# Airbus Industrie A310-222

- Type: Aircraft model (FAA registry)
- Registry code: 3930315
- Manufacturer (registry): AIRBUS INDUSTRIE
- Model: A310-222
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-jet
- Seats: 265
- 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: 2
- Page: https://openairdocs.org/model/airbus-industrie-a310-222

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 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 2024-26-05](https://openairdocs.org/ad/2024-26-05): Oxygen · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 87 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 2024-06-11](https://openairdocs.org/ad/2024-06-11): Time Limits/Maintenance Checks · Airbus A310-203, A310-204, A310-221 and 5 more. Effective May 2, 2024
- [AD 2023-24-07](https://openairdocs.org/ad/2023-24-07): Time Limits/Maintenance Checks · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Feb 6, 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 2023-09-03](https://openairdocs.org/ad/2023-09-03): Time Limits/Maintenance Checks · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Jun 6, 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 2023-04-09](https://openairdocs.org/ad/2023-04-09): Time Limits/Maintenance Checks · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Apr 24, 2023
- [AD 2022-22-06](https://openairdocs.org/ad/2022-22-06): Time Limits/Maintenance Checks · Airbus A310-203, A310-204, A310-222 and 5 more. Effective Mar 27, 2023
- [AD 2022-25-03](https://openairdocs.org/ad/2022-25-03): Fuselage · Airbus A300 B4-603, A300 B4-622, A300 B4-605R and 7 more. Effective Jan 23, 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 2022-25-12](https://openairdocs.org/ad/2022-25-12): Time Limits/Maintenance Checks · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Jan 6, 2023
- [AD 2022-25-11](https://openairdocs.org/ad/2022-25-11): Time Limits/Maintenance Checks · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Jan 6, 2023
- [AD 2022-19-06](https://openairdocs.org/ad/2022-19-06): Time Limits/Maintenance Checks · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Oct 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 2021-19-18](https://openairdocs.org/ad/2021-19-18): Time Limits/Maintenance Checks · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Oct 20, 2021
- [AD 2020-16-18](https://openairdocs.org/ad/2020-16-18): Fuselage · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Sep 9, 2020
- [AD 2020-02-22](https://openairdocs.org/ad/2020-02-22): Hydraulic power · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Mar 19, 2020
- [AD 2019-20-06](https://openairdocs.org/ad/2019-20-06): Time Limits/ Maintenance Checks · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Nov 22, 2019
- [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 2019-14-08](https://openairdocs.org/ad/2019-14-08): Electrical power · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Oct 2, 2019
- [AD 2019-14-14](https://openairdocs.org/ad/2019-14-14): Stabilizers · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Sep 19, 2019
- [AD 2019-05-13](https://openairdocs.org/ad/2019-05-13): Removal of AD 2007-22-05 and AD 2013-13-13 · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Mar 21, 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 2018-19-31](https://openairdocs.org/ad/2018-19-31): Time limits/maintenance checks · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Nov 2, 2018
- [AD 2018-18-21](https://openairdocs.org/ad/2018-18-21): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Oct 23, 2018
- [AD 2018-18-20](https://openairdocs.org/ad/2018-18-20): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Oct 23, 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 2018-17-16](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 2018-11-06](https://openairdocs.org/ad/2018-11-06): Wings · Airbus A310-203, A310-221, A310-222 and 4 more. Effective Jul 3, 2018
- [AD 2018-10-05](https://openairdocs.org/ad/2018-10-05): Wings · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Jun 19, 2018
- [AD 2018-06-03](https://openairdocs.org/ad/2018-06-03): Fuselage · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Apr 19, 2018
- [AD 2018-01-03](https://openairdocs.org/ad/2018-01-03): Equipment/furnishings · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Jan 18, 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 2017-24-09](https://openairdocs.org/ad/2017-24-09): Fuselage · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Jan 5, 2018
- [AD 2017-21-08](https://openairdocs.org/ad/2017-21-08): Time Limits/Maintenance Checks · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Nov 27, 2017
- [AD 2017-21-02](https://openairdocs.org/ad/2017-21-02): Fuselage · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Nov 27, 2017
- [AD 2017-20-04](https://openairdocs.org/ad/2017-20-04): Instruments · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Nov 15, 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 2017-18-19](https://openairdocs.org/ad/2017-18-19): Wings · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Oct 19, 2017
- [AD 2017-18-15](https://openairdocs.org/ad/2017-18-15): Fuselage · Airbus A300 B4-603, A300 B4-605R, A300 B4-622 and 11 more. Effective Oct 19, 2017
- [AD 2017-17-12](https://openairdocs.org/ad/2017-17-12): Wings · Airbus A310-203, A310-221, A310-222 and 4 more. Effective Oct 2, 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

