# N454FE: 1983 Airbus Industrie A310-222

- Status: Valid registration
- Airframe: [Airbus Industrie A310-222](https://openairdocs.org/model/airbus-industrie-a310-222) (registry code 3930315, 265 seats)
- Engine: [Pratt & Whitney JT9D series](https://openairdocs.org/engine/pratt-whitney-jt9d-series) (registry code 52054)
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) (Airbus SAS) (OpenAirDocs)
- Serial number: 278
- Year built: 1983
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: April 29, 2000
- Certificate issued: October 18, 1999
- Expires: August 31, 2028
- Mode S code: A5817A
- 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=454FE
- Page: https://openairdocs.org/aircraft/N454FE

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 Pratt & Whitney JT9D model are included.

## ADs that may apply (OpenAirDocs): 342 in force

### Matched by airframe (Airbus Industrie A310-222)

- [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 2022-25-03](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
- [AD 2017-12-06](https://openairdocs.org/ad/2017-12-06): Doors · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Jul 25, 2017

### Matched by engine (Pratt & Whitney JT9D series)

- [AD 2021-09-10](https://openairdocs.org/ad/2021-09-10): Turbine Engine Compressor Section · Pratt & Whitney JT9D-20, JT9D-20J, JT9D-3A and 17 more. Effective May 27, 2021
- [AD 2012-06-14](https://openairdocs.org/ad/2012-06-14): HPT 1st stage air seals · Pratt & Whitney Division JT9D-7R4G2 and JT9D-7R4H1. Effective Apr 27, 2012
- [AD 2011-25-10](https://openairdocs.org/ad/2011-25-10): High-pressure compressor (HPC) shafts · Pratt & Whitney Division JT9D-7R4H1. Effective Jan 17, 2012
- [AD 2009-10-01](https://openairdocs.org/ad/2009-10-01): High-pressure turbine (HPT) vane assemblies · Pratt & Whitney Division JT9D-7R4E1, JT9D-7R4E4, JT9D-7R4G2 and 1 more. Effective May 18, 2009
- [AD 2009-04-18](https://openairdocs.org/ad/2009-04-18): 2nd stage high pressure turbine (HPT) · Pratt & Whitney Division JT9D-7, JT9D-7A, JT9D-7AH and 3 more. Effective May 5, 2009
- [AD 2007-18-06](https://openairdocs.org/ad/2007-18-06): Inspection of the blade root thickness · Pratt & Whitney Division JT9D-7R4D, JT9D-7R4D1, JT9D-7R4E and 4 more. Effective Oct 5, 2007
- [AD 2005-05-13](https://openairdocs.org/ad/2005-05-13): High pressure turbine (HPT) second stage airseals · Pratt & Whitney Division JT9D-59A, JT9D-70A, JT9D-7Q and 1 more. Effective Apr 14, 2005
- [AD 2004-10-01](https://openairdocs.org/ad/2004-10-01): 6th Stage Low Pressure Turbine (LPT) Air Seals · Pratt & Whitney Division JT9D-20, JT9D-20J, JT9D-3A and 6 more. Effective Jun 15, 2004
- [AD 2004-01-08](https://openairdocs.org/ad/2004-01-08): One-piece fan case shield · Pratt & Whitney Division JT9D-7R4D, JT9D-7R4D1, JT9D-7R4E and 4 more. Effective Feb 10, 2004
- [AD 2003-24-12 R1](https://openairdocs.org/ad/2003-24-12-R1): Gearbox Pressure Tube · Pratt & Whitney Division JT9D-3A, JT9D-7, JT9D-7A and 4 more. Effective Dec 18, 2003
- [AD 2002-07-04](https://openairdocs.org/ad/2002-07-04): Low Pressure Turbine (LPT) 5th Stage Disks · Pratt & Whitney Division JT9D-7R4D, JT9D-7R4D1, JT9D-7R4E and 4 more. Effective May 14, 2002
- [AD 2001-17-30](https://openairdocs.org/ad/2001-17-30): High Pressure Turbine 1st Stage Disk Aft Lugs · Pratt & Whitney Division JT9D-7R4D, JT9D-7R4D1, JT9D-7R4E and 4 more. Effective Oct 4, 2001
- [AD 2001-04-11](https://openairdocs.org/ad/2001-04-11): High Pressure Turbine (HPT) Disks · Pratt & Whitney Division JT9D-20, JT9D-7, JT9D-7A and 7 more. Effective May 7, 2001
- [AD 2000-23-14](https://openairdocs.org/ad/2000-23-14): No. 4 Bearing Area · Pratt & Whitney Division JT9D-20, JT9D-20J, JT9D-3A and 11 more. Effective Jan 19, 2001
- [AD 98-21-22 R1](https://openairdocs.org/ad/98-21-22-R1): High Pressure Compressor Disks · Pratt & Whitney Division JT9D-59A, JT9D-70A, JT9D-7Q and 8 more. Effective Jan 18, 2000
- [AD 99-20-04](https://openairdocs.org/ad/99-20-04): High Pressure Turbine Disks · Pratt & Whitney Division JT9D-7R4D, JT9D-7R4D1, JT9D-7R4E and 4 more. Effective Oct 29, 1999
- [AD 99-14-08](https://openairdocs.org/ad/99-14-08): Pratt & Whitney Division JT9D-59A, JT9D-70A, JT9D-7Q and 1 more. Effective Sep 13, 1999
- [AD 99-15-02](https://openairdocs.org/ad/99-15-02): Pratt & Whitney Division JT9D-20, JT9D-20J, JT9D-3A and 6 more. Effective Aug 16, 1999
- [AD 99-11-09](https://openairdocs.org/ad/99-11-09): Diffuser Case Rear Rail · Pratt & Whitney Division JT9D-59A, JT9D-70A, JT9D-7Q and 1 more. Effective Jul 26, 1999
- [AD 99-04-05](https://openairdocs.org/ad/99-04-05): Rear Skirt Ddiffuser Case Inspection · Pratt & Whitney Division JT9D-59A, JT9D-70A, JT9D-7Q and 1 more. Effective Apr 12, 1999
- [AD 97-25-10 R1](https://openairdocs.org/ad/97-25-10-R1): (HPT) Disks · Pratt & Whitney Division JT9D-59A, JT9D-70A, JT9D-7Q and 5 more. Effective Jul 29, 1998
