# British Aerospace BAE 146 SERIES 300A

- Type: Aircraft model (FAA registry)
- Registry code: 1500267
- Manufacturer (registry): BRITISH AEROSPACE
- Model: BAE 146 SERIES 300A
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 4 · Turbo-jet
- Seats: 100
- 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-300a

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 2010-02-11](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 2009-15-08](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
- [AD 2006-07-22](https://openairdocs.org/ad/2006-07-22): Left bulkhead structure · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective May 16, 2006
- [AD 2006-05-10](https://openairdocs.org/ad/2006-05-10): Left and right main landing gear (MLG) doors · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more. Effective Apr 13, 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 164: https://openairdocs.org/model/british-aerospace-bae-146-series-300a/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 (2)

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 CHI95IA079](https://openairdocs.org/ntsb/CHI95IA079), Jan 27, 1995: British Aerospace BAE-146-300 (N611AW), Madison, WI, incident, no damage. Probable cause: A fuel leak in the no. 2 engine left fuel manifold segment due to a design defect which led to a fatigue crack.
- [NTSB CHI93IA312](https://openairdocs.org/ntsb/CHI93IA312), Jul 21, 1993: British Aerospace 146-300A (N611AW), Chicago, IL, incident, minor damage. Probable cause: was a crack in the fuel system fuel flow distribution manifold which resulted from an inadequate design by the manufacturer.

## FAA accident and incident reports (4)

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 19960513019109I](https://openairdocs.org/incident/19960513019109I), May 13, 1996: Bag BAE146300A (N612AW), Denver, CO. Narrative: aircraft was dispatched from springfield, IL (sgf) with #14800 of fuel. Crew confirmed the fuel on board, per their statements. Over goodland, KS…
- [Incident 19920310008439I](https://openairdocs.org/incident/19920310008439I), Mar 10, 1992: Bag BAE146300A (N614AW), Cedar Rapids, IA. Unable to lower gear on approach. After orbiting airport gear extended and locked spontaneously. Landed safely.
- [Incident 19910325011989I](https://openairdocs.org/incident/19910325011989I), Mar 25, 1991: Bac 146300A (N616AW), Huntsville, AL, Minor damage. Four main tires blew on rollout. Appears brake selector not in correct position. Back up system failed,brakes locked
- [Incident 19901017051659I](https://openairdocs.org/incident/19901017051659I), Oct 17, 1990: Bac 146300A (N615AW), Cedar Rapids, IA. Unable to retract gear. Returned. Replaced electrical rotary actuator.

