# Airbus A310-324 - Type: Aircraft model (FAA registry) - Registry code: 3940014 - Manufacturer (registry): AIRBUS - Model: A310-324 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - 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-a310-324 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 2020-26-11](https://openairdocs.org/ad/2020-26-11): Equipment/furnishings · Airbus A300 F4-605R and A310-324. Effective Jan 27, 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 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 346: https://openairdocs.org/model/airbus-a310-324/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 (1,439, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR FDEA201909112203](https://openairdocs.org/sdr/FDEA201909112203), Sep 11, 2019: GEARBOX. FAILED. PDIS 809 27-80 2171 11SEP19 SAT OPEN U LOGPAGES:2553291 DURING EXTENSION OF FLAPS AT 40 DEGREES, RECEIVED SLATS FAULT SYS 1 AND 2. CYCLED PER ECAM, FAULT REILLU - [SDR FDEA201909102197](https://openairdocs.org/sdr/FDEA201909102197), Sep 10, 2019: COMPUTER. FAULTY. PDIS 809 27-80 2168 10SEP19 AFW OPEN U DURING ARRIVAL TO KAFW WHILE EXTENDING THE SLATS HAD SLATS 1&2 FAULT. SLATS WERE STUCK AT 5 DEGREE. RETRACTED SLATS AND I - [SDR FDEA2019060311203](https://openairdocs.org/sdr/FDEA2019060311203), May 31, 2019: SEQUENCE VALVE. MISALIGNED. 6685 ON GEAR EXTENSION RECEIVED UNSAFE INDICATION FOR RT MLG ON SYS 1 SYS 2. COMPLIED WITH QRH PROCEDURES AND LG GRAVITY EXTENSION CHECKLIST. GEAR DOORS REMAINE - [SDR FDEA201903010528](https://openairdocs.org/sdr/FDEA201903010528), Mar 1, 2019: LINKAGE. BROKEN. PDIS 811 32-30 4584 01MAR19 GRR DURING LANDING GEAR RETRACTION. L/G RETRACTION FAULT. THE LEFT GEAR DOOR AMBER LIGHT WAS LIT AND THE RED UNLOCKED LIGHT WAS LIT. - [SDR FDEA201902120385](https://openairdocs.org/sdr/FDEA201902120385), Feb 12, 2019: STRUT. INOPERATIVE. ON APPROACH INITIAL GEAR EXTENSION DID NOT SHOW NOSE GEAR GREEN LOCKED INDICATION BUT RED UNLOCKED. RAN QRH AND ATTEMPTED MANUAL GEAR EXTENSION. ON FIRST ATTEMP - [SDR FDEA2019020870269](https://openairdocs.org/sdr/FDEA2019020870269), Feb 7, 2019: SEQUENCE VALVE. MALFUNCTIONED. ON APPR FOR 20 YEG, GEAR DOWN SELECTED, GOT AN UNSAFE GEAR INDICATION ON NOSE GEAR. FOLLOWED ECAM & QRH. EXTENDED GEAR W/GRAVITY PROCEDURE. TUG TO GATE. CARRIED - [SDR FDEA201901030010](https://openairdocs.org/sdr/FDEA201901030010), Jan 3, 2019: ACTUATOR. MALFUNCTIONED. AT FL340 GOT YELLOW SYS HYD RESERVOIR ECAM WITH CONFIRMED LOW QTY. EMER RTN TO MEM. COMPLETED INSTALL OF #4 LH SPOILER ACTUATOR REFERENCE AIRBUS A310-300 AMM 27 - [SDR FDEA2018040853507](https://openairdocs.org/sdr/FDEA2018040853507), Dec 15, 2018: ARM. FAILED. AFTER EXTENDING THE LANDING GEAR, THE NOSE GEAR INDICATED UNLOCKED ON SYSTEM 1 AND 2. AFTER ABOUT 3 MINUTES,, SHOWED LOCKED ON SYSTEM 1 AND 2. REMOVED AND REPLA - [SDR FDEA201812153507](https://openairdocs.org/sdr/FDEA201812153507), Dec 15, 2018: WARNING SYSTEM. MALFUNCTIONED. AFTER EXTENDING THE LANDING GEAR, THE NOSE GEAR INDICATED UNLOCKED ON SYSTEM 1 AND 2. AFTER ABOUT 3 MINUTES, SHOWED LOCKED ON SYSTEM 1 AND 2. - [SDR FDEA201811053107](https://openairdocs.org/sdr/FDEA201811053107), Nov 5, 2018: TEE FITTING. CRACKED. CNTR WING INSP REAR SPAR INTERNAL ANGLE/TEE FITTING FR44 RT SIDE FWD HOLE