# Airbus A310-203 - Type: Aircraft model (FAA registry) - Registry code: 3940008 - Manufacturer (registry): AIRBUS - Model: A310-203 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-jet - Seats: 280 - 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-a310-203 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 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 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 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-a310-203/ads.md ## Information bulletins (advisory) (4) - [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-08-31](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 (2,392, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR FDEA201511093525](https://openairdocs.org/sdr/FDEA201511093525), Nov 9, 2015: BATTERY. INOPERATIVE. DURING SERVICE CHECK, FOUND ASPSU FAULTED NR 2 BATTERY REASON CODE. R & R NR 2 BATTERY ON ASPSU IAW AMM 52-73-18-04. PERFORMED BITE TEST IAW AMM 52-73-00-05, SY - [SDR FDEA201510293405](https://openairdocs.org/sdr/FDEA201510293405), Oct 29, 2015: GEARBOX. LACK OF LUBE. SELECTED FLAPS 15 DEGREES AT 200 KTS. FLAPS SYS 1 & 2 FAULT LIGHTS & ON ECAM. CYCLED HANDLE WITH SAME RESULT. FOLLOWED ECAM & QRH. LANDED SLATS 30, FLAPS 0 UNEV - [SDR FDEA201509042800](https://openairdocs.org/sdr/FDEA201509042800), Sep 4, 2015: SENSOR. FAILED. AUTO THROTTLES OFF, SET N1 TO 107% ON BOTH ENGS. THERE WAS SIGNIFICANT THRUST DIFFERENCE CAUSING YAW ON CLIMB OUT. WE GOT ECAM ENG EXCEEDENCE WARNING & REDUCED - [SDR FDEA201507202272](https://openairdocs.org/sdr/FDEA201507202272), Jul 20, 2015: ANGLE. CORRODED. AFT UPPER CORNER OF L1 ENTRY DOOR CORNER ANGLE CORRODED. FABRICATED IAW EA 6-5210-T0318924 AND INSTALLED IAW SRM 51-40-20. - [SDR FDEA201506031688](https://openairdocs.org/sdr/FDEA201506031688), Jun 3, 2015: UNKNOWN. MALFUNCTIONED. LOST CABIN AT APPROX 18 - 210 FL, THE MAN PRESS VLV SHOWED OPEN & TRIED MANUAL CONTROL & IT DID NOT FIX PROBLEMS. NEITHER PRESSURIZATION SYS FAULTED. TROUBLESHO - [SDR FDEA201504141230](https://openairdocs.org/sdr/FDEA201504141230), Apr 14, 2015: NUT. LACK OF LUBE. ON APPROACH, WHEN CONFIG FROM SLATS 15 TO FLAPS 15, RECEIVED FLAPS SYS 1 & SYS 2 FAULT. RECYCLED HANDLE TO SLATS 15 IAW PHASE ONES THEN RE-ATTEMPTED FLAPS 15, S - [SDR FDEA201503271107](https://openairdocs.org/sdr/FDEA201503271107), Mar 27, 2015: CONTROL UNIT. FAULTY. AUTO BRAKE FAIL LIGHT ILLUMINATED LATE ON TAKEOFF ROLL. IN ADDITION TO AUTO BRAKE FAIL LIGHT, ALL TRIPLE BAR LIGHTS ON MAX, MED & LOW, NO RELATED ECAM WARNING T - [SDR FDEA201502240588](https://openairdocs.org/sdr/FDEA201502240588), Feb 24, 2015: VALVE. UNKNOWN. IAW MOCC REQUEST NEED TO R & R DEPRESSURIZATION VLV 93 HM. PART ON ORDER. R & R DEPRESSURIZATION VLV 93 HM IAW 21-31-15-04-01. - [SDR FDEA201410042967](https://openairdocs.org/sdr/FDEA201410042967), Oct 4, 2014: WARNING LIGHT. FALSE ACTIVATION. AFTER TAKEOFF WITH LANDING GEAR RETRACTION, NOSE GEAR DOOR INDICATED UNSAFE, AMBER ON BOTH INDICATORS. FELT FLUTTER INDICATING DOOR WAS IN FACT STILL OPEN. AIR - [SDR FDEA201404260861](https://openairdocs.org/sdr/FDEA201404260861), Apr 26, 2014: PRESSURE SWITCH. MALFUNCTIONED. ON APPROACH WHEN WE SELECTED, SLATS EXT, GOT ECAM SLATS SYS NR 1 & NR 2 FAULT. CYCLED & SLATS EXTENDED, WHEN