# N689FE: 2007 Airbus A300 F4-605R

- Status: Valid registration
- Airframe: [Airbus A300 F4-605R](https://openairdocs.org/model/airbus-a300-f4-605r) (registry code 3930343, 347 seats)
- Engine: [GE CF6-80C2A5F](https://openairdocs.org/engine/ge-cf6-80c2a5f) (registry code 30113)
- 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: 0875
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 6, 2007
- Certificate issued: June 5, 2007
- Expires: July 31, 2027
- Mode S code: A92528
- 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=689FE
- Page: https://openairdocs.org/aircraft/N689FE

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): 340 in force

### Matched by airframe (Airbus A300 F4-605R)

- [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 2024-01-08](https://openairdocs.org/ad/2024-01-08): Doors · Airbus A300 F4-605R and A300 F4-622R. Effective Mar 21, 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 2022-25-08](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 2022-24-02](https://openairdocs.org/ad/2022-24-02): Doors · Airbus A300 F4-605R and A300 F4-622R. Effective Jan 9, 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 2020-26-11](https://openairdocs.org/ad/2020-26-11): Equipment/furnishings · Airbus A300 F4-605R and A310-324. Effective Jan 27, 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 2020-21-04](https://openairdocs.org/ad/2020-21-04): Fuselage · Airbus A300 F4-605R and A300 F4-622R. Effective Nov 18, 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

### Matched by engine (GE CF6-80C2A5F)

- [AD 2021-26-22](https://openairdocs.org/ad/2021-26-22): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 14, 2022
- [AD 2022-02-18](https://openairdocs.org/ad/2022-02-18): Engine Mount Section · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 3 more. Effective Feb 25, 2022
- [AD 2021-14-11](https://openairdocs.org/ad/2021-14-11): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 25 more. Effective Aug 27, 2021
- [AD 2021-03-02](https://openairdocs.org/ad/2021-03-02): Fuel Control/Turbine Engines · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Mar 31, 2021
- [AD 2020-22-02](https://openairdocs.org/ad/2020-22-02): Engine Fuel and Control · General Electric CF6-80C2A5F, CF6-80C2B1F, CF6-80C2B2F and 13 more. Effective Dec 3, 2020
- [AD 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 2007-21-06](https://openairdocs.org/ad/2007-21-06): Electronic control unit (ECU) · General Electric CF6-80C2A5F. Effective Nov 15, 2007
- [AD 2007-11-20](https://openairdocs.org/ad/2007-11-20): Fuel shroud retaining rings · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 22 more. Effective Jul 10, 2007
- [AD 2007-05-14](https://openairdocs.org/ad/2007-05-14): Cast titanium weld- repaired forward engine mount platforms · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 9, 2007
- [AD 2006-16-06](https://openairdocs.org/ad/2006-16-06): Certain stage 1 high- pressure turbine (HPT) rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Sep 5, 2006
- [AD 2005-17-05](https://openairdocs.org/ad/2005-17-05): High pressure compressor rotor (HPCR) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Sep 27, 2005
- [AD 2005-06-07](https://openairdocs.org/ad/2005-06-07): Directional pilot valve (DPV) assembly · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Apr 25, 2005
- [AD 2004-22-07](https://openairdocs.org/ad/2004-22-07): Stage 2 nozzle guide vanes (HPT S2 NGVs) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 1, 2004
- [AD 2004-07-13](https://openairdocs.org/ad/2004-07-13): High pressure turbine (HPT) stage 1 disks · General Electric CF6-80C2A5F, CF6-80C2B5F, CF6-80C2B7F and 1 more. Effective May 6, 2004
- [AD 2003-12-08](https://openairdocs.org/ad/2003-12-08): Directional pilot valve · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Jul 23, 2003
- [AD 2003-02-07](https://openairdocs.org/ad/2003-02-07): Low pressure turbine (LPT) shrouds · General Electric CF6-50A, CF6-50C, CF6-50C1 and 30 more. Effective Mar 3, 2003
- [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08): High pressure compressor rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Jan 23, 2003
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 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

### 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 2019-16-11](https://openairdocs.org/ad/2019-16-11) (historical): Doors · Airbus A300 F4-605R and A300 F4-622R. Effective Oct 2, 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 2018-20-06](https://openairdocs.org/ad/2018-20-06) (historical): Doors · Airbus A300 F4-605R and A300 F4-622R. Effective Nov 5, 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 2016-15-01](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 2012-15-14](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 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
- [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

All 457: https://openairdocs.org/aircraft/N689FE/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 N689FE.