## Service difficulty reports (481, newest 50)

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

- [SDR AU510002205](https://openairdocs.org/sdr/AU510002205), Dec 12, 2005: HOSE. FAILED. NOSE LANDING GEAR RETRACTION ACTUATOR FLEXIBLE HYDRAULIC HOSE RUPTURED. LOSS OF GREEN SYSTEM HYDRAULIC FLUID.
- [SDR AU510001941](https://openairdocs.org/sdr/AU510001941), Dec 12, 2005: FRAME. CRACKED. (AUS) FUSELAGE FRAME 41 AND FRAME 43 CRACKED. FOUND DURING INSPECTION IAW AD/BAE146/116. (OTHER CAUSE: MATERIAL ) (CASA NR 510001941)
- [SDR AU510001940](https://openairdocs.org/sdr/AU510001940), Dec 12, 2005: FRAME. CRACKED. (AUS) FUSELAGE FRAME 43 CRACKED. FOUND DURING INSPECTION IAW AD/BAE146/116. (OTHER CAUSE: MATERIAL ) (CASA NR 510001940)
- [SDR AU510001797](https://openairdocs.org/sdr/AU510001797), Dec 12, 2005: JACKSHAFT. CORRODED. (AUS) LT CENTER AND RT OB LIFT SPOILER JACKS CORRODED BEYOND LIMITS IN PISTON THREADS FOR EYE ENDS. FOUND DURING INSPECTION IAW AAES ER BA6-27-60-23B AND BAE SY
- [SDR AU510001750](https://openairdocs.org/sdr/AU510001750), Dec 12, 2005: INDICATOR. DAMAGED. (AUS) AIRCRAFT EXPERIENCED A HIGH SINK RATE DURING LANDING. INVESTIGATION FOUND THAT THE MAIN LANDING GEAR AND TAILSKID CONTACTED THE GROUND CAUSING DAMAGE TO T
- [SDR AU510001495](https://openairdocs.org/sdr/AU510001495), Dec 12, 2005: SELECTOR. FAILED. LANDING GEAR SELECTOR LEVER WOULD NOT MOVE TO THE `UP` POSITION.
- [SDR AU510001709](https://openairdocs.org/sdr/AU510001709), Oct 8, 2005: WIRE. SHORTED. RT INNER FUEL BOOST PUMP PRESSURE SWITCH TO PRINTED CIRCUIT BOARD WIRE SHORT CIRCUITED.
- [SDR AU510001967](https://openairdocs.org/sdr/AU510001967), Jun 10, 2005: BOLT. SHEARED. CENTER FUEL TANK WING SPAR ATTACHMENT BOLTS (4OFF) HAD SHEAR BOLT HEADS. FUEL LEAKING FROM CENTER TANK AT RT FRONT CORNER ABOVE THE WING TO FUSELAGE ATTACHMENT 
- [SDR AU510001664](https://openairdocs.org/sdr/AU510001664), Feb 8, 2005: HINGE. CORRODED. RT MAIN LANDING GEAR DOOR HINGE FITTINGS CORRODED IN BORES. BEARING HOUSINGS ALSO CONTAINED PITTING AND RUST DEPOSITS ON THE OUTER SURFACES. FOUND DURING INSPEC
- [SDR A6WA200460066](https://openairdocs.org/sdr/A6WA200460066), Dec 30, 2004: ACM. ODOR. NR 2 PACK WAS INADVERTENTLY SWITCHED ON FOR APPROX 10 MINUTES ENROUTE. PILOTS NOTICED ODOR IN COCKPIT, PACK SWITCHED OFF AND A PUFF OF WHITE SMOKE CAME OUT OF V
- [SDR A6WA200460054](https://openairdocs.org/sdr/A6WA200460054), Nov 10, 2004: OXYGEN MASK. MISSING. ROWS 14 AND 16 DEF HAVE NR O2 MASKS INSTALLED IN PSU BOXES. MAINTENANCE INSTALLED PASSENGER ALL O2 MASKS AS REQUIRED IAW 35-20-45.
- [SDR AUS20040512](https://openairdocs.org/sdr/AUS20040512), Jun 15, 2004: RIB. CRACKED. (AUS) NR 1, NR 3 AND NR 4 PYLONS HAD NR 4 RIB CRACKED IN THE LOWER FLANGE RADIUS. PYLON NR 1, CRACK LENGTH 22.86MM (0.9IN) PYLON NR 3, CRACK LENGTH 12.7MM (0.5I
- [SDR AUS20040501](https://openairdocs.org/sdr/AUS20040501), Jun 10, 2004: FIREWALL. CRACKED. (AUS) APU FIREWALL CRACKED AT 7 O'CLOCK POSITION. FOUND DURING INSPECTION IAW AD/BAE146/053.
