# N731FD: 1993 Airbus Industrie A300 B4-605R

- Status: Valid registration
- Airframe: [Airbus Industrie A300 B4-605R](https://openairdocs.org/model/airbus-industrie-a300-b4-605r) (registry code 3930308, 380 seats)
- Engine: [GE CF6-80C2A5](https://openairdocs.org/engine/ge-cf6-80c2a5) (registry code 30104)
- 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: 709
- Year built: 1993
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 9, 2007
- Certificate issued: August 22, 2006
- Expires: February 29, 2028
- Mode S code: A9CF43
- 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=731FD
- Page: https://openairdocs.org/aircraft/N731FD

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.

## ADs that may apply (OpenAirDocs): 352 in force

### Matched by airframe (Airbus Industrie A300 B4-605R)

- [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 2025-23-02](https://openairdocs.org/ad/2025-23-02): Wings · Airbus A300 B4-603, A300 B4-605R, A300 B4-622 and 4 more. Effective Jan 13, 2026
- [AD 2025-19-09](https://openairdocs.org/ad/2025-19-09): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Dec 22, 2025
- [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 2025-18-07](https://openairdocs.org/ad/2025-18-07): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Oct 23, 2025
- [AD 2025-16-05](https://openairdocs.org/ad/2025-16-05): Wings · Airbus A300 B4-2C, A300 B4-203, A300 B4-603 and 4 more. Effective Sep 22, 2025
- [AD 2025-05-01](https://openairdocs.org/ad/2025-05-01): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Apr 15, 2025
- [AD 2025-01-07](https://openairdocs.org/ad/2025-01-07): Wings · Airbus A300 B4-2C, A300 B4-103, A300 B4-203 and 9 more. Effective Mar 11, 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 2024-16-02](https://openairdocs.org/ad/2024-16-02): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Oct 21, 2024
- [AD 2024-14-07](https://openairdocs.org/ad/2024-14-07): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Sep 25, 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 2023-12-07](https://openairdocs.org/ad/2023-12-07): Time Limits/Maintenance Checks · Airbus A300 C4-605R Variant F, A300 F4-605R, A300 F4-622R and 6 more. Effective Aug 7, 2023
- [AD 2023-11-02](https://openairdocs.org/ad/2023-11-02): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Jul 11, 2023
- [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 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 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 2022-21-02](https://openairdocs.org/ad/2022-21-02): Fuselage · Airbus A300 B2-1C, A300 B2K-3C, A300 B2-203 and 8 more. Effective Dec 14, 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 2021-11-18](https://openairdocs.org/ad/2021-11-18): Landing Gear · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Jul 16, 2021
- [AD 2020-22-11](https://openairdocs.org/ad/2020-22-11): Fuselage · Airbus A300 B4-603, A300 B4-605R, A300 B4-620 and 5 more. Effective Dec 14, 2020
- [AD 2020-02-22](https://openairdocs.org/ad/2020-02-22): Hydraulic power · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Mar 19, 2020
- [AD 2020-01-15](https://openairdocs.org/ad/2020-01-15): Fuel · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 9 more. Effective Mar 17, 2020
- [AD 2019-19-17](https://openairdocs.org/ad/2019-19-17): Wings · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 5 more. Effective Nov 14, 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 2019-15-08](https://openairdocs.org/ad/2019-15-08): Fuselage · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Sep 19, 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 2019-12-04](https://openairdocs.org/ad/2019-12-04): Wings · Airbus A300 B4-603, A300 B4-605R, A300 B4-620 and 5 more. Effective Aug 7, 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 2018-18-21](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 2018-17-10](https://openairdocs.org/ad/2018-17-10): Wings · Airbus A300 B4-605R, A300 B4-622R, A300 C4-605R Variant F and 2 more. Effective Sep 24, 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 2017-21-02](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 2017-18-15](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 2017-17-05](https://openairdocs.org/ad/2017-17-05): Fuselage · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Sep 25, 2017

### Matched by engine (GE CF6-80C2A5)

- [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 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 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 2009-07-03](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 2007-11-20](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 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 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 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 95-10-11](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 94-06-03](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
- [AD 93-14-18](https://openairdocs.org/ad/93-14-18): High pressure turbine (HPT) thermal shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Oct 4, 1993
- [AD 91-15-25](https://openairdocs.org/ad/91-15-25): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Sep 6, 1991
- [AD 91-11-05](https://openairdocs.org/ad/91-11-05): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Jul 5, 1991
- [AD 91-05-21](https://openairdocs.org/ad/91-05-21): High Pressure Turbine · General Electric CF6-80C2A5, CF6-80C2B6, CF6-80C2B6F and 1 more. Effective Mar 27, 1991