## FAA accident and incident reports

None matched to N689FE.

## Service difficulty reports (96, 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 FDEA202608181142](https://openairdocs.org/sdr/FDEA202608181142), Aug 18, 2026: PROCESSOR. FAULTED. TAKEOFF AT IND, MLG WOULD NOT RETRACT. C-W QRH. RETURNED. EMERG DECLARED. AMM 32-31-00-05, NLG RETRACT FULLY, GREEN ON BOTH MLG INDS, BOTH LT & RT MLG STAYED GR
- [SDR FDEA202507081309](https://openairdocs.org/sdr/FDEA202507081309), Jul 8, 2025: SKIN. DENTED. FABRICATE NEW LOWER INNER SKIN PER EA NO:T6-5230-T0382227 AT MDCD FR21~26,LONGN 8 ~ STGR 30L FABRICATED AND INSTALLED NEW LOWER INNER SKIN AT MDCD FR21-26, LONG
- [SDR FDEA202507081308](https://openairdocs.org/sdr/FDEA202507081308), Jul 8, 2025: FORK. DAMAGED. FABRICATE NEW REAR FORK FRAME 21 PER EA NO:T6-5230-T0382227 AT MDCD FR21,LONGN 6~STGR 30L FABRICATED AND INSTALLED NEW REAR FORK FRAME 21 AT MDCD FR21, LONGN 6 
- [SDR FDEA202507081306](https://openairdocs.org/sdr/FDEA202507081306), Jul 8, 2025: SKIN. DENTED. PER EA NO:T6-5230-T0382227 PERFORM SPLICE REPAIR ON MDCD INNER SKIN AT FR21,LONGN 4~5 FABRICATED AND INSTALLED NEW REPAIR SPLICE AND CONNECTING CLIP AT MDCD FR2
- [SDR FDEA202506301307](https://openairdocs.org/sdr/FDEA202506301307), Jun 30, 2025: SKIN. DENTED. AIRCRAFT REPAIR ASSESSMENT: EXISTING REPAIR SPLICE FOUND ON MAIN CARGO DOOR INNER SKIN BTW FR20~21, BEAM 3~4 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7
- [SDR FDEA202506261053](https://openairdocs.org/sdr/FDEA202506261053), Jun 26, 2025: FLOOR SUPPORT. CRACKED. M/D FLOOR SUPPORT FOUND CRACK AT FR37~FR38, -Y2462. REMOVED CRACK SUPPORT AT M/D FLOOR FR37~38,-Y2462,THEN INSTALLED NEW ONE WITH FASTENERS I.A.W A300-600F SRM 
- [SDR FDEA202506191079](https://openairdocs.org/sdr/FDEA202506191079), Jun 19, 2025: SKIN. GOUGED. A GOUGE WAS FOUND ON OUTBD EDGE LOWER SIDE OF L2 SPLR. ACCOMPLISHED DOUBLER REPAIR WITH FASTENERS AT OUTBD EDGE OF L2 SPLR RIB 18 POSITION I.A.W FEDEX EA NO:T6-
- [SDR FDEA202506141122](https://openairdocs.org/sdr/FDEA202506141122), Jun 14, 2025: SKIN. DENTED. RH WING OUTER FLAP D-NOSE SKIN GOT DENT BETWEEN RIB15~17 ,S-1.1~1.2 ACCOMPLISHED THE NOSE SKIN FLUSH REPAIR AT RH WING OUTER FLAP RIB15~17, S-1.1~1.2 I.A.W A300
- [SDR FDEA202506131016](https://openairdocs.org/sdr/FDEA202506131016), Jun 13, 2025: SEAT TRACK. CORRODED. M/D SEAT TRACK FOUND CORROSION AT FR80-4", Y0 POS. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK AT FR80~FR78 PLUS 13" Y0 IAW A300-600
- [SDR FDEA202506131017](https://openairdocs.org/sdr/FDEA202506131017), Jun 13, 2025: SEAT TRACK. CORRODED. M/D SEAT TRACK FOUND CORROSION AT FR80-5", Y1221.2 POS. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK AT FR80~FR78 PLUS 13" Y1221.2 IA
