# Airbus A300 B4-103

- Type: Aircraft model (FAA registry)
- Registry code: 3940020
- Manufacturer (registry): AIRBUS
- Model: A300 B4-103
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 343
- 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-a300-b4-103

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 2025-01-07](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 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 2022-05-06](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 2016-13-08](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
- [AD 2015-06-05](https://openairdocs.org/ad/2015-06-05): Fuselage · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective May 1, 2015
- [AD 2015-03-03](https://openairdocs.org/ad/2015-03-03): Fuel · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Apr 6, 2015
- [AD 2015-02-24](https://openairdocs.org/ad/2015-02-24): Wings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Mar 17, 2015
- [AD 2015-02-19](https://openairdocs.org/ad/2015-02-19): Wings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 12 more. Effective Mar 11, 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 304: https://openairdocs.org/model/airbus-a300-b4-103/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

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (38)

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

- [SDR DHL2001362019](https://openairdocs.org/sdr/DHL2001362019), Jun 8, 2001: COMPUTER. MALFUNCTIONED. NR 1 AUTOPILOT WOULD NOT ENGAGE. RESET NR 1 LOGIC MONITOR COMPUTER GROUND CHECKS GOOD PER M/M 22-10-00.
- [SDR DHL2001363006](https://openairdocs.org/sdr/DHL2001363006), Jun 8, 2001: COMPUTER. MALFUNCTIONED. AUTOPILOT NR 1 WILL NOT ENGAGE. RESEATED ALL THREE A/P, F/O COMPUTERS. NR 1 A/P OP CHECKS GOOD PER M/M 22-10-00. NO FAULTS IN SELF TEST.
- [SDR DHL2001362018](https://openairdocs.org/sdr/DHL2001362018), May 30, 2001: COMPUTER. FAULTY. PRIOR TO LEVEL OFF, A/P NR 1 DISENGAGED, UPON RE-ENGAGEMENT, CAPT FPI INDICATES NORMAL. HOWEVER, A/C DIDN'T CAPTURE ALT. DISENGAGED A/P AND FLEW BACK TO LEVEL. 
- [SDR DHL2001362017](https://openairdocs.org/sdr/DHL2001362017), May 30, 2001: SWITCH. LOOSE. INFLIGHT SPEED BRAKE ANNUNCIATOR LIGHT REMAINED ILLUMINATED WITH HANDLE STOWED. RECYCLED SPEED BRAKES FOUR TIMES TO GET ANNUNCIATOR TO EXTINGUISH. FOUND MICROSW
- [SDR DHL2001362016](https://openairdocs.org/sdr/DHL2001362016), May 30, 2001: AUTOPILOT SYS. MALFUNCTIONED. AUTOPILOT HAS DIFFICULTY MAINTAINING ALTITUDE PLUS OR MINUS 200 FT WITH CONFIGURATION CHANGES IE, FLAPS 0 DEGREE TO FLAPS 8 DEGREE. RESEATED NR 1 AND 2 ADC ALTI
- [SDR DHL2001362014](https://openairdocs.org/sdr/DHL2001362014), May 9, 2001: TRANSFORMER. FAILED. ESS TR OFF LIGHT ILLUMINATED DURING FLIGHT. CREW PERFORMED ABNORMAL PROCEDURE BY AOM. REMOVED AND REPLACED ESS T/R AS PER MM 24-32-11. OPS CHECKED GOOD