- [AD 96-25-10](https://openairdocs.org/ad/96-25-10): Design Turbine Exhaust Case · Pratt & Whitney Division JT9D-20, JT9D-20J, JT9D-3A and 17 more. Effective Feb 18, 1997
- [AD 96-17-11](https://openairdocs.org/ad/96-17-11): Low pressure turbine (LPT) vane · Pratt & Whitney Division JT9D-7R4D, JT9D-7R4D1, JT9D-7R4E and 4 more. Effective Nov 18, 1996
- [AD 93-19-02 R1](https://openairdocs.org/ad/93-19-02-R1): Diffuser Cases · Pratt & Whitney Division JT9D-20, JT9D-20J, JT9D-3A and 6 more. Effective Oct 17, 1994
- [AD 94-15-16](https://openairdocs.org/ad/94-15-16): Engine Control System Accessories · Pratt & Whitney Division JT9D-20, JT9D-20J, JT9D-3A and 9 more. Effective Oct 14, 1994
- [AD 94-08-06](https://openairdocs.org/ad/94-08-06): Fan Blade · Pratt & Whitney Division JT9D-7R4D, JT9D-7R4D1, JT9D-7R4E and 4 more. Effective Jul 5, 1994
- [AD 93-15-04](https://openairdocs.org/ad/93-15-04): Fuel Nozzle And Support Assembly · Pratt & Whitney Division JT9D-59A, JT9D-70A, JT9D-7Q and 1 more. Effective Nov 19, 1993
- [AD 93-14-20](https://openairdocs.org/ad/93-14-20): Vane Cluster Assembly · Pratt & Whitney Division JT9D-59A, JT9D-70A, JT9D-7Q and 1 more. Effective Aug 27, 1993
- [AD 91-03-03](https://openairdocs.org/ad/91-03-03): High Pressure Compressor Turbine Driveshaft · Pratt & Whitney Division JT9D-7R4D, JT9D-7R4D1, JT9D-7R4E and 4 more. Effective Feb 22, 1991
- [AD 90-23-19](https://openairdocs.org/ad/90-23-19): Air Seal · Pratt & Whitney Division JT9D-20, JT9D-20J, JT9D-3A and 13 more. Effective Nov 23, 1990
- [AD 90-15-11](https://openairdocs.org/ad/90-15-11): Fuel Control Unit · Pratt & Whitney Division JT9D-7R4D1, JT9D-7R4E1 and JT9D-7R4H1. Effective Jul 16, 1990
- [AD 90-14-08](https://openairdocs.org/ad/90-14-08): High Pressure Compressor · Pratt & Whitney Division JT9D-7R4D and JT9D-7R4E. Effective Jul 2, 1990
- [AD 87-23-05 R1](https://openairdocs.org/ad/87-23-05-R1): Fan Case Assembly · Pratt & Whitney Division JT9D-7R4D, JT9D-7R4D1, JT9D-7R4E and 4 more. Effective Mar 23, 1990
- [AD 89-10-07](https://openairdocs.org/ad/89-10-07): Strut Insert Assembly · Pratt & Whitney Division JT9D-20, JT9D-3A, JT9D-7 and 5 more. Effective May 30, 1989
- [AD 88-24-05](https://openairdocs.org/ad/88-24-05): Inner Airseal · Pratt & Whitney Division JT9D-20, JT9D-3A, JT9D-7 and 5 more. Effective Dec 15, 1988
- [AD 86-09-01 R1](https://openairdocs.org/ad/86-09-01-R1): Turbine Vane Antirotation Pin Failure · Pratt & Whitney Division JT9D-20, JT9D-3A, JT9D-59A and 9 more. Effective Jul 6, 1988
- [AD 86-25-51](https://openairdocs.org/ad/86-25-51): Low Altitude Surges · Pratt & Whitney Division JT9D-7R4D, JT9D-7R4D1, JT9D-7R4E and 3 more. Effective Mar 20, 1987
- [AD 86-23-03](https://openairdocs.org/ad/86-23-03): Second Stage High Pressure Turbine Rotor (HPTR) Airseal · Pratt & Whitney Division JT9D-7R4D, JT9D-7R4D1, JT9D-7R4E and 1 more. Effective Dec 8, 1986
- [AD 86-10-01](https://openairdocs.org/ad/86-10-01): Second Stage Turbine Disk · Pratt & Whitney Division JT9D-3A. Effective Jun 5, 1986
- [AD 86-07-12](https://openairdocs.org/ad/86-07-12): Engine Support Clevis · Pratt & Whitney Division JT9D-7R4G2. Effective Apr 11, 1986
- [AD 86-03-03](https://openairdocs.org/ad/86-03-03): Fuel Nozzle Flow And Spray Cone Angle · Pratt & Whitney Division JT9D-7R4D, JT9D-7R4E and JT9D-7R4E4. Effective Mar 14, 1986
- [AD 85-12-02](https://openairdocs.org/ad/85-12-02): Centrifugal Oil Filter (COF) Bearings · Pratt & Whitney Division JT9D-3A, JT9D-7, JT9D-7A and 4 more. Effective Jul 17, 1985
- [AD 83-22-52 R1](https://openairdocs.org/ad/83-22-52-R1): Refurbishing Fuel Nozzles · Pratt & Whitney Division JT9D-7R4D, JT9D-7R4D1, JT9D-7R4E and 4 more. Effective Feb 21, 1984
- [AD 82-26-03](https://openairdocs.org/ad/82-26-03): Manifold Assembly · Pratt & Whitney Division JT9D-7, JT9D-7A, JT9D-7AH and 3 more. Effective Jan 27, 1983
- [AD 82-16-10](https://openairdocs.org/ad/82-16-10): Fan Exit Case Assembly · Pratt & Whitney Division JT9D-20. Effective Aug 16, 1982
- [AD 74-10-05 R1](https://openairdocs.org/ad/74-10-05-R1): Turbine Nozzle Guide Vane · Pratt & Whitney Division JT9D-20, JT9D-7 and JT9D-7A. Effective Nov 17, 1980
- [AD 78-08-13](https://openairdocs.org/ad/78-08-13): Main Gearbox · Pratt & Whitney Division JT9D-3A, JT9D-7, JT9D-7A and 4 more. Effective Apr 18, 1980
- [AD 78-16-05](https://openairdocs.org/ad/78-16-05): Sixth Stage Turbine Disks · Pratt & Whitney Division JT9D-20, JT9D-20J, JT9D-3A and 17 more. Effective Sep 12, 1978
- [AD 78-17-08](https://openairdocs.org/ad/78-17-08): Fifteenth Stage Compressor Disks · Pratt & Whitney Division JT9D-20, JT9D-3A, JT9D-7 and 5 more. Effective Sep 1, 1978
- [AD 76-20-03](https://openairdocs.org/ad/76-20-03): Seal Clearances · Pratt & Whitney Division JT9D-20, JT9D-3A, JT9D-7 and 4 more. Effective Nov 16, 1977

