# N430FE: 1985 Airbus Industrie A310-203

- Status: Valid registration
- Airframe: [Airbus Industrie A310-203](https://openairdocs.org/model/airbus-industrie-a310-203) (registry code 3930313, 280 seats)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) (Airbus SAS), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 394
- Year built: 1985
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: January 23, 1997
- Certificate issued: September 18, 1996
- Expires: May 31, 2028
- Mode S code: A523A0
- Registered owner: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP)
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Corporation
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=430FE
- Page: https://openairdocs.org/aircraft/N430FE

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every GE CF6-80 model are included.

## ADs that may apply (OpenAirDocs): 347 in force

### Matched by airframe (Airbus Industrie A310-203)

- [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

### Matched by engine (GE CF6-80 series)

- [AD 2024-24-03](https://openairdocs.org/ad/2024-24-03): Engine Exhaust · Boeing MD-11, MD-11F and CF6-80C2D1F. Effective Jan 13, 2025
- [AD 2023-20-08](https://openairdocs.org/ad/2023-20-08): Engine (Turbine/Turboprop) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 4 more. Effective Oct 19, 2023
- [AD 2021-26-22](https://openairdocs.org/ad/2021-26-22): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 14, 2022
- [AD 2022-02-18](https://openairdocs.org/ad/2022-02-18): Engine Mount Section · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 3 more. Effective Feb 25, 2022
- [AD 2021-14-11](https://openairdocs.org/ad/2021-14-11): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 25 more. Effective Aug 27, 2021
- [AD 2021-03-02](https://openairdocs.org/ad/2021-03-02): Fuel Control/Turbine Engines · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Mar 31, 2021
- [AD 2020-22-02](https://openairdocs.org/ad/2020-22-02): Engine Fuel and Control · General Electric CF6-80C2A5F, CF6-80C2B1F, CF6-80C2B2F and 13 more. Effective Dec 3, 2020
- [AD 2018-07-05](https://openairdocs.org/ad/2018-07-05): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 11, 2018
- [AD 2017-11-15](https://openairdocs.org/ad/2017-11-15): Turbine/ Turboprop Engine--Turbine Section · General Electric CF6-80C2L1F. Effective Jul 13, 2017
- [AD 2016-08-10](https://openairdocs.org/ad/2016-08-10): Accessory heat shield · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Jun 1, 2016
- [AD 2014-21-01](https://openairdocs.org/ad/2014-21-01): Fuel manifold · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Nov 28, 2014
- [AD 2013-08-20](https://openairdocs.org/ad/2013-08-20): Fuel tube · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 14 more. Effective May 31, 2013
- [AD 2012-03-12](https://openairdocs.org/ad/2012-03-12): No. 3 bearing packing · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Apr 5, 2012
- [AD 2012-04-05](https://openairdocs.org/ad/2012-04-05): Electronic control unit (ECU) · General Electric CF6-80C2B1F, CF6-80C2B1F1, CF6-80C2B1F2 and 8 more. Effective Mar 30, 2012
- [AD 2011-23-04](https://openairdocs.org/ad/2011-23-04): Forward engine mount assembly side links · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Dec 12, 2011
- [AD 2009-21-07](https://openairdocs.org/ad/2009-21-07): Thrust and thrust control · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Dec 1, 2009
- [AD 2009-14-08](https://openairdocs.org/ad/2009-14-08): High-pressure compressor rotor (HPCR) stages 11-14 spool/ shafts · General Electric CF6-80C2B5F. Effective Aug 5, 2009
- [AD 2009-08-06](https://openairdocs.org/ad/2009-08-06): Stage 1 high-pressure turbine (HPT) rotor  
 disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 18, 2009
- [AD 2009-07-10](https://openairdocs.org/ad/2009-07-10): High-pressure turbine rotor (HPTR) · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 6, 2009
- [AD 2009-07-03](https://openairdocs.org/ad/2009-07-03): Eddy current inspection (ECI) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Apr 30, 2009
- [AD 2009-04-10](https://openairdocs.org/ad/2009-04-10): Critical life-limited parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 30 more. Effective Mar 30, 2009