- [SDR A6WA200460019](https://openairdocs.org/sdr/A6WA200460019), Jun 2, 2004: SKIN. SCRATCHED. AFT CARGO DOOR SCRATCHES BEYOND THE ALLOWABLE SRM LIMITS. MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS. MAINTENANCE CUT DAMAGED AREA OUT IAW BAE SRM 52-32-11 F
- [SDR A6WA200460016](https://openairdocs.org/sdr/A6WA200460016), May 26, 2004: FLOORBEAM. CRACKED. CRACK LOCATED IN THE LOWER RADIUS OF FLOORBEAM 33B AT LBL 62.0 INCHES. MAINTENANCE REQUESTED REPAIRS FROM MFG SYSTEMS REF AVMAX FAX 611-1908002. REPAIRED IAW BA
- [SDR AUS20040444](https://openairdocs.org/sdr/AUS20040444), May 20, 2004: COMPUTER. FAULTY. (AUS) FLAP COMPUTER FAULTY.
- [SDR AUS20040429](https://openairdocs.org/sdr/AUS20040429), May 17, 2004: LINK. FRACTURED. (AUS) MAIN LANDING GEAR ASSISTOR JACK TRIANGULAR LINK FAILED AT JACK ATTACHMENT POINT.
- [SDR AUS20040410](https://openairdocs.org/sdr/AUS20040410), May 17, 2004: INTERCOSTAL. CORRODED. (AUS) AFT CABIN FLOOR INTERCOSTAL CONTAINED LEVEL 2 CORROSION ON THESIDE AND UPPER SURFACES. THE INTERCOSTAL DAMAGE WAS LOCATED INZONE 251 BETWEEN FRAMES 41 AND
- [SDR AUS20040405](https://openairdocs.org/sdr/AUS20040405), May 17, 2004: FRAME. CORRODED. (AUS) LT FUSELAGE FRAME 43 CONTAINED LEVEL 2 CORROSION ON THE FORWARD FACE AT FLOOR LEVEL. DAMAGE WAS LOCATED AT ZONE 20 FRAME 43 STA 726.9 AND WAS 38.1MM (1.5I
- [SDR AUS20040401](https://openairdocs.org/sdr/AUS20040401), May 17, 2004: ACTUATOR. SEIZED. (AUS) RT NR 2 LIFT SPOILER ACTUATOR SPINDLE SEIZED IN LOCKED POSITION WITH THE ACTUATOR EXTENDED. FOUND DURING INSPECTION IAW AD/BA6-27-60-16D BAE MANDATORY ISB
- [SDR A6WA200460014](https://openairdocs.org/sdr/A6WA200460014), May 9, 2004: FUEL CONTROL. FLUCTUATES. WHILE IN VMC CLIMBING THROUGH 16000 FEET THE NR 3 ENGINE N1 FLUCTUATION FOLLOWED BY FUEL FLOW DROPPING TO ZERO. ENGINE WAS SHUTDOWN, REMAINDER OF FLT MIN N2 OF 
- [SDR AUS20040372](https://openairdocs.org/sdr/AUS20040372), May 7, 2004: ANGLE. CORRODED. (AUS) RT REAR ENTRY SILL PLATE ATTACHMENT ANGLE CONTAINED LEVEL 2 CORROSION ON THE UPPER SURFACE. AREA OF CORROSION 48.26MM (1.9IN) LONG BY 20.8MM (0.82IN) WIDE
- [SDR AUS20040351](https://openairdocs.org/sdr/AUS20040351), May 6, 2004: SEAT TRACK. CORRODED. (AUS) SEAT TRACKS CORRODED. PN HC538J0343-001 RT IB SEAT TRACK FOUND CORRODED ON UPPER SURFACE. CORROSION MEASURES 106.68MM (4.2IN) LENGTH, 24.13MM (0.95IN) WID
- [SDR AUS20040345](https://openairdocs.org/sdr/AUS20040345), May 6, 2004: BOLT. CORRODED. (AUS) FORWARD OUTER ATTACHMENT SPECIAL BOLT SHAFT CORRODED AND PLATING MISSING. CORROSION WAS LOCATED APPROXIMATELY 12.7MM (0.5IN) DOWN FROM THE BOLT HEAD. AREA
- [SDR AUS20040379](https://openairdocs.org/sdr/AUS20040379), May 5, 2004: SEAT TRACK. CORRODED. (AUS) CABIN FLOOR STRUCTURE CONTAINED LEVEL 2 CORROSION IN THE FOLLOWING AREAS: PN HC536H1063-001 RT OB SEAT TRACK END ON UPPER SURFACE. AREA OF CORROSION MEASU
- [SDR AUS20040357](https://openairdocs.org/sdr/AUS20040357), May 5, 2004: FRAME. CRACKED. (AUS) CABIN CROWN FRAME TO SKIN STRUCTURE ANGLE CLEATS (8OFF) CRACKED FROM BEND RADIUS EDGE. THE ANGLE CLEATS ARE LOCATED IN FOLLOWING AREAS: FRAME 19A BETWEEN 
- [SDR AUS20040339](https://openairdocs.org/sdr/AUS20040339), May 5, 2004: PLATE. CORRODED. (AUS) INSP OF REAR CABIN WET AREA AT FLOOR LEVEL FOUND CORROSION IN FOLLOWING PLATES: SHEAR PLATE PN HC538H1183-000 LOCATED ON TOP OF LONGITUDINAL BEAM FRAME 43
