# British Aerospace BAE 146 SERIES 100A

- Type: Aircraft model (FAA registry)
- Registry code: 1500260
- Manufacturer (registry): BRITISH AEROSPACE
- Model: BAE 146 SERIES 100A
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 4 · Turbo-jet
- Seats: 93
- 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: 0
- Page: https://openairdocs.org/model/british-aerospace-bae-146-series-100a

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 170: https://openairdocs.org/model/british-aerospace-bae-146-series-100a/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

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports (1)

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 19910224012209I](https://openairdocs.org/incident/19910224012209I), Feb 24, 1991: Bac 146100A (N463AP), Aspen, CO, Minor damage. Captain discovered wrinkles in fuselage exterior metal skin on walk-around. Aircraft taken out of service.

## Service difficulty reports (188, newest 50)

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

- [SDR AU510001710](https://openairdocs.org/sdr/AU510001710), Oct 8, 2005: FRAME. CRACKED. FUSELAGE FRAME 15 AND FRAME 41 CRACKED. FOUND DURING INSPECTION IAW AD/BAE146/116.
- [SDR AU510001880](https://openairdocs.org/sdr/AU510001880), May 9, 2005: FRAME. CRACKED. FUSELAGE FRAMES 15 AND 18 CRACKED, FOUND DURING INSPECTION IAW AD/BAE146/116.
- [SDR AUS20010835](https://openairdocs.org/sdr/AUS20010835), Aug 1, 2001: FASTENER. CORRODED. (AUS) DURING INSPECTION FOR LOCATION OF CENTRE FUEL TANK LEAK THE FOLLOWING DEFECTS WERE FOUND: 1. FRAME 29 LT HAND UPPER SIDE (AFT WING ATTACHMENTS) FASTENER I
- [SDR AUS20010857](https://openairdocs.org/sdr/AUS20010857), Jul 16, 2001: SKIN. CORRODED. (AUS) LT WING LOWER SKIN CORRODED IN AREA BETWEEN RIB 13 AND RIB 15.CORROSION WAS BEYOND ALLOWIABLE LIMITS.
- [SDR AUS20010619](https://openairdocs.org/sdr/AUS20010619), Jun 16, 2001: ENGINE. LEAKING. (AUS) NR 2 ENGINE LEAKING CONTAMINATED AIR INTO CABIN.
- [SDR AUS20010421](https://openairdocs.org/sdr/AUS20010421), May 14, 2001: FIRE BOTTLE. MISINSTALLED. (AUS) NR 3 ENGINE FIRE BOTTLE FIRING SWITCH WIRING CONTAINED TWO INLINESPLICES FITTED WITH SMALLER GAUGE WIRES. UNAPPROVED MODIFICATION. PERSONNEL/MAINTENANCE E
- [SDR AUS20010480](https://openairdocs.org/sdr/AUS20010480), May 5, 2001: COOLING FAN. FAILED. (AUS) CABIN FAN FAILED. INVESTIGATION FOUND BOTH FORE AND AFT FAN MOTOR SHAFT BEARINGS FAILED. THE MOTOR ALSO FAILED ELECTRICALLY WITHSIGNS OF OVERHEATING. BEAR
- [SDR AUS20010424](https://openairdocs.org/sdr/AUS20010424), May 3, 2001: TRANSCEIVER. INTERMITTENT. (AUS) RADIO ALTIMETER TRANSCEIVER INTERMITTENT OPERATION. INVESTIGATION FOUND THE FAULT WAS DUE TO A STRAY VOLTAGE ON A SPARE PIN IN THETRANSCEIVER DUE TO A WIR
- [SDR AUS20010535](https://openairdocs.org/sdr/AUS20010535), Apr 26, 2001: SPAR. CORRODED. (AUS) LT AND RT WING FORWARD AND AFT SPAR LOWER FLANGES CORRODED IN AREA BETWEEN RIB 13 AND RIB 18.
- [SDR AU010321](https://openairdocs.org/sdr/AU010321), Apr 10, 2001: PIPE. LOOSE. (AUS) NO3 ENGINE P3 SENSE LINE TO FCU LOOSE. THE AIRCRAFT HAD A NO3 ENGINE AND FCU CHANGED THE PREVIOUS DAY. PERSONNEL/MAINTENANCEERROR.
- [SDR AU010192](https://openairdocs.org/sdr/AU010192), Mar 12, 2001: WIRE. LOOSE. (AUS) NR 2 COMPASS SYSTEM FAULTY. INVESTIGATION FOUND A LOOSE WIRE TERMINAL AND NUT ON THE RT FLUX VALVE TERMINAL BLOCK LOCATED AT THE RH OUTER WING TRAILING ED
- [SDR AU010257](https://openairdocs.org/sdr/AU010257), Feb 13, 2001: SPAR. CORRODED. (AUS) LT AND RT WING FORWARD AND AFT SPAR LOWER FLANGES CORRODED.
- [SDR AU010259](https://openairdocs.org/sdr/AU010259), Feb 12, 2001: SKIN. CORRODED. (AUS) LT WING LOWER SKIN CORRODED AT RIB BAYS NR 14 TO NR 16. RT WING LOWER SKIN CORRODED AT RIB BAYS NR 14 AND NR 15.