### 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 406: https://openairdocs.org/aircraft/N454FE/ads.md

## Information bulletins (advisory) (12 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-08-43](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
- [SAIB NE-07-41](https://openairdocs.org/saib/NE-07-41): Pratt & Whitney (P&W) JT9D HPT 2nd Stage Vane/Disk Failures. Issued Aug 3, 2007
- [SAIB NE-04-51](https://openairdocs.org/saib/NE-04-51): . Issued Feb 12, 2004
- [SAIB NE-04-44](https://openairdocs.org/saib/NE-04-44): . Issued Jan 14, 2004
- [SAIB NE-02-30](https://openairdocs.org/saib/NE-02-30): . Issued Jun 3, 2002
- [SAIB NE-02-21](https://openairdocs.org/saib/NE-02-21): . Issued Mar 15, 2002
- [SAIB NE-02-01](https://openairdocs.org/saib/NE-02-01): . Issued Oct 5, 2001
- [SAIB ANE-97-03](https://openairdocs.org/saib/ANE-97-03): . Issued Apr 25, 1997

## NTSB investigations

None matched to N454FE.

## 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 20030202006209I](https://openairdocs.org/incident/20030202006209I), Feb 2, 2003: Airbus A310222 (N454FE), Indianapolis, IN. (-23) On feb 02 2003 while enroute roc to mem at FL 350, all four left wheel temps went to 400 degrees. Right wheels remained at 5 degrees. The crew suspected…