### Historical (superseded or no longer in force)

- [AD 2023-26-06](https://openairdocs.org/ad/2023-26-06) (historical): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Mar 7, 2024
- [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 2023-09-05](https://openairdocs.org/ad/2023-09-05) (historical): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Jul 11, 2023
- [AD 2023-05-13](https://openairdocs.org/ad/2023-05-13) (historical): Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective May 12, 2023
- [AD 2022-14-06](https://openairdocs.org/ad/2022-14-06) (historical): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-622 and 6 more. Effective Aug 19, 2022
- [AD 2022-13-09](https://openairdocs.org/ad/2022-13-09) (historical): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Aug 9, 2022
- [AD 2022-11-01](https://openairdocs.org/ad/2022-11-01) (historical): Wings · Airbus A300 B2-1A, A300 B2-1C, A300 B2K-3C and 13 more. Effective Jul 5, 2022
- [AD 2021-26-20](https://openairdocs.org/ad/2021-26-20) (historical): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective May 3, 2022
- [AD 2022-04-09](https://openairdocs.org/ad/2022-04-09) (historical): Oxygen System · Airbus A300 B2-1A, A300 B2-1C, A300 B2K-3C and 94 more. Effective Apr 4, 2022
- [AD 2020-23-11](https://openairdocs.org/ad/2020-23-11) (historical): Fuselage; Wings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Jan 4, 2021
- [AD 2019-21-01](https://openairdocs.org/ad/2019-21-01) (historical): Time Limits/ Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 more. Effective Nov 29, 2019
- [AD 2019-03-10](https://openairdocs.org/ad/2019-03-10) (historical): Landing Gear · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Mar 29, 2019
- [AD 2018-19-18](https://openairdocs.org/ad/2018-19-18) (historical): Wings · Airbus A300 B4-603, A300 B4-605R, A300 B4-620 and 4 more. Effective Nov 7, 2018
- [AD 2018-19-33](https://openairdocs.org/ad/2018-19-33) (historical): Time limits/maintenance checks · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 more. Effective Nov 2, 2018
- [AD 2018-01-07](https://openairdocs.org/ad/2018-01-07) (historical): Time limits/maintenance checks · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 more. Effective Feb 20, 2018
- [AD 2017-23-04](https://openairdocs.org/ad/2017-23-04) (historical): Wings · Airbus A300 B4-603, A300 B4-605R, A300 B4-620 and 4 more. Effective Dec 20, 2017
- [AD 2017-18-17](https://openairdocs.org/ad/2017-18-17) (historical): Fuselage · Airbus A300 B4-603, A300 B4-605R, A300 B4-620 and 5 more. Effective Oct 19, 2017
- [AD 2017-15-17](https://openairdocs.org/ad/2017-15-17) (historical): Wings · Airbus A300 B4-605R, A300 B4-622R, A300 C4-605R Variant F and 2 more. Effective Sep 5, 2017
- [AD 2017-07-05](https://openairdocs.org/ad/2017-07-05) (historical): Landing Gear · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Apr 17, 2017
- [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 2016-16-06](https://openairdocs.org/ad/2016-16-06) (historical): Fuslage · Airbus A300 B4-603, A300 B4-605R, A300 B4-622R and 3 more. Effective Sep 8, 2016
- [AD 2016-15-01](https://openairdocs.org/ad/2016-15-01) (historical): Flight controls · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Aug 26, 2016