WITH CRACK SIGNAL. COMPLIED WITH EA:6-5710-T0343040 PT1 REPAIRED CENTER WING REAR SPAR - [SDR FDEA201811053106](https://openairdocs.org/sdr/FDEA201811053106), Nov 5, 2018: TEE FITTING. CRACKED. CNTR WING INSP REAR SPAR INTERNAL ANGLE/TEE FITTING FR44 LT SIDE MID HOLE WITH CRACK SIGNAL. COMPLIED WITH EA:6-5710-T0343040 PT1 REPAIRED CENTER WING REAR SPAR - [SDR FDEA201810202960](https://openairdocs.org/sdr/FDEA201810202960), Oct 20, 2018: SUPPORT BEAM. DAMAGED. MDCC FWD UTILITY AREA FR14-FR17, -Y1456 LONGITUDINAL SUPPORT BEAM FOUND 1EA HOLE ENLARGED REFER TO SRM 53-12-15 FIG. 207 REPAIRED THE -Y1456 LONGITUDINAL SUPPOR - [SDR FDEA2018042601120](https://openairdocs.org/sdr/FDEA2018042601120), Apr 25, 2018: POWER SUPPLY. FAILED. EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY 29WLI IAW AMM 33-51-14-04-09. OPS CHECKED GOOD. - [SDR FDEA201802220470](https://openairdocs.org/sdr/FDEA201802220470), Feb 22, 2018: SLAT SYSTEM. FAULTED. DURING APPROACH, SLATS SYSTEMS 1 & 2 FAULTED, SLATS STUCK IN THE RETRACTED POSITION, RAN THE QRH, PERFORMED A NO SLAT LANDING. NO TRIPPED INDICATIONS. COMPLIED - [SDR FDEA201802140400](https://openairdocs.org/sdr/FDEA201802140400), Feb 14, 2018: BUSHING. WORN. R1 DOOR HARD TO OPEN FROM THE INSIDE AND OUTSIDE. INSPECTED THE R1 DOOR, AND FOUND UPPER AND LOWER HINGE SUPPORT ARM HAT BUSHINGS MIGRATED. NO DAMAGE FOUND ON R - [SDR FDEA201710193010](https://openairdocs.org/sdr/FDEA201710193010), Oct 19, 2017: SLIDE. INOPERATIVE. L1 DOOR SLIDE IS INOPERATIVE. - [SDR FDEA201709182589](https://openairdocs.org/sdr/FDEA201709182589), Sep 18, 2017: STIFFENER. CORRODED. LOWER SKIN STIFFENER CORRODED BETWEEN FRAMES 43 & 46, Y1456. COMPLIED WITH EA6-5710-T0335320 P1. MAJOR REPAIR IAW GMM6-2-100. - [SDR FDEA201709132525](https://openairdocs.org/sdr/FDEA201709132525), Sep 13, 2017: STIFFENER. CORRODED. LOWER SKIN STIFFENER CORRODED,BETWEEN FRAMES 43 AND 47, Y-1456. COMPLIED WITH EA 6-5710-T0335320 P1. MAJOR REPAIR IAW GMM6-2-100. - [SDR FDEA201709072463](https://openairdocs.org/sdr/FDEA201709072463), Sep 7, 2017: STRINGER. DAMAGED. AFT CABIN UNDERFLOOR COMPT FR74-FR75, S45R STRINGER 1EA FASTENER HOLE DAMAGED. AFT CABIN UNDERFLOOR COMPT FR74-FR75,S-45R STRINGER 1EA FASTENER HOLE DAMAGED. RE - [SDR FDEA201708282387](https://openairdocs.org/sdr/FDEA201708282387), Aug 28, 2017: SPAR. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 1 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201708282385](https://openairdocs.org/sdr/FDEA201708282385), Aug 28, 2017: SPAR. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 4 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201708282384](https://openairdocs.org/sdr/FDEA201708282384), Aug 28, 2017: SPAR. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 10 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201708282383](https://openairdocs.org/sdr/FDEA201708282383), Aug 28, 2017: SPAR. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 52 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201708282382](https://openairdocs.org/sdr/FDEA201708282382), Aug 28, 2017: SPAR. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 60 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201708282381](https://openairdocs.org/sdr/FDEA201708282381), Aug 28, 2017: SPAR. