# Airbus Industrie A300 B4-203

- Type: Aircraft model (FAA registry)
- Registry code: 3930306
- Manufacturer (registry): AIRBUS INDUSTRIE
- Model: A300 B4-203
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 341
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Data sheet: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) (OpenAirDocs)
- Holder: Airbus SAS
- Registered aircraft: 0
- Page: https://openairdocs.org/model/airbus-industrie-a300-b4-203

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 2025-19-06](https://openairdocs.org/ad/2025-19-06): Doors · Conversion of Passenger to Freighter configuration (Airbus Deutschland STC ST00100NY or 3 others). Effective Oct 31, 2025
- [AD 2025-16-05](https://openairdocs.org/ad/2025-16-05): Wings · Airbus A300 B4-2C, A300 B4-203, A300 B4-603 and 4 more. Effective Sep 22, 2025
- [AD 2025-01-07](https://openairdocs.org/ad/2025-01-07): Wings · Airbus A300 B4-2C, A300 B4-103, A300 B4-203 and 9 more. Effective Mar 11, 2025
- [AD 2024-19-15](https://openairdocs.org/ad/2024-19-15): Oxygen · Safran Aerosystems Oxygen Cylinder, Valve Assembly, Oxygen Valve and 103 more. Effective Nov 26, 2024
- [AD 2024-11-01](https://openairdocs.org/ad/2024-11-01): Electrical Power · Airbus A300 B4-2C, A300 B4-103, A300 B4-203 and 94 more. Effective Jul 3, 2024
- [AD 2024-08-08](https://openairdocs.org/ad/2024-08-08): Electrical Power · Airbus A300 B4-2C, A300 B4-103, A300 B4-203 and 94 more. Effective Jun 6, 2024
- [AD 2023-25-04](https://openairdocs.org/ad/2023-25-04): Time Limits/Maintenance · Airbus A300 B4-2C, A300 B4-103 and A300 B4-203. Effective Jan 17, 2024
- [AD 2016-15-01 R1](https://openairdocs.org/ad/2016-15-01-R1): Flight controls · Airbus A300 B2-1A, A300 B2-1C, A300 B2K-3C and 21 more. Effective Jun 23, 2023
- [AD 2023-07-12](https://openairdocs.org/ad/2023-07-12): Time Limits/Maintenance Checks · Airbus A300 B2-1A, A300 B2-1C, A300 B2K-3C and 4 more. Effective May 30, 2023
- [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 2023-02-07](https://openairdocs.org/ad/2023-02-07): Hydraulic power · Airbus A300 B2K-3C, A300 B2-203, A300 B4-2C and 1 more. Effective Mar 14, 2023
- [AD 2022-25-08](https://openairdocs.org/ad/2022-25-08): Windows · Airbus A300 B2-1A, A300 B2-1C, A300 B2K-3C and 21 more. Effective Jan 20, 2023
- [AD 2022-21-02](https://openairdocs.org/ad/2022-21-02): Fuselage · Airbus A300 B2-1C, A300 B2K-3C, A300 B2-203 and 8 more. Effective Dec 14, 2022
- [AD 2022-20-08](https://openairdocs.org/ad/2022-20-08): Fuselage · Airbus A300 B2K-3C, A300 B2-203, A300 B4-2C and 1 more. Effective Nov 25, 2022
- [AD 2022-05-06](https://openairdocs.org/ad/2022-05-06): Time Limits/Maintenance Checks · Airbus A300 B2-1C, A300 B2K-3C, A300 B2-203 and 3 more. Effective Apr 4, 2022
- [AD 2022-01-08](https://openairdocs.org/ad/2022-01-08): Hydraulic power · Airbus A300 B2-1A, A300 B2K-3C, A300 B2-1C and 21 more. Effective Mar 8, 2022
- [AD 2021-11-18](https://openairdocs.org/ad/2021-11-18): Landing Gear · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Jul 16, 2021
- [AD 2020-01-14](https://openairdocs.org/ad/2020-01-14): Hydraulic power · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 4 more. Effective Feb 28, 2020
- [AD 2019-19-07](https://openairdocs.org/ad/2019-19-07): Flight controls · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Nov 5, 2019
- [AD 2019-18-04](https://openairdocs.org/ad/2019-18-04): Stabilizers · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Oct 30, 2019
- [AD 2019-15-08](https://openairdocs.org/ad/2019-15-08): Fuselage · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Sep 19, 2019
- [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 2018-19-07](https://openairdocs.org/ad/2018-19-07): Landing Gear · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Nov 13, 2018
- [AD 2018-19-17](https://openairdocs.org/ad/2018-19-17): Time Limits/Maintenance Checks · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 4 more. Effective Oct 29, 2018
- [AD 2018-18-19](https://openairdocs.org/ad/2018-18-19): Time limits/maintenance checks · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Oct 23, 2018
- [AD 2018-18-18](https://openairdocs.org/ad/2018-18-18): Time Limits/Maintenance Checks · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 4 more. Effective Oct 23, 2018
- [AD 2018-17-16](https://openairdocs.org/ad/2018-17-16): Wings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Oct 2, 2018
- [AD 2017-25-09](https://openairdocs.org/ad/2017-25-09): Fuel · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Jan 18, 2018
- [AD 2017-21-07](https://openairdocs.org/ad/2017-21-07): Navigation · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 4 more. Effective Nov 27, 2017
- [AD 2017-19-12](https://openairdocs.org/ad/2017-19-12): Fuel · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Oct 24, 2017
- [AD 2017-17-05](https://openairdocs.org/ad/2017-17-05): Fuselage · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Sep 25, 2017
- [AD 2017-16-06](https://openairdocs.org/ad/2017-16-06): Fuselage · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Sep 22, 2017
- [AD 2017-12-06](https://openairdocs.org/ad/2017-12-06): Doors · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Jul 25, 2017
- [AD 2017-10-05](https://openairdocs.org/ad/2017-10-05): Wings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Jun 29, 2017
- [AD 2017-08-13](https://openairdocs.org/ad/2017-08-13): Fuselage · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective May 30, 2017
- [AD 2017-05-01](https://openairdocs.org/ad/2017-05-01): Fuselage · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 4 more. Effective Apr 7, 2017
- [AD 2017-04-05](https://openairdocs.org/ad/2017-04-05): Doors; Fuselage; Nacelles/pylons;Stabilizers; and Wings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 4 more. Effective Mar 28, 2017
- [AD 2017-02-08](https://openairdocs.org/ad/2017-02-08): Wings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 11 more. Effective Mar 17, 2017
- [AD 2016-25-15](https://openairdocs.org/ad/2016-25-15): Fuselage · Airbus A300 B2-1C, A300 B2-203, A300 B2K-3C and 3 more. Effective Jan 23, 2017
- [AD 2016-20-08](https://openairdocs.org/ad/2016-20-08): Wings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Nov 22, 2016
- [AD 2016-19-10](https://openairdocs.org/ad/2016-19-10): Nacelles/pylons · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 20 more. Effective Oct 31, 2016
- [AD 2016-18-08](https://openairdocs.org/ad/2016-18-08): Wings · Airbus A300 B2-1C, A300 B2-203, A300 B2K-3C and 8 more. Effective Oct 20, 2016
- [AD 2016-18-12](https://openairdocs.org/ad/2016-18-12): Nacelles/Pylons · Airbus A300 B4-203 and A300 B4-2C. Effective Oct 13, 2016
- [AD 2016-13-08](https://openairdocs.org/ad/2016-13-08): Wings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Aug 9, 2016
- [AD 2016-05-05](https://openairdocs.org/ad/2016-05-05): Fuselage · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Apr 13, 2016
- [AD 2016-01-10](https://openairdocs.org/ad/2016-01-10): Fuselage · Airbus A300 B4-103, A300 B4-203, A300 B4-2C and 9 more. Effective Mar 10, 2016
- [AD 2015-25-06](https://openairdocs.org/ad/2015-25-06): Nacelles/Pylons · Airbus A300 B2-1C, A300 B2-203, A300 B2K-3C and 17 more. Effective Feb 2, 2016
- [AD 2015-22-05](https://openairdocs.org/ad/2015-22-05): Landing Gear · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Dec 17, 2015
- [AD 2015-15-02](https://openairdocs.org/ad/2015-15-02): Electrical Power · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Aug 28, 2015
- [AD 2015-12-05](https://openairdocs.org/ad/2015-12-05): Wings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Jul 21, 2015