- [SDR FDEA202506121064](https://openairdocs.org/sdr/FDEA202506121064), Jun 12, 2025: SEAT TRACK. CRACKED. M/D FLOOR SUPPORT FOUND CRACK AT FR38.1~FR38.2, -Y2462 POS REMOVED CRACK SUPPORT AT M/D FLOOR FR38.1~38.2,-Y2462,THEN INSTALLED NEW ONE WITH FASTENERS I.A.W A30
- [SDR FDEA202506121052](https://openairdocs.org/sdr/FDEA202506121052), Jun 12, 2025: STRUT. CRACKED. M/D FLOOR SUPPORT FOUND CRACK AT FR38.1~FR38.2, Y2462 POS. REPLACED THE CRACK STRUT WITH NEW PART ON M/D FLOOR SUPPORT AT FR38.1 ~FR38.2 Y2462 I.A.W A300-600F S
- [SDR FDEA202506111081](https://openairdocs.org/sdr/FDEA202506111081), Jun 11, 2025: FITTING. NOT REPORTED. REPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23 PER EO NO:E6- 5230-E0378588 B P5 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK 
- [SDR FDEA202506111005](https://openairdocs.org/sdr/FDEA202506111005), Jun 11, 2025: SHEAR WEB. CRACKED. M/D FLOOR STRUCTURE FOUND A SHEAR WEB CRACK AT FR77-1', S-26R. REPLACED THE CRACK SHEAR WEB WITH NEW PART ON M/D FLOOR STRUCTURE AT FR77-1", S- 26R I.A.W A300-6
- [SDR FDEA202506091078](https://openairdocs.org/sdr/FDEA202506091078), Jun 9, 2025: SUPPORT. CRACKED. LH WING TE CAVITY LOWER FACE OF UPPER FIXED PNL FOUND SUPPORT WEB CRACK NEAR L5 SPLR INBD. TRIMMED OUT AND INSTALLED REPAIR BRACKET REPAIR AT LH WING SKIN SUPPO
- [SDR FDEA202506031080](https://openairdocs.org/sdr/FDEA202506031080), Jun 3, 2025: FITTING. CRACKED. THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING WAS FOUND CRACK AT FRAME 24 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR24, LONG
- [SDR FDEA202410061431](https://openairdocs.org/sdr/FDEA202410061431), Oct 6, 2024: SUPPORT FITTING. CORRODED. RH MLG FWD LUG RIB 5 CORROSION IN BORE. REMOVED CORROSION FROM RH MLG FWD LUG RIB 5 PER AIRBUS R57240425 AND EA # 6-5710-T0380814 P1.
- [SDR FDEA202409271380](https://openairdocs.org/sdr/FDEA202409271380), Sep 27, 2024: SUPPORT FITTING. CORRODED. BUSH E HAS DAMAGE TO CHROME FACE. REMOVED AND REPLACED BUSHING D AND E PER AIRBUS R57240425.
- [SDR FDEA202408271176](https://openairdocs.org/sdr/FDEA202408271176), Aug 27, 2024: PROXIMITY SENSOR. FAILED. ON DEPARTURE LG WOULD NOT RETRACT ON SYS 2, SWITCHED TO SYS 1 & GEAR WOULD STILL NOT RETRACT. ALL GEAR REMAINED GREEN & DOORS SHOWED UNLOCK UNTIL HANDLE PLACED 
- [SDR FDEA202407040936](https://openairdocs.org/sdr/FDEA202407040936), Jul 4, 2024: FIRE DETECTOR. FAILED. ENG1 LOOP A FAULT DURING CLIMB OUT. APPEARED AND WENT AWAY AFTER A SHORT TIME ON FIRST FLIGHT, OCCURRED AGAIN TWICE DURING 2ND FLIGHT (ALSO DURING CLIMB OUT). R
- [SDR FDEA202305120862](https://openairdocs.org/sdr/FDEA202305120862), May 12, 2023: CONTROLLER. FAILED. ON FINAL, CONFIGURED SLATS/FLAPS 15/15, WE SELECTED 15\20. AFTER SEVERAL SECONDS WE RECEIVED SLATS/FLAPS FAULT ECAM. IAW ECAM, WE CYCLED FLAP LEVER WITH NO CHAN
- [SDR FDEA202301280170](https://openairdocs.org/sdr/FDEA202301280170), Jan 28, 2023: WEB. CRACKED. MDCC UNDER FLOOR 1EA WEB CRACKED AT FR47, Y953-Y1456. REPAIRED MDCC UNDER FLOOR CRACKED WEB AT FR47, Y953-Y1456 PER A300-600F SRM53-15-15- 201 FIG.201.THIS IS C