- [AD 2016-07-22](https://openairdocs.org/ad/2016-07-22) (historical): Electrical Power · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective May 16, 2016
- [AD 2013-13-13](https://openairdocs.org/ad/2013-13-13) (historical): Wings · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Sep 23, 2014
- [AD 2014-13-17](https://openairdocs.org/ad/2014-13-17) (historical): Fuel · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Aug 19, 2014
- [AD 2014-12-06](https://openairdocs.org/ad/2014-12-06) (historical): Fuselage · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Jul 2, 2014
- [AD 2014-08-02](https://openairdocs.org/ad/2014-08-02) (historical): Wings · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 3 more. Effective May 21, 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 2012-15-14](https://openairdocs.org/ad/2012-15-14) (historical): Wings · Airbus A300 B4-103, A300 B4-203, A300 B4-2C and 9 more. Effective Sep 11, 2012
- [AD 2012-13-06](https://openairdocs.org/ad/2012-13-06) (historical): Electrical Power · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Aug 14, 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 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 2010-23-26](https://openairdocs.org/ad/2010-23-26) (historical): Wings · Airbus A300 B2-1C, A300 B2-203, A300 B2K-3C and 10 more. Effective Jan 5, 2011
- [AD 2010-06-05](https://openairdocs.org/ad/2010-06-05) (historical): Fuselage · Airbus A300 B4-103, A300 B4-203, A300 B4-2C and 6 more. Effective Apr 15, 2010
- [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 2007-10-10 R1](https://openairdocs.org/ad/2007-10-10-R1) (historical): Fuel tank systems · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 more. Effective Dec 28, 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 2009-11-09](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 2009-02-04](https://openairdocs.org/ad/2009-02-04) (historical): Fuel level sensor-amplifier (FLSA) · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 more. Effective Mar 27, 2009
- [AD 2008-06-18](https://openairdocs.org/ad/2008-06-18) (historical): Lower skin panel · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Apr 23, 2008
- [AD 2008-03-04](https://openairdocs.org/ad/2008-03-04) (historical): P-clips · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 more. Effective Mar 6, 2008
- [AD 2007-25-15](https://openairdocs.org/ad/2007-25-15) (historical): Main landing gear (MLG) · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Jan 14, 2008
- [AD 2007-22-05](https://openairdocs.org/ad/2007-22-05) (historical): Center box assembly · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 more. Effective Nov 28, 2007
- [AD 2007-20-03](https://openairdocs.org/ad/2007-20-03) (historical): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 more. Effective Oct 31, 2007
- [AD 2007-18-02](https://openairdocs.org/ad/2007-18-02) (historical): Fuel pump cables · Airbus A300 Model B2-1A, A300 Model B2-1C, A300 Model B2-203 and 13 more. Effective Oct 2, 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 2007-03-09](https://openairdocs.org/ad/2007-03-09) (historical): Ram air turbine (RAT) · Airbus A300B4-601, A300B4-603, A300B4-605R and 6 more. Effective Mar 12, 2007
- [AD 2007-03-18](https://openairdocs.org/ad/2007-03-18) (historical): Wing main landing gear (MLG) · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Feb 23, 2007