- [AD 2008-21-11](https://openairdocs.org/ad/2008-21-11): Low-pressure turbine (LPT) cases · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Nov 28, 2008
- [AD 2008-02-17](https://openairdocs.org/ad/2008-02-17): Thrust reverser actuation systems · General Electric CF6-50A, CF6-50C, CF6-50C1 and 16 more. Effective Feb 28, 2008
- [AD 2007-24-07](https://openairdocs.org/ad/2007-24-07): Thermal spray coating on certain stage 1 fan disks · General Electric CF6-80C2B1. Effective Jan 2, 2008
- [AD 2007-22-07](https://openairdocs.org/ad/2007-22-07): Electronic control unit (ECU) · General Electric CF6-80C2D1F. Effective Nov 28, 2007
- [AD 2007-21-06](https://openairdocs.org/ad/2007-21-06): Electronic control unit (ECU) · General Electric CF6-80C2A5F. Effective Nov 15, 2007
- [AD 2007-11-20](https://openairdocs.org/ad/2007-11-20): Fuel shroud retaining rings · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 22 more. Effective Jul 10, 2007
- [AD 2007-05-14](https://openairdocs.org/ad/2007-05-14): Cast titanium weld- repaired forward engine mount platforms · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 9, 2007
- [AD 2006-16-06](https://openairdocs.org/ad/2006-16-06): Certain stage 1 high- pressure turbine (HPT) rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Sep 5, 2006
- [AD 2006-06-08](https://openairdocs.org/ad/2006-06-08): Latching system of the fan reverser · General Electric CF6-80C2D1F. Effective Apr 25, 2006
- [AD 2005-17-05](https://openairdocs.org/ad/2005-17-05): High pressure compressor rotor (HPCR) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Sep 27, 2005
- [AD 2005-06-07](https://openairdocs.org/ad/2005-06-07): Directional pilot valve (DPV) assembly · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Apr 25, 2005
- [AD 2004-22-07](https://openairdocs.org/ad/2004-22-07): Stage 2 nozzle guide vanes (HPT S2 NGVs) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 1, 2004
- [AD 2004-07-13](https://openairdocs.org/ad/2004-07-13): High pressure turbine (HPT) stage 1 disks · General Electric CF6-80C2A5F, CF6-80C2B5F, CF6-80C2B7F and 1 more. Effective May 6, 2004
- [AD 2003-12-08](https://openairdocs.org/ad/2003-12-08): Directional pilot valve · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Jul 23, 2003
- [AD 2003-02-07](https://openairdocs.org/ad/2003-02-07): Low pressure turbine (LPT) shrouds · General Electric CF6-50A, CF6-50C, CF6-50C1 and 30 more. Effective Mar 3, 2003
- [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08): High pressure compressor rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Jan 23, 2003
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2001-06-09](https://openairdocs.org/ad/2001-06-09): Aft Engine Mount Link Assemblies · General Electric CF6-80A3. Effective May 1, 2001
- [AD 2000-12-08](https://openairdocs.org/ad/2000-12-08): Mount Link Assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 4 more. Effective Aug 28, 2000
- [AD 2000-03-04](https://openairdocs.org/ad/2000-03-04): General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Apr 10, 2000
- [AD 99-01-01](https://openairdocs.org/ad/99-01-01): Accessory Gearbox (AGB) idler adapters · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jan 21, 1999
- [AD 98-22-06](https://openairdocs.org/ad/98-22-06): Fan Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 41 more. Effective Nov 23, 1998
- [AD 97-22-14](https://openairdocs.org/ad/97-22-14): (HPCR) 3-9 Spool · General Electric CF6-50A, CF6-50C, CF6-50C1 and 29 more. Effective Nov 17, 1997
- [AD 96-16-07](https://openairdocs.org/ad/96-16-07): Rear Right Hand Mount Link · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective Aug 28, 1996
- [AD 95-17-16](https://openairdocs.org/ad/95-17-16): Compressor Rear Frame · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Nov 7, 1995
- [AD 95-10-11](https://openairdocs.org/ad/95-10-11): Fan Reversers · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective May 31, 1995
- [AD 94-20-06](https://openairdocs.org/ad/94-20-06): Oil System · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 27, 1994
- [AD 94-07-04](https://openairdocs.org/ad/94-07-04): High Pressure Turbine Disk · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 23, 1994
- [AD 94-06-03](https://openairdocs.org/ad/94-06-03): High Pressure Turbine Disk · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 29, 1994

