# Airbus A310-322

- Type: Aircraft model (FAA registry)
- Registry code: 3940016
- Manufacturer (registry): AIRBUS
- Model: A310-322
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-jet
- Seats: 380
- 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-a310-322

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 2022-21-09](https://openairdocs.org/ad/2022-21-09): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 13 more. Effective Mar 14, 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 2020-01-15](https://openairdocs.org/ad/2020-01-15): Fuel · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 9 more. Effective Mar 17, 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 2019-03-09](https://openairdocs.org/ad/2019-03-09): Wings · Airbus A310-304, A310-322, A310-324 and 1 more. Effective Mar 29, 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

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 337: https://openairdocs.org/model/airbus-a310-322/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

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 (42)

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

- [SDR FDEA200903161405](https://openairdocs.org/sdr/FDEA200903161405), Mar 16, 2009: FLOORBEAM. CORRODED. AREA 100 - PREVIOUS REPAIR AT FLOORBEAM FOUND LOCATED AT FR 63 BTW Y420 AND Y-420. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMP
- [SDR FDEA200902250721](https://openairdocs.org/sdr/FDEA200902250721), Feb 25, 2009: SMOKE WARNING. FALSE ACTIVATION. JUST BEFORE TAKEOFF, MAIN DECK CARGO SMOKE (ECAM). WORKED QRH PROCEDURE AND THEN HAD ECAM, CARGO LOOP FAULT FOR MID-DECK. WHILE RUNNING CHECKLIST FOR CARGO LOOP
- [SDR FDEA200901080081](https://openairdocs.org/sdr/FDEA200901080081), Jan 8, 2009: FRAME. CORRODED. AFT CARGO DOOR CUTOUT FRAME 59A CORROSION AT LOWER END OF DOOR FRAME. PERFORMED REPAIR PER SRM 53-17 FIG 201 AND 202A AND EA NR 6-5320-125509.
- [SDR 08FDEA00563](https://openairdocs.org/sdr/08FDEA00563), Feb 22, 2008: FITTING. CRACKED. LT WING, THREE CRACKS AT CENTRAL FITTING ATTACHMENT TO ACTUATOR AT NUMBER 4 LT SPOILER REPLACED FITTING IN ACCORDANCE WITH EA 6-5750-115315, SB A310-57-2057, IP
- [SDR 07FDEA04554](https://openairdocs.org/sdr/07FDEA04554), Oct 10, 2007: STRINGER SPLICE. MISREPAIRED. AFT PIT STRINGER SPLICE REPAIR AT STRINGER 52L FRAME 60/61 REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED D
- [SDR 07FDEA04475](https://openairdocs.org/sdr/07FDEA04475), Oct 2, 2007: FLOOR SUPPORT. CORRODED. FOUND BETWEEN FRAME 67 AND FRAME 64 RBL44 FLOOR SUPPORT STRUCTURE IS CORRODED. 10-22-07 REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00; REMOV
- [SDR 07FDEA04433](https://openairdocs.org/sdr/07FDEA04433), Oct 1, 2007: MOUNT. GOUGED. NR 2 PYLON TO ENGINE FWD MOUNT PLATE, AFT INBD HOLE GOUGED. BLENDED AREA IAW A310-200 SRM 54-51-81. HOLE SIZE IS .842 WITHIN LIMITS IAW A310-200 SRM 54-51-81. C
- [SDR 07FDEA04248](https://openairdocs.org/sdr/07FDEA04248), Sep 24, 2007: SPAR. FAILED. LEFT HORIZONTAL STAB ON UPPER REAR SPAR BETWEEN RIBS 4/5 REPAIR STRAP IN WRONG MATERIAL TYPE. REMOVE AND REPLACE AS REQUIRED REMOVED STRAP IAW A310-200 FX SRM 5
- [SDR 07FDEA04251](https://openairdocs.org/sdr/07FDEA04251), Sep 24, 2007: SPAR. DAMAGED. LEFT HORIZONTAL STAB ON UPPER REAR SPAR BETWEEN RIBS 10 AND 11 REPAIR STRAP REQUIRES REMOVAL FOR MATERIAL TYPE VERIFICATION REMOVED STRAP IAW A310-200 SRM 55-11
- [SDR 07FDEA03727](https://openairdocs.org/sdr/07FDEA03727), Sep 14, 2007: STRAP. CRACKED. AREA IS RT FWD PAX/CREW DOOR CUTOUT, 3 5/8 INCH CRACK WITH POSSIBLE EXFOLIATION CORROSION EXISTS ALONG TOP EDGE OF AFT CORNER STRAP, BEGINNING 1" FROM FWD EDGE 
- [SDR 07FDEA04012](https://openairdocs.org/sdr/07FDEA04012), Aug 28, 2007: DOOR FRAME. CORRODED. AFT CARGO COMPARTMENT DOOR FRAME FOUND CORRODED, FR59A, BETWEEN STRG27 RT AND 36 RT. THE AFFECTED FRAME WAS REPAIRED BETWEEN STRG 27-36RT.
