# Airbus A310-304

- Type: Aircraft model (FAA registry)
- Registry code: 3940061
- Manufacturer (registry): AIRBUS
- Model: A310-304
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- 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: 0
- Page: https://openairdocs.org/model/airbus-a310-304

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 2016-16-06](https://openairdocs.org/ad/2016-16-06) (historical): Fuslage · Airbus A300 B4-603, A300 B4-605R, A300 B4-622R and 3 more. Effective Sep 8, 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

All 343: https://openairdocs.org/model/airbus-a310-304/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 (238, newest 50)

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

- [SDR CA190708004](https://openairdocs.org/sdr/CA190708004), Jul 7, 2019: O-RING. FAILED. (CAN) PILOT CALLED OVER PHONE PATCH TO REPORT THAT THEY GOT THE ECAM MESSAGE FOR GREEN SYSTEM HYDRAULIC LOW LEVEL. THEY HAVE PERFORMED THE ECAM AND QRH, SO THE 
- [SDR CA190403011](https://openairdocs.org/sdr/CA190403011), Apr 2, 2019: ENGINE. STALLED. (CAN) AFTER TAKE OFF ENGINE #1 ENCOUNTERED AN ENGINE STALL AT INITIAL CLIMB PASSING 1500FT, THE CREW REPORTS THAT THEY HEARD A COUPLE OF `THUMPS`, AND THEN NOTI
- [SDR CA180925007](https://openairdocs.org/sdr/CA180925007), Sep 21, 2018: FITTING. CORRODED. (CAN) STRONG WHISTLE SOUND FROM RL DOOR IN CRUISE. AFTER INVESTIGATION INSIDE OF DOOR,FITTING FOUND CORRODED. FITTING REPLACED. (TC# 20180925007)
- [SDR CA180910001](https://openairdocs.org/sdr/CA180910001), Sep 7, 2018: PUMP. LEAKING. (CAN) CREW REPORTED DURING FLIGHT: `GREEN HYD QTY SHOW LOW QTY ON THE NEEDLE GAGE QTY ON ECAM IS STEADY` LATER REPORT: `HYD LOW QTY WARNING ON ECAM1 LANDING GEA
- [SDR CA180423016](https://openairdocs.org/sdr/CA180423016), Apr 21, 2018: COMPUTER. FALSE INDICATION. (CAN) DURING TAKEOOF ROLL AT 80KTS ECAM ENG INDICATION REJECTED TAKEOFF AT FULL STOP ECAM FWC AMBER CRT CAUTIONS NOT AVAIL. FWC 1 REPLACED AND CHECKED SERV, IAW
- [SDR CA151013012](https://openairdocs.org/sdr/CA151013012), Oct 13, 2015: VALVE. FAILED. (CAN) DURING PUSHBACK OF ACFT FOR DEPARTURE, THE CREW TRIED TO SET THE PARKING BRAKE. THEY WERE UNSUCCESSFULL AND A LEAK WAS NOTED IN THE MAIN WHEEL WELL AREA. 
- [SDR CA151007011](https://openairdocs.org/sdr/CA151007011), Oct 1, 2015: ATTACH FITTING. BROKEN. (CAN) LEFT WING NR 3 SPOILER BROKEN AT ACTUATOR ATTACHMENT. SPOILER WAS FREE TO MOVE EXTEND/RETRACT DURING FLIGHT.
- [SDR CA150820009](https://openairdocs.org/sdr/CA150820009), Aug 20, 2015: SKIN. DELAMINATED. (CAN) THE FLIGHT CREW WAS APPROXIMATELY 4 HRS INTO THEIR FLIGHT WHEN THEY FELT A SIGNIFICANT, SUDDEN VIBRATION THAT LASTED AROUND 3-4 SECONDS AND WAS FELT IN TH
- [SDR CA150810001](https://openairdocs.org/sdr/CA150810001), Aug 7, 2015: PUMP. CRACKED. (CAN) CREW REPORTED HYDRAULIC FLUID ON BLUE SYS LOW LEVEL ECAM WARNING AND FAULT IN CRUISE. CREW DECLARED A PAN PAN, QRH PROCEDURE CARRIED AND ACFT DIVERTED. AC
- [SDR CA140919007](https://openairdocs.org/sdr/CA140919007), Sep 16, 2014: BATTERY. DAMAGED. (CAN) DURING ROUTINE VISIT IN AVIONIC SHOP FOR REGULAR BATTERY CHECK, THE CASE OF EPSU BATTERY WAS FOUND WITH A SMALL BURN. THE ASSY WAS OPENED AND CELLS NR 4 A