Historical (superseded or no longer in force):

- [AD 2023-13-11](https://openairdocs.org/ad/2023-13-11) (historical): Oxygen · AVOX Systems Oxygen valve assemblies (body and gage assemblies), Oxygen cylinder and valve assemblies, A300 B2-1A and 102 more. Effective Sep 5, 2023
- [AD 2022-11-01](https://openairdocs.org/ad/2022-11-01) (historical): Wings · Airbus A300 B2-1A, A300 B2-1C, A300 B2K-3C and 13 more. Effective Jul 5, 2022
- [AD 2022-08-04](https://openairdocs.org/ad/2022-08-04) (historical): Time Limits/Maintenance Checks · Airbus A300 B2-1A, A300 B2-1C, A300 B2K-3C and 4 more. Effective Jun 16, 2022
- [AD 2022-04-09](https://openairdocs.org/ad/2022-04-09) (historical): Oxygen System · Airbus A300 B2-1A, A300 B2-1C, A300 B2K-3C and 94 more. Effective Apr 4, 2022
- [AD 2020-23-11](https://openairdocs.org/ad/2020-23-11) (historical): Fuselage; Wings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Jan 4, 2021
- [AD 2019-03-10](https://openairdocs.org/ad/2019-03-10) (historical): Landing Gear · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Mar 29, 2019
- [AD 2017-07-05](https://openairdocs.org/ad/2017-07-05) (historical): Landing Gear · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Apr 17, 2017
- [AD 2016-15-01](https://openairdocs.org/ad/2016-15-01) (historical): Flight controls · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Aug 26, 2016
- [AD 2014-13-17](https://openairdocs.org/ad/2014-13-17) (historical): Fuel · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Aug 19, 2014
- [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013
- [AD 2012-21-04](https://openairdocs.org/ad/2012-21-04) (historical): Fuel · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Nov 27, 2012
- [AD 2012-15-14](https://openairdocs.org/ad/2012-15-14) (historical): Wings · Airbus A300 B4-103, A300 B4-203, A300 B4-2C and 9 more. Effective Sep 11, 2012
- [AD 2012-13-06](https://openairdocs.org/ad/2012-13-06) (historical): Electrical Power · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Aug 14, 2012
- [AD 2012-08-03](https://openairdocs.org/ad/2012-08-03) (historical): Wings · Airbus A300 B4-103, A300 B4-203, A300 B4-2C and 17 more. Effective May 29, 2012
- [AD 2011-17-05](https://openairdocs.org/ad/2011-17-05) (historical): Fuselage · Airbus A300 B2-1C, A300 B2-203, A300 B2K-3C and 3 more. Effective Nov 16, 2011
- [AD 2011-10-17](https://openairdocs.org/ad/2011-10-17) (historical): Doors, Fuselage, Nacelles/pylons, Stabilizers, Wings, and Powerplant · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Jun 17, 2011
- [AD 2010-23-26](https://openairdocs.org/ad/2010-23-26) (historical): Wings · Airbus A300 B2-1C, A300 B2-203, A300 B2K-3C and 10 more. Effective Jan 5, 2011
- [AD 2010-06-05](https://openairdocs.org/ad/2010-06-05) (historical): Fuselage · Airbus A300 B4-103, A300 B4-203, A300 B4-2C and 6 more. Effective Apr 15, 2010
- [AD 2010-06-04](https://openairdocs.org/ad/2010-06-04) (historical): Nacelles/Pylons · Airbus A300 B2-1C, A300 B2-203, A300 B2K-3C and 17 more. Effective Apr 15, 2010
- [AD 2009-18-15](https://openairdocs.org/ad/2009-18-15) (historical): Landing gear · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Oct 27, 2009
- [AD 2008-06-18](https://openairdocs.org/ad/2008-06-18) (historical): Lower skin panel · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Apr 23, 2008
- [AD 2007-25-15](https://openairdocs.org/ad/2007-25-15) (historical): Main landing gear (MLG) · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Jan 14, 2008
- [AD 2007-04-11](https://openairdocs.org/ad/2007-04-11) (historical): Inspection intervals, and repairs; and repair of any damaged, cracked, or corroded structure. · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 4 more. Effective Apr 3, 2007
- [AD 2007-03-18](https://openairdocs.org/ad/2007-03-18) (historical): Wing main landing gear (MLG) · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Feb 23, 2007
- [AD 2006-12-13](https://openairdocs.org/ad/2006-12-13) (historical): Main landing gear (MLG) attachment fittings at the lower flange · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Jul 18, 2006
- [AD 2005-17-14](https://openairdocs.org/ad/2005-17-14) (historical): Rudder servo actuators · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Sep 30, 2005
- [AD 2004-23-20](https://openairdocs.org/ad/2004-23-20) (historical): Fuselage attachment holes · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 11 more. Effective Jan 3, 2005
- [AD 2004-20-14](https://openairdocs.org/ad/2004-20-14) (historical): Fuselage frame (FR) 47 between stringers 24 and 25 · Airbus A300 B4-103, A300 B4-203, A300 B4-2C and 7 more. Effective Nov 17, 2004
- [AD 2002-07-05](https://openairdocs.org/ad/2002-07-05) (historical): Frame 40 Aft Fittings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 10 more. Effective May 14, 2002
- [AD 2002-08-51](https://openairdocs.org/ad/2002-08-51) (historical): Thrust Reverser · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 4 more. Effective May 6, 2002
- [AD 2000-23-07](https://openairdocs.org/ad/2000-23-07) (historical): Autotrim Function · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Dec 20, 2000
- [AD 2000-20-15](https://openairdocs.org/ad/2000-20-15) (historical): Fuselage Frame · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Nov 15, 2000
- [AD 2000-12-12](https://openairdocs.org/ad/2000-12-12) (historical): Nacelle Pylon · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Jul 28, 2000
- [AD 2000-10-18](https://openairdocs.org/ad/2000-10-18) (historical): Pylons Lower Spar Axis · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Jun 30, 2000
- [AD 2000-02-39](https://openairdocs.org/ad/2000-02-39) (historical): Longitudinal Skin Splice Cracking above Mid-Passenger Door Panels · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 11 more. Effective Feb 22, 2000
- [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 95-24-04](https://openairdocs.org/ad/95-24-04) (historical): Rear Spar Web · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 11 more. Effective Dec 27, 1995
- [AD 95-21-09](https://openairdocs.org/ad/95-21-09) (historical): Inspect For Cracks No. 2 Flap Beams · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 11 more. Effective Nov 17, 1995
- [AD 90-11-05](https://openairdocs.org/ad/90-11-05) (historical): Shroud Box Brackets · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 4 more. Effective Jun 19, 1990
- [AD 90-03-08](https://openairdocs.org/ad/90-03-08) (historical): Inspect For Cracks & Corrosion · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 4 more. Effective Feb 23, 1990
- [AD 90-01-10](https://openairdocs.org/ad/90-01-10) (historical): Longitudinal Lap Joints · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 4 more. Effective Feb 5, 1990

All 312: https://openairdocs.org/model/airbus-industrie-a300-b4-203/ads.md

## Information bulletins (advisory) (2)

- [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-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 DCA06WA036](https://openairdocs.org/ntsb/DCA06WA036), May 2, 2006: Airbus A-300-B4 (N372PC), Toronto, Canada, incident, minor damage
- [NTSB MIA88IA176](https://openairdocs.org/ntsb/MIA88IA176), May 23, 1988: Airbus Industrie A-300 (N209PA), Near San Juan, PR, incident, no damage