SELECTING FLAPS 15, GOT FLAP SYS NR 1 & NR 2 FAULT. - [SDR FDEA201402240394](https://openairdocs.org/sdr/FDEA201402240394), Feb 24, 2014: COALESCER BAG. DIRTY. AS TAKEOFF POWER WAS APPLIED ACRID SMELL DETECTED BY FIRST OFFICER THEN CAPTAIN, NOT VISIBLE, LOW SPEED REJECT AT 50 - 60 KTS. SHUTDOWN ON RWY & TUGGED TO GATE. - [SDR FDEA201312283062](https://openairdocs.org/sdr/FDEA201312283062), Dec 28, 2013: WIRE. BROKEN. R1 DOOR SLIDE ARMING LIGHT ASSEMBLY HAS BROKEN WIRES. TERMINATED WIRES TO 8WN FWD RT DOOR ESCAPE SLIDE WARNING LIGHT ASSEMBLY IAW A310-200 AWM 52-73-01. TESTED - [SDR FDEA201312132980](https://openairdocs.org/sdr/FDEA201312132980), Dec 13, 2013: VALVE. FAILED. ON DEPARTURE, CLIMBING THROUGH 10,000' CABIN ADVISORY HIGH RATE, THEN EXCESS CABIN ALTITUDE COMPLIED WITH ECAM & QRH. ACFT WOULD NOT PRESSURIZE. RETURNED TO A/P - [SDR FDEA201312102960](https://openairdocs.org/sdr/FDEA201312102960), Dec 10, 2013: CONTROL UNIT. FAULTY. COMPLETE LOSS OF COMM ON VHF 1, 2 & 3 AT 1:15 INTO 2 HR FLIGHT. WE CHECKED QRH, NO HELP. CHECK 02 MASK DOORS & RESET. UNPLUGGED & PLUGGED IN AUXILIARY HEADSETS. - [SDR FDEA201311282888](https://openairdocs.org/sdr/FDEA201311282888), Nov 28, 2013: UNKNOWN. ABNORMAL. WHEN TAKEOFF THRUST APPLIED & TOGA SELECTED ATS LEVER TRIPPED OFF. LOW SPEED REJECT ACCOMPLISHED ECAM ATTEMPTED NO HELP. REMOVED AND REPLACED THRUST CONTROL COM - [SDR FDEA201311102720](https://openairdocs.org/sdr/FDEA201311102720), Nov 10, 2013: TEE FITTING. CRACKED. CENTER WING REAR SPAR INTERNAL ANGLE LOWER SKIN TEE FITTING RT SIDE FOUND CRACKED. REPAIRED IAW EA 6-5710-T0303521. - [SDR FDEA201311102719](https://openairdocs.org/sdr/FDEA201311102719), Nov 10, 2013: TEE FITTING. CRACKED. CENTER WING REAR SPAR INTERNAL ANGLE LOWER SKIN TEE FITTING LEFT FOUND CRACKED. REPAIRED IAW EA 6-5710-T0303521. - [SDR FDEA201311052688](https://openairdocs.org/sdr/FDEA201311052688), Nov 5, 2013: FITTING. CRACKED. FRAME 40 RT UPPER CORNER FITTING FOUND CRACKED. COMPLIED WITH EA 6-5710-0303103. - [SDR FDEA201311052687](https://openairdocs.org/sdr/FDEA201311052687), Nov 5, 2013: FITTING. CRACKED. FRAME 40 LT UPPER CORNER FITTING FOUND CRACKED. COMPLIED WITH EA 6-5710-T0303103. - [SDR FDEA201311052686](https://openairdocs.org/sdr/FDEA201311052686), Nov 5, 2013: FITTING. CRACKED. FUSELAGE CENTER BOX FRAME 45 RT UPPER FRAME BASE-TO-ARCH JUNCTION FOUND CRACK AT HOLE H22 COMPLIED WITH EA 6-5310-T0303124. - [SDR FDEA201311052685](https://openairdocs.org/sdr/FDEA201311052685), Nov 5, 2013: FITTING. CRACKED. FUSELAGE CENTER BOX FRAME 44 RT UPPER FRAME BASE-TO-ARCH JUNCTION FOUND CRACKS AT H5 & H13. R & R THE SUPPORT FITTING IAW SRM 51-40-21 & EA 6-5310-T0303124. - [SDR FDEA201311052684](https://openairdocs.org/sdr/FDEA201311052684), Nov 5, 2013: FITTING. CRACKED. FUSELAGE CENTER BOX FRAME 43 RT UPPER FRAME BASE-TO-ARCH JUNCTION FOUND CRACK AT HOLE H2. R & R NEW SUPPORT FITTING IAW SRM 51-40-21 & EA 6-5310-T0303124. - [SDR FDEA201311052683](https://openairdocs.org/sdr/FDEA201311052683), Nov 5, 2013: FITTING. CRACKED. FUSELAGE CENTER BOX FRAME 45, LT UPPER FRAME BASE-TO-ARCH JUNCTION FOUND CRACK AT HOLE H22 COMPLIED WITH EA 6-5310-T0303124. - [SDR FDEA201311042676](https://openairdocs.org/sdr/FDEA201311042676), Nov 4, 2013: FITTING. CRACKED. FUSELAGE CENTER