- [SDR DHL2001362012](https://openairdocs.org/sdr/DHL2001362012), Apr 28, 2001: AUTOTHRUST SYS. MALFUNCTIONED. AUTO THROTTLE DOES NOT WORK IN THE N1 MODE. DEFERRED N1 PER MEL 22-31-01. PLACARD INSTALLED. UNABLE TO DUPLICATE PROBLEM. AUTO THROTTLE N1 MODE CHECKS NORMAL IA
- [SDR DHL2001362013](https://openairdocs.org/sdr/DHL2001362013), Apr 28, 2001: CONTROLLER. FAILED. AUTO PILOT WILL NOT ENGAGE. DEFERRED NR 1 AP PER MEL 22-11-01. PLACARD INSTALLED. R&R AUTOPILOT CONT MODULE IAW M/M CH 22-11-12. OPS CHECK GOOD.
- [SDR DHL2001362011](https://openairdocs.org/sdr/DHL2001362011), Apr 14, 2001: AUTOPILOT SYS. FAILED. NR 1 AUTOPILOT WILL NOT ENGAGE, NR 2 A/P OPERATES NORMALLY. DEFERRED NR 1 AUTOPILOT AS PER MEL 22-11-01.
- [SDR DHL2001363004](https://openairdocs.org/sdr/DHL2001363004), Apr 14, 2001: COMPUTER. FAILED. AUTOPILOTS NR 1 AND NR 2 TRIPPED OFF REPEATEDLY DURING APPROACH. AFCS SHOWS BOTH LOGIC MONITOR COMPUTERS TRIPPED. RESET AFCS AND RESEATED BOTH LOGIC MONITOR COM
- [SDR DHL2001362010](https://openairdocs.org/sdr/DHL2001362010), Apr 4, 2001: COMPUTER. MALFUNCTIONED. AUTO PILOT NUMBER ONE WILL NOT ENGAGE IN MAN, OR CMD MODES. REPLACED NR 1 AP/FD LOGIC & MONITOR COMP WITH A SERV. UNIT. OPS CK IS GOOD IAW MM 22-13-34. COMPUTER
- [SDR DHL2001362009](https://openairdocs.org/sdr/DHL2001362009), Mar 26, 2001: SKIN. DENTED. RT FUSELAGE FWD OF LOWER CARGO DOOR FRAME 1383 SKIN SURFACE HAS A DENT (ADJACENT AFT OF ICE LIGHT). E&E COMP, RT AFT OF AC BATTS, REPOSITIONED FOR SM ACCESS, RE
- [SDR DHL2001362007](https://openairdocs.org/sdr/DHL2001362007), Mar 6, 2001: SPOILER. MALFUNCTIONED. DURING FLIGHT CONTL CHK, RT SPOILER ONLY INDICATES 7 DEG DEFLECTION. TRANSFERRED TO DMI 4626 PER MEL 27-15-01-1 CAT B, SPECIAL PROCEDURE COMPLIED WITH.
- [SDR DHL2001362008](https://openairdocs.org/sdr/DHL2001362008), Mar 6, 2001: SPOILER. MALFUNCTIONED. DURING FLIGHT CONTL CHK, RT SPOILER ONLY INDICATES 7 DEG DEFLECTION. TRANSFERRED TO DMI 4626 PER MEL 27-15-01-1 CAT B, SPECIAL PROCEDURE COMPLIED WITH.
- [SDR DHL2001362006](https://openairdocs.org/sdr/DHL2001362006), Feb 20, 2001: ALTIMETER. FAILED. DURING TAXI-OUT, FLAG INST ON MWP WITH CAPTAINS OFF FLAG ON ALTIMETER. REMOVED AND REPLACED CAPT ALTIMETER INDICATOR. OPS CHECK OK PER MM 34-11-30.
- [SDR DHL2001362005](https://openairdocs.org/sdr/DHL2001362005), Feb 10, 2001: CONTROL UNIT. MALFUNCTIONED. NR 1 FUEL FLOW VARIES BETWEEN 6000 TO 20000 LBS. NR 2 FUEL FLOW VARIES BETWEEN 6000 TO 22000. ALL OTHER ENG INDICATIONS INDICATED STEADY AND NORMAL INDICATIONS.
- [SDR DHL2001362004](https://openairdocs.org/sdr/DHL2001362004), Feb 9, 2001: SERVO. FAILED. UPON NR 2 ENGINE START, YELLOW SYSTEM JAM SERVO LIGHT ILLUMINATED. T/S TO LT LOW SPEED AILERON DISCONNECT SAME AND DEFERRED PEN.