All 468: https://openairdocs.org/aircraft/N731FD/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 N731FD.

## FAA accident and incident reports

None matched to N731FD.

## Service difficulty reports (202, 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 FDEA202609271454](https://openairdocs.org/sdr/FDEA202609271454), Sep 27, 2026: SPOILER. DELAMINATED. RIGHT WING SPOILER NR 5. CENTER OTBD HINGE ARM, OTBD SURFACE FOUND DELAMINATED. COMPLIED WITH EA: 6-5750-T0388918 P1 TO REPAIR RT WING SPOILER NR 5 CENTER OTBD 
- [SDR FDEA202609091463](https://openairdocs.org/sdr/FDEA202609091463), Sep 9, 2026: FITTING. DAMAGED. CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24 COMPLIED WITH E
- [SDR FDEA202609061306](https://openairdocs.org/sdr/FDEA202609061306), Sep 6, 2026: REPAIR. NONE. EXISTING REPAIR ON RUDDER TRAILING EDGE RH AFT LOWER SKIN BTW RR0-BR1 REQUIRES EVALUATION FOR CONFORMITY. EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM 55
- [SDR FDEA202609051321](https://openairdocs.org/sdr/FDEA202609051321), Sep 5, 2026: REPAIR. NONE. EXISTING REPAIR ON FRAME FR12 AT 8-9 O'CLOCK REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON FRAME FR12 AT 8-9 O'CLOCK WAS EVALUATED AND FOUND NOT IN
- [SDR FDEA202609041453](https://openairdocs.org/sdr/FDEA202609041453), Sep 4, 2026: BACKBOARD. PUNCTURED. LH PAX DOOR SLIDE BACK-PLATE PUNCTURED. REPLACED THE LH PASSENGER/CREW DOOR SLIDE/RAFT PER AMM 25-61-22-04-01. MINOR REPAIR IAW FEDEX GMM 6-2-100.
- [SDR FDEA202609041305](https://openairdocs.org/sdr/FDEA202609041305), Sep 4, 2026: REPAIR. MISINSTALLED. EXISTING REPAIR ON FWD CARGO FLOOR BEAM AT FR30,Y140~Y805 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON FWD CARGO FLOOR BEAM AT FR30,Y140~Y805 WAS 
- [SDR FDEA202609041304](https://openairdocs.org/sdr/FDEA202609041304), Sep 4, 2026: REPAIR. NO DISCREPANCY. EXISTING REPAIR ON FWD CARGO ROLLER TRACK AT -Y140 BETWEEN FR35 AND FR36 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON FWD CARGO ROLLER TRACK AT -Y
- [SDR FDEA202609031303](https://openairdocs.org/sdr/FDEA202609031303), Sep 3, 2026: ROLLER TRACK. MISREPAIRED. EXISTING REPAIR ON AFT CARGO ROLLER TRACK AT Y805 BETWEEN FR59 AND FR60 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON AFT CARGO ROLLER TRACK AT Y80
- [SDR FDEA202605090576](https://openairdocs.org/sdr/FDEA202605090576), May 9, 2026: PUMP. LOW PRESSURE. ON TAKEOFF ROLL AT 30KTS, RECEIVED A YELLOW HYD PUMP LOW PR ECAM. TAKEOFF WAS REJECTED. ECAM CLEARED ON ITS OWN SHORTLY AFTER. 2ND ATTEMPT WAS MADE, SAME RESULT
- [SDR FDEA202411061637](https://openairdocs.org/sdr/FDEA202411061637), Nov 6, 2024: COVER. INSTALLED. THERE WAS A 40 KNOT DIFFERENCE BETWEEN CAPT S AND F/O AIRSPEED INDICATION ON TAKEOFF ROLL. CAPT REJECTED T/O AT APPROXIMATELY 80 KNOTS. ON WALK AROUND, FOUND CA
- [SDR FDEA202405190696](https://openairdocs.org/sdr/FDEA202405190696), May 19, 2024: RIB. CRACKED. RH WING CENTER FLAP RIB UPR FLANGE FOUND 3EA CRACKS AT RIB25 BETWEEN STGR2.8 AND REAR SPAR, AND RIB26 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0
- [SDR FDEA202405190695](https://openairdocs.org/sdr/FDEA202405190695), May 19, 2024: RIB. CRACKED. RH WING CENTER FLAP RIB UPR FLANGE FOUND 3EA CRACKS AT RIB20 BETWEEN STGR2.7 AND REAR SPAR, AND RIB21 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA: 6-5750-T0379