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 2016-20-11](https://openairdocs.org/ad/2016-20-11) (historical): Fuselage · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Jan 3, 2017
- [AD 2016-23-01](https://openairdocs.org/ad/2016-23-01) (historical): Fatigue cracking · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Dec 15, 2016
- [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 2016-07-22](https://openairdocs.org/ad/2016-07-22) (historical): Electrical Power · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective May 16, 2016
- [AD 2013-13-13](https://openairdocs.org/ad/2013-13-13) (historical): Wings · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Sep 23, 2014
- [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 2014-12-06](https://openairdocs.org/ad/2014-12-06) (historical): Fuselage · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Jul 2, 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 2012-08-03](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 2012-03-04](https://openairdocs.org/ad/2012-03-04) (historical): Fuel · Airbus A310-203, A310-204, A310-221 and 5 more. Effective May 15, 2012
- [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 2010-06-04](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 2010-04-03](https://openairdocs.org/ad/2010-04-03) (historical): Wings · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Mar 19, 2010
- [AD 2007-21-14 R1](https://openairdocs.org/ad/2007-21-14-R1) (historical): Ignition sources · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Nov 12, 2009
- [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 2009-18-16](https://openairdocs.org/ad/2009-18-16) (historical): Fuselage · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Oct 14, 2009
- [AD 2009-11-09](https://openairdocs.org/ad/2009-11-09) (historical): Equipment/Furnishings · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Jun 12, 2009
- [AD 2009-06-06](https://openairdocs.org/ad/2009-06-06) (historical): Transmission shafts · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Apr 28, 2009
- [AD 2008-17-02](https://openairdocs.org/ad/2008-17-02) (historical): Main landing gear (MLG) · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Sep 17, 2008
- [AD 2008-01-05](https://openairdocs.org/ad/2008-01-05) (historical): Right-hand (RH) wing · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Feb 20, 2008
- [AD 2007-25-02](https://openairdocs.org/ad/2007-25-02) (historical): New and revised structural inspections and inspection intervals. · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Jan 14, 2008
- [AD 2007-21-14](https://openairdocs.org/ad/2007-21-14) (historical): Limitations for fuel tank systems · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Nov 20, 2007
- [AD 2007-14-05](https://openairdocs.org/ad/2007-14-05) (historical): Airworthiness Limitations · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Aug 22, 2007
- [AD 2007-02-22](https://openairdocs.org/ad/2007-02-22) (historical): Wiper rings in the splined couplings of the flap transmission shafts · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Mar 2, 2007
- [AD 2007-02-09](https://openairdocs.org/ad/2007-02-09) (historical): Wing main landing gear (MLG) · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Feb 6, 2007
- [AD 2006-15-10](https://openairdocs.org/ad/2006-15-10) (historical): Trimmable horizontal stabilizer actuator (THSA) · Airbus A300-600 Series (all), A300B4-601, A300B4-603 and 17 more. Effective Aug 29, 2006
- [AD 2006-15-09](https://openairdocs.org/ad/2006-15-09) (historical): Wing and center fuel tanks · Airbus A300-600 Series (all), A300 Series (all), A300B4-601 and 18 more. Effective Aug 29, 2006
- [AD 2006-10-11](https://openairdocs.org/ad/2006-10-11) (historical): Flap transmission shafts · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Jun 20, 2006
- [AD 2006-09-05](https://openairdocs.org/ad/2006-09-05) (historical): Rear spar internal angle · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Jun 7, 2006
- [AD 2006-02-06](https://openairdocs.org/ad/2006-02-06) (historical): Frame foot and adjacent frames · Airbus A310-203, A310-204, A310-222 and 4 more. Effective Feb 24, 2006
- [AD 2005-26-17](https://openairdocs.org/ad/2005-26-17) (historical): Elevators · Airbus A300B4-601, A300B4-603, A300B4-605R and 14 more. Effective Feb 3, 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 2004-15-07](https://openairdocs.org/ad/2004-15-07) (historical): Aileron access doors · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Aug 31, 2004
- [AD 2004-14-06](https://openairdocs.org/ad/2004-14-06) (historical): Chafing plates of the wing root · Airbus A310-203, A310-204, A310-221 and 5 more. Effective Aug 13, 2004
- [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 2000-12-12](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 2000-02-04](https://openairdocs.org/ad/2000-02-04) (historical): Autopilot Disconnect, Out-Of-Trim Condition · Airbus Industrie A300 Model B2-1A, A300 Model B2-1C, A300 Model B2-203 and 22 more. Effective Feb 9, 2000
- [AD 99-27-10](https://openairdocs.org/ad/99-27-10) (historical): Fire Warning System · Airbus Industrie A300 Model B4-600 Series, A300 Model B4-600R Series, A300 Model F4-600R Series and 15 more. Effective Feb 8, 2000
- [AD 99-19-40](https://openairdocs.org/ad/99-19-40) (historical): Terminal Lugs on 12XC & 15XE Connectors Inspection · Airbus Industrie A300 Model B4-600 Series, A300 Model B4-600R Series, A300 Model F4-600R Series and 15 more. Effective Oct 27, 1999
- [AD 98-26-01](https://openairdocs.org/ad/98-26-01) (historical): Fuselage, Horizontal Stabilizer, and Wings · Airbus A310-203, A310-221, A310-222 and 4 more. Effective Jan 20, 1999
- [AD 98-25-51](https://openairdocs.org/ad/98-25-51) (historical): Thrust Reverser · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 11 more. Effective Dec 28, 1998
- [AD 98-19-22](https://openairdocs.org/ad/98-19-22) (historical): Aft Pressure Bulkhead Lower Rim Crack Inspection · Airbus Industrie A300 Model B4-600 Series, Industrie A300 Model B4-600R Series, Industrie A300 Model F4-600R Series and 15 more. Effective Oct 22, 1998
- [AD 98-16-09](https://openairdocs.org/ad/98-16-09) (historical): Test The Fire Shut-Off Valves (FSOV) · Airbus Industrie A300 Model B2-1A, A300 Model B2-1C, A300 Model B2-203 and 22 more. Effective Sep 4, 1998
- [AD 98-16-06](https://openairdocs.org/ad/98-16-06) (historical): Door Scuff Plates Inspection · Airbus A310-203, A310-221, A310-222 and 4 more. Effective Sep 4, 1998
- [AD 98-13-33](https://openairdocs.org/ad/98-13-33) (historical): Desynchronization Of Rudder Servo Actuators · Airbus A300 Model B2-1A, A300 Model B2-1C, A300 Model B2-203 and 22 more. Effective Jul 30, 1998
- [AD 98-09-20](https://openairdocs.org/ad/98-09-20) (historical): Inspect Chafing Plates Of Wing Root · Airbus A310-203, A310-221, A310-222 and 4 more. Effective Jun 3, 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

