# N676FE: 1998 Airbus Industrie A300 F4-605R

- Status: Valid registration
- Airframe: [Airbus Industrie A300 F4-605R](https://openairdocs.org/model/airbus-industrie-a300-f4-605r) (registry code 3930327, 380 seats)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) (Airbus SAS), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 790
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: August 24, 1998
- Certificate issued: July 19, 2023
- Expires: July 31, 2030
- Mode S code: A8F284
- 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=676FE
- Page: https://openairdocs.org/aircraft/N676FE

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

## ADs that may apply (OpenAirDocs): 365 in force

### Matched by airframe (Airbus Industrie 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 CF6-80 series)

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

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

- [AD 2023-26-06](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 488: https://openairdocs.org/aircraft/N676FE/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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB LAX03IA137](https://openairdocs.org/ntsb/LAX03IA137), Apr 10, 2003: Airbus Industrie A300F4-605R (N676FE), Oakland, CA, incident, no damage. Probable cause: the failure of the 1R evacuation slide to inflate because the transport-locking pin had not been removed from the regulator during the slide's installation on the 1R door. The cause of the…

## FAA accident and incident reports (2)

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

- [Incident 20060320009319I](https://openairdocs.org/incident/20060320009319I), Mar 20, 2006: Airbus A300F4605R (N676FE), Minneapolis, MN. (-23) There was a loss of control on landing causing the aircraft to slide off the north side of runway 10L at msp. The captain was given a line check as a…
- [Incident 20030410004379I](https://openairdocs.org/incident/20030410004379I), Apr 10, 2003: Airbus A300F4605R (N676FE), Oakland, CA. (-23) Federal express flight 3859, Airbus A-300 N676FE made an unscheduled landing at Oakland international airport. At approximately 600' AGL during takeoff,…