## Service difficulty reports (57, 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 FDEA201412184149](https://openairdocs.org/sdr/FDEA201412184149), Dec 18, 2014: PANEL. DAMAGED. ON ARRIVAL LT WING TE DAMAGE FOUND. R & R THE LT WING OTBD TE PANEL IAW SRM 57-51-12.
- [SDR FDEA201312243034](https://openairdocs.org/sdr/FDEA201312243034), Dec 24, 2013: PLATE. WORN. NR 2 ENG OTBD T/R COWL UPPER MID-SECTION INNER FACE FOUND ONE EACH PLATE WORN BY SPRING SEAL. ACCOMPLISHED THE WORK IAW EA 6-5410-T0208220.
- [SDR FDEA201312243033](https://openairdocs.org/sdr/FDEA201312243033), Dec 24, 2013: FRAME. CORRODED. FORWARD CARGO COMPARTMENT BILGE FRAME FOUND CORROSION AT FR 39, STRINGER 51R POSITION. CORROSION AREA CUT OUT & REINFORCED WITH REPAIR PART & FITTING TO INSTALL
- [SDR FDEA201211103930](https://openairdocs.org/sdr/FDEA201211103930), Nov 10, 2012: WINDSHIELD. CRACKED. IN CRUISE FL340, CAPTAIN'S WINDOW CRACKED IN TWO PLACES. CAPTAINS WINDOW HEAT FAULTED SHORTLY AFTER CRACK APPEARED. TURNED OFF WINDOW HEAT, NO FURTHER CRACKING.
- [SDR FDEA201208092925](https://openairdocs.org/sdr/FDEA201208092925), Aug 9, 2012: HINGE FITTING. GOUGED. RIGHT NLG AFT DOOR UPPER FWD HINGE FITTING HAS .2500" X .5" GOUGE FROM CONTACT WITH DOOR CONTROL ROD (ON AFT FACE OF HINGE FITTING) R & R RT NLG AFT DOOR UPPER 
- [SDR FDEA201208092923](https://openairdocs.org/sdr/FDEA201208092923), Aug 9, 2012: HINGE FITTING. GOUGED. LT NLG AFT DOOR UPPER FWD HINGE FITTING HAS .2500" X .5" GOUGE FROM CONTACT WITH DOOR CONTROL ROD (ON AFT FACE OF HINGE FITTING) R & R LT NLG AFT DOOR UPPER FWD
- [SDR FDEA201205302015](https://openairdocs.org/sdr/FDEA201205302015), May 30, 2012: PRESSURE SWITCH. FAILED. NR 2 FUEL FLITER CLOG WOULD NOT GO AWAY AFTER QRH PROCEDURE. FOLLOWED ECAM AND QRH. DECLARED PRECAUTIONARY EMERGENCY. NR 2 ENG REMAINED AT IDLE REMAINDER OF FLI
- [SDR FDEA201202130564](https://openairdocs.org/sdr/FDEA201202130564), Feb 13, 2012: COUPLING. LEAKING. AFTER STARTING THE ENGINES DURING PUSHBACK THE COCKPIT FILLED WITH A LIGHT SMOKE WITH EYES AND THROAT BURNING. THERE WERE NO COCKPIT INDICATIONS OF ANY FIRE OR 
- [SDR FDEA201112215409](https://openairdocs.org/sdr/FDEA201112215409), Dec 21, 2011: LINE. LEAKING. BLUE SYS HYD QUANTITY DECREASED IN FLIGHT SLOWLY UNTIL REACHED LO LEVEL WARNING, SECURED PUMP IAW ECAM AND QUANTITY STOPPED DECREASING, PRESSURE REMAINED ABOVE 
- [SDR FDEA201111305082](https://openairdocs.org/sdr/FDEA201111305082), Nov 30, 2011: SIGNAL COND UNIT. FAILED. DURING T/O AT TYS AT 90 KNOTS - ECAM AND ENG 1 LIGHT - OIL HI PRESS - ILLUMINATED. CREW REJECTED T/O - LIGHT WENT OUT IMMEDIATLY. COMPLETED RTO CK LIST & QRH FO
- [SDR FDEA201106162300](https://openairdocs.org/sdr/FDEA201106162300), Jun 16, 2011: SKIN. DELAMINATED. AFTER SKIN REMOVED FOR REPAIR, FOUND FURTHER DELAMINATION APPROX. 8 SQ". REPAIRED RT ELEVATOR LOWER SURFACE EXISTING REPAIR DELAMINATED IAW SRM 55-21-11 PAR.5J 
- [SDR FDEA201106162297](https://openairdocs.org/sdr/FDEA201106162297), Jun 16, 2011: BRACKET. DAMAGED. NR 1 ENGINE, NR 2 HYD SUCTION LINE HAS EXCESSIVE PLAY AT WING ATTACH POINT INSIDE NR 1 PYLON. LEFT WING, REWORKED HOLES 1,2,3,AND 4. R & R SUPPORT BRACKET BUSHI