All 341: https://openairdocs.org/model/airbus-industrie-a310-222/ads.md

## Information bulletins (advisory) (5)

- [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-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008
- [SAIB NM-08-43](https://openairdocs.org/saib/NM-08-43): Cabin Equipment/Furnishings - Seats. Issued Sep 3, 2008
- [SAIB NM-08-31](https://openairdocs.org/saib/NM-08-31): Equipment/Furnishings:  Non-Textile Floors. Issued Jul 2, 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 (2)

- [N453FE](https://openairdocs.org/aircraft/N453FE): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1983, S/N 267
- [N454FE](https://openairdocs.org/aircraft/N454FE): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1983, S/N 278

## NTSB investigations (1)

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 DCA99WA064](https://openairdocs.org/ntsb/DCA99WA064), Jun 28, 1999: Airbus Industrie A310 (N420FE), Manila, Philippines, substantial damage

## FAA accident and incident reports (7)

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 20130313005629I](https://openairdocs.org/incident/20130313005629I), Mar 13, 2013: Airbus Industrie A310-222 (N455FE), Omaha, NE, No damage. Landing gear could not be extended using number one or number two system. Emergency extension system used and uneventful landing completed.
- [Incident 20110223001739I](https://openairdocs.org/incident/20110223001739I), Feb 23, 2011: Airbus A310-222 (N456FE), Harrisburg, PA, No damage. Spoke with fedex station manager [privacy data omitted] as crew had already departed for newark with replacement aircraft. Upon landing at MDT on runway 31,…
- [Incident 20040213002429I](https://openairdocs.org/incident/20040213002429I), Feb 13, 2004: Airbus A310222 (N449FE), Indianapolis, IN, Minor damage. (-23) On landing roll out between approx 60-80 knots crew observed a flash on l/h side of a/c. after exiting runway they were informed by the tower that the #1…
- [Incident 20030820023929I](https://openairdocs.org/incident/20030820023929I), Aug 20, 2003: Airbus A310222 (N446FE), Columbus, OH, Minor damage. (-23) While enroute right side sliding window heat power cord caught fire. Switch was turned off and fire was extinguished. Landed klck. The maintenance action…
- [Incident 20030202006209I](https://openairdocs.org/incident/20030202006209I), Feb 2, 2003: Airbus A310222 (N454FE), Indianapolis, IN. (-23) On feb 02 2003 while enroute roc to mem at FL 350, all four left wheel temps went to 400 degrees. Right wheels remained at 5 degrees. The crew suspected…
- [Incident 20020926026599I](https://openairdocs.org/incident/20020926026599I), Sep 26, 2002: Airbus A310222 (N449FE), Burbank, CA. (-23) Federal express flight 1417 landed at Burbank airport on 9/26/02. On rollout the Burbank tower reported to the aircrew that the number one engine was on…
- [Incident 20011228033649I](https://openairdocs.org/incident/20011228033649I), Dec 28, 2001: Airbus A310222 (N448FE), Pittsburgh, PA. (-23) On December 28, 2001, federal express flight #1446 an A-310-222 declared an emergency due to a cargo smoke indication. The aircraft landed at runway 10L…