- [SDR DHL2001362003](https://openairdocs.org/sdr/DHL2001362003), Jan 30, 2001: WARNING LIGHT. ILLUMINATED. DOORS LIGHT ILLUMINATED ON MWP DURING TAXI OUT. NO INDICATION ON S/O PANEL. E&E COMPARTMENT LT DOOR HANDLE RESET, OPS CHECK GOOD PER MM 52-11-14. OK FOR SERVICE
- [SDR DHL2000362002](https://openairdocs.org/sdr/DHL2000362002), Nov 22, 2000: WINDSHIELD. CRACKED. CLIMBING THROUGH F/L255 F/O WINDSHIELD OUTER PAIN CRACKED. REPLACED F/O WINSHIELD PER M/M 56-11-11.
- [SDR DHL2000362001](https://openairdocs.org/sdr/DHL2000362001), Nov 8, 2000: INU. MALFUNCTIONED. CAPTS ADI ATT FLAG APPEARS INTERMITTENTLY WITH MWP FLAG INST WARNING. REPLACED NR 1 INU, OPS CKS GOOD PER 34-25-00.
- [SDR DHL2000367001](https://openairdocs.org/sdr/DHL2000367001), Jan 13, 2000: DETECTOR. MALFUNCTIONED. AFTER TAKEOFF, SMOKE LIGHT ILLUMINATED. DECLARED EMERGENCY. ACCOMPLISHED SMOKE SOURCE IDENTIFICATION CHECKLIST, SMOKE LIGHT EXTINGUISHED. REMOVED AND REPLACED N
- [SDR 97ZZZX4310](https://openairdocs.org/sdr/97ZZZX4310), Sep 26, 1997: RIB FITTING. CRACKED. AFTER REMOVING THE INNER FLAP L/E SKIN FROM AROUND THE INBOARD FLAP ATTACHMENT POINT, THE RIB FITTING (5TH FROM INBOARD) WAS FOUND TO HAVE SIDE FLANGE WITH A SM
- [SDR CAL950498](https://openairdocs.org/sdr/CAL950498), Jun 18, 1995: COMPRESSOR. DAMAGED. LAX - FLT 0290 - TAKEOFF WAS REJECTED AT APPROXIMATELY 100 KNOTS AFTER A LOUD BANG WAS HEARD WITH THE NR 2 ENGINE EGT POINTER AT MAX. MAINTENANCE REMOVED AND RE
- [SDR CALA950495](https://openairdocs.org/sdr/CALA950495), Jun 17, 1995: HYD PUMP. LEAKING. LAX - FLT 0187- THE YELLOW HYDRAULIC SYSTEM FLUID DROPPED TO THE ORANGE DOT DURING CRUISE. THE HYDRAULIC PUMP WAS DUMPED AND THE FLUID LEVEL REMAINED AT THE ORA
- [SDR CAL950426](https://openairdocs.org/sdr/CAL950426), May 29, 1995: DUCT ASSY. RUPTURED. EWR - FLT 0487 - THE NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINT
- [SDR CAL950221](https://openairdocs.org/sdr/CAL950221), Mar 18, 1995: O-RING. LEAKING. EWR - FLT 0750 - THE GREEN SYSTEM HYDRAULIC FLUID DECREASED INTO THE YELLOW ARC ABOUT 2 HOURS AFTER TAKEOFF. TURNING BOTH ENGINE DRIVEN PUMPS TO 'DUMP' STOPPED 
- [SDR CAL950174](https://openairdocs.org/sdr/CAL950174), Mar 2, 1995: GEARBOX. BINDING. EWR - FLT 668 - THE ACFT HAD A HISTORY OF THE FLAPS NOT EXTENDING FOR LANDING. THE 'ABNORMAL' PROCEDURES WERE COMPLIED WITH AND THE ACFT LANDED WITHOUT INCIDENT
- [SDR CAL950143](https://openairdocs.org/sdr/CAL950143), Feb 22, 1995: DUCT ASSY. RUPTURED. FLT NR 668 - MCO - THE NR 1 ENG EXPERIENCED BLEED LOSS AND FIRE WARNING AFTER TAKEOFF. THE EGT ROSE TO 955 DEGREES. THE NR 1 ENGINE THRUST WAS REDUCED AND THE F
- [SDR CAL950140](https://openairdocs.org/sdr/CAL950140), Feb 20, 1995: DUCT. RUPTURED. FLT NR 288 - EWR - TAKEOFF WAS ABORTED AT 60 KNOTS AFTER THE NR 1 ENGINE N1 DROPPED AND THE EGT ROSE TO 950 DEGREES. MAINTENANCE FOUND THE NR 1 ENGINE 14TH STAG