- [SDR AU010258](https://openairdocs.org/sdr/AU010258), Feb 12, 2001: SPAR. CRACKED. (AUS) LT AND RT WING FORWARD AND AFT LOWER SPAR CAPS CRACKED IN AREABETWEEN RIBS NR 13 AND NR 18. CORROSION ALSO FOUND ON LOWER SKINS AT RIB BAYS NR 13 TO NR 18
- [SDR AU001029](https://openairdocs.org/sdr/AU001029), Oct 23, 2000: GENERATOR. FAULTY. (AUS) NR 1 GENERATOR WENT OFF LINE. GENERATOR CONTROL UNIT AND LINE CONTACTOR CHANGED AND WIRING INSPECTED WITH NIL FAULTS FOUND. INVESTIGATION CONTINUING.
- [SDR AU000935](https://openairdocs.org/sdr/AU000935), Sep 16, 2000: CDU. FAULTY. (AUS) GPS CENTRAL DATA UNIT (CDU) LOCKED UP. GPS WOULD NOT TRACK.
- [SDR AU000829](https://openairdocs.org/sdr/AU000829), Sep 6, 2000: WIRE. FAULTY. (AUS) GROUND CALL HORN WIRE FAULTY.
- [SDR AU000828](https://openairdocs.org/sdr/AU000828), Sep 5, 2000: LIGHT. FAILED. (AUS) LAMP HOLDERS LOCATED AT ROW 14 AND ROW 10 ON THE RT SIDE WALLS BURNED OUT.
- [SDR AU000943](https://openairdocs.org/sdr/AU000943), Sep 4, 2000: INDICATOR. FLUCTUATES. (AUS) NR 2 ENGINE EGT INDICATOR FLUCTUATING.
- [SDR AU000690](https://openairdocs.org/sdr/AU000690), Sep 1, 2000: SPAR. CRACKED. (AUS) LT AND RT WINGS FORWARD AND REAR SPARS CRACKED IN AREA LOCATED OUTBOARD OF RIB NR 13.
- [SDR AU000689](https://openairdocs.org/sdr/AU000689), Sep 1, 2000: INDICATOR. FAULTY. (AUS) AIR SPEED INDICATOR FAULTY.
- [SDR AU000666](https://openairdocs.org/sdr/AU000666), Sep 1, 2000: ENGINE. FAILED. (AUS) NR 2 ENGINE TGT EXCEEDED 900 DEGREES AND FLAMES CAME FROM THEENGINE. THE ENGINE WAS REMOVED AND SENT FOR INVESTIGATION AND REPAIR.
- [SDR AU000651](https://openairdocs.org/sdr/AU000651), Sep 1, 2000: SEAL. LEAKING. (AUS) ENGINE NR 1 BEARING SEAL LEAKING.
- [SDR AU000631](https://openairdocs.org/sdr/AU000631), Sep 1, 2000: TURBINE NOZZLE. FAILED. (AUS) NR 2 ENGINE FAILED ON TAKEOFF WITH THE TGT EXCEEDING 1000 DEGREESC. SUSPECT CAUSED BY FAILURE OF THE SECOND STAGE HP TURBINE NOZZLE.
- [SDR AU000630](https://openairdocs.org/sdr/AU000630), Sep 1, 2000: ENGINE. VIBRATES. (AUS) NO1 ENGINE VIBRATION WITH INDICATION OF 1.5. GROUND CHECKS COULDFIND NO PROBLEMS AND AIRCRAFT RETURNED TO SERVICE. SUSPECT ICING.
- [SDR AU000936](https://openairdocs.org/sdr/AU000936), Jul 16, 2000: TRIM TAB. DAMAGED. (AUS) LT AILERON TRIM TAB DAMAGED DURING GROUND OPERATION.
- [SDR AU000219](https://openairdocs.org/sdr/AU000219), Apr 24, 2000: PIPE. FAILED. (AUS) ENGINE FUEL PIPE FAILED. FUEL LEAK.
- [SDR AU000277](https://openairdocs.org/sdr/AU000277), Apr 11, 2000: INDICATOR. SHORTED. (AUS) RT MAIN LANDING GEAR STANDBY INDICATOR LAMP SHORT CIRCUIT.
- [SDR CA000320002](https://openairdocs.org/sdr/CA000320002), Mar 8, 2000: WIRE. CHAFED. (CAN) NR 1 GENERATOR HARNESS WIRE FOUND CHAFED. WIRE REPAIRED.
- [SDR 2000ZZZX179](https://openairdocs.org/sdr/2000ZZZX179), Dec 22, 1999: DRIVESHAFT. WORN. ENGINE SHUTDOWN IN-FLIGHT. DRIVE SPLINES ON FUEL PUMP SEVERELY WORN. PUMP TO BE OVERHAULED. HIGH OPERATING TIME LED TO FAILIURE.
- [SDR AU990787](https://openairdocs.org/sdr/AU990787), Aug 9, 1999: SKIN. CRACKED. (AUS) FUSELAGE SKIN CRACKED IN THE AREA OF FRAME 29 LOCATED BETWEEN STRINGER NR 12 AND STRINGER NR 13. FOUND DURING INSPECTION IAW AD/BAE/146/70. LIMITED INFORM
- [SDR AU990804](https://openairdocs.org/sdr/AU990804), Jul 26, 1999: GCU. FAULTY. (AUS) NR 2 AC BUS FAILED. GENERATOR CONTROL UNIT REPLACED.
- [SDR A6WA9900049](https://openairdocs.org/sdr/A6WA9900049), May 29, 1999: ANGLE. CRACKED. FORWARD PASSENGER DOOR, INTERNAL ANGLE CRACKED. REPLACED ANGLE. (X)
- [SDR A6WA9900048](https://openairdocs.org/sdr/A6WA9900048), May 29, 1999: SKIN. DAMAGED. REPAIR TO RIGHT SIDE OF FUSELAGE AT FRAMES 11-13 AT LAP 'E' AREA. C/W REPAIR IAW BAE 146 SRM AND FAX CW/RJ/0754-99, CW/RJ/0761-99 AND DRAWING HC537H9411. (X)