## Service difficulty reports (1,281, newest 50)

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

- [SDR FDEA201512194038](https://openairdocs.org/sdr/FDEA201512194038), Dec 19, 2015: FAIRING. DAMAGED. LEFT WING INBD FLAP FAIRING HANGING DOWN ON ARRIVAL. RELEASED FOR SERVICE IAW CDL 27-01, B CATEGORY. FLAP TRACK FAIRING MISSING, REFER TO CDL 27-01-B FOR RESTRI
- [SDR FDEA201512023853](https://openairdocs.org/sdr/FDEA201512023853), Dec 2, 2015: ADAPTER. LOOSE. DEPARTED WITH 62,000 POUNDS OF FUEL, AT LANDING FUEL QTY INDICATES 61,400 POUNDS OF FUEL. REMOVED AND REPLACED LEFT OUTER ADAPTER PLUGS 42QT1 & 43QT1 PER AMM 28
- [SDR FDEA201511043464](https://openairdocs.org/sdr/FDEA201511043464), Nov 4, 2015: COMPUTER. FAILED. SHORTLY AFTER CLEANUP ON TAKEOFF, MULTIPLE & VARIOUS AURAL & ECAM ALERTS & WARNINGS BEGAN. DECLARED AN EMER & RETURNED, WARNINGS CONTINUED ALL THE WAY TO BLOCK 
- [SDR FDEA201507092174](https://openairdocs.org/sdr/FDEA201507092174), Jul 9, 2015: SEAT TRACK. DAMAGED. RAMP REPORTS AFT LOCK IN POSITION 8R LOOSE IN FLOOR, LATCH N1288. LATCH RESTRAINT DEVICE N1288 AT 8R INOPERATIVE, BROKEN OR MISSING. INSTALLED NEW SEAT TRACK SE
- [SDR FDEA201507092173](https://openairdocs.org/sdr/FDEA201507092173), Jul 9, 2015: SEAT TRACK. DAMAGED. FOUND AT POS 8R, LOCK S1288 TO HAVE SEAT TRACK LOBE DAMAGE CAUSING LOCK TO BE LOOSE. LOBE DAMAGE AT LOCK S1288 POS 8R, LOCK INSTALLED BUT LOOSE IN FLOOR. ACFT O
- [SDR FDEA201505221623](https://openairdocs.org/sdr/FDEA201505221623), May 22, 2015: SWITCH. FAULTY. LOWERED GEAR, GOT SAFE INDICATION OF GEAR DOWN. A FEW SECONDS LATER GOT UNSAFE GEAR WARNING. LIGHT & HORN IN POS 2 SELECTED SYS 1 & THE LIGHT QAND WARNING HORN 
- [SDR FDEA201504101202](https://openairdocs.org/sdr/FDEA201504101202), Apr 10, 2015: COMPENSATOR. FAILED. DURING APPROACH, 2000 & 6 MILES, THE HOT BRAKE LIGHT IN THE CUBE ON THE LG TEST PANEL FLICKERED, FOLLOWED BY ECAM HOT BRAKE WARNINGS FOR ALL 4 WHEELS ON THE LT 
- [SDR FDEA201502120515](https://openairdocs.org/sdr/FDEA201502120515), Feb 12, 2015: ENGINE. VIBRATION. ON TAKEOFF, ACFT STARTED VIBRATING VERY BADLY. FELT MORE LIKE AN AIRFRAME FLUTTER RATHER THAN ENG VIBRATION. CHECKED ENG PAGE, ALL NORMAL. CLIMBING THROUGH 2500
- [SDR FDEA201412184149](https://openairdocs.org/sdr/FDEA201412184149), Dec 18, 2014: PANEL. DAMAGED. ON ARRIVAL LT WING TE DAMAGE FOUND. R & R THE LT WING OTBD TE PANEL IAW SRM 57-51-12.
- [SDR FDEA201409102582](https://openairdocs.org/sdr/FDEA201409102582), Sep 10, 2014: ACTUATOR. FAILED. UPON GEAR RETRACTION, RECEIVED A LT MAIN GEAR RED UNLOCK INDICATION WITH AN AMBER LT DOOR LIGHT. COMPLIED WITH ECAM EXTENDED GEAR & LANDED. WE DID HAVE A LOUD W
- [SDR FDEA201408212293](https://openairdocs.org/sdr/FDEA201408212293), Aug 21, 2014: SEQUENCE VALVE. FAULTY. DURING CLIMB OUT AT GEAR RETRACTION, LT MAIN GEAR DID NOT APPEAR TO RETRACT & DOOR SHOWED OPEN. ECAM INDICATED LG RETRACTION INOPERATIVE. FUEL CONSUMPTION INCRE
- [SDR FDEA201407131756](https://openairdocs.org/sdr/FDEA201407131756), Jul 13, 2014: DAMPER. LEAKING. ON DEPARTURE LG WOULD NOT RETRACT. TRIED BOTH SYS 1 & SYS 2 & QRH, NO HELP. RT GEAR PITCH DAMPER POPPED WITH THE REAR SEAL BLOWN ALL THE WAY OUT. R & R RT MAIN 
- [SDR FDEA201406021269](https://openairdocs.org/sdr/FDEA201406021269), Jun 2, 2014: SKIN. CRACKED. POSSIBLE CRACK ON LT WING INBD SLAT CUT OUT, BOTH CORNERS. PERFORMED HFEC OF AREA IAW NTM 51-10-08 BLOCK 601, TWO CRACK INDICATIONS. REPAIRED AREAS, INSTALLED F
- [SDR FDEA201405221136](https://openairdocs.org/sdr/FDEA201405221136), May 22, 2014: VALVE. FAILED. NR 1 SLAT SYS FAULT LIGHT DURING FINAL. RECYCLING DID NOT CORRECT, QRH PROCEDURES ACCOMPLISHED. SLAT FAULT LIGHT REMAINED ON, BUT SPFI SHOWED SLATS & FLAPS 30 &
- [SDR FDEA201403050452](https://openairdocs.org/sdr/FDEA201403050452), Mar 5, 2014: SWITCH. FAILED. ACCELERATING ABOVE 10,000 & 250 KTS, NR 1 ENGINE THRUST REVERSER UNLOCK ILLUMINATED STEADY. ALL OTHER INDICATIONS NORMAL. TROUBLESHOT IAW TSM 78-31-00, FOUND TH
- [SDR FDEA201402030253](https://openairdocs.org/sdr/FDEA201402030253), Feb 3, 2014: PRESSURE SWITCH. FAULTY. NR 2 ENG GREEN HYD PUMP LOW PRESS WHEN SETTING TAKEOFF POWER. DISCONTINUED TAKEOFF. REMOVED OLD NR 2 ENG GREEN PUMP PRESS SWITCH 112GK & REPLACED WITH NEW SWITC