BOX FRAME 43, LT UPPER FRAME BASE-TO-ARCH JUNCTION FOUND CRACKED. R & R SUPPORT FITTING SRM 51-40-21 & EA 6-5310-T0303124. - [SDR FDEA201311042677](https://openairdocs.org/sdr/FDEA201311042677), Nov 4, 2013: SUPPORT FITTING. CRACKED. FUSELAGE CENTER BOX, FRAME 44 LT UPPER FRAME SUPPORT FITTING FOUND CRACKED. R & R NEW SUPPORT FITTING IAW SRM 51-40-21 & EA 6-5310-T0303124. - [SDR FDEA201310312659](https://openairdocs.org/sdr/FDEA201310312659), Oct 31, 2013: SKIN. CRACKED. FUSELAGE SKIN UNDER PICKUP ANGLE AT FRAME 40 LT, FASTER HOLE 14 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0303309. - [SDR FDEA201310202557](https://openairdocs.org/sdr/FDEA201310202557), Oct 20, 2013: SEAT TRACK. CORRODED. MAIN DECK FRAMES 47-48 -Y953, SEAT TRACK CORRODED. SPLICE REPAIRED SEAT TRACK IAW EA 6-5315-T0303255 & SRM 53-10-16. - [SDR FDEA201310182549](https://openairdocs.org/sdr/FDEA201310182549), Oct 18, 2013: FLOOR SUPPORT. CORRODED. MAIN DECK FR 12A-14 Y770, FLOOR SUPPORT CORRODED REPLACED THE CORRODED FLOOR SUPPORT IAW SRM 51-40-21. - [SDR FDEA201310072434](https://openairdocs.org/sdr/FDEA201310072434), Oct 7, 2013: ENGINE. FAILED. DURING CLIMBOUT, NR 1 ENGINE OVERTEMPED. HEARD A LOUD POP WITH A YAW TO THE LEFT. ALL ENG INDICATIONS WERE NORMAL EXCEPT EGT WHICH WAS 700 DEGREES HIGHER THEN N - [SDR FDEA201309282335](https://openairdocs.org/sdr/FDEA201309282335), Sep 28, 2013: ENGINE. POWER LOSS. THROTTLE KNOBS STAYED WITH A HALF A KNOB. ON TAXI OUT ENG 1 LAGGED ENG NR 2 N1 UP TO 30 PERCENT ACCELARATION. FOR TAKEOFF, TRIED TO SET 40 PERCENT N1 AND ENG NR - [SDR FDEA201309212274](https://openairdocs.org/sdr/FDEA201309212274), Sep 21, 2013: JACKSCREW. WORN. ON APPLICATION OF SLATS 1 & 2, FAULT LIGHT CAME ON. SLATS LESS THAN 15- CYCLED HANDLE & NO CHANGE. RAN CHECKLIST & MADE NO SLAT LANDING. AFTER LANDING TRIED SLA - [SDR FDEA201309042115](https://openairdocs.org/sdr/FDEA201309042115), Sep 4, 2013: SELECTOR VALVE. FAILED. ON LANDING, NOSE TILLER COULD NOT BE MOVED. DIFFERENTIAL BRAKING USED TO CLEAR RWY. TROUBLESHOT IAW TSM 32-51-00 FIG 103 TO STEP 4. NOSE GEAR DOORS WILL NOT RAI - [SDR FDEA201308242031](https://openairdocs.org/sdr/FDEA201308242031), Aug 24, 2013: WINDOW. CRACKED. CAPTAIN'S FRONT FIXED WINDOW CRACKED AT FL 390. INSTALLED SERVICEABLE WINDSHIELD TO STEP 1.E.17, REF MM 56-11-11-04. WINDOW IS INSTALLED SEALED & TORQUED. - [SDR FDEA201308201962](https://openairdocs.org/sdr/FDEA201308201962), Aug 20, 2013: FITTING. CRACKED. FRAME 43A UPPER FITTING JUNCTION WITH FUSELAGE PANEL LWR FASTENER HOLE FOUND CRACK. COMPLETED WITH EA 6-5710-T0301826. - [SDR FDEA201308201961](https://openairdocs.org/sdr/FDEA201308201961), Aug 20, 2013: FITTING. CRACKED. FRAME 43A UPPER FITTING JUNCTION WITH FUSELAGE PANEL LWR FASTENER HOLE FOUND CRACK. COMPLETED WITH EA 6-5710-T0301826. - [SDR FDEA201308171919](https://openairdocs.org/sdr/FDEA201308171919), Aug 17, 2013: SPAR. DAMAGED. RT PYLON LWR SPAR BETWEEN RIBS 6 AND 7. REPAIRED IAW EA 6-5450-117917C, PART 2. COMPLIED WITH EA 6-5450-117917C PART2. REMOVED AND INSTALLED THE REPAIR DOUBLER - [SDR FDEA201308171918](https://openairdocs.org/sdr/FDEA201308171918), Aug 17, 2013: SKIN. CORRODED. LT WING ROOT CENTER WING BOX BOTTOM SKIN LWR SURFACE FOUND CORRODED BETWEEN FR44-45. REMOVED CORROSION IAW