- [SDR FDEA202405190694](https://openairdocs.org/sdr/FDEA202405190694), May 19, 2024: RIB. CRACKED. RH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB11 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0379257 P1. TITLE: WING - FLIGHT SURFACES 
- [SDR FDEA202405190693](https://openairdocs.org/sdr/FDEA202405190693), May 19, 2024: RIB. CRACKED. LH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB25 BETWEEN STGR2.8 AND REAR SPAR, AND RIB26 BETWEEN STGR2.8 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0
- [SDR FDEA202405190692](https://openairdocs.org/sdr/FDEA202405190692), May 19, 2024: RIB. CRACKED. LH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB18 BETWEEN STGR2.8 AND REAR SPAR, AND RIB19 BETWEEN STGR2.8 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0
- [SDR FDEA202405190691](https://openairdocs.org/sdr/FDEA202405190691), May 19, 2024: RIB. CRACKED. LH WING CENTER FLAP RIB UPR FLANGE FOUND 4EA CRACKS AT RIB11 BETWEEN STGR2.8 AND REAR SPAR, RIB12 BETWEEN STGR2.8 AND REAR SPAR, AND RIB13 BETWEEN STGR2.7 AND R
- [SDR FDEA202405190690](https://openairdocs.org/sdr/FDEA202405190690), May 19, 2024: SKIN. DELAMINATED. LH WING #3 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 30MM*15MM, DEPTH: 1.51MM. COMPLIED WITH EA: 6-5750-T0379154 P1. TITLE: WING - 
- [SDR FDEA202401260115](https://openairdocs.org/sdr/FDEA202401260115), Jan 26, 2024: APU. FAILED. AFTER CLOSING THE DOORS FOR DEPARTURE, SMELLED ELECTRICAL SMOKE. DISCOVERED SMOKE OF UNKNOWN ORIGIN IN COURIER COMPART & CARGO AREA. APU AUTO SHUTDOWN. NOT SURE
- [SDR FDEA202312131936](https://openairdocs.org/sdr/FDEA202312131936), Dec 13, 2023: PRESSURE SWITCH. FAILED. L1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHT INOP. BUZZER WORKS NORMALLY. ENT BY: 691135 RPT BY:691135 MEL 13DEC23 17:31 MEM U RELEASED FOR SERVICE PER 
- [SDR FDEA202308021345](https://openairdocs.org/sdr/FDEA202308021345), Aug 2, 2023: TRANSMITTER. FAILED. AROUND 45 MIN INTO CRUISE FLIGHT WE NOTICED THE GREEN HYD REVISOR QUANTITY DECREASING. SHORTLY AFTER WE RECEIVED AN ECAM - GREEN RSVR LO LEVEL. COMPLIED WITH EC
- [SDR FDEA202303240498](https://openairdocs.org/sdr/FDEA202303240498), Mar 24, 2023: LINE. LEAKING. DURING CRUISE FLIGHT ECAM DISPLAYED HYD , HYD RSVR LO LEVEL , GREEN SYSTEM OVERHEAD GAUGE SHOWED QTY AT APPROX RED DOT , ECAM HYD PAGE DISPLAYED APPROX THE SAME
- [SDR FDEA202303230497](https://openairdocs.org/sdr/FDEA202303230497), Mar 23, 2023: TRANSMITTER. FAILED. PDIS 731 29-02 6666 23MAR23 OMA FACT AFTER CLEANUP DEPARTING KMEM, RECEIVED ECAM INDICATION OF LOW LEVEL ON GREEN HYD SYSTEM. LVL INDICATED ZERO ON ECAM AND OVE
- [SDR FDEA202303010355](https://openairdocs.org/sdr/FDEA202303010355), Mar 1, 2023: HOSE. LEAKING. PDIS 731 29-02 6592 01MAR23 IND OPEN U UPON GEAR EXTENSION AT KIND GREEN HYDRAULIC QUANTITY WENT TO ZERO. ACCOMPLISHED ECAM/QRH AND LANDED ON 05L. TOWED INTO CH
- [SDR FDEA202203080524](https://openairdocs.org/sdr/FDEA202203080524), Mar 8, 2022: NONE. NONE. REF ORIGINAL WRI ATA 22-10-XXX 08MAR22, TECH SERVICE ITEM ISSUED AND C/W. DUE TO A/P2, AND 2X'S FO'S SPEED DISPLAY DROPPING BACK TO 35 KNOTS THEN RECOVERING QUI