- [SDR FDEA201312243034](https://openairdocs.org/sdr/FDEA201312243034), Dec 24, 2013: PLATE. WORN. NR 2 ENG OTBD T/R COWL UPPER MID-SECTION INNER FACE FOUND ONE EACH PLATE WORN BY SPRING SEAL. ACCOMPLISHED THE WORK IAW EA 6-5410-T0208220.
- [SDR FDEA201312243033](https://openairdocs.org/sdr/FDEA201312243033), Dec 24, 2013: FRAME. CORRODED. FORWARD CARGO COMPARTMENT BILGE FRAME FOUND CORROSION AT FR 39, STRINGER 51R POSITION. CORROSION AREA CUT OUT & REINFORCED WITH REPAIR PART & FITTING TO INSTALL
- [SDR FDEA201310252615](https://openairdocs.org/sdr/FDEA201310252615), Oct 25, 2013: SKIN. DENTED. LT INBD FLAPS T/E LOWER SURFACE HAS NUMEROUS DENTS. FOUND WITHIN LIMITS IAW SRM 57-52-12, FIG 101, DETAIL IV. TWO DENTS, PUNCTURED, REPAIRED DENTS IAW SRM 57-52
- [SDR FDEA201310202564](https://openairdocs.org/sdr/FDEA201310202564), Oct 20, 2013: SUPPORT. CORRODED. RIGHT MLG RIB 5, FWD LUG LOWER SURFACE IS CORRODED. RT MLG RIB 5 FWD LUG CORROSION. R & R IAW REPAIR DWG R57249389, REV B IAW EA 6-5710-T0302172, PART 1. REPAIR
- [SDR FDEA201310172530](https://openairdocs.org/sdr/FDEA201310172530), Oct 17, 2013: SKIN. DAMAGED. FOUND DAMAGE TO SKIN AT FRAME 87 BETWEEN STRINGERS 25-30R, REPAIRED IAW EA 6-5330-T0302997, PART 1. REPAIR CLASSIFIED AS MINOR.
- [SDR FDEA201310172528](https://openairdocs.org/sdr/FDEA201310172528), Oct 17, 2013: SKIN. DAMAGED. RIGHT WING INBD TE FLAPS LOWER SURFACE HAS IMPACT DAMAGE. REPAIRED IAW SRM 57-52-12, PARA 4.D, FIG 204. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310172532](https://openairdocs.org/sdr/FDEA201310172532), Oct 17, 2013: SKIN. CORRODED. LEFT OTBD FLAPS T/E LOWER SURFACE HAS CORROSION LOCATED 22 INCHES INBD OF NR 5 FLAP TRACK. PERFORMED REPAIR IAW SRM 57-53-12, FIG 209. REPAIR CLASSIFIED AS MAJO
- [SDR FDEA201310172529](https://openairdocs.org/sdr/FDEA201310172529), Oct 17, 2013: LUG. CORRODED. LEFT MLG RIB 5 FWD LUG LOWER SURFACE IS CORRODED. R & R IAW REPAIR DWG R57249389, REV B IAW EA 6-5710-T0302173. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310152508](https://openairdocs.org/sdr/FDEA201310152508), Oct 15, 2013: SKIN. CORRODED. LEFT ELEVATOR LOWER SKIN HAS A SPOT OF CORROSION LOCATION 5 INCHES FROM T/E, 15 INCHES FROM TIP. PERFORMED REPAIR ON LT ELEVATOR SKIN IAW SRM 55-21-11, FIG 209.
- [SDR FDEA201310152509](https://openairdocs.org/sdr/FDEA201310152509), Oct 15, 2013: SKIN. CRACKED. RT WING, RIB 9 LOWER SKIN FWD EDGE CRACKED. REPAIRED SKIN IAW DWG R572-57208 & EA 6-5710-T0302280. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310132493](https://openairdocs.org/sdr/FDEA201310132493), Oct 13, 2013: STRINGER. CORRODED. STRINGER 44R FWD OF FRAME 17 HAS CORROSION AROUND RIVET. REPAIRED STRINGER IAW SRM 53-12-14. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310132494](https://openairdocs.org/sdr/FDEA201310132494), Oct 13, 2013: MOUNT. CORRODED. TWO FWD ENGINE MOUNTS HAVE PITTING CORROSION IN BOTH FWD MOUNT HOLES AND THE AFT OTBD MOUNT HOLE. PERFORMED REPAIR IAW SRM 54-51-18 WITH FABRICATED BUSHINGS.
- [SDR FDEA201310132492](https://openairdocs.org/sdr/FDEA201310132492), Oct 13, 2013: ANGLE. BENT. AFT FUSELAGE THS BAY WEB AT FRAMES 89 & 84 UPPER ANGLE BENT STRINGER 32L. REPLACED WEB UPPER ANGLE IAW SRM 51-40-21. F
- [SDR FDEA201310132491](https://openairdocs.org/sdr/FDEA201310132491), Oct 13, 2013: ANGLE. BENT. THS BAY WEB UPPER ANGLE BENT LOCATION, STRINGER 32R, BETWEEN FRAMES 86 & 87. REPLACED WEB UPPER ANGLE IAW SRM 53-19-18.
- [SDR FDEA201310092461](https://openairdocs.org/sdr/FDEA201310092461), Oct 9, 2013: MOUNT. CORRODED. NR 2 PYLON AFT ENGINE MOUNT HAS CORROSION ON FWD & AFT SIDES OF MOUNT, ON INBD AND OTBD, HORIZONTALLY POSITIONED BOLTS, RECESSED AREAS. REPAIRED IAW EA 6-5451-T
- [SDR FDEA201310092460](https://openairdocs.org/sdr/FDEA201310092460), Oct 9, 2013: SKIN. DENTED. RIGHT WING ALL SPEED AILERON BOTTOM SKIN HAS DENT LOCATION 27.5 IN FROM INBD, 17IN FROM FWD END. REPAIRED IAW SRM 57-61-12, PB 201, PARAGRAPH 4.A. REPAIR CLASSI
- [SDR FDEA201310082451](https://openairdocs.org/sdr/FDEA201310082451), Oct 8, 2013: SEAT TRACK. DAMAGED. SEAT TRACK DAMAGED AT FRAME 40-42, -Y1959 REPAIRED IAW SRM 53-10-16, PARA 5, FIG 203, SH 5, FABRICATED & INSTALLED SEAT TRACK IAW SRM 51-27-11 & SRM 51-40-21. R