## FAA accident and incident reports (5)

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 20060801020419I](https://openairdocs.org/incident/20060801020419I), Aug 1, 2006: Airbus A300B4203 (N365DH), Wilmington, OH, Minor damage. (-23) Crew received a hot brake annunciation during take-off roll at 140KIAS. V1 speed was 152KIAS. Crew elected to reject take-off. Aircraft remained on…
- [Incident 20060501009049I](https://openairdocs.org/incident/20060501009049I), May 1, 2006: Airbus A300B4203 (N372PC), Toronto, CN, Minor damage. (-23) Express net airlines operated an Airbus A-300-B4203 aircraft (N372PC) from dayton, Ohio usa (kday) to Toronto, Canada (cyyz). While on approach into…
- [Incident 20050210004379I](https://openairdocs.org/incident/20050210004379I), Feb 10, 2005: Airbus A300B4203 (N502TA), Indianapolis, IN. (-23) Pilot item: #7 brake over 700 deg. C after landing. #7 tire deflated due to fusable plug melting. Note! Fire and rescue responded due to #7 wheel and…
- [Incident 20010221005369I](https://openairdocs.org/incident/20010221005369I), Feb 21, 2001: Airbus A300B4203 (N474AS), Fort Wayne, IN. (-23) Landing gear would not retract after takeoff. A/c returned to Fort Wayne. Landed without incident. Maintenance serviced nose gear centering strut, a/c…
- [Incident 19951216043759I](https://openairdocs.org/incident/19951216043759I), Dec 16, 1995: Airbus A300B4203 (N226KW), Los Angeles, CA, Minor damage. Narrative: on 16 December 1995, at approximately 13:30 local time at lax, an A-300 owned and operated by carnival air lines, inc. was being pushed back from…