- [SDR A6WA200460012](https://openairdocs.org/sdr/A6WA200460012), Apr 12, 2004: ANGLE. CRACKED. FOUND CRACK IN THE NR 4 PYLON AT THE FORWARD END OF THE CENTER ANGLE JUST AFT OF RIB NR 3. REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 615-18830001. (M)
- [SDR AUS20040237](https://openairdocs.org/sdr/AUS20040237), Mar 31, 2004: PIN. CRACKED. (AUS) FAIL SAFE PIN ASSEMBLY OF THE RT FLAP TAB NR 2 HINGE BOLT CRACKED. FOUND DURING NDT INSPECTION.
- [SDR AUS20040148](https://openairdocs.org/sdr/AUS20040148), Mar 3, 2004: PLATE. CORRODED. (AUS) RT ELEVATOR TAB NR 1 HINGE UPPER REINFORCEMENT PLATE CONTAINED LEVEL 2 CORROSION. CORROSION DIMENSIONS WERE 25.4MM (1IN) BY50.8MM (2IN) AND PENETRATING TO
- [SDR AUS20040129](https://openairdocs.org/sdr/AUS20040129), Feb 26, 2004: BOLT. CRACKED. (AUS) RUDDER FIXED HINGE BOLT CRACKED UNDER BOLT HEAD. BOLT IS LOCATED AT VERTICAL STABILISER RIB 5. CRACK LENGTH 2.286MM (0.090IN). FOUND DURING NDT INSPECTION
- [SDR AUS20040065](https://openairdocs.org/sdr/AUS20040065), Feb 5, 2004: HARNESS. FAULTY. (AUS) NR 4 ENGINE FIRE WARNING SYSTEM WIRING HARNESS FAULTY.
- [SDR AUS20031342](https://openairdocs.org/sdr/AUS20031342), Dec 12, 2003: DISPLAY. WRONG PART. (AUS) ELECTRONIC DISPLAY UNIT (EDU) WAS INCORRECT PART. MANUFACTURERS AME PLATE WAS IN RED WHICH INDICATED THAT IT WAS AN ENGINEERING EVALUATION UNIT. THE AIRWO
- [SDR A6WA200360044](https://openairdocs.org/sdr/A6WA200360044), Oct 2, 2003: SKIN. LIGHTNING STRIKE. DAMAGE NOTED ON LEFT SIDE OF FUSELAGE DURING LIGHTNING STRIKE INSPECTION. EXIT BURN MARK LOCATED 8 INCHES AFT OF FRAME 19C BETWEEN STRINGER 21 AND 22 AT CENTER 
- [SDR AUS20030929](https://openairdocs.org/sdr/AUS20030929), Sep 12, 2003: GCU. FAILED. (AUS) NR 1 GENERATOR CONTROL UNIT (GCU) FAILED.
- [SDR AUS20030922](https://openairdocs.org/sdr/AUS20030922), Sep 10, 2003: HOSE. RUPTURED. (AUS) LT MLG RETRACTION JACK FLEXIBLE HYDRAULIC HOSE RUPTURED. LOSS OF GREEN SYSTEM HYD FLUID.
- [SDR AUS20030830](https://openairdocs.org/sdr/AUS20030830), Aug 17, 2003: SEAL. FAILED. (AUS) LT GROUND SPOILER FLOW VALVE RETURN LINE CONNECTOR O-RING SEAL LEAKING. GRADUAL LOSS OF APPROXIMATELY TEN LITRES OF HYDRAULIC FLUID.
- [SDR AUS20030555](https://openairdocs.org/sdr/AUS20030555), Jun 4, 2003: SKIN. CORRODED. (AUS) LT AND RT LOWER WING SKINS CORRODED IN AREA OF FUEL PUMP WATER SCAVENGE GUARDS AT RIB 15. FOUND DURING INSPECTION IAW ER BA6-28-10-7 AND ISB 28-028.
- [SDR AUS20030410](https://openairdocs.org/sdr/AUS20030410), Apr 9, 2003: SPEED BRAKE. FAULTY. (AUS) UNCOMMANDED AIRBRAKE OPERATION. EXTENSIVE INVESTIGATION AND TESTING COULD FIND NO CAUSE FOR THE PROBLEM.
- [SDR AUS20030363](https://openairdocs.org/sdr/AUS20030363), Mar 23, 2003: PIN. DAMAGED. (AUS) LT MAIN LANDING GEAR DIRECTIONAL LINK UPPER ATTACHMENT PIN FOUND TO BE MIGRATING FROM THE LUG LOCATED AT FRAME 29. LOCKING PLATE AND PIN INCORRECTLY FITTE
- [SDR AUS20030121](https://openairdocs.org/sdr/AUS20030121), Feb 6, 2003: SKIN. CORRODED. (AUS) RT LOWER WING SKIN CHAFED ON WATER SCAVENGE PIPE DEBRIS GUARDS. CORROSION WAS ALSO FOUND IN THE SAME AREA BETWEEN FRAME 14 AND FRAME 15.