- [SDR CAL950138](https://openairdocs.org/sdr/CAL950138), Feb 18, 1995: TRANSMISSION. LACK OF LUBE. EWR - FLT 0750 - WHEN FLAP HANDLE MOVED TO 8 DEGREES ON APPROACH TO EWR, FLAPS WOULD NOT EXTEND. CYCLING FLAP HANDLE HAD NO EFFECT. 'ABNORMAL' RPOCEDURES WERE C
- [SDR CAL950125](https://openairdocs.org/sdr/CAL950125), Feb 13, 1995: CLOG LIGHT. ILLUMINATED. EWR - FLT 0701 - THE NR 1 ENGINE FUEL CLOG LIGHT ILLUMINATED ON CLIMB-OUT OF EWR. FUEL WAS DUMPED AND AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCID
- [SDR CAL950102](https://openairdocs.org/sdr/CAL950102), Feb 8, 1995: HYD LINE. LOOSE. EWR - FLT 0261 - THE GREEN SYSTEM HYDRAULIC FLUID QUANTITY DROPPED TO 1.3 GALLONS WHILE IN-FLIGHT AND WAS ACCOMPANIED BY ILLUMINATION OF WARNING LIGHT. THE HYDR
- [SDR CAL950090](https://openairdocs.org/sdr/CAL950090), Feb 5, 1995: DUCT ASSY. RUPTURED. FLT 288 - EWR - THE NR 1 ENGINE HAD A FIRE WARNING ON TAKEOFF. THE A/C WAS RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE 14TH
- [SDR CAL950087](https://openairdocs.org/sdr/CAL950087), Feb 5, 1995: PITCH DAMPER. INOPERATIVE. EWR - FLT 0288 - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF USING EITHER SYSTEMS 1 OR 2. THE AIRCRAFT WAS RETURNED TO WHERE WHERE IT LANDED WITHOUT INCIDE
- [SDR CAL950083](https://openairdocs.org/sdr/CAL950083), Jan 31, 1995: AXLE. DAMAGED. FLT NR 0117 - EWR - THE AIRCRAFT WAS RETURNED TO THE GATE AFTER THE NR 1 MLG BRAKE LOCKED UP. THE AIRCRAFT WAS TAKEN OUT OF SERVICE. INITIAL INSPECTION FOUND TH
- [SDR CAL950071](https://openairdocs.org/sdr/CAL950071), Jan 25, 1995: FLAP TRANS. INOPERATIVE. MCO - FLT 117 - THE FLAPS WOULD NOT EXTEND ON APPROACH. THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 AND NR 6 FLAP TRANSMISSIONS AT FAULT. BOTH 
- [SDR CAL950063](https://openairdocs.org/sdr/CAL950063), Jan 23, 1995: INPUT ROD. OUT OF ADJUST. SDQ - FLT 702 - TAKEOFF WAS ABORTED AT LESS THAN 50 KNOTS DUE TO THE TAKEOFF WARNING HORN COMING ON, ACCOMPANIED BY AN INTERMITTENT CONFIGURATION LIGHT AND SPEE
- [SDR CAL950037](https://openairdocs.org/sdr/CAL950037), Jan 15, 1995: ACTUATOR. LEAKING. FLL - FLT 0249 - THE GREEN SYSTEM HYDRAULIC QUANTITY DROPPED TO WITHIN ONE-EIGHTH OF RED DOT ON GAUGE WHILE EN ROUTE TO FLL. MAINTENANCE FOUND THE LT KRUGER FLA

## STCs that may be installed (OpenAirDocs) (138, 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 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 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 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 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
- [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

All 138: https://openairdocs.org/model/airbus-a300-b4-103/stcs.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Airbus Industrie A300 B4-103](https://openairdocs.org/model/airbus-industrie-a300-b4-103): 0 registered aircraft, registry code 3930331

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.