## Service difficulty reports (1,357, newest 50)

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

- [SDR WRNA201200006](https://openairdocs.org/sdr/WRNA201200006), May 11, 2012: GYRO. UNSERVICEABLE. BOTH NR 1 & NR 2 YAW DAMPERS WOULD NOT ENGAGE. AIRCRAFT RETURNED TO AIRFIELD. LANDING NORMAL. MX FOUND NR 1 & NR 2 YAW RATE GYRO'S AT FAULT. REMOVED AND REPLACE
- [SDR WRNA201110210010](https://openairdocs.org/sdr/WRNA201110210010), Oct 21, 2011: GPS. MALFUNCTIONED. NR 1 GPS MESSAGE "HEADING REQUIRED" RENDERING, GPS AND NR 1 AUTOPILOT INOPERATIVE. VECTORED SO ACFT STAYED ON HEADING MODE. AUTOPILOT NR 2 SELECTED BUT DID NOT 
- [SDR WRNA2009004](https://openairdocs.org/sdr/WRNA2009004), Dec 30, 2009: PITOT LINE. CLOGGED. ON TAKEOFF ROLL, DEPARTING FROM SJU, CREW NOTICED THAT THERE WAS NO AIRSPEED INDICATION FROM F/O INDICATOR. CAPTAIN INDICATOR SHOWING BETWEEN 75-80 KTS AND FLUC
- [SDR DHLA200900025](https://openairdocs.org/sdr/DHLA200900025), Apr 14, 2009: COALESCER BAG. DIRTY. REPLACED NR 2 COALESCER P/N 20D10-3 IAW MM 21-51-16. THIS DOES NOT CLOSE DMI.
- [SDR DHLA200900021](https://openairdocs.org/sdr/DHLA200900021), Apr 1, 2009: UNKNOWN. ODOR. ACFT HAS AN UNUSUAL ODOR COMING THRU THE A/C PACKS FLT DECK DUCT TEMP WAS AT 150 COMPT TEMP 68. RAN NR 1 AND NR 2 PACK SYS OPS CKED NORMAL ON GROUND IAW AMM 21-
- [SDR WRNA2009001](https://openairdocs.org/sdr/WRNA2009001), Mar 17, 2009: GROUND WIRE. LOOSE. AFTER TAKEOFF, KRUEGER FLAP FAILED TO RETRACT. CREW REPORTED A "CONFIG" LIGHT ON MWP. ALSO, FLIGHT CHARACTERISTICS OF AIRCRAFT SEEMED DIFFERENT. DECISION MADE T
- [SDR DHLA200800011A](https://openairdocs.org/sdr/DHLA200800011A), Feb 12, 2009: ENGINE. POWER LOSS. DURING T/O ENG. 1 & 2 SPOOLED TO 60% N1, GO LEVERS SELECTED NR 1 ENG SPOOLED TO 80% N1 MAX, THROTTLE FULL FORWARD NO RESPONSE. OAT +5º C TAS LESS THAN 60KTS. RE
- [SDR WRN2009F00000](https://openairdocs.org/sdr/WRN2009F00000), Dec 19, 2008: FIRE LOOP. DEFECTIVE. ENGINE NR 1 SHUT DOWN IN FLIGHT DUE TO A FIRE INDICATION DURING FLIGHT FROM BDL TO BQN. BOTH FIRE BOTTLES WERE DISCHARGED. WARNING LIGHT EXTINGUISHED. ACFT LAND
- [SDR DHLA200800137](https://openairdocs.org/sdr/DHLA200800137), Dec 15, 2008: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS BATTERIES 0 VOLTS.
- [SDR DHLA200800108](https://openairdocs.org/sdr/DHLA200800108), Sep 30, 2008: BATTERY PACK. INOPERATIVE. ON PRE-DEPARTURE CHECK, EMERGENCY LIGHT OVER R1 DOOR INOPERATIVE, ACFT GROUNDED. R&R POWER SUPPLY IAW MM 33-51-14. OPS CHECKED OK IAW 33-51-00.
- [SDR DHLA200800107](https://openairdocs.org/sdr/DHLA200800107), Sep 30, 2008: BATTERY PACK. INOPERATIVE. ON PRE-DEPARTURE CHECK, EMERGENCY LIGHT OVER R1 DOOR INOPERATIVE, ACFT GROUNDED. R&R POWER SUPPLY IAW MM 33-51-14. OPS CHECKED OK IAW 33-51-00.
- [SDR DHLA200800106](https://openairdocs.org/sdr/DHLA200800106), Sep 30, 2008: POWER SUPPLY. INOPERATIVE. ON PRE-DEPARTURE CHECK, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE, ACFT GROUNDED. R&R POWER SUPPLY IAW MM 33-51-14. OPS CHECKED GOOD IAW 33-51-00.
- [SDR WRN2008F00004](https://openairdocs.org/sdr/WRN2008F00004), Jun 23, 2008: SILL. FOD. AC AFTER TAKEOFF, LOUD WHISTLING NOISE HEARD AND AC HAD PROBLEMS PRESSURIZING. AC MADE UNSCHEDULED STOP, WITH NORMAL LANDING. FOUND F.O.D. AND DEBRIS IN MAIN CA