- [SDR CA140903013](https://openairdocs.org/sdr/CA140903013), Sep 3, 2014: COFFEEMAKER. ODOR. (CAN) CREW REPORTED FWD COFFEE MAKER BURNING ODOR IN FLIGHT. CIRCUIT BREAKER WAS PULLED AND ODOR DISSIPATED.
- [SDR FDEA201405211117](https://openairdocs.org/sdr/FDEA201405211117), May 21, 2014: FITTING. DAMAGED. LEFT RIB 5 FWD LUG BORE OUT OF ROUND REPAIRED LT RIB 5 FWD LUG BORE OUT OF ROUND IAW DWG R57249389 & COMPLIED WITH EA 6-5710-T0308275.
- [SDR FDEA201401030015](https://openairdocs.org/sdr/FDEA201401030015), Jan 3, 2014: SWITCH. MALFUNCTIONED. LEFT CABIN DOOR SHOWED UNLOCKED AT FL 240. LEVELED OFF, PERFORMED QRH & PUSHED ON THE HANDLE. DOOR SHOWED LOCKED. CONTINUED TO CLIMB & DOOR SHOWED UNLOCKED AT F
- [SDR FDEA201312142981](https://openairdocs.org/sdr/FDEA201312142981), Dec 14, 2013: JACKSCREW. LACK OF LUBE. ON APPROACH, FLAPS DID NOT EXTEND. FLAPS SYS 1 & SYS 2 FAULT LIGHTS ILLUMINATED UPON MOVING FLAP HANDLE TO ANY EXTENDED POSITION. ALTITUDE 6200 FEET AT KGTF, TE
- [SDR FDEA201312122966](https://openairdocs.org/sdr/FDEA201312122966), Dec 12, 2013: HINGE FITTING. NICKED. NOSE LANDING GEAR, RT AFT DOOR HINGE FITTING, BEARING HOLE FOUND TWO NICKS. REPAIRED IAW EA 6-5310-99725B PART 2.
- [SDR CA130531004](https://openairdocs.org/sdr/CA130531004), May 26, 2013: SWITCH. SHORTED. (CAN) DURING TROUBLESHOOTING OF UPPER BEACON SYSTEM C/B POPPING. C/B WAS PUSHED IN AND A NOISE WAS HEARD & SPARK CAME OUT FROM PANEL 426VU. FOUND TOGGLE SWITCH 
- [SDR FDEA201304240855](https://openairdocs.org/sdr/FDEA201304240855), Apr 24, 2013: WIRE HARNESS. FAILED. AFTER TOUCHDOWN, DURING ROLLOUT NR 5 AND NR 6 TIRES BLEW. ACFT REMAINED ON CENTERLINE. REMOVED AND INSTALLED AND ROUTED LT MLG HARNESS LOOM THRU NR 5 AND NR 6 B
- [SDR FDEA201304100772](https://openairdocs.org/sdr/FDEA201304100772), Apr 10, 2013: DOOR. DAMAGED. EXTENDING LANDING GEAR, RECEIVED ECAM WARNING THAT NLG DOOR WAS NOT CLOSED. BOTH PANELS SHOWED DOOR. FOLLOWED QRH LANDED UNEVENTFULLY. AFTER TAXING IN NOSE GEAR
- [SDR CA130411009](https://openairdocs.org/sdr/CA130411009), Apr 8, 2013: BRACKET. CRACKED. (CAN) DAMAGE WAS INITIALLY DISCOVERED ON MSN 482 DURING WORK PERFORMANCE IN AVIONIC BAY AS CRACK WAS APPARENT ON ONE FITTING. BASED ON REVIEW OF DAMAGE, REVIEW 
- [SDR CA120827017](https://openairdocs.org/sdr/CA120827017), Aug 25, 2012: CONTROL PANEL. OVERHEATED. (CAN) DURING CRUISE FLIGHT, FLIGHT CREW REPORTED SMOKE COMING OUT OF ADF NR 2 CONTROL PANEL. ADF2 CIRCUIT BREAKER WAS PULLED BUT SMOKE CONTINUED TO COME OUT OF 
- [SDR CA120504003](https://openairdocs.org/sdr/CA120504003), Apr 25, 2012: BULKHEAD. CORRODED. (CAN) FOUND BULKHEAD AT FRAME 39, CORRODED AND PERFORATED BETWEEN STRINGERS 54-55L AND BELOW WATERLINE Z-2557.
- [SDR CA120330005](https://openairdocs.org/sdr/CA120330005), Mar 27, 2012: TANK. RUPTURED. (CAN) ACFT RETURNED TO BLOCK AFTER A LOUD BANG HEARD IN CLIMB FOLLOWED BY WATER QTY AND PRESSURE INDICATE ZERO ON FAP PANEL. ON ARRIVAL, FOUND WATER TANK RUPTUR
- [SDR FDEA201203160978](https://openairdocs.org/sdr/FDEA201203160978), Mar 16, 2012: SHEAR PLATE. CORRODED. FWD END SHEAR PLATE FOUND CORRODED AT SEVERAL LOCATIONS FROM BS 410 TO 440, BL 0 TO LBL 24.75 FWD END SHEAR PLATE REPAIRED IAW EA F-5310-157901.
- [SDR CA120224006](https://openairdocs.org/sdr/CA120224006), Feb 19, 2012: ACTUATOR. CRACKED. (CAN) CLOSE TO 90KTS, ECAM MESSAGE "SPEED BRAKE WARNING", ENGINE SETTING WAS 96 PERCENT N1, REJECTED TAKEOFF CALLED, AFTER A FEW SECONDS, A SECOND ECAM MESSAGE 