SRM 51-74-10. REPAIRED EA 6-5710-T0301458. - [SDR FDEA201308161913](https://openairdocs.org/sdr/FDEA201308161913), Aug 16, 2013: FRAME. CRACKED. FUSELAGE FRAME 40, UPPER CORNER FOUND CRACK IN RT NR 2 HOLE COMPLIED WITH EA 6-5710-T0301577. - [SDR FDEA201308131861](https://openairdocs.org/sdr/FDEA201308131861), Aug 13, 2013: FRAME. CRACKED. RIGHT FUSELAGE FRAME 45 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727. - [SDR FDEA201308131860](https://openairdocs.org/sdr/FDEA201308131860), Aug 13, 2013: FRAME. CRACKED. RT FUSELAGE FRAME 44 FOUND CRACKED. REPAIRED IAW EA 6-5330-T0301676. - [SDR FDEA201308131859](https://openairdocs.org/sdr/FDEA201308131859), Aug 13, 2013: FRAME. CRACKED. RT FUSELAGE FRAME 43 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727. - [SDR FDEA201308131858](https://openairdocs.org/sdr/FDEA201308131858), Aug 13, 2013: FRAME. CRACKED. LEFT FUSELAGE FRAME 45 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727. - [SDR FDEA201308131857](https://openairdocs.org/sdr/FDEA201308131857), Aug 13, 2013: FRAME. CRACKED. LEFT FUSELAGE FRAME 44 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727. - [SDR FDEA201308131856](https://openairdocs.org/sdr/FDEA201308131856), Aug 13, 2013: FRAME. CRACKED. LEFT FUSELAGE FRAME 43 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727. - [SDR FDEA201308101829](https://openairdocs.org/sdr/FDEA201308101829), Aug 10, 2013: ENGINE. FAILED. DURING CLIMB ENG NR 1 OIL LOW QTY ADVISORY CAME ON, SHOWED 2 QUARTS. ALL OTHER INDICATIONS NORMAL. IAW QRH, MONITORED QTY. ABOUT 15 MINUTES LATER, DECIDED TO DI - [SDR FDEA201308091817](https://openairdocs.org/sdr/FDEA201308091817), Aug 9, 2013: SKIN. DELAMINATED. LEFT FWD FUSELAGE TOILET SERVICE PANEL LOWER SKIN CUTOUT DELAMINATED. REPAIRED IAW EA 6-5330-T0301676. - [SDR FDEA201308061782](https://openairdocs.org/sdr/FDEA201308061782), Aug 6, 2013: SILL. CORRODED. BULK CARGO DOOR SILL FOUND CORROSION SURROUNDING FASTENER HOLES BETWEEN FR 68 & 69. REPLACED SILL IAW SRM 51-40-21. - [SDR FDEA201307261665](https://openairdocs.org/sdr/FDEA201307261665), Jul 26, 2013: FLOOR SUPPORT. CORRODED. MAIN DECK FR 14-14B, Y730, FLOOR SUPPORT CORRODED. REPAIRED FLOOR SUPPORT IAW SRM 53-12-15/201, FIG 207. - [SDR FDEA201307261666](https://openairdocs.org/sdr/FDEA201307261666), Jul 26, 2013: FLOOR SUPPORT. CORRODED. MAIN DECK FR 12A-15A Y1456 FLOOR SUPPORT CORRODED. REPAIRED THE FLOOR SUPPORT IAW SRM 53-12-15/201, FIG 207. - [SDR FDEA201306181339](https://openairdocs.org/sdr/FDEA201306181339), Jun 18, 2013: SEAL. LEAKING. AFTER TAKE OFF, BLEED LEAK RT SIDE. REF QRH- LIGHT OUT IN FLIGHT. ON APPROACH LOWER ACCESS DOOR LIGHT CAME ON. FOUND LEAK TO BE COMING FROM THE UPPER RT CORNER All 2,392: https://openairdocs.org/model/airbus-a310-203/reports.md ## STCs that may be installed (OpenAirDocs) (99, 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 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 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 All 99: https://openairdocs.org/model/airbus-a310-203/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Airbus Industrie A310-203](https://openairdocs.org/model/airbus-industrie-a310-203): 2 registered aircraft, registry code 3930313 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.