- [SDR AU990524](https://openairdocs.org/sdr/AU990524), May 28, 1999: SPOILER. FAULTY. (AUS) MANUAL SPOILER CAUTION LIGHT ILLUMINATED AFTER TAKEOFF. THE FAULT WAS UNABLE TO BE REPRODUCED ON THE GROUND AND THE AIRCRAFT HAS SINCE FLOWN SERVICEABLE. 
- [SDR AU990512](https://openairdocs.org/sdr/AU990512), May 28, 1999: WARNING SYSTEM. ILLUMINATED. (AUS) MANUAL SPOILER FAULT LIGHT ILLUMINATED. INVESTIGATION COULD FIND NO DEFECT. PCB CHX6 RE-RACKED.
- [SDR A6WA9900054](https://openairdocs.org/sdr/A6WA9900054), May 7, 1999: STIFFENER. CRACKED. LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER NR 176 BEWEEN RIBS 7 AND 8 CRACKED, FORWARD END. REPLACED LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENE
- [SDR A6WA9900053](https://openairdocs.org/sdr/A6WA9900053), May 7, 1999: STIFFENER. CRACKED. RIGHT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 176 BETWEEN RIBS 7 AND 8, CRACKED FORWARD END. REPAIRED RT WING TRAILING EDGE UPPER SHROUD SKIN STIFFEN
- [SDR A6WA9900052](https://openairdocs.org/sdr/A6WA9900052), May 7, 1999: STIFFENER. CRACKED. RIGHT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 172 BETWEEN RIBS 3 AND 4, CRACKED FORWARD END. REPLACED RT WING TRAILING EDGE UPPER SHROUD SKIN STIFFEN
- [SDR A6WA9900051](https://openairdocs.org/sdr/A6WA9900051), May 7, 1999: STIFFENER. CRACKED. LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 178 BETWEN RIBS 8 AND 9, CRACKED FORWARD END. REPLACED LT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER
- [SDR 17WA9900050](https://openairdocs.org/sdr/17WA9900050), May 7, 1999: STIFFENER. CRACKED. LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER NR 177 BETWEEN RIBS 8 AND 9 CRACKED FORWARD END. REPAIRED LEFT WING SKIN TRAILING EDGE, UPPER WING SKIN TRAI
- [SDR AU990442](https://openairdocs.org/sdr/AU990442), May 6, 1999: TRANSDUCER. MALFUNCTIONED. (AUS) NR 3 ENGINE OIL PRESSURE TRANSDUCER FAULTY.
- [SDR AU990423](https://openairdocs.org/sdr/AU990423), May 4, 1999: SWITCH. FAULTY. (AUS) AIR CONDITIONING PACK FLOW SWITCH FAULTY.
- [SDR A6WA9900055](https://openairdocs.org/sdr/A6WA9900055), Apr 21, 1999: STIFFENER. CRACKED. UPPER WING SKIN TRAILING EDGE STIFFENER IS CRACKED AT FORWARD END LOCATED BETWEEN RIBS 9 AND 10, LEFT WING. REPAIRED LT WING SKIN TRAILING EDGE UPPER WING SKIN 
- [SDR AU990415](https://openairdocs.org/sdr/AU990415), Apr 7, 1999: FLOORBEAM. CRACKED. (AUS) CRACKS FOUND IN FLOOR BEAM AT FRAME 18 LOCATED ON THE RIGHT SIDE JUST BELOW THE FLOOR LINE.
- [SDR 99ZZZX2700](https://openairdocs.org/sdr/99ZZZX2700), Jan 1, 1999: SLIDE. DEPLOYED. ORD - FLT 545 - WHILE INSPECTING GIVE BAR MECHANISM ON FORWARD PASSENGER DOOR, SLIDE PARTIALLY DEPLOYED. REMOVED AND REPLACED FORWARD PASSENGER DOOR SLIDE IAW M
- [SDR 99ZZZM548](https://openairdocs.org/sdr/99ZZZM548), Jan 1, 1999: SLIDE. OUT OF POSITION. WHILE INSPECTIONG GIVE BAR MECHANISM ON FORWARD PASSENGER DOOR SLIDE PARTIALLY DEPLOYED. REMOVED AND REPLACED FORWARD PASSENGER DOOR SLIDE IAW MM. (M)
- [SDR AU981563](https://openairdocs.org/sdr/AU981563), Nov 22, 1998: LINK. CORRODED. (AUS) MAIN LANDING GEAR DOOR RT AND LT FORWARD HINGE LINKS CORRODED BEYOND LIMITS. LINKS P/N HC321H0026-002, P/N HC321B0045-002, AND P/N HC321B0043-001.
- [SDR AU981461](https://openairdocs.org/sdr/AU981461), Nov 7, 1998: SENSOR. MALFUNCTIONED. (AUS) EFT MAIN LANDING GEAR UPLOCK PROXIMITY SENSOR FAULTY.
- [SDR AU981205](https://openairdocs.org/sdr/AU981205), Sep 21, 1998: WARNING SYSTEM. ACTIVATED. (AUS) MANUAL SPOILER FAULT LIGHT ILLUMINATED. SYSTEM CHECKED, BUT NO REASON FOR THE FAULT COULD BE FOUND. DEFECT HAS NOT OCCURRED SINCE.