- [SDR FDEA202204140959](https://openairdocs.org/sdr/FDEA202204140959), Apr 14, 2022: WARNING MESSAGE. FALSE ACTIVATION. DURING APPROACH AND SLAT EXTENSION, RECEIVED ECAM. SLAT SYS 1 FAULT. & FLAPS SYS 1 & 2 FAULT. CYCLE PER ECAM. FAULT DID NOT CLEAR. ALL 3 FAULTS RETURNED INCLUDI
- [SDR FDEA202009012076](https://openairdocs.org/sdr/FDEA202009012076), Sep 1, 2020: HINGE. DELAMINATED. LH WING - 4# SPOILER I/B HINGE LOWER SURFACE DELAMINATED (S=20MM X 15MM,D=2.18MM), I/B HINGE INBD SURFACE DELAMINATED (S=60MM X 60MM,D=1.90MM). LH WING - 4# SPO
- [SDR FDEA202009012075](https://openairdocs.org/sdr/FDEA202009012075), Sep 1, 2020: HINGE ARM. DELAMINATED. RH WING - #3 SPOILER O/B CTR HINGE ARM LWR SURFACE DELAMINATED (S=10MM X 15MM,D=2.0MM), I/B CTR HINGE ARM I/B SURFACE DELAMINATED (S=30MM X 40MM,D=1.5MM). RH WI
- [SDR FDEA202008292064](https://openairdocs.org/sdr/FDEA202008292064), Aug 29, 2020: HINGE ARM. DELAMINATED. RT WING, NR 4 SPOILER I/B CTR HINGE ARM I/B SURFACE DELAMINATED (S=30MM X 40MM,D=1.5MM), O/B CTR HINGE ARM O/B SURFACE DELAMINATED (S=30MM X 25MM,D=1.45MM). RT 
- [SDR FDEA202008292063](https://openairdocs.org/sdr/FDEA202008292063), Aug 29, 2020: SKIN. DELAMINATED. RT WING NR 5 SPOILER I/B CTR HINGE ARM I/B SURFACE DELAMINATED (S=30MM X 40MM, D=1.3MM), O/B CTR HINGE ARM O/B SURFACE DELAMINATED (S=30MM X 40MM, D=1.5MM), O/B
- [SDR FDEA2020083192064](https://openairdocs.org/sdr/FDEA2020083192064), Aug 29, 2020: HINGE ARM. DELAMINATED. RH WING - #4 SPOILER I/B CTR HINGE ARM I/B SURFACE DELAMINATED (S=30MM X 40MM,D=1.5MM), O/B CTR HINGE ARM O/B SURFACE DELAMINATED (S=30MM X 25MM,D=1.45MM).
- [SDR FDEA2020091124201](https://openairdocs.org/sdr/FDEA2020091124201), Aug 24, 2020: FRAME. CRACKED. NDT INSP RT CENTER WING JOINT AT FR40 UPPER HOLE FOUND CRACKED SIGNAL. NDT INSP RT CENTER WING JOINT AT FR40 UPPER HOLE FOUND CRACKED SIGNAL. COMPLIED WITH EA: 
- [SDR FDEA2020082642001](https://openairdocs.org/sdr/FDEA2020082642001), Aug 24, 2020: JOINT. CRACKED. NDT INSPECTION, RT CENTER WING JOINT AT FR40 UPPER HOLE FOUND CRACKED SIGNAL.
- [SDR FDEA2020052211014](https://openairdocs.org/sdr/FDEA2020052211014), May 21, 2020: GCU. MALFUNCTIONED. PDIS 689 24-20 1465 20MAY20 GENERATOR #2 FAULT @ CLIMB FROM FL 300 TO FL 330. TRIED RESET GENERATOR #2 WOULD NOT RESET .ATTEMPTED START OF APU @ FL 330 WOULD NO
- [SDR FDEA20180515224](https://openairdocs.org/sdr/FDEA20180515224), May 14, 2018: SKIN. DENTED. CARGO DOOR EXTERNAL SKIN HAS TWO DENTS. 5 INCHES FROM FWD LOWER CORNER, 1 INCH. AND 4 INCHES FROM FWD EDGE. FOUND TO BE OUT OF LIMITS IAW SRM 52-30-00, CUT OUT 
- [SDR FDEA201804301146](https://openairdocs.org/sdr/FDEA201804301146), Apr 30, 2018: SEAT TRACK. DAMAGED. MAIN CABIN SEAT TRACK -Y1959 DAMAGED BETWEEN FRAMES 63 AND 64. REMOVED DAMAGED SECTION FROM THE SEAT TRACK IAW SRM 51-40-21. FABRICATED A REPAIR IAW SRM 53-10-1