- [SDR FDEA201106162296](https://openairdocs.org/sdr/FDEA201106162296), Jun 16, 2011: SKIN. CHAFED. RIGHT WING AFT SPAR ABOVE PYLON HYD LINE JAM NUT, LOOSE. REWORKED OVERSIZE HOLE IAW E-5720-145615. REWORKED AND INSTALLED NEW SUPPORT BRACKET BUSHING. REPAIRED 
- [SDR FDEA201106162295](https://openairdocs.org/sdr/FDEA201106162295), Jun 16, 2011: SKIN. CORRODED. LEFT WING TOP SKIN HAS CORROSION AT REAR SPAR FASTENER, 6" OTBD OF RIB-4. LT WING CORROSION REMOVED BY BLENDING, NDT INSPECTED (NIL FINDINGS), NEW OVERSIZE TAPE
- [SDR FDEA201105031744](https://openairdocs.org/sdr/FDEA201105031744), May 3, 2011: SKIN. DELAMINATED. AFTER SKIN REMOVAL FOR REPAIR, FOUND FURTHER DELAMINATION APPROX 8 SQ IN. REPAIRED RT ELEVATOR LOWER SURFACE IAW SRM 55-21-11, PAR 5J, PGS 257-262 AT RIB 14 AND
- [SDR FDEA201105031745](https://openairdocs.org/sdr/FDEA201105031745), May 3, 2011: SKIN. CORRODED. LT ELEVATOR LOWER SURFACE AT RIB 9 HAS 6 SQ IN TOTAL AREA OF CORROSION. REPAIRED LT ELEVATOR LOWER SURFACE AT RIB 9 IAW SRM 55-21-11, PARA I, PGS 247-252 REF EA
- [SDR FDEA201105031743](https://openairdocs.org/sdr/FDEA201105031743), May 3, 2011: SKIN. CORRODED. RT ELEVATOR UPPER SURFACE AT RIB 17 HAS 2 SQ IN OF CORROSION. REMOVED LEVEL 1 CORROSION. REPAIRED RT ELEVATOR UPPER SURFACE IAW SRM 55-21-11, PARA 5L PAGES 257-
- [SDR FDEA201105031742](https://openairdocs.org/sdr/FDEA201105031742), May 3, 2011: SKIN. CORRODED. RT ELEVATOR LOWER SURFACE OTBD OF RIB 14 HAS 4 SQ IN OF CORROSION. REMOVED LEVEL 1 CORROSION. REPAIRED RIGHT HAND ELEVATOR LOWER SURFACE IAW SRM 55-21-11,PARA 5
- [SDR FDEA201105031741](https://openairdocs.org/sdr/FDEA201105031741), May 3, 2011: SKIN. CORRODED. LOWER SURFACE LT ELEVATOR AT RIB 96 SQ IN CORROSION.
- [SDR FDEA200903241027](https://openairdocs.org/sdr/FDEA200903241027), Mar 24, 2009: TRANSMITTER. MALFUNCTIONED. ENG 1 AFTER START, AMBER ECAM HIGH OIL PRESSURE IND (64PSI), MOMENTARILY ON TAKEOFF ROLL AMBER ECAM-HIGH OIL PRESSURE, RTO. HIGH OIL PRESS (64PSI). LOWER OIL PR
- [SDR FDEA200903241026](https://openairdocs.org/sdr/FDEA200903241026), Mar 24, 2009: COMPUTER. MALFUNCTIONED. ENG 1 AFTER START, AMBER ECAM HI OIL PRESSURE IND (64 PSI), MOMENTARILY ON TAKEOFF ROLL AMBER ECAM-HI OIL PRESSURE, RTO. HI OIL PRESS (64PSI). LOWER OIL PRESSUR
- [SDR FDEA200903220999](https://openairdocs.org/sdr/FDEA200903220999), Mar 22, 2009: SIGNAL COND UNIT. MALFUNCTIONED. REJECTED TAKEOFF. NR 1 ENGINE HIGH OIL PRESSURE WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL APPROXIMATELY 85KTS. INDICATION DEFERRED PER MEL 79-33-01-02. REMOVED 
- [SDR FDEA200901080081](https://openairdocs.org/sdr/FDEA200901080081), Jan 8, 2009: FRAME. CORRODED. AFT CARGO DOOR CUTOUT FRAME 59A CORROSION AT LOWER END OF DOOR FRAME. PERFORMED REPAIR PER SRM 53-17 FIG 201 AND 202A AND EA NR 6-5320-125509.
- [SDR 08FDEA02075](https://openairdocs.org/sdr/08FDEA02075), Jun 1, 2008: REGULATOR. FAILED. DURING CLIMB-OUT WITH NR 1 REG DEFERRED, LOST NR 2 REG. USED MANUAL PRESSURIZATION FOR THE REST OF FLIGHT. ACN RELEASED FOR SERVICE PER MEL/CDL: 21-31-04-01-A. 