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 62 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201708282380](https://openairdocs.org/sdr/FDEA201708282380), Aug 28, 2017: SPAR. CRACKED. RIGHT REAR SPAR INTERNAL ANGLE NR 2 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201708282379](https://openairdocs.org/sdr/FDEA201708282379), Aug 28, 2017: SPAR. CRACKED. RIGHT REAR SPAR INTERNAL ANGLE NR 8 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201708282378](https://openairdocs.org/sdr/FDEA201708282378), Aug 28, 2017: SPAR. CRACKED. RIGHT REAR SPAR INTERNAL ANGLE, NR 14 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201708282377](https://openairdocs.org/sdr/FDEA201708282377), Aug 28, 2017: FRAME ANGLE. CRACKED. RIGHT REAR FRAME INTERNAL ANGLE NR 23 HOLE, NDT INSPECTION FOUND A CRACK. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201707151956](https://openairdocs.org/sdr/FDEA201707151956), Jul 15, 2017: SPAR. CRACKED. RIGHT WING REAR SPAR INTERNAL ANGLE NR 60 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201707151951](https://openairdocs.org/sdr/FDEA201707151951), Jul 15, 2017: SPAR. CRACKED. RIGHT WING REAR SPAR INTERNAL ANGLE NR 16 HOLE, NDT INSPECTION FOUND CRACK SIGNAL. COMPLED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201707151950](https://openairdocs.org/sdr/FDEA201707151950), Jul 15, 2017: SPAR. CRACKED. RIGHT WING REAR SPAR INTERNAL ANGLE NR 12 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW IAW GMM 6-2-100. - [SDR FDEA201707151949](https://openairdocs.org/sdr/FDEA201707151949), Jul 15, 2017: SPAR. CRACKED. RIGHT REAR SPAR INTERNAL ANGLE NR 7 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201707151948](https://openairdocs.org/sdr/FDEA201707151948), Jul 15, 2017: ANGLE. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 61 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0334453 P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201707151947](https://openairdocs.org/sdr/FDEA201707151947), Jul 15, 2017: SPAR. CRACKED. LEFT WING REAR SPAR INTERNAL ANGLE NR 13 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0334453 P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201707151959](https://openairdocs.org/sdr/FDEA201707151959), Jul 15, 2017: SKIN. CRACKED. RIGHT WING RIB 11, CRACKED ON LOWER SKIN ACROSS A FASTENER HOLE APPROX 1.0 INCH IN LENGTH NEAR ACCESS PANEL 681AB. COMPLIED WITH EA 6-5730-T0334254 P1. MAJOR RE - [SDR FDEA201707151958](https://openairdocs.org/sdr/FDEA201707151958), Jul 15, 2017: SKIN. CRACKED. LEFT WING RIB 11, CRACKED ON THE LOWER SKIN ACCROSS A FASTENER HOLE APPROX 1.5 INCH IN LENGTH, NEAR ACCESS PANEL 581AB. COMPLIED WITH EA 6-5730-T0334254, P1. MA - [SDR FDEA201707151946](https://openairdocs.org/sdr/FDEA201707151946), Jul 15, 2017: ANGLE. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 53 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAM THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM51 - [SDR FDEA201707151957](https://openairdocs.org/sdr/FDEA201707151957), Jul 15, 2017: SPAR. CRACKED. RIGHT REAR SPAR INTERNAL ANGLE NR 63 HOLE NDT INSPECTION FOUND CRACK SIGNAL. RIGHT REAR SPAR INTERNAL ANGLE 63 HOLE NDT INSPECTION FOUND CRACK SIGNAL. REAM THE - [SDR FDEA201707151955](https://openairdocs.org/sdr/FDEA201707151955), Jul 15, 