Float Assy, Vent Valve. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces 62-0132-1 · Dec 11, 2023
- [804-1216](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188408148520240924135408.0001): miniQAR MKIII. Avionica LLC. · PMA pq1734ce · Modification part · Dec 8, 2023
- [804-1216](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141900212420240924135404.0001): miniQAR MKIII. Avionica LLC. · PMA pq1734ce · Modification part · Dec 8, 2023
- [SG8916](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196021379720230918113603.0001): Filler. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8916 · Sep 13, 2023
- [10-50009-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192158707920230918113446.0001): SSUL-X18 Lateral Extension Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50009-XFCCC · Sep 13, 2023
- [30-50001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189576184820230918113659.0001): Scapa 5169 Filler. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 30-50001 · Sep 13, 2023
- [10-50049-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186729362720230918113552.0001): SSUL-X36 Lateral Extension Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50049-XFCCC · Sep 13, 2023
- [10-50008-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184059125020230918113434.0001): SSUL-X18 Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50008-XFCCC · Sep 13, 2023
- [10-50024-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181753876320230918113530.0001): SSUL-X23 Lateral Extension Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50024-XFCCC · Sep 13, 2023
- [10-50010-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179472989420230918113457.0001): SSUL-X11 Lateral Extension Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50010-XFCCC · Sep 13, 2023
- [SG8996](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171950792520230918113648.0001): Flexible Overcarpet End Cap for SSUL with Tape. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8996 · Sep 13, 2023
- [SG8857](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169114400120230918113614.0001): Track SSUL Overcarpet 1.5-3mm. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8857 · Sep 13, 2023

All of them: https://openairdocs.org/model/british-aerospace-bae-146-series-200a/pma.md

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