- [SDR FDEA201310062421](https://openairdocs.org/sdr/FDEA201310062421), Oct 6, 2013: LUG. DAMAGED. LEFT MLG WW RIB 5 FITTING FWD LUG DAMAGED. REPAIRED IAW EA 6-5750-T0302477 P1, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
- [SDR FDEA201310042404](https://openairdocs.org/sdr/FDEA201310042404), Oct 4, 2013: LUG. CORRODED. CORROSION WAS FOUND ON THE LUG BORE AND AFT SPOTFACE OF RT RIB5 FWD LUG. ACCOMPLISHED CORROSION REPAIR IAW GMM 6-2-100 REPAIR CLASSIFIEID AS MINOR.
- [SDR FDEA201310042403](https://openairdocs.org/sdr/FDEA201310042403), Oct 4, 2013: LUG. CORRODED. CORROSION WAS FOUND ON LUG BORE AND FWD SPOTFACE OF LT RIB 5. ACCOMPLISHED THE CORROSION REPAIR IAW GMM 6-2-100, IAW EA 6-5750-T0302477 P1. REPAIR CLASSIFED AS 
- [SDR FDEA201310032398](https://openairdocs.org/sdr/FDEA201310032398), Oct 3, 2013: WEB. CRACKED. FOUND WEB BETWEEN FRAMES 86 - 87 STRINGER 35R CRACKED. R & R WEB IAW SRM 51-40-21. REPAIR CLASSIFIED AS MINOR.
- [SDR FDEA201309302352](https://openairdocs.org/sdr/FDEA201309302352), Sep 30, 2013: SKIN. DAMAGED. ACCESS DOOR 136AR EXTERNAL SKIN CUTOUT RADIUS IS OUT OF TOLERANCE. REPLACED ACCESS DOOR 136AR SKIN IAW SRM 52-41-15 & DWG 14A52475000.
- [SDR FDEA201309302338](https://openairdocs.org/sdr/FDEA201309302338), Sep 30, 2013: BEAM. CRACKED. THREE CRACKS WERE FOUND AT LT INNER LONGITUDINAL BEAM FLANGE STR 11 BETWEEN FRAMES 73A AND 74A. CUT OUT DAMAGE PORTION OF BEAM AND REWORK MILLED STEP. INSTALL T
- [SDR FDEA201309292337](https://openairdocs.org/sdr/FDEA201309292337), Sep 29, 2013: PROFILE. CHAFED. AFT CABIN PROFILE TEE, FRAME 80, STR 34L, WEB CHORD CHAFED. REPLACED DAMAGED PROFILE TEE IAW SRM 51-40-21.
- [SDR FDEA201309262322](https://openairdocs.org/sdr/FDEA201309262322), Sep 26, 2013: TEE FITTING. CHAFED. AFT CABIN FRAME 80, S34R WEB ANGLE CHAFED REPLACED DAMAGED PROFILE TEE WITH FABRICATED PROFILE TEE AT FRAME 80, STR 34R IAW SRM 51-40-21. PROFILE FABRICATED IAW
- [SDR FDEA201309252309](https://openairdocs.org/sdr/FDEA201309252309), Sep 25, 2013: FLOORBOARD. DELAMINATED. FWD MAIN DECK CARGO UTILITY AREA LAVATORY FLOORBOARD, MULTIPLE AREAS HAS DAMAGED AND DELAMINATION. FABRICATED FLOORBOARD IAW SRZ-25-005. AND INSTALLED. REPAIR C
- [SDR FDEA201309252308](https://openairdocs.org/sdr/FDEA201309252308), Sep 25, 2013: FLOORBOARD. DAMAGED. FWD CABIN FLOORBOARD 222DF EDGE HAS HONEYCOMB CHIPPED OFF, FABRICATED FLOORBOARD IAW SRZ-25-005 AND INSTALLED. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309232287](https://openairdocs.org/sdr/FDEA201309232287), Sep 23, 2013: SKIN. DENTED. LOWER FUSELAGE SKIN, FRAME 19- 20, STR 34 -35R DENTED. REPAIRED IAW SRM 53-10-12 FIG 226 (SHEET 2). REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309232292](https://openairdocs.org/sdr/FDEA201309232292), Sep 23, 2013: FLOOR PANEL. CRACKED. MAIN DECK CARGO FRAMES 60-62, BETWEEN Y953 AND Y1456 FLOOR PANEL 251UF CRACKED. REPLACED PANEL. PANEL FABRICATED IAW DWG SRZ-25-005.
- [SDR FDEA201309232289](https://openairdocs.org/sdr/FDEA201309232289), Sep 23, 2013: FLOORBOARD. CRACKED. FLOORBOARD 231BG HAS A CRACK. REPLACED FLOORBOARD. FLOORBOARD FABRICATED ON TRAVELER T13/1025840 IAW DWG SRZ-25-005 & INSTALLED ON WC 230-SWC-FIT.
- [SDR FDEA201309232288](https://openairdocs.org/sdr/FDEA201309232288), Sep 23, 2013: FLOORBOARD. DAMAGED. FLOORBOARD 231ZF HAS DAMAGE IN SEVERAL AREAS. FABRICATED & REPLACED FLOORBOARD.
- [SDR FDEA201309232286](https://openairdocs.org/sdr/FDEA201309232286), Sep 23, 2013: SKIN. DAMAGED. DURING ACCOMPLISHMENT OF STRINGER REPAIR AT FR 72 2 EA HOLES HAVE EXCESSIVE PITCH AT STRINGER 41R. ACCOMPLISHED CATEGORY B SKIN REPAIR AT FR 72 STR 41R IAW SRM 
- [SDR FDEA201309232283](https://openairdocs.org/sdr/FDEA201309232283), Sep 23, 2013: FLOOR PANEL. DAMAGED. FLOOR PANEL 132RF IN LOWER FWD CARGO BAY WAS FOUND SOFT. FABRICATED A NEW PANEL WITH INSERTS AND ADHESIVE IAW SRM 53-10-20 & IRM 9701. REPAIR WAS CLASSIFIED AS 
- [SDR FDEA201309232282](https://openairdocs.org/sdr/FDEA201309232282), Sep 23, 2013: FLOOR PANEL. DENTED. FLOOR PANEL 162HF IN BULK CARGO, FOUND SERIOUS DENT IN SKIN. FABRICATED A NEW PANEL WITH INSERTS AND ADHESIVE IAW SRM 53-10-20 & IRM 9701. REPAIR WAS CLASSIFIED