- [SDR FDEA201202160591](https://openairdocs.org/sdr/FDEA201202160591), Feb 16, 2012: COMPUTER. MALFUNCTIONED. APPROX 1.5 HRS INTO FLIGHT, RT OTBD FUEL TANK QTY BEGAN TO DECREASE RAPIDLY. TANK WENT TO EMPTY, XX, AND REMAINED UNTIL IN DESCENT AT 16,000 FT, THEN QTY RETURN
- [SDR FDEA201112155280](https://openairdocs.org/sdr/FDEA201112155280), Dec 15, 2011: FUEL CELL. LEAKING. RT WING BOTTOM SKIN HAD FUEL SEEPAGE AT SLAT TRACK NR9 CANISTER DRAIN PORT FASTENER. REMOVED AND CLEANED THE DAMAGED SEALANT AREA. RE-APPLIED NEW SEALANT FOR RE
- [SDR FDEA201112155276](https://openairdocs.org/sdr/FDEA201112155276), Dec 15, 2011: FUEL CELL. LEAKING. RT WING FRONT SPAR HAD FUEL SEEPAGE AT RIB 18. REMOVED AND CLEANED THE DAMAGED SEALANT AREA. RE-APPLIED NEW SEALANT FOR REPAIRING IAW EO 6-5710-7-3304, PT3 AND 
- [SDR FDEA201112155274](https://openairdocs.org/sdr/FDEA201112155274), Dec 15, 2011: CANISTER. LEAKING. RT WING SLAT JACKSCREW NR 3 CANISTER DRAIN PORT HAD FUEL SEEPAGE IAW EA 6-5710-149029. REMOVED FUEL PANEL 540BB, 540CB IAW AMM 28-11-22. RE-SEALED SCREWJACK CAN
- [SDR FDEA201112025116](https://openairdocs.org/sdr/FDEA201112025116), Dec 2, 2011: SKIN. DENTED. RT WING T/E OTBD FLAP UPPER SURFACE DENTED. REPAIRED IAW SRM 57-53-12 FIG 210. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA201112025115](https://openairdocs.org/sdr/FDEA201112025115), Dec 2, 2011: DOOR. GOUGED. FOUND CREW DOOR GOUGED. REPAIRED IAW EA 6-52-50-149021 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
- [SDR FDEA201111295067](https://openairdocs.org/sdr/FDEA201111295067), Nov 29, 2011: FITTING. CRACKED. LEFT NOSE SECTION/ FR 12A STIFFENER FITTING WAS FOUND 1 EA CRACK ABOUT .7500" IN LENGTH . ON ZONE B,J AREA IAW NTM 51-10-08, PART 1. REMOVED STIFFENER FITTING A
- [SDR FDEA201111224994](https://openairdocs.org/sdr/FDEA201111224994), Nov 22, 2011: FLOOR PANEL. DAMAGED. AFT CARGO COMPARTMENT FLOOR PANEL 162AF HAS EDGE IMPACT DAMAGED. FOUND OUT OF LIMITS. REPLACED THE FLOOR PANEL BY FABRICATION OF A NEW PANEL WITH ADHESIVE AND I
- [SDR CA111116008](https://openairdocs.org/sdr/CA111116008), Nov 12, 2011: MEC. FAILED. (CAN) AFTER NORMAL ENGINE NR 2 START, NO THROTTLE RESPONSE N1 15 PERCENT, TGT 660 DEGREES, N2 60 PERCENT, FF 0.05. NR 2 ENGINE, MAIN ENGINE CONTROL (MEC) REPLAC
- [SDR FDEA201110154538](https://openairdocs.org/sdr/FDEA201110154538), Oct 15, 2011: POWER SUPPLY. NO TEST. EMERGENCY LIGHTS WOULD NOT TEST PROPERLY. R & R EMERGENCY LIGHT POWER SUPPLY AND BATTERY IAW MM 33-51-14-04-09. OK FOR SERVICE.
- [SDR FDEA201107032558](https://openairdocs.org/sdr/FDEA201107032558), Jul 3, 2011: FLOORBEAM. DAMAGED. BULK CARGO COMPARTMENT, FR 63 FLOORBEAM BOTTOM CEILING PANEL ATTACHMENT BETWEEN SEAT TRACK 1 AND 2L HAS A DRILL START. COMPLIED WITH EA 6-5310-145342 PT1.
- [SDR FDEA201107012531](https://openairdocs.org/sdr/FDEA201107012531), Jul 1, 2011: STRINGER. GOUGED. AFT CARGO COMPARTMENT LT SIDE FWD OF FR 54.1, STR 37 HAS GOUGE. REMOVED, REPAIRED AND RE-INSTALLED STRINGER SECTION IAW SRM 53-10-14, PGS 201 THROUGH 231 SRM 51
- [SDR FDEA201107012532](https://openairdocs.org/sdr/FDEA201107012532), Jul 1, 2011: SEAL. CRACKED. METALLIC VAPOR SEAL CRACKED ON LT SIDE AT FR 42-43, R & R METALLIC VAPOR SEAL ON LT SIDE FR 42-43.