### 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 421: https://openairdocs.org/aircraft/N430FE/ads.md

## Information bulletins (advisory) (9 in force)

- [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
- [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023
- [SAIB NE-11-27](https://openairdocs.org/saib/NE-11-27): Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel Nozzles. Issued Apr 5, 2011
- [SAIB NE-10-37](https://openairdocs.org/saib/NE-10-37): Engine Fuel and Control: FADEC Fuel Metering Valve Resolver Feedback Faults. Issued Jul 12, 2010
- [SAIB NE-08-44](https://openairdocs.org/saib/NE-08-44): Engine Thrust Reverser  Transcowl Clevis Pin. Issued Sep 3, 2008
- [SAIB NE-07-01](https://openairdocs.org/saib/NE-07-01): Dual engine flameouts on twin engine airplanes. Issued Oct 12, 2006

## NTSB investigations

None matched to N430FE.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19980701024669I](https://openairdocs.org/incident/19980701024669I), Jul 1, 1998: Airbus A310203 (N430FE), Boise, ID. Overheat a/c pack light and cargo smoke detect lights illuminated due faulty.

## Service difficulty reports (110, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [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 FDEA201304150784](https://openairdocs.org/sdr/FDEA201304150784), Apr 15, 2013: SKIN. CRACKED. NDT INSPECTION OF LT FRAME 54, SKIN JOINT BETWEEN S36 AND 37L, SHOWS SIX HOLES WITH POSITIVE CRACK INDICATIONS. INDICATIONS ARE AT MULTIPLE CLOCK POSITIONS. POS
- [SDR FDEA201304020712](https://openairdocs.org/sdr/FDEA201304020712), Apr 2, 2013: SHEAR TIE. DAMAGED. WHILE ACCOMPLISHING WC E6-5310-7-5020 A PT2, FOUND FR 43 SHEAR TIE HAS SHORT E.D. REMOVED AND REPLACED IAW SRM 51-72-10 AND DWG 57112116
- [SDR FDEA201303170590](https://openairdocs.org/sdr/FDEA201303170590), Mar 17, 2013: SEAT TRACK. DAMAGED. DUMMY TRACK 4L FR 54 / 54.2 FAILED GAP CHECK. REMOVED, REPAIRED AND INSTALLED DUMMY TRACK IAW SRM 53-15-16, FIG 203.
- [SDR FDEA201303150574](https://openairdocs.org/sdr/FDEA201303150574), Mar 15, 2013: SEAT TRACK. LOOSE. DUMMMY TRACK 3R FR 38.2 /40 FAILS GAP CHECK. REMOVED DUMMY TRACK AT FR 38.2 /40 IAW SRM 51-40-21, PAR 5 & PAR 7. REPAIRED DUMMY TRACK IAW SRM 53-15-16 PG 209 -2
- [SDR FDEA201303140568](https://openairdocs.org/sdr/FDEA201303140568), Mar 14, 2013: SEAT TRACK. WORN. DUMMY TRACK 2R FR 54 TO 54.2 FAILS GAP CHECK. REMOVED DUMMY TRACK 2R FR 54/54.2 IAW SRM 53-15-16. REPAIRED DUMMY TRACK 2R FR 54/54.2 IAW SRM 53-15-16. INSTALLED
- [SDR FDEA201303130567](https://openairdocs.org/sdr/FDEA201303130567), Mar 13, 2013: FLOORBEAM. CORRODED. UPON REMOVAL OF SEAT TRACK SECTION, FOUND CORROSION ON FLOORBEAM UPPER TEE TOP SURFACE AT FR 16A, Y1959 (5L)(APPROX 1 SQ IN TOTAL)