- [SDR FDEA201710112906](https://openairdocs.org/sdr/FDEA201710112906), Oct 11, 2017: SOLENOID VALVE. INOPERATIVE. SLATS & FLAPS SYSTEM 1 AND 2 FAULTED WHEN THE HANDLE WAS SELECTED TO 15/20. FLAPS WOULD RETRACT TO 0 WHEN SELECTED, BUT ONLY EXTEND TO 15/15 WITHOUT A FAULT IND
- [SDR FDEA201705031349](https://openairdocs.org/sdr/FDEA201705031349), May 3, 2017: VALVE. CRACKED. AT TOP OF DESCENT, THE GREEN SYS HYD QTY LOW ECAM ILLUMINATED. ECAM AND OVERHEAD BOTH INDICATED QTY LOSS. NO AIR LIGHT WAS ASSOCIATED WITH THIS PROBLEM. MANUALL
- [SDR FDEA201705021317](https://openairdocs.org/sdr/FDEA201705021317), May 2, 2017: GAUGE. LEAKING. R1 ENTRY DOOR EMERGENCY CYLINDER PRESSURE GAUGE IS MISSING CENTER PLUG IN LENS AND IS LEAKING OIL FROM GAUGE. REMOVED AND REPLACED R1 DOOR DAMPER EMERGENCY OPER
- [SDR FDEA201704291297](https://openairdocs.org/sdr/FDEA201704291297), Apr 29, 2017: RELIEF VALVE. FAILED. RIGHT AFTER DEPARTING AT FL 340, DURING DESCENT, RECEIVED A GREEN HYD RESERVOIR LOW LEVEL WARNING. CONFIRMED ON OVERHEAD AND ECAM. FOLLOWED ECAM AND QRH PROCEDU
- [SDR FDEA201704281292](https://openairdocs.org/sdr/FDEA201704281292), Apr 28, 2017: VALVE. STUCK. ON DESCENT TO KMEM, GOT GREEN HYD RESERVOIR LO LEVEL. CONFIRMED ON OVERHEAD & ECAM. FOLLOWED QRH PROCEDURE & MANUAL EXTENDED GEAR AND SHUT DOWN AFFECTED EQUIPME
- [SDR FDEA201512214062](https://openairdocs.org/sdr/FDEA201512214062), Dec 21, 2015: FLUID. LOW. ON TAKEOFF ROLL, JUST AFTER SETTING TAKEOFF POWER, ECAM FLASHED LOW OIL PRESS, THEN WENT AWAY, GEN NR 2 FAILED SHORTLY AFTER. REJECTED TAKEOFF PRIOR TO 70 KTS. 
- [SDR FDEA201511183700](https://openairdocs.org/sdr/FDEA201511183700), Nov 18, 2015: FLOOR PANEL. DELAMINATED. MAIN DECK FLOOR PANEL 251 CH IS DELAMINATED. FABRICATED NEW PANEL ON T15 1172111 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511183698](https://openairdocs.org/sdr/FDEA201511183698), Nov 18, 2015: FLOOR PANEL. BROKEN. MCD FLOOR PANEL 232 ZG HAS BROKEN BOTTOM COMPOSITE LAYER ON RT EDGE CORNER. FABRICATED NEW PANEL ON T15 1172044 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CA
- [SDR FDEA201511183697](https://openairdocs.org/sdr/FDEA201511183697), Nov 18, 2015: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 232 VH DAMAGED. FABRICATED NEW PANEL ON T15 1172146 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511183696](https://openairdocs.org/sdr/FDEA201511183696), Nov 18, 2015: FLOOR PANEL. DAMAGED. MDCC FLOOR PANEL 231 JG PUNCTURED ON SEVERAL PLACES. FABRICATED NEW PANEL ON T15 1172142 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511183699](https://openairdocs.org/sdr/FDEA201511183699), Nov 18, 2015: FLOOR PANEL. CRACKED. FLOORBOARD PANEL 241 LK HAS CRACKED. FABRICATED NEW PANEL ON T15 1172117 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511173678](https://openairdocs.org/sdr/FDEA201511173678), Nov 