- [SDR FDEA201106142246](https://openairdocs.org/sdr/FDEA201106142246), Jun 14, 2011: WEB. DAMAGED. AFT PIT FR 69 RBL 26 VERTICAL WEB PUNCTURED AT CARGO FLOOR LEVEL REMOVED AND REPLACED VERTICAL WEB AT FR 69 RBL 26 IAW SRM 51-40-21
- [SDR FDEA201106122211](https://openairdocs.org/sdr/FDEA201106122211), Jun 12, 2011: SEAT TRACK. CRACKED. SEAT TRACK NR 3 LT CORRODED AT FR 19. REMOVED CORROISON FROM NR 3 SEAT TRACK AT FR 19 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED NR 3 
- [SDR FDEA201106122212](https://openairdocs.org/sdr/FDEA201106122212), Jun 12, 2011: SEAT TRACK. CORRODED. MDCC SEAT TRACK, NR 6, RT CORRODED INSIDE TRACK. REMOVED LEVEL 1 CORROSION ON SEAT TRACK NR 6 AT FR 19 AND FOUND TO BE OUT OF LIMITS IAW AIRBUS SRM 53-10-16. RE
- [SDR FDEA201106122210](https://openairdocs.org/sdr/FDEA201106122210), Jun 12, 2011: SEAT TRACK. CORRODED. RIGHT SEAT TRACK NR6 BETWEEN FRAME 19 & 20 HAS CORRSION 1 SQ INCH. REMOVED LEVEL 1 CORROSION FROM RT NR 6 SEAT TRACK BETWEEN FRAME 19 & 20 AND FOUND BEYOND LIMI
- [SDR FDEA201106122213](https://openairdocs.org/sdr/FDEA201106122213), Jun 12, 2011: FLOORBEAM. CORRODED. MDC UNDERFLOOR TEE HAS 1 SQ INCH OF CORROSION FWD OF SEAT TRACK NR LT AT FR 12A. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. REMOVED AND R
- [SDR FDEA201106102204](https://openairdocs.org/sdr/FDEA201106102204), Jun 10, 2011: SEAT TRACK. DAMAGED. SEAT TRACK 4L AT FRAME 54.3 HAS DAMAGE TO TACK AND SCALLOPS. BLENDED DAMAGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 4L SECTION AT
- [SDR FDEA201106102201](https://openairdocs.org/sdr/FDEA201106102201), Jun 10, 2011: SEAT TRACK. DAMAGED. MDC SEAT TRACK 5R HAS 2 GOUGES AT SCALLOPS, 1 AT 54.2 AND 1 7 INCHES AFT OF 54.2. BLENDED DAMAGED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SE
- [SDR FDEA201106102203](https://openairdocs.org/sdr/FDEA201106102203), Jun 10, 2011: SEAT TRACK. DAMAGED. 2 EA GOUGES ON SEAT TRACK 3R FROM FRAME 54.2 TO FRAME 55/58. BLENDED GOUGED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 3R SECTION AT
- [SDR FDEA201106102202](https://openairdocs.org/sdr/FDEA201106102202), Jun 10, 2011: SEAT TRACK. DAMAGED. SEAT TRACK 2R AT FRAME 54.2 HAS GOUGE AT SCALLOP. BLENDED GOUGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 2R SECTION AT AT FR 54.2 
- [SDR FDEA201106052123](https://openairdocs.org/sdr/FDEA201106052123), Jun 5, 2011: FITTING. CORRODED. NR2 PYLON SPIGOT RECEPTACLE FITTING HAS PITTING CORROSION ON UPPER PLATE. REMOVED NR 2 PYLON IAW AMM 54-50-00-4 REMOVED AND REPLACED UPPER AND LOWER SPIGOT FITT
- [SDR FDEA201106052121](https://openairdocs.org/sdr/FDEA201106052121), Jun 5, 2011: FITTING. CORRODED. NR 1 PYLON SPIGOT RECEPTACLE FITTING HAS PITTING CORROSION ON UPPER PLATE. REMOVED NR 1 PYLON IAW AMM 54-50-00-4. REMOVED AND REPLACED UPPER AND LOWER SPIGOT FI
- [SDR FDEA201106012083](https://openairdocs.org/sdr/FDEA201106012083), Jun 1, 2011: SEAT TRACK. MISINSTALLED. MAIN CABIN SEAT TRACK NR 2 LT Y450 BETWEEN FRAMES 47/48 TO 49 HAS AN EXISTING REPAIR WITH INCORRECT FASTENERS INSTALLED ON TOP FLANGE. REMOVED AND REPLACED 20 E
- [SDR CA110513007](https://openairdocs.org/sdr/CA110513007), May 9, 2011: BUSHING. SEIZED. WHEN PERFORMING TASK 292500-16-1 (OPS CHECK OF RAT UPLOCK MECHANISM) DURING A-06 CHECK, RAM AIR TURBINE (RAT) FAILED TO DEPLOY FROM EITHER THE CAPTAINS` AND FIR