- [SDR WRN2008F00003](https://openairdocs.org/sdr/WRN2008F00003), Jun 18, 2008: INDICATOR. UNSERVICEABLE. DURING CRUISE, ENG NR1 EGT OFF SCALE HIGH INDICATION. POINTER AT 6 O`CLOCK POSITION. POINTER AND DIGITAL READOUT AGREED. AMBER EGT LIGHT ON, ENGINE EGT LIGHT ON
- [SDR WRN2008F00002](https://openairdocs.org/sdr/WRN2008F00002), Jun 16, 2008: VALVE. STUCK. AFTER TAKEOFF, PRESSURIZATION MALFUNCTION OCCURRED. ACCOMPLISHED ABNORMAL PROCEDURES. AC RETURNED TO FIELD. LANDING NORMAL. MX FOUND GROUND VENT VALVE STUCK CLO
- [SDR WRN2008F00001](https://openairdocs.org/sdr/WRN2008F00001), Jun 16, 2008: CONNECTOR. DIRTY. AFTER TAKEOFF, APPROX 40 MINUTES INTO FLIGHT, AC TURNED BACK DUE TO NAV PROBLEMS WITH GPS SYSTEM. GPS SYS NR 2 PREVIOUSLY MEL, NR 1 GPS SYS WENT TO DR MODE. AIR
- [SDR WRN2008F00000](https://openairdocs.org/sdr/WRN2008F00000), Jun 7, 2008: GEARBOX. CONTAMINATED. ON CLIMBOUT STJ FL230, OIL QTY DECREASING RAPIDLY. PERFORMED PRECAUTIONARY SHUTDOWN PROCEDURES, OIL PRESSURE WAS NOT LOST, OIL TEMP RISE TO 130 DEGREES. REPLACE
- [SDR WRNA20080039](https://openairdocs.org/sdr/WRNA20080039), May 26, 2008: CONTROL VALVE. FAULTY. DURING APPROACH TO BQN, LANDING GEAR FAILED TO EXTEND WITH SYSTEM 1 OR 2, RETURNED TO 2,000 FEET TO HOLD WHILE LOWERING GEAR MANUALLY. AFTER SUCCESSFUL EXTENSIO
- [SDR WRNA20080038](https://openairdocs.org/sdr/WRNA20080038), May 2, 2008: UPLOCK. UNSERVICEABLE. AFTER TAKEOFF, NOSE LANDING GEAR FAILED TO RETRACT. DUMPED FUEL AND RETURNED TO FIELD FOR A SAFE LANDING. REPLACED NOSE GEAR UP-LOCK ASSY IAW MM 32-31-14 PG 401
- [SDR WRNA200800037](https://openairdocs.org/sdr/WRNA200800037), Apr 29, 2008: CSD. MALFUNCTIONED. DURING FLIGHT, NR 1 CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY RISING OIL TEMPERATURE. DISCONNECTED CSD AND RETURNED TO MFM FOR A SAFE 
- [SDR WRNA20080011](https://openairdocs.org/sdr/WRNA20080011), Apr 8, 2008: SLIDE. NO TEST. DURING OPERATIONAL TEST, THE R-1 DOOR ESCAPE SLIDE/RAFT FAILED TEST, DID NOT FULLY INFLATE. REPLACED ESCAPE SLIDE/RAFT CONTACTED MAINTENANCE STATION WERE TEST W
- [SDR WRNA20080010](https://openairdocs.org/sdr/WRNA20080010), Apr 8, 2008: DUCT. CRACKED. AFTER TAKEOFF, NR 1 AND NR 2 BLEED FAULT LIGHTS AND APU MANIFOLD LIGHTS CAME ON AND WOULD NOT RESET. DUMPED 18,000 POUNDS OF FUEL AND RETURNED TO FIELD FOR A SA
- [SDR WRNA20080009](https://openairdocs.org/sdr/WRNA20080009), Mar 28, 2008: PIN. DISCONNECTED. DURING DAILY CHECK, MAINTENANCE FOUND R1 EMERGENCY EXIT LIGHTS INOP. FOUND PIN NR 3 DISCONNECTED FROM LIGHT ASSY, RECONNECTED, OPS CHECKED GOOD. AIRCRAFT RELEAS
- [SDR WRNA200800014](https://openairdocs.org/sdr/WRNA200800014), Mar 26, 2008: SKIN. CORRODED. DURING M96 CHECK, FOUND OUT OF LIMIT CORROSION ON FUSELAGE AT STR 6 TO FRAME 76. CUT OUT DAMAGED AREA 2.75 INCHES BY .75 INCHES AND INSTALLED FILLER FABRICATED 
- [SDR DHLA200800035](https://openairdocs.org/sdr/DHLA200800035), Mar 18, 2008: APU. LEAKING. BEFORE FLIGHT 102 ON GROUND IN SFO, 3 CABIN SMOKE DETECTORS ILLUMINATED ON THE GROUND. ON INSP FOUND APU TO BE LEAKING OIL. INGESTED INTAKE, SMOKE DET OK IAW AM