17, 2015: FLOOR PANEL. DAMAGED. MCD FLOOR PANEL 232 HG LOWER SURFACE DAMAGED AT FASTENER HOLE. FABRICATED NEW PANEL ON T15 1172057 IAW DWG SRZ 25-005 REV L CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511173677](https://openairdocs.org/sdr/FDEA201511173677), Nov 17, 2015: FLOOR PANEL. DELAMINATED. MCD FLOOR PANEL 232 BH HAS DELAMINATED ON RT FWD EDGE CORNER. FABRICATED NEW PANEL ON T15 1172035 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511173676](https://openairdocs.org/sdr/FDEA201511173676), Nov 17, 2015: FLOOR PANEL. CRACKED. MCD FLOOR PANEL 232 QG HAS CRACK ON MID AFT AREA. FABRICATED NEW PANEL ON T15 1172120 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511173674](https://openairdocs.org/sdr/FDEA201511173674), Nov 17, 2015: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 231 BH DAMAGED. FABRICATED NEW PANEL ON T15 1172143 IAW DWG SRZ 25-005 REV L CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511173673](https://openairdocs.org/sdr/FDEA201511173673), Nov 17, 2015: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 231 UG DAMAGED. FABRICATED NEW PANEL ON T15 1172121 IAW DWG SRZ 25-005 REV L CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511173672](https://openairdocs.org/sdr/FDEA201511173672), Nov 17, 2015: FLOOR PANEL. CRACKED. MAIN CABIN DECK FLOOR PANEL 241 KJ HAS CRACKED. FABRICATED NEW PANEL ON T15 1172744 IAW DWG SRZ 25-005 REV L CLASSIFIED AS MAJOR CAT A REPAIR.

All 96: https://openairdocs.org/aircraft/N689FE/reports.md

## STCs that may be installed (OpenAirDocs) (132, 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 A300 F4-605R)

- [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 ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [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 ST02487LA](https://openairdocs.org/stc/ST02487LA): Installation of main deck cargo loading system. Ancra International 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 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 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 ST01644LA](https://openairdocs.org/stc/ST01644LA): Installation of Ancra cargo system. Ancra International LLC
- [STC ST02488LA](https://openairdocs.org/stc/ST02488LA): 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 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 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 ST04240AT](https://openairdocs.org/stc/ST04240AT): Installs a standalone Astronics AES 110V AC 60 Hz and 5V DC power system. FedEx Express

All 132: https://openairdocs.org/aircraft/N689FE/stcs.md

## Related

- Other Airbus A300 F4-605R aircraft: https://openairdocs.org/model/airbus-a300-f4-605r/aircraft.md
- The GE CF6-80C2A5F engine: https://openairdocs.org/engine/ge-cf6-80c2a5f.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.