- [SDR 07FDEA02562](https://openairdocs.org/sdr/07FDEA02562), Jul 20, 2007: AUTOPILOT SYS. UNKNOWN. CLOSE R AP 1 AND 2 DO NOT ENGAGE. MTP FAULT REVIEW FOUND FCC 1/ FCC 2/FCU/TORQUE LIMIT RESET A/P 1 AND 2 BOTH FCC AND FCU. PERFORMED AFS/LAND ENGAGE TEST AS PER
- [SDR 07FDEA02366](https://openairdocs.org/sdr/07FDEA02366), Jul 3, 2007: UNKNOWN. WARNING LIGHT. FWD CARGO DOOR UNLOCK INDICATION NUMEROUS TIMES AFTER TAKEOFF. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01, CATEGORY: C EXPIRATION: 13JUL07.
- [SDR 06FDEA04333](https://openairdocs.org/sdr/06FDEA04333), Dec 28, 2006: BULKHEAD. CORRODED. FUSE AFT PRESSURE BULKHEAD LOWER RIM FWD SIDE FR 80/82 FROM STR 50L TO STR 51L. CORROSION REPAIRED IAW FEDEX EA6-5310-106280.
- [SDR 06FDEA04332](https://openairdocs.org/sdr/06FDEA04332), Dec 28, 2006: BEARING. FROZEN. A FROZEN BEARING EXIST AT LT NR 3 RUDDER HINGE ARM COMPLIED WITH FEDEX EA6-5540-106279.
- [SDR 06FDEA04312](https://openairdocs.org/sdr/06FDEA04312), Dec 26, 2006: SEAT TRACK. DAMAGED. DUMMY TRACK FS 54 TO 54.2 LT NR 5 HAS SLOTTED HOLE ATTACHMENT POINT HAS WEAR MEASURING .051 IN. REMOVED AND INSTALLED FLOORBOARD IAW A310/200 AMM 53-10-254. ROU
- [SDR 06FDEA04311](https://openairdocs.org/sdr/06FDEA04311), Dec 26, 2006: HINGE. CORRODED. RT ELEVATOR T/E AT AT 4 HINGE ARM HAS LIGHT CORROSION TOP AND BOTTOM AS MARKED REPAIRED CORROSION ON RT, ELEVATOR AT NR 4 HINGE ON CORNER SKIN IAW A310/200 SRM 
- [SDR 06FDEA04307](https://openairdocs.org/sdr/06FDEA04307), Dec 22, 2006: SKIN. MISREPAIRED. PREVIOUS REPAIR, FUSELAGE SKIN RT SIDE HAS EXTERNAL REPAIR DOUBLE BETWEEN FR 54.1 TO 54.2, BETWEEN STR 38 RT TO STR 40 RT, MEASURES 6.3" BY 6.2" PREVIOUSLY INST
- [SDR 06FDEA04306](https://openairdocs.org/sdr/06FDEA04306), Dec 22, 2006: SEAT TRACK. BROKEN. MDCC SEAT TRACK R1 AT FR 38.1 HAS (1) BROKEN SCALLOP AND (1) BENT SCALLOP. REMOVED AND INSTALLED REPAIR SEAT TRACK IAW A310-200 SRM 53-10-16 PB 201 FIG 208.
- [SDR 06FDEA04304](https://openairdocs.org/sdr/06FDEA04304), Dec 22, 2006: SEAT TRACK. GOUGED. MDCC SEAT TRACK L4 FR 54.2 - 58 GOUGED REMOVED AND REINSTALLED 4EA FLOORBOARDS IAW A310-200 SRM 53-10-25-4. REMOVED AND INSTALLED NEW SEAT TRACK IAW A310-200 DW
- [SDR 06FDEA04302](https://openairdocs.org/sdr/06FDEA04302), Dec 22, 2006: HINGE FITTING. CORRODED. CORROSION EXIST AT VERT STAB REAR SPAR NR 3 RUDDER ATTACHMENT HINGE FITTING COMPLIED WITH EA NR 6-5540-106300. RUDDER RIB 12 AND 13 ATTACH FITTINGS CORROSION. M
- [SDR 06FDEA04301](https://openairdocs.org/sdr/06FDEA04301), Dec 22, 2006: HINGE FITTING. CORRODED. VERT STAB REAR SPAR NR 2 RUDDER ATTACHMENT HINGE FITTING HAS CORROSION. COMPLIED WITH EA NR 6-5540-106300 RUDDER RIB 12 AND 13 ATTACH FITTINGS CORROSION. MAJOR 
- [SDR 06FDEA04300](https://openairdocs.org/sdr/06FDEA04300), Dec 22, 2006: SKIN. DELAMINATED. RT WING, INBD FLAP, LWR EXT SKIN AT MID T/E, (1)EA AREA OF DELAMINATION APPROX 6" * 6" DIA. REPAIRED (1EA) AREA OF DELAMINATION ON RT WING I/B FLAP LOWER SKIN I
- [SDR 06FDEA2068](https://openairdocs.org/sdr/06FDEA2068), May 30, 2006: REGULATOR. MALFUNCTIONED. ENGINE NR 1 REV UNLK ILLUMINATED ON TAKEOFF ROLL, REJECTED TAKEOFF, WHEN THROTTLES PULLED TO IDLE REV UNLK LIGHT ENGINE NR 1 EXTINGUISHED. REJECTED TAKEOFF AT A