- [SDR 07FDEA03716](https://openairdocs.org/sdr/07FDEA03716), Aug 24, 2007: SEAT TRACK. CORRODED. AFT SEAT TRACK AT Y 1390 WITH CORROSION OUT OF SRM ALLOWABLE VALUES NEXT TO FR68. SEAT TRACK REPAIRED IAW SRM 53-16-10, FIG 202.
- [SDR 07FDEA01880](https://openairdocs.org/sdr/07FDEA01880), May 21, 2007: NONE. NONE. PREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE T/E OF INBOARD FLAP WS207-270 RIB4-5. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE R
- [SDR 07FDEA01890](https://openairdocs.org/sdr/07FDEA01890), May 21, 2007: SKIN. MISREPAIRED. PREVIOUS REPAIR FOUND LOCATED ON LT WING, L/E OF SLAT 3 WS 1835-1868 RIB 30-31. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS A
- [SDR 06FDEA04307](https://openairdocs.org/sdr/06FDEA04307), Dec 22, 2006: SKIN. MISREPAIRED. PREVIOUS REPAIR, FUSELAGE SKIN RT SIDE HAS EXTERNAL REPAIR DOUBLE BETWEEN FR 54.1 TO 54.2, BETWEEN STR 38 RT TO STR 40 RT, MEASURES 6.3" BY 6.2" PREVIOUSLY INST
- [SDR 06FDEA04301](https://openairdocs.org/sdr/06FDEA04301), Dec 22, 2006: HINGE FITTING. CORRODED. VERT STAB REAR SPAR NR 2 RUDDER ATTACHMENT HINGE FITTING HAS CORROSION. COMPLIED WITH EA NR 6-5540-106300 RUDDER RIB 12 AND 13 ATTACH FITTINGS CORROSION. MAJOR 
- [SDR 06FDEA04300](https://openairdocs.org/sdr/06FDEA04300), Dec 22, 2006: SKIN. DELAMINATED. RT WING, INBD FLAP, LWR EXT SKIN AT MID T/E, (1)EA AREA OF DELAMINATION APPROX 6" * 6" DIA. REPAIRED (1EA) AREA OF DELAMINATION ON RT WING I/B FLAP LOWER SKIN I
- [SDR 06FDEA1864](https://openairdocs.org/sdr/06FDEA1864), May 12, 2006: NONE. NONE. COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED LT FS 3938-3956, FS 73 AND STR 53-54, EXTERNAL DOUBLER. REPAIR REQUIRES EVALUATION 
- [SDR 06FDEA1837](https://openairdocs.org/sdr/06FDEA1837), May 12, 2006: NONE. NONE. COMPLY WITH AGING 9-AGING-INSP, PREVIOUS REPAIR FOUND LOCATED RT FS 1340-1370, FS 18 AND STR 40-41, EXTERNAL DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR
- [SDR 06FDEA1435](https://openairdocs.org/sdr/06FDEA1435), Apr 12, 2006: SKIN. CORRODED. BELLY OF A/C EXTERIOR SKIN AT FS 82 20 SQ IN OF CORROSION AROUND FASTENER. REMOVED CORROSION IAW A310-200 SRM 51-74-10 FOUND OUT OF LIMITS REPAIRED IAW EA 6- 53
- [SDR 06FDEA1434](https://openairdocs.org/sdr/06FDEA1434), Apr 12, 2006: BULKHEAD. CORRODED. REAR PRESSURE BULKHEAD INTERIOR SIDE STRG 27 TO 27 FS 80/82 HAS 6 AREAS OF CORROSION AT APPROX STRG 27R, 33-34R, 43R AND 23L AND 31R ON THE INNER RIM ANGLE. REM
- [SDR 06FDEA1432](https://openairdocs.org/sdr/06FDEA1432), Apr 12, 2006: PRESSURE PANEL. CORRODED. FOUND MAIN WHEEL WELL LT SIDE FS 48-54 WEB HAS 50 SQ IN OF CORROSION. REMOVED CORROSION IAW A310-200 SRM 51-74-10 FOUND 3 SPOTS OUT OF LIMITS. REPAIRED IAW EA 6
- [SDR 06FDEA1431](https://openairdocs.org/sdr/06FDEA1431), Apr 12, 2006: SKIN. CORRODED. RT A/C BAY BETWEEN FS 43-44 FROM STRG 37 AND BETWEEN STRG 41 TO STRG 51 HAS NUMEROUS SPOTS OF CORROSION ON SKIN AROUND RIVETS FASTENERS ADJACENT AREAS. REMOVED 
- [SDR 06FDEA1430](https://openairdocs.org/sdr/06FDEA1430), Apr 12, 2006: STRINGER. CORRODED. RT A/C BAY STRG 40 BETWEEN FS 44-47 HAS NUMEROUS SPOTS OF CORROSION ON SKIN AROUND RIVETS AND ON TOP OF VERTICAL FLANGE REF N00733. REMOVED CORROSION IAW A310-2
- [SDR 06FDEA1295](https://openairdocs.org/sdr/06FDEA1295), Apr 3, 2006: SKIN. CORRODED. FOUND RIGHT WING T/E LOWER SKIN AT T/E OF NR 2 PYLON HAS 3 AREAS OF EXFOLIATED CORROSION. COMPLIED WITH EA 6-5730-99016 PART 1.
- [SDR 06FDEA1294](https://openairdocs.org/sdr/06FDEA1294), Apr 3, 2006: ACCESS PANEL. DAMAGED. VERTICAL STAB L/E FRONT SPAR ACCESS PNL ON RT SIDE HAS 2 HOLES DOUBLE DRILLED. COMPLIED WITH EA 6-5530-97607 PART 1.