2017: SPAR. CRACKED. RIGHT WING REAR SPAR INTERNAL ANGLE NR 38 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION IAW NTM 51-10 - [SDR FDEA201707151954](https://openairdocs.org/sdr/FDEA201707151954), Jul 15, 2017: SPAR. CRACKED. RIGHT WING REAR SPAR INTERNAL ANGLE NR 35 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION IAW NTM 51-10 - [SDR FDEA201707151953](https://openairdocs.org/sdr/FDEA201707151953), Jul 15, 2017: SPAR. CRACKED. RIGHT WING REAR SPAR INTERNAL ANGLE NR 33 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE I - [SDR FDEA201707151952](https://openairdocs.org/sdr/FDEA201707151952), Jul 15, 2017: SPAR. CRACKED. RIGHT REAR SPAR INTERNAL ANGLE NR 30 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAM THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM5 - [SDR FDEA201707151945](https://openairdocs.org/sdr/FDEA201707151945), Jul 15, 2017: SPAR. CRACKED. LEFT REAR SPAR INTERNAL ANGLE NR 35 HOLE NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE AFFECTED HOLE THROUGH ALL LAYERS IAW SRM 51-40-44, PERFORM ROTOTEST INS - [SDR FDEA201707111907](https://openairdocs.org/sdr/FDEA201707111907), Jul 11, 2017: ANGLE. CRACKED. LEFT WING REAR SPAR INERNAL ANGLE 16 HOLE FOUND CRACKED. REPAIRED IAW EA 6-5710-T0334453 P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201707051852](https://openairdocs.org/sdr/FDEA201707051852), Jul 5, 2017: SKIN. CORRODED. FWD TOILET SERVICE PANEL LOWER CUTOUT SKIN DELAMINATED. INSPECTED FOUND SKIN INNER STIFFENER CORRODED AND OUT OF LIMITS IAW SRM 51-40-21, & SRM 53-12-18, FIG 2, - [SDR FDEA201706201716](https://openairdocs.org/sdr/FDEA201706201716), Jun 20, 2017: PITOT TUBE. OBSTRUCTED. DURING TAKEOFF, FIRST OFFICER`S AIRSPEED TAPE SHOWED BETWEEN 40 - 45 KNTS, WITH CAPTAIN`S AIRSPEED TAPE AND STANDBY AIRSPEED BETWEEN 100 - 110 KNTS. ABORTED SHO - [SDR FDEA201706011556](https://openairdocs.org/sdr/FDEA201706011556), Jun 1, 2017: INDICATION SYS. INTERMITTENT. R1 ENTRY DOOR SLIDE ARMED INDICATOR DOES NOT SHOW ARMED ON ECAM. CLEANED CONNECTOR ON 14WN RT DOOR ESCAPE SLIDE ARM SWITCH. CLOSED AND ARMED R1 DOOR SLIDE AND S - [SDR FDEA201705031343](https://openairdocs.org/sdr/FDEA201705031343), May 3, 2017: JACKSCREW. LACK OF LUBE. WHEN SELECTING FLAPS TO 15, NOTICE BINDING LEAVING THE SLATS/FLAPS 15/0 GATE AT FLAPS 15 RECEIVED FLAP FAULT SYS 1 AND 2. CYCLED THE FLAP HANDLE, NO CHANGE. QRH - [SDR FDEA201704261272](https://openairdocs.org/sdr/FDEA201704261272), Apr 26, 2017: POWER SUPPLY. INOPERATIVE. R1 DOOR SLIDE FAIL TO ARM. REMOVED AND REPLACED AUTONOMOUS STANDBY POWER SUPPLY UNIT 70WN AND BATTERY 1 IAW AMM 52-73-18-04, BITE TESTED OK, R1 SLIDE INDICATION All 1,439: https://openairdocs.org/model/airbus-a310-324/reports.md ## STCs that may be installed (OpenAirDocs) (117, 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 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 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 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 All 117: https://openairdocs.org/model/airbus-a310-324/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Airbus Industrie A310-324](https://openairdocs.org/model/airbus-industrie-a310-324): 0 registered aircraft, registry code 3930318 --- 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.