- [SDR 06FDEA2064](https://openairdocs.org/sdr/06FDEA2064), May 29, 2006: SWITCH. FAULTY. ENGINE NR 1 REV UNLK ILLUMINATED ON TAKEOFF ROLL. REJECTED TAKEOFF APPROX 40 KTS REV UNLK LIGHT EXTINGUISHED WHEN THROTTLES PULLED TO IDLE. REMOVED AND REPLACED
- [SDR 05FDEA04016](https://openairdocs.org/sdr/05FDEA04016), Nov 29, 2005: REGULATOR. MALFUNCTIONED. NR 2 ENGINE INDICATED HIGH OIL PRESSURE, THEN FOLLOWED QRH & MONITORED PARAMETERS. OIL PRESS. WENT TO 20-32 PSI (LOW) FOLLOWED QRH AND SHUTDOWN ENGINE. DECLARED
- [SDR 05FDEA00036](https://openairdocs.org/sdr/05FDEA00036), Jan 6, 2005: RIB. CORRODED. ACCOMPLISH MAINTENANCE C-CHECK, NON-ROUTINE, LT WING - CORROSION FOUND ON UPPER SURFACE STA 1659 RIB 27 TO STA 1713 RIB 28 INTERSECTION WITH STRINGER 12. REPAIR
- [SDR 05FDEA00035](https://openairdocs.org/sdr/05FDEA00035), Jan 6, 2005: SKIN. DENTED. ACCOMPLISH MAINTENANCE C-CHECK, NON-ROUTINE, RT WING - DENTS AND DEBONDS AT LOWER SKIN SURFACE OF T/E OF FLAP INBOARD. REPAIRED IAW AIRBUS REF: 001-57-01-2005-A
- [SDR 05FDEA00039](https://openairdocs.org/sdr/05FDEA00039), Jan 6, 2005: SKIN. CORRODED. RT WING - CORROSION FOUND ON UPPER SURFACE STA 1659 RIB 27 TO STA 1713 RIB 28 INTERSECTION WITH STRINGER 12. CORROSION REMOVED AND REPAIRED IAW EA 6-5710-81827.
- [SDR 05FDEA00038](https://openairdocs.org/sdr/05FDEA00038), Jan 6, 2005: SKIN. CORRODED. RT WING CORROSION FOUND ON UPPER SURFACE STA 813 RIB 13 TO STA 874 RIB 14 INTERSECTION WITH STRINGER 7. CORROSION REMOVED AND REPAIRED IAW EA 6-5710-81827.
- [SDR 05FDEA00034](https://openairdocs.org/sdr/05FDEA00034), Jan 6, 2005: FAIRING. CRACKED. NR 2 PYLON, AFTER FIXED FAIRING WITH CRACK AT LT. REMOVED IAW AMM 54-55-00. REPAIRED IAW FEDEX EA 6-5480-81822. INSTALED IAW AMM 54-55-00.
- [SDR 05FDEA00033](https://openairdocs.org/sdr/05FDEA00033), Jan 6, 2005: SKIN. DAMAGED. NON-ROUTINE NR N00380. RT WING REPAIR ON INBD FLAP LWR SURFACE T/E. VERIFIED THAT THE EXISTING REPAIR WAS PERFORMED IAW FEDEX EA 6-5710-63790.
- [SDR 05FDEA00029](https://openairdocs.org/sdr/05FDEA00029), Jan 6, 2005: SKIN. DAMAGED. COMPLY WITH AGING 9-AGING-INSPECTION. NON-ROUTINE, FUSELAGE - REPAIR AT APPROX FS 69 STR 50 RT. *S/D* VERIFIED THAT THE EXISTING REPAIR WAS PERFORMED IAW SRM 53
- [SDR 05FDEA00027](https://openairdocs.org/sdr/05FDEA00027), Jan 6, 2005: SKIN. DAMAGED. FUSELAGE REPAIR AT APROX. FS 1 STR 56 LT. VERIFIED THAT THE EXISTING REPAIR WAS PERFORMED IAW FEDEX EA 6-5310-81826.
- [SDR 05FDEA00026](https://openairdocs.org/sdr/05FDEA00026), Jan 6, 2005: SKIN. DAMAGED. FUSELAGE - REPAIR AT APROX. FS 63 STR 42 RT. REPAIRED IAW SRM 53-17-12, FIG 203.
- [SDR 05FDEA00037](https://openairdocs.org/sdr/05FDEA00037), Jan 6, 2005: SKIN. CORRODED. ACCOMPLISH MAINTENANCE C-CHECK, ORIGINAL PLAN DATE WAS ENTERED ON: 23JUL04. NON-ROUTINE LT WING - CORROSION FOUND ON UPPER SURFACE STA 813 RIB 13 TO STA 874 RIB
- [SDR 04FDEA01815](https://openairdocs.org/sdr/04FDEA01815), Jun 20, 2004: ENGINE. FAILED. UNRECOVERABLE STALL ENG NR 2 DURING T/O AT 500 FT ATB. EGT WAS RAISING TO 670 DEG C, EGT LIGHT ON, PULLED BACK THE THROTTLE TO PREVENT FURTHER EGT INCREASE. FLA