- [SDR 06FDEA1293](https://openairdocs.org/sdr/06FDEA1293), Apr 3, 2006: FRAME. CORRODED. FOUND NOSE LANDING GEAR WHEEL WELL FWD WALL HAS NUMEROUS SPOTS OF CORROSION ON FR 11. COMPLIED WITH EA 6-5310-97511 PART 1 AND PART 2.
- [SDR 06FDEA1292](https://openairdocs.org/sdr/06FDEA1292), Apr 3, 2006: SKIN. CORRODED. LT A/C BAY BETWEEN FS 39-41 HAS NUMEROUS SPOTS OF CORROSION ON SKIN FS STRG 37- 47. REMOVED CORROSION IAW A310-200 SRM 51-74-10, ALL AREAS WITHIN LIMITS IAW A31
- [SDR 06FDEA1291](https://openairdocs.org/sdr/06FDEA1291), Apr 3, 2006: SKIN. CORRODED. FWD OF LT AIR COND CUT OUT EXTERNAL DOUBLER HAS NUMEROUS SPOTS OF CORROSION ON SKIN AND AROUND FASTENERS. REMOVED CORROSION IAW A310-200SRM 51-74-10 ALL AREAS F
- [SDR 06FDEA1290](https://openairdocs.org/sdr/06FDEA1290), Apr 3, 2006: STRUCTURE. DAMAGED. FOUND VERTICAL LEADING EDGE RIGHT SIDE ATTACH LANDING HAS ELONGATED FASTENER HOLE AT APPROXIMATELY RIB 14. COMPLIED WITH EA 6-5530-97607 PART 1.
- [SDR 06FDEA1289](https://openairdocs.org/sdr/06FDEA1289), Apr 3, 2006: REPAIR. UNKNOWN. REPAIR LOC, ON LT O/B FLAP UPPER SURFACE 48 INCH FROM I/B END REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVE
- [SDR 06FDEA1288](https://openairdocs.org/sdr/06FDEA1288), Apr 3, 2006: FLOOR SUPPORT. CRACKED. FOUND BULK CARGO BAY LEFT SIDE FLOOR SUPPORT BETWEEN FS 65 AND 66 IS CRACKED. REMOVED AND REPLACED SUPPORT SECTION IAW A310-200 SRM 51-72-10.
- [SDR 06FDEA1287](https://openairdocs.org/sdr/06FDEA1287), Apr 3, 2006: REPAIR. UNKNOWN. REPAIR LOC, ON R1 DOOR UPPER EDGE REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMPLIED WITH EA 6-5
- [SDR 06FDEA1286](https://openairdocs.org/sdr/06FDEA1286), Apr 3, 2006: REPAIR. UNKNOWN. REPAIR LOC, AT FS 87 STRG 34R REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMPLIED WITH EA 6-5330-
- [SDR 06FDEA1285](https://openairdocs.org/sdr/06FDEA1285), Apr 3, 2006: FLOORBEAM. CORRODED. BULK CARGO FLOOR STRUCTURE BEAM AT FR. 66 CENTER TOP BEAM HAS EXFOLIATED CORROSION MEASURING 2 INCH BY 3 IN. REMOVED AND REPLACED FLOORBEAM IAW A310-200 SRM 51-
- [SDR 06FDEA1284](https://openairdocs.org/sdr/06FDEA1284), Apr 3, 2006: REPAIR. UNKNOWN. REPAIR LOC, LT HORIZ STAB REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED IAW EA 6-5510-97564
- [SDR 06FDEA1283](https://openairdocs.org/sdr/06FDEA1283), Apr 3, 2006: SKIN. CORRODED. RT A/C BAY BETWEEN FS 45-46 BETWEEN STRG 37- 45 HAS NUMEROUS SPOTS OF CORROSION ON SKIN AROUND RIVETS FASTENERS AND SIDE OF 3 ANGLE WEB. REMOVED CORROSION IAW A
- [SDR 06FDEA1282](https://openairdocs.org/sdr/06FDEA1282), Apr 3, 2006: SKIN. CORRODED. BELLY OF A/C EXTERIOR SKIN FROM FS 86 TO 90 HAS 25 SQ IN OF CORROSION AROUND FASTENERS. REMOVED CORROSION IAW A310-200 SRM 51-74-10 MATERIAL WITHIN LIMITS IAW A
- [SDR 06FDEA1268](https://openairdocs.org/sdr/06FDEA1268), Mar 29, 2006: UNKNOWN. WARNING MESSAGE. DURING CLIMB-OUT FROM PEN MID2 'A' FAULT ILLUMINATED, FOLLOWED SHORTLY BY MID1 CARGO SMOKE LOOP FAULT. PERFORMED ECAM AND QRH PROCEDURES NO HELP. ECAM ADVISORY 
- [SDR 04FDEA03448](https://openairdocs.org/sdr/04FDEA03448), Dec 18, 2004: DISPLAY. INTERMITTENT. REJECTED TAKEOFF IND DUE TO F/O PFD & ND BLANKING AT ABOUT 95 KTS. DISPLAYS RETURNED BY THE TIME THE A/C STARTED SLOWING. BACK TO RAMP TO ALLOW BRAKES TEMPS TO 
- [SDR 20000911SH009](https://openairdocs.org/sdr/20000911SH009), Aug 28, 2000: STRUCTURE. CORRODED. WHILE C/W A DETAILED VISUAL INSPECTION OF THE LEFT PYLON SPIGOT BALL JOINT HOLE AS DIRECTED BY A310 MPD TASK NR 545017-02-1, CORROSION WAS NOTED. AFTER CORROSIO
- [SDR 20000911SH008](https://openairdocs.org/sdr/20000911SH008), Aug 28, 2000: STRUCTURE. CORRODED. WHILE C/W A DETAILED VISUAL INSPECTION OF THE RIGHT PYLON SPIGOT BALL JOINT HOLE AS DIRECTED BY A310 MPD TASK NR 545017-02-1, CORROSION WAS NOTED. AFTER CORROSI