All 1,281: https://openairdocs.org/model/airbus-industrie-a310-222/reports.md

## STCs that may be installed (OpenAirDocs) (97, 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 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 ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde 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 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 ST01694CH](https://openairdocs.org/stc/ST01694CH): Installation of Honeywell International Enhanced Ground Proximity Warning System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01754CH](https://openairdocs.org/stc/ST01754CH): Installation of an Airshow 420 system IAW ECS MDL ECS-201346, Rev. A, dtd 1/24/03 or later FAA approved revision. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST02161CH](https://openairdocs.org/stc/ST02161CH): Installation of GPS wiring and antenna provisions. Amphenol Cable and Interconnect Technologies Inc
- [STC ST02169CH](https://openairdocs.org/stc/ST02169CH): Installation of elementary and enhanced Mode S transponders. Amphenol Cable and Interconnect Technologies Inc
- [STC ST02866CH](https://openairdocs.org/stc/ST02866CH): Upgrade of the internal core software of the ACARS Data Link Management Unit (DLM-900). 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 ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [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 ST02896AT](https://openairdocs.org/stc/ST02896AT): Installation of a Kannad Model 406-AF Emergency Locator Transmittter (ELT). 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 ST00440SE](https://openairdocs.org/stc/ST00440SE): Installation of the Honeywelll Enhanced Ground Proximity Warning System. Honeywell International Inc
- [STC ST01235SE](https://openairdocs.org/stc/ST01235SE): Installation of the Honeywell Mark II ACARS (Aircraft Communication Addressing and Reporting 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 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 ST04092NY](https://openairdocs.org/stc/ST04092NY): Installation of Wireless PCMCIA for DFDAU. Delta Engineering Corporation
- [STC ST001214AT](https://openairdocs.org/stc/ST001214AT): Entered in error please see ST001214AT-D. HAECO Cabin Solutions LLC
- [STC ST001214AT-D](https://openairdocs.org/stc/ST001214AT-D): Installation of Airshow 210 System. HAECO Cabin Solutions LLC
- [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 ST04345NY](https://openairdocs.org/stc/ST04345NY): Upgrade from TCAS II software version 7.0 to 7.1. PMV Engineering
- [STC ST01891LA-D](https://openairdocs.org/stc/ST01891LA-D): Installation of a Commercial Medical Stretcher. LifePort LLC
- [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 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
- [STC ST04229NY](https://openairdocs.org/stc/ST04229NY): Introduction of a 16G New Generation Stretcher XL P/N 1120030-Series. Bucher Leichtbau AG
- [STC SA3185SO](https://openairdocs.org/stc/SA3185SO): Installation of a replacement coalescer filter. Purolator Facet, Inc
- [STC ST00104AT](https://openairdocs.org/stc/ST00104AT): Installation of a replacement cartridge filter assembly. Purolator Facet, Inc
- [STC ST02406LA](https://openairdocs.org/stc/ST02406LA): Installation of TCAS version 7.1. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST02626LA](https://openairdocs.org/stc/ST02626LA): Modification to the existing Mode S Transponder system to add NEXTGEN ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc
- [STC ST09859AC](https://openairdocs.org/stc/ST09859AC): Installation of a SkyTender Beverage Trolley. ASIG LLC
- [STC SA7076NM](https://openairdocs.org/stc/SA7076NM): Installation of Stretcher Carrier. Air Medic LLC
- [STC ST02540LA](https://openairdocs.org/stc/ST02540LA): Installation of Telair International LLC light weight P/Ns PMC100 and PAG100 series cargo pallets. Telair International LLC
- [STC ST02489LA](https://openairdocs.org/stc/ST02489LA): Installation of Telair International Inc. light weight LD3 (NAS3610 / SAE36100 - 2K2) cargo container P/N LD3100-31000ZZZ. Telair International LLC
- [STC SA5928NM](https://openairdocs.org/stc/SA5928NM): Installation of cargo liner detail design features. AviAero LLC
- [STC ST02524LA](https://openairdocs.org/stc/ST02524LA): Installation of TCAS version 7.0. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST03483AT](https://openairdocs.org/stc/ST03483AT): Installation of a Portable Beverage Dispensing System, P/N B43-FA-001. Dynamo Beverage Company, USA, L.L.C