All 57: https://openairdocs.org/aircraft/N454FE/reports.md

## STCs that may be installed (OpenAirDocs) (115, 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 A310-222)

- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST01999AT](https://openairdocs.org/stc/ST01999AT): This installation adds three recording parameters (pitch control, lateral control, and rudder) to the existing A300 and A310 Digital Flight Data Recorder (DFDR) to meet the requirements of 14 CFR 121.344. Acron Aviation Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST01694CH](https://openairdocs.org/stc/ST01694CH): Installation of Honeywell International Enhanced Ground Proximity Warning System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01754CH](https://openairdocs.org/stc/ST01754CH): Installation of an Airshow 420 system IAW ECS MDL ECS-201346, Rev. A, dtd 1/24/03 or later FAA approved revision. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST02161CH](https://openairdocs.org/stc/ST02161CH): Installation of GPS wiring and antenna provisions. Amphenol Cable and Interconnect Technologies Inc
- [STC ST02169CH](https://openairdocs.org/stc/ST02169CH): Installation of elementary and enhanced Mode S transponders. Amphenol Cable and Interconnect Technologies Inc
- [STC ST02866CH](https://openairdocs.org/stc/ST02866CH): Upgrade of the internal core software of the ACARS Data Link Management Unit (DLM-900). Amphenol Cable and Interconnect Technologies Inc
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST00691SE](https://openairdocs.org/stc/ST00691SE): Installation of lightweight window plugs. LiteAir Aviation Products Inc
- [STC ST02691AT](https://openairdocs.org/stc/ST02691AT): Installation of SAF-T-GLO Inc. Photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC ST02302CH](https://openairdocs.org/stc/ST02302CH): Install ERDA model 7004 HI-LO table with slide top. Collins Aerospace
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST02896AT](https://openairdocs.org/stc/ST02896AT): Installation of a Kannad Model 406-AF Emergency Locator Transmittter (ELT). Woven Electronics LLC
- [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [STC ST00440SE](https://openairdocs.org/stc/ST00440SE): Installation of the Honeywelll Enhanced Ground Proximity Warning System. Honeywell International Inc
- [STC ST01235SE](https://openairdocs.org/stc/ST01235SE): Installation of the Honeywell Mark II ACARS (Aircraft Communication Addressing and Reporting System). Honeywell International Inc
- [STC SA5672SW-D](https://openairdocs.org/stc/SA5672SW-D): Modification of air to air heat exchanger (P/N 187900-9). Honeywell International Inc
- [STC ST03574AT](https://openairdocs.org/stc/ST03574AT): Installation of a Talon Aerospace Anti-Collision Light. Aaxico Technical Services Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST04092NY](https://openairdocs.org/stc/ST04092NY): Installation of Wireless PCMCIA for DFDAU. Delta Engineering Corporation
- [STC 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
- [STC ST03483AT](https://openairdocs.org/stc/ST03483AT): Installation of a Portable Beverage Dispensing System, P/N B43-FA-001. Dynamo Beverage Company, USA, L.L.C

All 115: https://openairdocs.org/aircraft/N454FE/stcs.md

## Related

- Other Airbus Industrie A310-222 aircraft: https://openairdocs.org/model/airbus-industrie-a310-222/aircraft.md
- The Pratt & Whitney JT9D series engine: https://openairdocs.org/engine/pratt-whitney-jt9d-series.md

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