- [SDR FDEA201303120556](https://openairdocs.org/sdr/FDEA201303120556), Mar 12, 2013: SEAT TRACK. CORRODED. SEAT TRACK 5L AT FR 18 HAS CORROSION ON TOP SURFACE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED IAW DWG. A53610798, AND REPLACED SEAT TRA
- [SDR FDEA201303110547](https://openairdocs.org/sdr/FDEA201303110547), Mar 11, 2013: FLOOR PANEL. DAMAGED. FLOOR PANEL 252GF CRUSHED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV. J.
- [SDR FDEA201303110548](https://openairdocs.org/sdr/FDEA201303110548), Mar 11, 2013: FLOOR PANEL. DAMAGED. FLOOR PANEL 252MF CRUSHED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ25-005 REV J. REMOVED AND INSTALLED FLOOR PANEL IAW AMM 53-10-25-04
- [SDR FDEA201303090534](https://openairdocs.org/sdr/FDEA201303090534), Mar 9, 2013: ANGLE. CRACKED. UPON INSP/NDT OF HOLES H1 AND H2 AT ARCH FITTING AT FR43 LT SHOWS INDICATION OF CRACK ON BRACKET SIDE. REMOVED AND REPLACED ANGLE IAW SRM 51-72-10.
- [SDR FDEA201303090533](https://openairdocs.org/sdr/FDEA201303090533), Mar 9, 2013: ATTACH ANGLE. CRACKED. FOUND UPPER ATTACH ANGLE TO BE VISIBLY CRACKED. R & R FR 43 UPPER FWD ATTACH ANGLE AT ARCH FITTING IAW SRM 51-72-10.
- [SDR FDEA201303090530](https://openairdocs.org/sdr/FDEA201303090530), Mar 9, 2013: FLOOR PANEL. DAMAGED. PANEL 232XH CRUSHED AT CLS. FABRICATED REPLACEMENT PANEL232XH IAW DWG SRZ-25-005, REV Z.
- [SDR FDEA201303080526](https://openairdocs.org/sdr/FDEA201303080526), Mar 8, 2013: FLOOR PANEL. CRACKED. FLOOR PANEL 252 UF HAS 10 INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV. J.
- [SDR FDEA201303080522](https://openairdocs.org/sdr/FDEA201303080522), Mar 8, 2013: FLOOR PANEL. CRACKED. FLOOR PANEL 251GF HAS 12 INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ25-005 REV J. REMOVED AND REPLACED FLOOR PANEL IAW AMM 53-10-25-04.
- [SDR FDEA201303080518](https://openairdocs.org/sdr/FDEA201303080518), Mar 8, 2013: FLOOR PANEL. DAMAGED. FLOOR PANEL 252SF CRUSHED AT CUTOUTS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005, REV J.
- [SDR FDEA201303080517](https://openairdocs.org/sdr/FDEA201303080517), Mar 8, 2013: FLOOR PANEL. DAMAGED. FLOOR PANEL 252BF CRUSHED AT CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005, REV J.
- [SDR FDEA201303080527](https://openairdocs.org/sdr/FDEA201303080527), Mar 8, 2013: FLOORBOARD. DAMAGED. FLOORBOARD 242UJ CRUSHED AT CLS CUTOUT. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201303080525](https://openairdocs.org/sdr/FDEA201303080525), Mar 8, 2013: FLOORBOARD. DELAMINATED. FLOORBOARD 232LT IS CRUSHED AT CLS CUTOUT. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201303080524](https://openairdocs.org/sdr/FDEA201303080524), Mar 8, 2013: FLOORBOARD. DAMAGED. FLOORBOARD 232SF IS CRUSHED AT CLS CUTOUT. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201303080523](https://openairdocs.org/sdr/FDEA201303080523), Mar 8, 2013: FLOOR PANEL. DAMAGED. FLOOR PANEL 242QJ CRUSHED AT CLS CUTOUT. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201303070506](https://openairdocs.org/sdr/FDEA201303070506), Mar 7, 2013: FLOOR PANEL. CRUSHED. FLOOR PANEL 242ZJ CRUSHED AT CUTOUT. FABRICATED REPLACEMENT PANEL IAW DWG SRZ-25-005, REV J.
- [SDR FDEA201303070505](https://openairdocs.org/sdr/FDEA201303070505), Mar 7, 2013: FLOOR PANEL. CRUSHED. FLOOR PANEL 242EK CRUSHED AT CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005, REV J.
- [SDR FDEA201303070507](https://openairdocs.org/sdr/FDEA201303070507), Mar 7, 2013: FLOOR PANEL. DAMAGED. FLOOR PANEL 241NK IS BROKEN IN HALF AT CLS CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005 REV. J.
- [SDR FDEA201303060500](https://openairdocs.org/sdr/FDEA201303060500), Mar 6, 2013: FLOOR PANEL. DAMAGED. FLOOR PANEL 147AF EDGE SEALANT SOFTENED & MISSING BY A PERIMETER LENGTH OF 50". FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201203311201](https://openairdocs.org/sdr/FDEA201203311201), Mar 31, 2012: PRESSURE SWITCH. FAILED. NR 2 ENGINE FUEL FILTER CLOG ECAM/ MASTER CAUTION IMMEDIATELY AFTER TAKE OFF. ECAM CAUTION EXTINGUISHED AROUND 80 PERCENT N1 WHEN THROTTLES RETARDED. REMOVED AN
- [SDR FDEA201103010805](https://openairdocs.org/sdr/FDEA201103010805), Mar 1, 2011: FRAME. CRACKED. AVIONICS COMPARTMENT FORWARD DOOR INT SIDE, AFT FRAME IS CRACKED IN 2 PLACES AT LIGHTENING HOLES. CRACKED DOOR FRAME WAS REMOVED PER SRM 51-40-21, PARA 6. NEW F
- [SDR FDEA201102240727](https://openairdocs.org/sdr/FDEA201102240727), Feb 24, 2011: TRANSITION PANEL. CORRODED. FWD CARGO COMPARTMENT TRANSITION PANEL 131 WF HAS MULTIPLE AREAS OF CORROSION ON THE FRONT. TRANSITION PANEL WAS CORRODED AND FOUND TO BE OUT OF LIMITS IAW SRM 
- [SDR FDEA201102240726](https://openairdocs.org/sdr/FDEA201102240726), Feb 24, 2011: TRANSITION PANEL. CORRODED. FWD CARGO COMPARTMENT TRANSITION PANEL 132 WF HAS MULTIPLE AREAS OF CORROSION, FRONT AND BACK. TRANSITION PANEL WAS CORRODED AND FOUND TO BE OUT OF LIMITS IAW S
- [SDR FDEA201102230701](https://openairdocs.org/sdr/FDEA201102230701), Feb 23, 2011: SKIN. DENTED. LT WING INBD FLAP SKIN IS DENTED. BLENDED AREA NOTED; FOUND 100 PERCENT MATERIAL THICKNESS GONE IAW SRM 57-52-12, FIG 107. REMOVED DAMAGED SKIN AND REPAIRED IAW
- [SDR FDEA201102230697](https://openairdocs.org/sdr/FDEA201102230697), Feb 23, 2011: ARM. WORN. RT ELEVATOR AT 2 HINGE ARM LOWER FWD BEARING SWAGE LOOSE IN ARM - INBD TO OTBD MOVEMENT AS SEEN FROM THE TOP OF STAB. REMOVED RT ELEVATOR NR 2 HINGE ARM; R & R 