- [SDR WRNA200800006](https://openairdocs.org/sdr/WRNA200800006), Mar 16, 2008: ENGINE. FAILED. AFTER TAKEOFF FROM MFM, CLIMBING THROUGH 15,000 FEET A LOUD EXPLOSION WAS HEARD FROM NR 1 ENGINE FOLLOWED BY SEVERE VIBRATION, ENGINE WAS RETARDED TO IDLE POWER
- [SDR WRNA200800022](https://openairdocs.org/sdr/WRNA200800022), Mar 3, 2008: SEAT TRACK. CRACKED. DURING M96 CHECK, MAIN CABIN SEAT TRACK AT FRAME 40 RBL 54 WAS FOUND CRACKED. REPLACED SEAT TRACK AT RBL 54 FROM FRAME 40 TO FRAME 44 +12 INCHES IAW SRM 53-10-1
- [SDR DHLA200800019](https://openairdocs.org/sdr/DHLA200800019), Mar 1, 2008: BOTTLE. READS LOW. R1 DOOR ESCAPE SLIDE PRESSURE IN RED. REMOVED AND REPLACED SLIDE ASSY. AIRCRAFT WAS GROUNDED.
- [SDR WRNA200800020](https://openairdocs.org/sdr/WRNA200800020), Feb 28, 2008: TRACK. CORRODED. DURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD ZL-150-L403-501, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN AFT CARGO COMPARTMENT AT FRAME 57. REMOVE
- [SDR WRNA200800019](https://openairdocs.org/sdr/WRNA200800019), Feb 28, 2008: TRACK. CORRODED. DURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD Z:-150-L403-5-01, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN AFT CARGO COMPARTMENT BETWEEN FRAMES 58 
- [SDR WRNA200800021](https://openairdocs.org/sdr/WRNA200800021), Feb 28, 2008: TRACK. CORRODED. DURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD ZL-150-L403-501, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN AFT CARGO COMPARTMENT AT FRAMES 54 TO 57.
- [SDR WRNA200800018](https://openairdocs.org/sdr/WRNA200800018), Feb 26, 2008: SKIN. CORRODED. DURING M96 CHECK, WHEN ACCOMPLISHING CPCP TASK CARD 55-2007-0602-1-01 SEVERAL AREAS OF CORROSION WERE FOUND OUT OF LIMITS ON LT ELEVATOR SKIN FROM CENTER LINE R
- [SDR WRNA200800017](https://openairdocs.org/sdr/WRNA200800017), Feb 26, 2008: SEAT TRACK. CORRODED. DURING M96 CHECK, WHEN ACCOMPLISHING CPCP TASK CARD ZL-220-L403-9-01, CABIN SEAT TRACK WAS FOUND CORRODED AT FRAME 13B - 14C LBL 55. REMOVED AND REPLACED SEAT T
- [SDR WRNA200800016](https://openairdocs.org/sdr/WRNA200800016), Feb 26, 2008: SKIN. DAMAGED. DURING M96 CHECK, A 8 INCH BY 2 INCH CUT WAS FOUND IN SKIN BETWEEN FRAME 51 AND 52 AT STRINGER 36R TO 39R AFT OF RMLG DOOR CUT OUT. INSTALLED SKIN REPAIR DOUBLE
- [SDR WRNA200800023](https://openairdocs.org/sdr/WRNA200800023), Feb 23, 2008: ATTACH FITTING. CORRODED. DURING M96 CHECK, CORROSION WAS FOUND OUT OF LIMITS ON NR 3 (FROM OUTBOARD END) LEFT ELEVATOR ATTACH HINGE AT BONDING WIRE ATTACH POINT. REPLACED HINGE ATTACH I
- [SDR WRNA200800003](https://openairdocs.org/sdr/WRNA200800003), Jan 25, 2008: DAMPER. FAILED. AFTER TAKEOFF FROM IND, GEAR FAILED TO RETRACT ON BOTH SYSTEM A AND B, DIVERTED TO GSO, DUMPED APPROX 15,000 POUNDS OF FUEL AND MADE A SAFE LANDING. FOUND LEFT 
- [SDR DHLA200800004](https://openairdocs.org/sdr/DHLA200800004), Jan 10, 2008: UPLOCK SWITCH. MALFUNCTIONED. FLT 165, RIGHT MAIN GEAR DOOR DID NOT RETRACT AFTER GEAR EXTENDED. ABNORMAL PROCEDURE ACCOMPLISHED. CLEANED AND RESECURED RT MLG INBD DOOR UPLOCK SWITCHES, OPER