- [SDR AUS20030120](https://openairdocs.org/sdr/AUS20030120), Feb 6, 2003: SKIN. CORRODED. (AUS) LT WING LOWER SKIN CORRODED BEYOND LIMITS. FOUND DURING X-RAY INSPECTION.
- [SDR AUS20021456](https://openairdocs.org/sdr/AUS20021456), Dec 28, 2002: WIRE. WORN. (AUS) NR 4 GENERATOR DIFFERENTIAL PROTECTION CIRCUIT WIRE XB108 CHAFED IN AREA ADJACENT TO IDG.
- [SDR AUS20021452](https://openairdocs.org/sdr/AUS20021452), Dec 10, 2002: CIRCUIT BOARD. FAULTY. (AUS) RT MAIN LANDING GEAR UPLOCK SENSOR PRINTED CIRCUIT BOARD (GJ21) FAULTY.
- [SDR AUS20021338](https://openairdocs.org/sdr/AUS20021338), Nov 15, 2002: CABLE. CHAFED. (AUS) NR 4 THROTTLE LEVER CABLE FOULING ON CENTER ROOF PANEL. PREVIOUS MAINTENANCE HAD BEEN CARRIED OUT FOR BATTERY PACK REPLACEMENT. PERSONNEL/MAINTENANCE ERRO
- [SDR AUS20021184](https://openairdocs.org/sdr/AUS20021184), Oct 18, 2002: MANIFOLD. LEAKING. (AUS) NR 3 ENGINE RT FUEL MANIFOLD LEAKING AT MANIFOLD TO COMBUSTOR CASE JOIN. EVIDENCE OF FIRE AROUND LEAK.
- [SDR A6WA200260044](https://openairdocs.org/sdr/A6WA200260044), Oct 10, 2002: FLOOR SUPPORT. CORRODED. CORROSION FOUND ON FLOOR SUPPORT STRUCTURE FRAME 15 - 2.5 INCH PORT OF AIRCRAFT CENTERLINE RIL.
- [SDR AUS20021106](https://openairdocs.org/sdr/AUS20021106), Oct 7, 2002: COOLING FAN. FAILED. (AUS) LT ELECTRONIC FLIGHT INDICATION SYSTEM (EFIS) FAN FAILED. INVESTIGATION FOUND FAN BLADE CRACKED AND RUBBING ON GRILL.
- [SDR AUS20020714](https://openairdocs.org/sdr/AUS20020714), Jul 6, 2002: BRAKE. OVERHEATED. (AUS) BOTH LT MAIN LANDING GEAR BRAKES OVERHEATED TO 800 DEGREES C.
- [SDR AUS20020591](https://openairdocs.org/sdr/AUS20020591), Jun 13, 2002: BUSS. FAILED. (AUS) NR 2 AC BUS FAILED. THE FOLLOWING COMPONENTS WERE REPLACED:- 1. NR 4 GENERATOR CONTROL UNIT 2. GENERATOR LINE CONTACTOR 4XB33. NR 4 ENGINE GENERATOR AND C

All 481: https://openairdocs.org/model/british-aerospace-bae-146-series-300a/reports.md

## STCs that may be installed (OpenAirDocs) (29)

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 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 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 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 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 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 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 ST00579CH](https://openairdocs.org/stc/ST00579CH): Installation of a GTE Airfone Public Telephone System (Genstar). U.S. Technical Consultants 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 ST00705LA](https://openairdocs.org/stc/ST00705LA): Installation of Honeywell Traffic Alert and Collision Avoidance System (TCAS II). ACSS (Aviation Communication and Surveillance Syst
- [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 ST00609AT](https://openairdocs.org/stc/ST00609AT): Installation of 100 passenger interior. British Aerospace, Inc. Lists BAe 146 Series

## PMA parts (OpenAirDocs) (631, 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-300a/pma.md

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