## Service difficulty reports (178, 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 FDEA202603050313](https://openairdocs.org/sdr/FDEA202603050313), Mar 5, 2026: PANEL. DAMAGED. AT NR 2 PYLON INBD SIDE PANEL 415AL, HAD A LARGE CRACK. REMOVED AND REPLACED THE NR 2 PYLON INBD SIDE PANEL 415AL, NO FURTHER DEFECTS .
- [SDR FDEA202602190246](https://openairdocs.org/sdr/FDEA202602190246), Feb 19, 2026: BAR. BROKEN. L1 DOOR SLIDE INTERNAL LOCK BAR BROKE. PREMATURE REMOVAL/INSTALLATION OFF MPN: D31023-101 POS: L1 SRL: 0371TH ON MPN: D31023-101. AMM: 25-61-21-04 REMOVED AND R
- [SDR FDEA202510292104](https://openairdocs.org/sdr/FDEA202510292104), Oct 29, 2025: LIGHT. INOPERATIVE. L1 DOOR EMERGENCY EXIT SPOT LIGHT DOES NOT ILLUMINATE. AMM: 33-51-13-04 SERVICED L1 DOOR EMERGENCY LIGHT OPS GOOD OK FOR SVC.
- [SDR FDEA202505090732](https://openairdocs.org/sdr/FDEA202505090732), May 9, 2025: SKIN. DELAMINATED. LH WING #5 SPOILER CENTER I/B & O/B HINGE ARM UPR SKIN FOUND DELAMINATION. SIZE: (1)40MM*18MM, DEPTH: 2.40MM (2)83MM*40MM, DEPTH: 2.38MM COMPLIED WITH EA: 6-575
- [SDR FDEA202505040713](https://openairdocs.org/sdr/FDEA202505040713), May 4, 2025: DOOR. CRACKED. MAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR23 AND FR24 FOUND CRACK SIGNAL ON 3EA FASTENER HOLES COMPLIED WITH EA: 6-5230-T0383235 P1. TITLE: DOORS - CARGO D
- [SDR FDEA202504240640](https://openairdocs.org/sdr/FDEA202504240640), Apr 24, 2025: CROSSBEAM. UNKNOWN. MAIN DECK CARGO COMPARTMENT - EXISTING CROSSBEAM REPAIR FROM Y1959 TO Y2462 BETWEEN FR54.1 AND FR54.2 REQUIRES EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF 
- [SDR FDEA202504220624](https://openairdocs.org/sdr/FDEA202504220624), Apr 22, 2025: CARGO TRACK. BROKEN. MAIN DECK CARGO FR42-FR43 Y953 SEAT TRACK BROKEN REPLACED THE MAIN DECK CARGO BROKEN SEAT TRACK AT Y953 BETWEEN FR40 AND FR45 WITH A FABRICATED PART PER A300-60
- [SDR FDEA202504170609](https://openairdocs.org/sdr/FDEA202504170609), Apr 17, 2025: FLOOR SUPPORT. UNKNOWN. EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR11 - FR13A FLOOR SUPPORT AT Y232 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CARGO COM
- [SDR FDEA202504170607](https://openairdocs.org/sdr/FDEA202504170607), Apr 17, 2025: FLOOR SUPPORT. CORRODED. MAIN DECK FR11-FR13A Y730 FLOOR SUPPORT CORRODED. REPLACED THE CORRODED FLOOR SUPPORT AT MAIN DECK FR11-FR13A Y730 WITH NEW PART PER A300-600F SRM51-40-21. THIS
- [SDR FDEA202504170606](https://openairdocs.org/sdr/FDEA202504170606), Apr 17, 2025: SKIN. NO DISCREPANCY. EXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB16-RIB17 BETWEEN FRONT SPAR AND S2.3 REQUIRES EVALUATION FOR CONFORMITY. EXISTING REPAIR ON RH WING CENTER 
- [SDR FDEA202504170605](https://openairdocs.org/sdr/FDEA202504170605), Apr 17, 2025: SKIN. DAMAGED. EXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB15-RIB18 BETWEEN S2.2 AND REAR SPAR REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON RH WING CENT
- [SDR FDEA202504170604](https://openairdocs.org/sdr/FDEA202504170604), Apr 17, 2025: SKIN. NO DISCREPANCY. EXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB10-RIB12 BETWEEN S2.2 AND REAR SPAR REQUIRES EVALUATION FOR CONFORMITY. EXISTING REPAIR ON RH WING CENTER F
- [SDR FDEA202504160599](https://openairdocs.org/sdr/FDEA202504160599), Apr 16, 2025: BEARING. NOT REPORTED. COMPLY WITH EO 6-5230-E0378588 B P5 FOR MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS REPLACEMENT. COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGO 
- [SDR FDEA202504160598](https://openairdocs.org/sdr/FDEA202504160598), Apr 16, 2025: FRAME. CRACKED. CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "I" HOLE FOUND CRACK SIGNAL COMPLIED WITH EO 6-5710-
- [SDR FDEA202504160597](https://openairdocs.org/sdr/FDEA202504160597), Apr 16, 2025: FITTING. CRACKED. CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "I" HOLE FOUND CRACK SIGNAL COMPLIED WITH EO 6-5710-
- [SDR FDEA202504160596](https://openairdocs.org/sdr/FDEA202504160596), Apr 16, 2025: HINGE ARM. DELAMINATED. LH WING #3 SPOILER CENTER I/B & O/B HINGE ARM UPR SKIN FOUND DELAMINATION. SIZE: (1)14MM*7MM, DEPTH: 1.46MM (2)35MM*10MM, DEPTH: 1.56MM COMPLIED WITH EA: 6-5750
- [SDR FDEA202504160595](https://openairdocs.org/sdr/FDEA202504160595), Apr 16, 2025: HINGE ARM. DELAMINATED. LH WING #3 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE FOUND 2EA LOCATIONS DELAMINATION. SIZE: (1)25MM*25MM, DEPTH: 1.94MM (2)30MM*25MM, DEPTH: 1.51MM COMPLIED
- [SDR FDEA202504160594](https://openairdocs.org/sdr/FDEA202504160594), Apr 16, 2025: SEAT TRACK. BROKEN. MAIN DECK FR33-FR34 -Y1959 SEAT TRACK BROKEN. REPAIRED THE MAIN DECK BROKEN SEAT TRACK AT -Y1959 BETWEEN FR33 AND FR34 PER A300- 600F SRM53-10-16-201 FIG.201. T