- [SDR FDEA202203080523](https://openairdocs.org/sdr/FDEA202203080523), Mar 8, 2022: NONE. NONE. FL 350, AUTO PILOT #2, COST INDEX 200, SMOOTH AIR, IN CRUZ, IN PROFILE; TWO TIMES THE FO S SPEED ROLLED BACK TO 35 KNOTS ON THE SPEED TAPE. THE FIRST TIME FO SE
- [SDR FDEA202201160123](https://openairdocs.org/sdr/FDEA202201160123), Jan 16, 2022: SEAT TRACK. DAMAGED. N00464 MAIN DECK SEAT TRACK LOBE AT LOCKS L1206 & L1199 DAMAGED. REPLACED THE DAMAGED SEAT TRACK WITH NEW ONE. I.A.W. A300-600 SRM 51-72-10-001 PAGE. 1~3. SEE A
- [SDR FDEA202201140065](https://openairdocs.org/sdr/FDEA202201140065), Jan 14, 2022: NONE. NONE. N00446 AFTER REMOVE CENTER WING JOINT FR40 LH & RH UPPER HOLE BUSHES,FOUND BUSHES ID HOLE DAMAGE. I.A.W T6-5710-T0347753 B P2 PAGE 4 OF 4 STEP 3 FABRICATE NEW B
- [SDR FDEA202201110229](https://openairdocs.org/sdr/FDEA202201110229), Jan 11, 2022: DOUBLER. UNKNOWN. AT THE TIME OF RECORDS REVIEW THE FOLLOWING WAS IDENTIFIED ON MAJIOR REPAIR W/O 45404 SNRM N00072,DOCUMENTATION PROVIDED IS INCOMPLETE UNABLE TO VERIFY ALL PART
- [SDR FDEA202201110084](https://openairdocs.org/sdr/FDEA202201110084), Jan 11, 2022: FLOOR PANEL. DAMAGED. N00433 MAIN DECK CARGO COMPT #252WH FLOOR PANEL WAS FOUND EDGE DAMAGED. REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201 P.205-206 PARA.9A FIG.201.
- [SDR FDEA202201110083](https://openairdocs.org/sdr/FDEA202201110083), Jan 11, 2022: FLOOR PANEL. DAMAGED. N00432 MAIN DECK CARGO COMPT #252YH FLOOR PANEL WAS FOUND EDGE DAMAGED. REPAIRED THE FLOOR PANEL I.A.W A300-600 SRM 53-10-20-201 P.205-206 PARA.9A FIG.201.
- [SDR FDEA202201080114](https://openairdocs.org/sdr/FDEA202201080114), Jan 8, 2022: SEAT TRACK. UNKNOWN. N00373 AIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR55 TO FR57.3,-Y1959 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-
- [SDR FDEA202201080113](https://openairdocs.org/sdr/FDEA202201080113), Jan 8, 2022: SEAT TRACK. UNKNOWN. N00371 AIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR59 TO FR60,Y1959 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-500
- [SDR FDEA202201080112](https://openairdocs.org/sdr/FDEA202201080112), Jan 8, 2022: SEAT TRACK. UNKNOWN. N00370 AIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR61 TO FR62,Y1456 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-500
- [SDR FDEA202201080080](https://openairdocs.org/sdr/FDEA202201080080), Jan 8, 2022: SKIN. UNKNOWN. AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON R/H WING LWR SURFACE L/E PANEL 613AB CUTOUT FWD O/B AREA. COMPLIED WITH ATTACHMENT B OF EO: E6-510
- [SDR FDEA202201070079](https://openairdocs.org/sdr/FDEA202201070079), Jan 7, 2022: SKIN. UNKNOWN. AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON L/H WING LWR SURFACE L/E PANEL 513AB CUTOUT FWD O/B AREA. COMPLIED WITH ATTACHMENT B OF EO: E6-510
- [SDR FDEA202201070078](https://openairdocs.org/sdr/FDEA202201070078), Jan 7, 2022: NONE. UNKNOWN. AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON RUDDER TRAILING EDGE APEX AREA LOCATED BTW T/E SCREW LINE NO.21 AND NO.22 FASTENER COUNTED FROM LO
- [SDR FDEA202201030026](https://openairdocs.org/sdr/FDEA202201030026), Jan 3, 2022: NONE. CORRODED. MAIN DECK SEAT TRACK STRUCTURE FOUND CORROSION BTWN FR11~12A , Y730 REPLACED THE CORROSION SEAT TRACK WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001, PAGE2