- [SDR DHLA200800003](https://openairdocs.org/sdr/DHLA200800003), Jan 6, 2008: SKIN. DAMAGED. LOWER FORWARD CARGO DOOR FUSELAGE LOWER FORWARD FRAME IS SCUFFED. DEFERRED IAW GMM 3.5 CAT I & LETTER REF. 942-057506/014/2008 ACCEPTABLE FOR 10 F.C. PLACARD IN
- [SDR WRNA200700064](https://openairdocs.org/sdr/WRNA200700064), Dec 28, 2007: DAMPER. MALFUNCTIONED. AFTER DEPARTURE WHEN RAISING GEAR, LEVER WOULD NOT GO PAST THE MID POSITION, GEAR POSITION LIGHTS REMAINED 'GREEN'. RETURNED TO FIELD AND MADE A SAFE LANDING. A
- [SDR DHLA200700095](https://openairdocs.org/sdr/DHLA200700095), Dec 27, 2007: POWER SUPPLY. NO TEST. EMERGENCY EXIT LIGHT OVER THE R1 WILL NOT TEST. REPLACED R1 EMERGENCY LIGHT POWER SUPPLY AS PER MM 33-51-14. OPS NORM.
- [SDR WRNA200700062](https://openairdocs.org/sdr/WRNA200700062), Dec 18, 2007: B-NUT. LOOSE. AFTER LEVELING OFF AT 27,000' OBSERVED STEADY DECLINE IN OIL QUANTITY OF NUMBER 1 ENGINE, RETURNED TO FIELD AND MADE A SAFE LANDING, NO LOSS OF OIL PRESSURE. FO
- [SDR DHLA200700081](https://openairdocs.org/sdr/DHLA200700081), Dec 12, 2007: AUTOBRAKE SYS. MALFUNCTIONED. DURING ROLL OUT WITH AUTOBRAKES ENGAGE (MIN) AFTER PRESSING BRAKES AUTO BRAKES CONTINUED TO BRAKE THE AIRCRAFT EVEN WITH THE AUTO BRAKE OFF LIGHT ILLUMINATED AN
- [SDR DHLA200700079](https://openairdocs.org/sdr/DHLA200700079), Dec 8, 2007: SEQUENCE VALVE. MALFUNCTIONED. UPON GEAR RETRACTION, RT MAIN GEAR WOULD NOT RETRACT. UNSAFE LIGHT AND GEAR DOOR LIGHTS BOTH ILLUMINATED. PERFORMED LANDING GEAR UNSAFE INDICATION ABNORMAL PROC
- [SDR DHLA200700067](https://openairdocs.org/sdr/DHLA200700067), Nov 23, 2007: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT DISARM WARNING DOES NOT ILLUMINATE. REPLACED LIGHT BULBS ON DISARM CAPSULE PER MM 33-51-00. OPS TEST OK.
- [SDR WRNA200700060](https://openairdocs.org/sdr/WRNA200700060), Oct 31, 2007: DUCT. BROKEN. DURING TAKE OFF, NR 2 ENGINE EGT EXCEEDED 960 C, POWER WAS REDUCED BELOW TAKEOFF SETTING, EGT DROPPED BELOW 945 C. DURING CLIMB, NR 2 ENGINE MANIFOLD PRESS 10 P
- [SDR WRNA200700058](https://openairdocs.org/sdr/WRNA200700058), Oct 23, 2007: LINE. OBSTRUCTED. DURING TAKEOFF ROLL, FIRST OFFICERS AIR SPEED LAGGED BEHIND CAPTAINS BY 40-60 KNOTS, ABORTED TAKEOFF. FLUSHED DEBRIS FROM PITOT PRESSURE LINES, ACCOMPLISHED PIT
- [SDR WRNA200700057](https://openairdocs.org/sdr/WRNA200700057), Oct 23, 2007: PITOT TUBE. LEAKING. DURING TAKEOFF THE FIRST OFFICERS AIRSPEED INDICATOR LAGGED 40-60 KNOTS BEHIND CAPTAINS AIRSPEED INDICATOR. FOUND RT PITOT PROBE LEAKING, REPLACED RT PITOT PROB
- [SDR WRNA200700051](https://openairdocs.org/sdr/WRNA200700051), Oct 18, 2007: CIRCUIT BREAKER. WEAK. AFTER TAKEOFF, FUEL PUMP NR 1; 1A; 2 CIRCUIT BREAKERS POPPED, AND AFCS AND FLIGHT ENGINEER PANEL LIGHTS WENT OFF. RETURNED TO FIELD AND MADE A SAFE LANDIBG. REP
- [SDR DHLA200700053](https://openairdocs.org/sdr/DHLA200700053), Oct 12, 2007: HYDRAULIC SYSTEM. CONTAMINATED. WITH ANTI-SKID IN ON /ALT THE LEFT BRAKES GRAB AND PULL AIRCRAFT TO THE LEFT. BLED BRAKING SYS GREEN AND YELLOW AND OPS CK NORMAL PER MM 32-42-00.
- [SDR WRNA200700065](https://openairdocs.org/sdr/WRNA200700065), Oct 11, 2007: BULKHEAD. CRACKED. DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD AT STR TIE END ANGLE FITTING AT 35R. FABRIC