All 188: https://openairdocs.org/model/british-aerospace-bae-146-series-100a/reports.md

## STCs that may be installed (OpenAirDocs) (37)

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 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 ST02080CH](https://openairdocs.org/stc/ST02080CH): Installation of VHF-3 Antenna Structural Provisions. 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 ST00261DE-D](https://openairdocs.org/stc/ST00261DE-D): Installation of dual AlliedSignal GNS-XLs Flight Management System. 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 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 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 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 ST01855AT](https://openairdocs.org/stc/ST01855AT): Installation of a Corporate Interior. Innotech Aviation
- [STC ST00460LA](https://openairdocs.org/stc/ST00460LA): Installation of global positioning navigation system. Memphis International Inc
- [STC ST09387SC](https://openairdocs.org/stc/ST09387SC): Installation of dual Universal UNS-1K flight management system. Advanced Avionics Technologies
- [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 ST09121SC](https://openairdocs.org/stc/ST09121SC): Installation of a Safeflight Reactive Windshear System Model 6508. Advanced Avionics Technologies
- [STC SA3440NM](https://openairdocs.org/stc/SA3440NM): Installation of floor proximity emergency escape path marking system. Intl Valve Co
- [STC ST00609AT](https://openairdocs.org/stc/ST00609AT): Installation of 100 passenger interior. British Aerospace, Inc. Lists BAe 146 Series
- [STC SA4040NM](https://openairdocs.org/stc/SA4040NM): Installation of Foster AirData TCN 970 TACAN equipment. Aspen Airways Inc

## PMA parts (OpenAirDocs) (722, 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
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149749463320250923105932.0001): VOGT AERO · PMA PQ05310NM · Mar 4, 2025
- [3575-1251-05-VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103095121220260729202805.0001): Immersion Stick Heater Assy. Vogt Aero LLC · PMA PQ05310NM · Replaces 3575-1251-05 · Mar 4, 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
- [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
- [APMHC251H0317-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129822720920240301165906.0001): Visor, Sun. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces HC251H0317-002 · 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
- [APMHC251H0317-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156061612120231212163818.0001): Visor, Sun. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces HC251H0317-002 · 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

All of them: https://openairdocs.org/model/british-aerospace-bae-146-series-100a/pma.md

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