- [SDR FDEA202201020115](https://openairdocs.org/sdr/FDEA202201020115), Jan 2, 2022: STRINGER. CORRODED. FWD CGO COMP'T BILGE STGR CORROSION BTW FR38.2 AND FR39 ,S-44R POSITION. CUT-OUT THE DAMAGED AREA AND PERFORMED STRINGER REPAIR I.A.W. A300-600 SRM 53-10- 14-20
- [SDR FDEA202108312174](https://openairdocs.org/sdr/FDEA202108312174), Aug 31, 2021: BRAKE. OUT OF ALIGNMENT. AFTER T/O HAD ECAM ALERT WITH #2 TIRE EXCEEDING 300 DEGREES. GEAR WAS ALREADY RETRACTED AT THE TIME OF ALERT. ELECTED TO PRESS ON TO CLT WITH MAX 380 DEGREES ON
- [SDR FDEA202101090029](https://openairdocs.org/sdr/FDEA202101090029), Jan 9, 2021: PUMP. MALFUNCTIONED. AT APPROX 60 KTS ROLL GOT NR 2 GREEN HYD PUMP LOW PSI. SAME LIGHT CAME ON AFTER START OF NR 1 ENGINE, BUT WENT OUT ON ITS OWN AFTER A MINUTE. REJECTED TAKE OFF.
- [SDR FDEA2020090832113](https://openairdocs.org/sdr/FDEA2020090832113), Sep 3, 2020: FMC. ABNORMAL. PDIS 731, 34-63, 3866, 03SEP20, MEM FACT U. AT FL340 ADC 1 FAILED. AP 1 DISENGAGED, LOST PFD INSTRUMENTATION, ND UNAVAILABLE, FMC 1 FAILURE, ATS 2 TRIPPED OFF. 
- [SDR FDEA2019082191952](https://openairdocs.org/sdr/FDEA2019082191952), Aug 19, 2019: LANDING. DAMAGED. RIGHT HAND WING ON PANEL LANDS ON 650LB, 650MB AND 660BB HAVE BUSHINGS INSTALLED IN INSPECTION AREA WITH TWO EACH CRACKS AT PANEL LAND 660BB HOLES 1 AND 2. COMP
- [SDR FDEA2019082171924](https://openairdocs.org/sdr/FDEA2019082171924), Aug 17, 2019: FITTING. CORRODED. R/H CTR WING FR47 BOTTOM PANEL AT REAR SPAR JUNCTION, HOLE "F" HAS INDICATIONS FOUND DUE TO CORROSION PITS IN HOLE FROM 2ND TO END OF 3RD LAYER FROM LOWER SKIN.
- [SDR FDEA2019082171923](https://openairdocs.org/sdr/FDEA2019082171923), Aug 17, 2019: FITTING. CRACKED. INDICATIONS DURING ROTOPROBE INSPECTION OF HOLE "186" DUE TO VISUAL DAMAGE INSIDE HOLE RH WING COMPLIED WITH EA 6-5710-TO348474-P1
- [SDR FDEA2019082171922](https://openairdocs.org/sdr/FDEA2019082171922), Aug 17, 2019: FITTING. CRACKED. R/H CTR WING FR47 BOTTOM PANEL AT REAR JUNCTION , HOLE "S" HAS A CRACK INDICATIONS FOUND 3 & 9 O'CLOCK POSITION AT 3RD LAYER TO 5TH LAYER IN HOLE. COMPLIED WITH
- [SDR FDEA2019082171919](https://openairdocs.org/sdr/FDEA2019082171919), Aug 17, 2019: FITTING. CRACKED. CTR WING FR47 BOTTOM PANEL AT REAR JUNCTION, HOLE "G" HAS A CRACK INDICATION FOUND 10 O'CLOCK POSITION AT 3RD LAYER TO END OF HOLE. COMPLIED WITH EA 6-5710-T034
- [SDR FDEA2019082171918](https://openairdocs.org/sdr/FDEA2019082171918), Aug 17, 2019: FITTING. CRACKED. R/H FR47 FASTENER 11RH AND BUSHINGS REQUIRE REMOVAL FOR NDT ROTOTEST INSP. COMPLIED WITH EA 6-5710-T0348474-P1
- [SDR FDEA2019082171917](https://openairdocs.org/sdr/FDEA2019082171917), Aug 17, 2019: FITTING. CRACKED. INDICATIONS DURING ROTOPROBE INSPECTION OF HOLE "166" DUE TO VISIBLE DAMAGE INSIDE OF HOLE. RH WING COMPLIED WITH EA 6-5710-T0348474-P1
- [SDR FDEA2019082171916](https://openairdocs.org/sdr/FDEA2019082171916), Aug 17, 2019: FITTING. CRACKED. R/H WING INSPECTION OF FASTENER HOLE (C)FAILED ROTO PROBE INSPECTION DUE TO MULTIPLE CRACK INDICATIONS AT APOX. DEPTH OF .9" TO 1.4" INSPECTION FROM THE BOTTOM 
- [SDR FDEA2019082171915](https://openairdocs.org/sdr/FDEA2019082171915), Aug 17, 2019: FITTING. CRACKED. HOLE "I" RH SIDE HAS VISIBLE GOUGES ON TANK SIDE LAYER AT THE 9 AND 6 O'CLOCK POSITIONS GIVING INDICATIONS FROM ROTOPROBE INSPECTION COMPLIED WITH EA 6-5710-TO3