All 97: https://openairdocs.org/model/airbus-industrie-a310-222/stcs.md

## PMA parts (OpenAirDocs) (over 1,000, 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.

- [58163-4WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126394715220261009133948.0001): Ring-Piston. Wencor, LLC · PMA PQ1370NM · Replaces 58163-4 · Oct 1, 2026
- [108C0250-02KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196728359420260910164855.0001): Device-Locking Index. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces 108C0250-02 · Sep 4, 2026
- [RCMA3068-2KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179237934120260910164855.0001): Receiver Assy. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces RCMA3068-2 · Sep 4, 2026
- [RC3068-2KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103895633020260910164854.0001): Receiver. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces RC3068-2 · Sep 4, 2026
- [9143FR](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175949486320260909220943.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR-0100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152861273020260909220943.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR-0325](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131311693520260909220944.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR-0200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114706953320260909220943.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR-0315](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101461286820260909220943.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [ADP38004-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101418937120260705233224.0001): Rotor Assembly, Blower Motor. ADPma · PMA PQ1682CE · Replaces Honeywell 606389-1 · Jul 2, 2026
- [AF300P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185759106320260717175324.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026
- [AF300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148147963220260717175322.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026
- [AF302](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123755079120260717175326.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026
- [3826099-1NTMT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190206600720260616140939.0001): Inlet Vane. Source Manufacturing Inc · PMA PQ1549CE · Replaces 3826099-1 · Apr 10, 2026
- [3826160-2TMT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174810131620260616140939.0001): Retainer, Bearing. Source Manufacturing Inc · PMA PQ1549CE · Replaces 3826160-2 · Apr 10, 2026
- [3826099-1TMT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169912586520260616140938.0001): Inlet Vane. Source Manufacturing Inc · PMA PQ1549CE · Replaces 3826099-1 · Apr 10, 2026
- [J-082269-7TMT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137618139420260616141004.0001): Ball Transfer Unit. Source Manufacturing Inc · PMA PQ1549CE · Replaces J-082269-7 · Apr 10, 2026
- [J-082269-8TMT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122760419020260616141005.0001): Ball Transfer Unit. Source Manufacturing Inc · PMA PQ1549CE · Replaces J-082269-8 · Apr 10, 2026
- [10-AB0551-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182889034120260407171338.0001): Nut, Repair, Pivot Pin. Shock Absorber Main Landing Gear. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces CRA50551 · Mar 25, 2026
- [10-AB8063-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123735622620260407171340.0001): Bolt. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces D68063 · Mar 25, 2026
- [10-AB2270-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105947983720260407171339.0001): Upper Cam Dowel, Nose Landing Gear Shock Absorber. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces C62270 · Mar 25, 2026
- [10-AB2866-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103792452220260407171339.0001): Lower Cam Dowel, Nose Landing Gear Shock Absorber. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces C62866 · Mar 25, 2026
- [3880267-1AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106532337520260107201331.0001): Seal. Able Aerospace Services, Inc. · PMA PQ2487NM · Replaces 3880267-1 · Jan 5, 2026
- [3880267-1AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195083740820260108162805.0001): Seal. Able Aerospace Services, Inc. · PMA PQ2487NM · Replaces 3880267-1 · Dec 15, 2025
- [3844015-2WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197588208020260107201214.0001): Spacer-Turb Stator Assy. Wencor, LLC · PMA PQ1370NM · Replaces 3844015-2 · Oct 30, 2025
- [706578WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100952705320260107201417.0001): Flyweight-Governor. Wencor, LLC · PMA PQ1370NM · Replaces 706578 · Sep 30, 2025
- [D56700-0023KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195920419420250930174304.0001): Spring. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces D56700-0023 · Sep 26, 2025
- [3880267-1AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167366156920250930105825.0001): Seal. Able Aerospace Services, Inc. · PMA PQ2487NM · Replaces 3880267-1 · Sep 8, 2025
- [101349-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186616963620260511125506.0001): FINAL ASSEMBLY DOGHOUSE WHEEL-CHAIR EMIRATES AIRBUS. Safran Cabin Inc. · PMA PQ1176NM · Replaces 101349-101 · Aug 13, 2025
- [101932-102](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164624682820260113212928.0001): FINAL ASSEMBLY DOGHOUSE LH/RH 6 DAIMLER BENZA310-300. Safran Cabin Inc. · PMA PQ1176NM · Replaces 101932-102 · Aug 13, 2025
- [101929-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163334799420260113212927.0001): FINAL ASSEMBLY DOGHOUSE LH/RH 10 DAIMLER BENZ A310-300. Safran Cabin Inc. · PMA PQ1176NM · Replaces 101929-1 · Aug 13, 2025
- [101931-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156760554620260113212928.0001): FINAL ASSEMBLY DOGHOUSE CTR 8 DAIMLER BENZ A310-300. Safran Cabin Inc. · PMA PQ1176NM · Replaces 101931-1 · Aug 13, 2025
- [101933-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149576268920260113212928.0001): FINAL ASSEMBLY DOGHOUSE CTR 6 DAIMLER BENZA310-300. Safran Cabin Inc. · PMA PQ1176NM · Replaces 101933-1 · Aug 13, 2025
- [101929-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135101782420260113212927.0001): FINAL ASSEMBLY DOGHOUSE LH/RH 10 DAIMLER BENZ A310-300. Safran Cabin Inc. · PMA PQ1176NM · Replaces 101929-2 · Aug 13, 2025
- [101930-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125429230020260113212927.0001): FINAL ASSEMBLY DOGHOUSE LH/RH 8 DAIMLER BENZ A310-300. Safran Cabin Inc. · PMA PQ1176NM · Replaces 101930-1 · Aug 13, 2025
- [101930-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111265964820260113212928.0001): FINAL ASSEMBLY DOGHOUSE LH/RH 8 DAIMLER BENZ A310-300. Safran Cabin Inc. · PMA PQ1176NM · Replaces 101930-2 · Aug 13, 2025
- [101928-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108701352420260113212927.0001): FINAL ASSEMBLY DOGHOUSE CTR 10 DAIMLER BENZ A310-300. Safran Cabin Inc. · PMA PQ1176NM · Replaces 101928-1 · Aug 13, 2025
- [A35994KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157306003920250805133824.0001): Block, Drive. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces A35994 · Jul 31, 2025
- [3880267-1AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161240649820250731153510.0001): Seal. Able Aerospace Services, Inc. · PMA PQ2487NM · Replaces 3880267-1 · Jul 21, 2025
- [7583141](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183290318820251205185039.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 7579002 · Jul 18, 2025
- [7583141](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176242045720251205185040.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 56433 · Jul 18, 2025
- [7583141](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173114878720251205185038.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 1744586-01 · Jul 18, 2025
- [7583141](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168898837520251205185038.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 174486-01 · Jul 18, 2025
- [7583141](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153283445420251205185040.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 56400 · Jul 18, 2025
- [7583141](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144984800320251205185039.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 7579077 · Jul 18, 2025
- [7583141](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144330721220251205185038.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces AC9780F15 · Jul 18, 2025
- [7583141](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133619176920251205185039.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 038498-15 · Jul 18, 2025
- [7583141](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116146929220251205185039.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces 1744586 · Jul 18, 2025
- [7583141](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103797630820251205185038.0001): Filter Element. PTI Technologies Inc · PMA PQ1341NM · Replaces AC9780F15Y6 · Jul 18, 2025
- [A32266KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184849160420250718155441.0001): Bolt. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces A32266 · Jul 14, 2025

All of them: https://openairdocs.org/model/airbus-industrie-a310-222/pma.md

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