## STCs that may be installed (OpenAirDocs) (106, 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 ST04299CH](https://openairdocs.org/stc/ST04299CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) OUT System utilizing upgraded Aviation Communication & Surveillance Systems (ACSS) XS-950 Mode-S Transponders paired with the aircraft's existing GPS Source or newly installed ADS-B dedicated GPS source listed on AML number ST04299CH, and in accordance with Global Aerospace Design Corp. Master Drawing List, No. GR0252-MDL listed on AML number ST04299CH. Global Aerospace Design 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 ST04218AT](https://openairdocs.org/stc/ST04218AT): Version 7.1 Software upgrade or Installation of the Aviation Communication & Surveillance Systems (ACSS) TCAS II, Model TCAS 2000, P/N 7517900-10020. The installation also includes a Mode S ATC Transponder System, Model XS-950, P/N 7517800-10007. Aviation Communication and Surveillance Systems (ACSS) LLC
- [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 ST00947LA](https://openairdocs.org/stc/ST00947LA): Installation of a main deck cargo handling system. 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

All 106: https://openairdocs.org/model/airbus-a310-322/stcs.md

## The same model under other registry codes

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

- [Airbus Industrie A310-322](https://openairdocs.org/model/airbus-industrie-a310-322): 0 registered aircraft, registry code 3930334

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