All 202: https://openairdocs.org/aircraft/N731FD/reports.md

## STCs that may be installed (OpenAirDocs) (168, 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 A300 B4-605R)

- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [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 SA5040NM](https://openairdocs.org/stc/SA5040NM): Installation of cargo pallet and net. Satco Inc
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC SA3400NM](https://openairdocs.org/stc/SA3400NM): Installation of floor proximity emergency escape path marking system. Bruce Aerospace Inc. Lists A300 Series
- [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 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 ST11861AT](https://openairdocs.org/stc/ST11861AT): Installation of a new Control Wheel Push-to-Talk (PTT) switch with three positions and latchable in accordance with the MDL shown in the attached AML No. ST11861AT. FedEx Express
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST00691SE](https://openairdocs.org/stc/ST00691SE): Installation of lightweight window plugs. LiteAir Aviation Products Inc
- [STC ST02302CH](https://openairdocs.org/stc/ST02302CH): Install ERDA model 7004 HI-LO table with slide top. Collins Aerospace
- [STC ST01940CH](https://openairdocs.org/stc/ST01940CH): Installation of a Honeywell RESCU 406AF 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 ST00181SE](https://openairdocs.org/stc/ST00181SE): Installation of Model 4033, 4034 and 4038 Transient Suppression Units. Honeywell International Inc
- [STC ST00440SE](https://openairdocs.org/stc/ST00440SE): Installation of the Honeywelll Enhanced Ground Proximity Warning 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 SA7565SW](https://openairdocs.org/stc/SA7565SW): Rebuild A300 Auxiliary Power Unit Oil Cooler Assembly by manufacturing a new core assembly. Honeywell International Inc. Lists A300 Series
- [STC SA4821NM](https://openairdocs.org/stc/SA4821NM): Installation of a Hughes-Avicom video entertainment system. Burrana Inc. Lists A300 Series
- [STC SA3483NM](https://openairdocs.org/stc/SA3483NM): Installation of Trans Com video projection system. Burrana Inc. Lists A300 Series
- [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 SA6082NM](https://openairdocs.org/stc/SA6082NM): Installation of audio entertainment system. Burrana Inc. Lists A300 B4 Series
- [STC ST04092NY](https://openairdocs.org/stc/ST04092NY): Installation of Wireless PCMCIA for DFDAU. Delta Engineering Corporation
- [STC ST04511AT](https://openairdocs.org/stc/ST04511AT): Installation of Whelen LED logo lights. Avionics Support Group Inc
- [STC ST02686LA](https://openairdocs.org/stc/ST02686LA): Installation of an alternate part number. Honeywell International Inc
- [STC ST04049NY](https://openairdocs.org/stc/ST04049NY): Installation of a Hoffman Engineering LLC LED Landing Light to replace the OEM Q4559 Series Incandescent Lamp, used as a Landing/Takeoff Light. Hoffman Engineering LLC
- [STC ST00855LA](https://openairdocs.org/stc/ST00855LA): Installation of ANCRA main deck cargo handling system. Ancra International LLC. Lists A300 B4 Series
- [STC ST01644LA](https://openairdocs.org/stc/ST01644LA): Installation of Ancra cargo system. Ancra International LLC
- [STC ST02482LA](https://openairdocs.org/stc/ST02482LA): Installation of main deck cargo loading system. Ancra International LLC
- [STC ST04345NY](https://openairdocs.org/stc/ST04345NY): Upgrade from TCAS II software version 7.0 to 7.1. PMV Engineering
- [STC ST01891LA-D](https://openairdocs.org/stc/ST01891LA-D): Installation of a Commercial Medical Stretcher. LifePort LLC
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST09962SC](https://openairdocs.org/stc/ST09962SC): Installation of X-Band nose radome shell assembly. The NORDAM Group LLC
- [STC ST01215AT-D](https://openairdocs.org/stc/ST01215AT-D): Installation of Collins SAT-906 SATCOM System with Canadian Marconi CMA-2102 antenna system. TIMCO. Lists A300 Series
- [STC ST01223AT-D](https://openairdocs.org/stc/ST01223AT-D): Installation of Airshow 210 System with Dual RADVR and with Airshow Provisions. HAECO Cabin Solutions LLC
- [STC ST01361AT-D](https://openairdocs.org/stc/ST01361AT-D): Installation of Dual Mode "S" Transponders. HAECO Cabin Solutions LLC
- [STC ST03848NY](https://openairdocs.org/stc/ST03848NY): Installation of SuperSeal UltraLite (SSUL) PHOTOLUMINESCENT AISLE PATH MARKING SYSTEM. STG Aerospace Ltd
- [STC ST02639LA](https://openairdocs.org/stc/ST02639LA): Replace the existing Mode S Transponder system. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST04229NY](https://openairdocs.org/stc/ST04229NY): Introduction of a 16G New Generation Stretcher XL P/N 1120030-Series. Bucher Leichtbau AG
- [STC ST04309CH](https://openairdocs.org/stc/ST04309CH): Installation of ADS-B OUT Global Positioning Satellite System (GPSS)/Space-Based Augmentation System (SBAS) & ADS-B IN Flight Information Services-Broadcast (FIS-B) system. Innoviator LLC
- [STC ST04221AT](https://openairdocs.org/stc/ST04221AT): The installation of a Honeywell Enhanced Ground Proximity Warning System (EGPWS). United Parcel Service Company
- [STC SA3185SO](https://openairdocs.org/stc/SA3185SO): Installation of a replacement coalescer filter. Purolator Facet, Inc
- [STC ST04372AT](https://openairdocs.org/stc/ST04372AT): Installation of Wireless Data Loader Provisions. Chippewa Aerospace Inc
- [STC ST02406LA](https://openairdocs.org/stc/ST02406LA): Installation of TCAS version 7.1. Aviation Communication and Surveillance Systems (ACSS) LLC

All 168: https://openairdocs.org/aircraft/N731FD/stcs.md

## Earlier aircraft with N731FD

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N731FD before.

- [Cancelled 1978-04-17](https://openairdocs.org/deregistered/N731FD-1978-04-17): Cessna A188B, S/N 18802856T. Exported to Libya. Owner: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)

## Related

- Other Airbus Industrie A300 B4-605R aircraft: https://openairdocs.org/model/airbus-industrie-a300-b4-605r/aircraft.md
- The GE CF6-80C2A5 engine: https://openairdocs.org/engine/ge-cf6-80c2a5.md

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