All 238: https://openairdocs.org/model/airbus-a310-304/reports.md

## STCs that may be installed (OpenAirDocs) (124, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC 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 ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. 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 ST02166CH](https://openairdocs.org/stc/ST02166CH): Installation of a Honeywell RESCU 406AF/AFN Emergency Locator Transmitter (ELT) System. Honeywell International Inc
- [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 ST00101LA](https://openairdocs.org/stc/ST00101LA): Installation of Hughes-Avicom Passenger Entertainment. Burrana 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 ST04555NY](https://openairdocs.org/stc/ST04555NY): Installation of the Aircraft Data Link System. Mid Canada Mod Center
- [STC ST04536NY](https://openairdocs.org/stc/ST04536NY): Installation of the CMC 9000 Flight Management System. Mid Canada Mod Center
- [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 ST02510LA](https://openairdocs.org/stc/ST02510LA): Installation of main deck cargo loading system. Ancra International LLC
- [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 ST04309CH](https://openairdocs.org/stc/ST04309CH): Installation of ADS-B OUT Global Positioning Satellite System (GPSS)/Space-Based Augmentation System (SBAS) & ADS-B IN Flight Information Services-Broadcast (FIS-B) system. Innoviator LLC
- [STC ST04149NY](https://openairdocs.org/stc/ST04149NY): Installation of Star Navigation Systems In-Flight Safety Monitoring System (ISMS). Star Navigation Systems Inc
- [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

All 124: https://openairdocs.org/model/airbus-a310-304/stcs.md

## The same model under other registry codes

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

- [Airbus Industrie A310-304](https://openairdocs.org/model/airbus-industrie-a310-304): 0 registered aircraft, registry code 3930339

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