All 1,357: https://openairdocs.org/model/airbus-industrie-a300-b4-203/reports.md

## STCs that may be installed (OpenAirDocs) (145, 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 ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC SA3481NM](https://openairdocs.org/stc/SA3481NM): Installation of C&D closet. Safran Cabin Inc
- [STC SA3400NM](https://openairdocs.org/stc/SA3400NM): Installation of floor proximity emergency escape path marking system. Bruce Aerospace Inc. Lists A300 Series
- [STC ST01999AT](https://openairdocs.org/stc/ST01999AT): This installation adds three recording parameters (pitch control, lateral control, and rudder) to the existing A300 and A310 Digital Flight Data Recorder (DFDR) to meet the requirements of 14 CFR 121.344. Acron Aviation 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 ST00982CH](https://openairdocs.org/stc/ST00982CH): Installation of dual Universal Avionics UNS-1C GPS Flight Management Systems. Amphenol Cable and Interconnect Technologies Inc
- [STC ST01113CH](https://openairdocs.org/stc/ST01113CH): Installation of dual Universal Avionics UNS-1K GPS flight management systems. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01233CH](https://openairdocs.org/stc/ST01233CH): Installation of dual Honeywell Super Attitude heading Reference Systems (SAHRS). Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01235CH](https://openairdocs.org/stc/ST01235CH): Installation of dual Honeywell HT-9100 GPS flight management systems. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01430CH](https://openairdocs.org/stc/ST01430CH): Installation of Universal Avionics System Corporation Electronic Horizontal Situation Indicators. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01694CH](https://openairdocs.org/stc/ST01694CH): Installation of Honeywell International Enhanced Ground Proximity Warning System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00691SE](https://openairdocs.org/stc/ST00691SE): Installation of lightweight window plugs. LiteAir Aviation Products Inc
- [STC ST02691AT](https://openairdocs.org/stc/ST02691AT): Installation of SAF-T-GLO Inc. Photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC ST02302CH](https://openairdocs.org/stc/ST02302CH): Install ERDA model 7004 HI-LO table with slide top. Collins Aerospace
- [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 ST02022AT](https://openairdocs.org/stc/ST02022AT): Installation of a Dual Canadian Marconi CMA-900 Flight Management System. Woven Electronics, LLC
- [STC ST02297AT](https://openairdocs.org/stc/ST02297AT): This installation added three additional parameters to be recorded by the existing Flight Data Recorder. Woven Electronics LLC
- [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [STC SA3025SO](https://openairdocs.org/stc/SA3025SO): Installation of dual TRA-67A Mode S transponder system. Honeywell International Inc
- [STC SA3026SO](https://openairdocs.org/stc/SA3026SO): Installation Of an CAS-81 TCAS II system. Honeywell International Inc
- [STC ST00181SE](https://openairdocs.org/stc/ST00181SE): Installation of Model 4033, 4034 and 4038 Transient Suppression Units. Honeywell International Inc
- [STC ST00783AT](https://openairdocs.org/stc/ST00783AT): Installation of a dual RDR-4B Weather Radar/Windshear System. Honeywell International Inc
- [STC ST02010AT](https://openairdocs.org/stc/ST02010AT): Installation of a RTA-83A VHF Communication System. Honeywell International Inc
- [STC SA5672SW-D](https://openairdocs.org/stc/SA5672SW-D): Modification of air to air heat exchanger (P/N 187900-9). Honeywell International Inc
- [STC SA8947SW](https://openairdocs.org/stc/SA8947SW): Replace core assembly of AiResearch Bleed Air Precooler, part number 189120-1 and -3. Honeywell International Inc
- [STC SA7565SW](https://openairdocs.org/stc/SA7565SW): Rebuild A300 Auxiliary Power Unit Oil Cooler Assembly by manufacturing a new core assembly. Honeywell International Inc. Lists A300 Series
- [STC SA4821NM](https://openairdocs.org/stc/SA4821NM): Installation of a Hughes-Avicom video entertainment system. Burrana Inc. Lists A300 Series
- [STC SA3483NM](https://openairdocs.org/stc/SA3483NM): Installation of Trans Com video projection system. Burrana Inc. Lists A300 Series
- [STC ST03574AT](https://openairdocs.org/stc/ST03574AT): Installation of a Talon Aerospace Anti-Collision Light. Aaxico Technical Services Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC SA6082NM](https://openairdocs.org/stc/SA6082NM): Installation of audio entertainment system. Burrana Inc. Lists A300 B4 Series
- [STC ST04092NY](https://openairdocs.org/stc/ST04092NY): Installation of Wireless PCMCIA for DFDAU. Delta Engineering Corporation
- [STC ST02686LA](https://openairdocs.org/stc/ST02686LA): Installation of an alternate part number. Honeywell International Inc
- [STC ST04372NY](https://openairdocs.org/stc/ST04372NY): Installation of saf-Tglo® SSUL23 Photoluminescent Aisle Path Marking System. STG Aerospace Ltd
- [STC ST04049NY](https://openairdocs.org/stc/ST04049NY): Installation of a Hoffman Engineering LLC LED Landing Light to replace the OEM Q4559 Series Incandescent Lamp, used as a Landing/Takeoff Light. Hoffman Engineering LLC
- [STC ST00855LA](https://openairdocs.org/stc/ST00855LA): Installation of ANCRA main deck cargo handling system. Ancra International LLC. Lists A300 B4 Series
- [STC ST04345NY](https://openairdocs.org/stc/ST04345NY): Upgrade from TCAS II software version 7.0 to 7.1. PMV Engineering
- [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 ST09962SC](https://openairdocs.org/stc/ST09962SC): Installation of X-Band nose radome shell assembly. The NORDAM Group LLC
- [STC ST01215AT-D](https://openairdocs.org/stc/ST01215AT-D): Installation of Collins SAT-906 SATCOM System with Canadian Marconi CMA-2102 antenna system. TIMCO. Lists A300 Series
- [STC ST01223AT-D](https://openairdocs.org/stc/ST01223AT-D): Installation of Airshow 210 System with Dual RADVR and with Airshow Provisions. HAECO Cabin Solutions LLC
- [STC ST01361AT-D](https://openairdocs.org/stc/ST01361AT-D): Installation of Dual Mode "S" Transponders. HAECO Cabin Solutions LLC
- [STC ST03848NY](https://openairdocs.org/stc/ST03848NY): Installation of SuperSeal UltraLite (SSUL) PHOTOLUMINESCENT AISLE PATH MARKING SYSTEM. STG Aerospace Ltd
- [STC ST02639LA](https://openairdocs.org/stc/ST02639LA): Replace the existing Mode S Transponder system. Aviation Communication and Surveillance Systems (ACSS) LLC

All 145: https://openairdocs.org/model/airbus-industrie-a300-b4-203/stcs.md

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