- [SDR FDEA201102230696](https://openairdocs.org/sdr/FDEA201102230696), Feb 23, 2011: STRUCTURE. DAMAGED. LT WING T/E THROUGH HOLES FOR HYD LINES ARE ELONGATED AT WS OWS 1083.
- [SDR FDEA201102210646](https://openairdocs.org/sdr/FDEA201102210646), Feb 21, 2011: WEB. CRACKED. FWD CARGO COMPARTMENT UNDER FLOOR VERTICAL WEB IS CRACKED BETWEEN FRAME 37 & FRAME 38; LBL 56. REMOVED AND REINSTALLED PALLET LATCH AT FRAME 37, RBL 33 IAW AMM 
- [SDR FDEA201102210645](https://openairdocs.org/sdr/FDEA201102210645), Feb 21, 2011: WEB. CRACKED. FWD CARGO COMPARTMENT UNDER FLOOR VERTIVAL WEB IS CRACKED BETWEEN FRAME 36 & FRAME 37; LBL 56. UPPER AND LOWER WEBS WERE REMOVED IAW SRM 51-40-21, PARA 6. NEW W
- [SDR FDEA201102180603](https://openairdocs.org/sdr/FDEA201102180603), Feb 18, 2011: FLOOR PANEL. DELAMINATED. TAIL COMPARTMENT WORK PLATFORM IS SPONGY AND HAS EXPOSED CORE - DIRECTLY INBD OF ACCESS DOOR 312 AR CUTOUT. REPAIRED TAIL COMPARTMENT WORK PLATFORM WITH THE FAB
- [SDR FDEA201102180606](https://openairdocs.org/sdr/FDEA201102180606), Feb 18, 2011: ANGLE. DAMAGED. AFT PIT SHEAR PLATE TOP "L" ANGLE HAS PREVIOUSLY DOUBLE DRILLED HOLES BETWEEN FRAME 64 AND FRAME 65; STRINGER 44L. REMOVED ANGLE IAW SRM 51-40-21, PARA 6. FABBE
- [SDR FDEA201102180605](https://openairdocs.org/sdr/FDEA201102180605), Feb 18, 2011: ANGLE. DAMAGED. AFT PIT SHEAR PLATE TOP "L" ANGLE HAS PREVIOUS DOUBLE DRILLED HOLES BETWEEN FRAME 65 AND FRAME 66; STRINGER 44LT. REMOVED ANGLE IAW SRM 51-40-21, PARA 6. FABRIC
- [SDR FDEA201102180604](https://openairdocs.org/sdr/FDEA201102180604), Feb 18, 2011: WEB. DENTED. FWD CARGO COMPARTMENT UNDER FLOOR VERTICAL WEB IS DENTED BETWEEN FRAME 34 - FRAME 35; LBL 56. REMOVED WEB IAW SRM 51-40-21, PARA 6. DISPLACED, CAPPED AND STOWED
- [SDR FDEA201102170592](https://openairdocs.org/sdr/FDEA201102170592), Feb 17, 2011: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK BETWEEN FRAME 72 AND 73 LBL 34 IS CORRODED. REMOVED CORROSION IAW SRM 53-10-16. CHECKED LIMITS, ORIGINAL THICKNESS 0.140. MATERIAL LOSS 0.
- [SDR FDEA201102160571](https://openairdocs.org/sdr/FDEA201102160571), Feb 16, 2011: SPAR. CRACKED. NR 2 PYLON HORIZ HEAT SHIELD BELOW THE LOWER SPAR IS CRACKED AND MISSING PIECES. WELD REPAIRED IAW EA 6-5750-136739.
- [SDR FDEA201102160570](https://openairdocs.org/sdr/FDEA201102160570), Feb 16, 2011: SPAR. CRACKED. LT PYLON HORIZ HEAT SHIELD BELOW THE LOWER SPAR IS CRACKED AND MISSING PIECES. WELD REPAIRED IAW EA 6-5750-136739.
- [SDR FDEA201102160572](https://openairdocs.org/sdr/FDEA201102160572), Feb 16, 2011: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK IS CORRODED BETWEEN FRAME 75 AND FRAME 76; LBL 30. REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS, ORIGINAL THICKNESS 0.0140. MATERIAL 
- [SDR FDEA201102140565](https://openairdocs.org/sdr/FDEA201102140565), Feb 14, 2011: FLOORBOARD. CORRODED. BULK CARGO COMPARTMENT FLOORBOARD 162 HF METAL TOP IS CORRODED. REMOVED TOP SHEET IAW DWG SRZ 25-011, REV "C". TOP SHEET MATERIAL ID 2024-T3 IAW DWG SRZ 25-011,
- [SDR FDEA201102140556](https://openairdocs.org/sdr/FDEA201102140556), Feb 14, 2011: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK IS CORRODED BETWEEN FRAME 75 & FRAME 76; LBL 43. REPAIRED MAIN DECK SEAT TRACK BETWEEN FRAME 74 TO FRAME 76 WITH 35 INCHES OF SEAT TRACK SE
- [SDR FDEA201102090511](https://openairdocs.org/sdr/FDEA201102090511), Feb 9, 2011: SKIN. CORRODED. FWD CARGO DOOR INNER SKIN IS CORRODED UNDER THE LOWER SEAL RETAINER. REMOVED AND REPLACED SECTION OF SKIN IAW A310-200 SRM 51-40-21, PARA 6, 7 & 13.
- [SDR FDEA201102090512](https://openairdocs.org/sdr/FDEA201102090512), Feb 9, 2011: SKIN. CORRODED. FUSELAGE INTERGAL PLATE HAS CORROSION AT FRAME 38.2; STRINGER 52R. REMOVED CORROSION PER SRM 51-74-10. FOUND TO BE OUT OF LIMITS PER SRM 53-14-12, FIG 101. FABR
- [SDR FDEA201102080499](https://openairdocs.org/sdr/FDEA201102080499), Feb 8, 2011: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 241 YN IN ZONE 240 IS CRACKED. FABRICATED NEW FLOOR PANEL 241 YN IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201102080498](https://openairdocs.org/sdr/FDEA201102080498), Feb 8, 2011: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 231 R IN ZONE 230 IS CRACKED. FABRICATED NEW FLOOR PANEL 231 RG IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201102080497](https://openairdocs.org/sdr/FDEA201102080497), Feb 8, 2011: FLOOR PANEL. CRACKED. MAIN CABIN FLOOR PANEL 241 NK IS CRACKED ; ZONE 240. FABRICATED NEW FLOOR PANEL 241 NK IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201102080496](https://openairdocs.org/sdr/FDEA201102080496), Feb 8, 2011: FLOORBOARD. DAMAGED. MAIN CABIN FLOORBOARD HAS A BROKEN OFF OTBD FWD CORNER FROM FRAME 25-FRAME 27; RBL 78 TO RBL 100. FABRICATED NEW FLOORBOARD 231 VG IAW DWG SRZ 25-005, REV "H".

All 110: https://openairdocs.org/aircraft/N430FE/reports.md

## STCs that may be installed (OpenAirDocs) (105, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Airbus Industrie A310-203)

- [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 105: https://openairdocs.org/aircraft/N430FE/stcs.md

## Related

- Other Airbus Industrie A310-203 aircraft: https://openairdocs.org/model/airbus-industrie-a310-203/aircraft.md
- The GE CF6-80 series engine: https://openairdocs.org/engine/ge-cf6-80-series.md

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