- [SDR FDEA202504150608](https://openairdocs.org/sdr/FDEA202504150608), Apr 15, 2025: SEAT TRACK. NO DISCREPANCY. EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR20 - FR21 SEAT TRACK AT Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPART
- [SDR FDEA202308201465](https://openairdocs.org/sdr/FDEA202308201465), Aug 20, 2023: TRANSMITTER. FAILED. PDIS 676 29-01 2402 19AUG23 MEM OPEN U GREEN HYD RSVR LO LEVEL ECAM MESSAGE IN CRUISE. COMPLIED WITH ECAM AND QRH PROCEDURES. DIVERTED TO MEM. GREEN HYD QUANTIT
- [SDR FDEA202308081374](https://openairdocs.org/sdr/FDEA202308081374), Aug 8, 2023: HOSE. LEAKING. YELLOW HYD SYS LO PR ECAM CLIMBING THROUGH FL260. COMPLIED WITH ECAM AND QRH. YELLOW SYSTEM RESERVOIR QUANTITY INDICATOR FLUCTUATION IN YELLOW ABOVE AND BELOW R
- [SDR FDEA202307121742](https://openairdocs.org/sdr/FDEA202307121742), Jul 12, 2023: FITTING. CORRODED. CORROSION FOUND IN THE RIB 5 FITTING. REPAIR PER AIRBUS REPAIR INSTRUCTIONS R57240425
- [SDR FDEA202301190138](https://openairdocs.org/sdr/FDEA202301190138), Jan 19, 2023: CROSSBEAM. CRACKED. MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BETWEEN Y1456 AND Y1959. REPAIRED THE CRACKED CROSSBEAM IN THE MAIN DECK CARGO COMPART
- [SDR FDEA202301190137](https://openairdocs.org/sdr/FDEA202301190137), Jan 19, 2023: CROSSBEAM. CRACKED. MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR61, BETWEEN -Y1456 AND -Y1959. REPAIRED THE CRACKED CROSSBEAM IN THE MAIN DECK CARGO COMPA
- [SDR FDEA202301190136](https://openairdocs.org/sdr/FDEA202301190136), Jan 19, 2023: CROSSBEAM. CRACKED. MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR32, BETWEEN -Y450 AND -Y953. COMPLIED WITH EA: 6-5310-T0372499 P1. MAJOR REPAIR IAW FEDEX 
- [SDR FDEA202301190135](https://openairdocs.org/sdr/FDEA202301190135), Jan 19, 2023: CROSSBEAM. CRACKED. MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR31, BETWEEN -Y450 AND -Y953. COMPLIED WITH EA: 6-5310-T0372501 P1. MAJOR REPAIR IAW GMM6-2
- [SDR FDEA202301190134](https://openairdocs.org/sdr/FDEA202301190134), Jan 19, 2023: CROSSBEAM. CRACKED. MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR28, BETWEEN -Y450 AND -Y953. COMPLIED WITH EA: 6-5310-T0372502 P1. MAJOR REPAIR IAW GMM6-2
- [SDR FDEA202301090053](https://openairdocs.org/sdr/FDEA202301090053), Jan 9, 2023: UNKNOWN. UNKNOWN. EMERGENCY DECLARED: RECEIVED GREEN HYD LOW LVL. COMPLIED WITH ECAM AND QRH DECLARED EMERGENCY AND PERFORMED LANDING GEAR GRAVITY EXTEND. 1. PER AMM 29-21-00-03 
- [SDR FDEA202301080051](https://openairdocs.org/sdr/FDEA202301080051), Jan 8, 2023: TRANSMISSION. INOPERATIVE. EMERGENCY DECLARED RECEIVED GREEN HYD LOW LVL. COMPLIED WITH ECAM AND QRH DECLARED EMERGENCY AND PERFORMED LANDING GEAR GRAVITY EXTEND. PRESS'D THE GRN HYD SYS 
- [SDR FDEA202212152923](https://openairdocs.org/sdr/FDEA202212152923), Dec 15, 2022: HYDRAULIC SYSTEM. MALFUNCTIONED. AT BEGINNING OF DESCENT, RECEIVED ECAM GREEN HYD LOW LEVEL. INDICATION WAS ON THE RED. AFTER MANUALLY LOWERING MLG, GREEN QTY RETURNED TO NORMAL. EMERGENCY DECL
- [SDR FDEA202209102718](https://openairdocs.org/sdr/FDEA202209102718), Sep 10, 2022: SKIN. NOT REPORTED. CENTER SKIN SECTION NEEDS REMOVED FROM FR78.5 TO FR72 STRINGER 52L TO 52R REPLACED CENTER SKIN SECTION FROM FR72 TO FR80 STRINGER 51L TO 51R IAW E.A. 6-5330- T0
- [SDR FDEA202209092732](https://openairdocs.org/sdr/FDEA202209092732), Sep 9, 2022: FRAME. DENTED. FR77 CENTER FRAME AT STRINGER 47R AND 48R IS DEFORMED 0000433443 : PATE, ROBERT L - 05-NOV-2022 06:14 REMOVED AND REPLACED LEFT-HAND STUB FRAME, RIGHT-HAND STUB
- [SDR FDEA202209042699](https://openairdocs.org/sdr/FDEA202209042699), Sep 4, 2022: SKIN. DEFORMED. SKIN DEFORMATION AT FR 77 AT STR 47R (MEASURED 0.142? TO 0.172?) REPAIRED SKIN DEFORMATION AT FR76 AND FR77 STRINGER 47R IAW EA 6-5330-T0370451 PART 2 STEPS 13 
- [SDR FDEA202209032708](https://openairdocs.org/sdr/FDEA202209032708), Sep 3, 2022: SKIN. DEFORMED. SKIN DEFORMATION AT FR 77 AT STR 47L (MEASURED 0.082? TO 0.087?) REPAIRED SKIN DEFORMATION AT FRAME 76.5 TO FR77.5 STRINGER 47L TO 51L IAW EA 6-5330- T0370451 P
- [SDR FDEA202208171990](https://openairdocs.org/sdr/FDEA202208171990), Aug 17, 2022: POWER SUPPLY. FAILED. MDIS 676 33-50 1687 17AUG22 BUR FACT U COURIER AREA EMERGERNCY LIGHTING WILL NOT TEST OR TURN ON R/I 17AUG22 19:12 BUR U REASON CODE : PREMATURE REMOVAL/INSTALL
- [SDR FDEA202110182558](https://openairdocs.org/sdr/FDEA202110182558), Oct 18, 2021: NONE. NONE. PDIS 676 73-35 0791 18OCT21 OKC OPEN U IN CRUISE FLIGHT AT FL340 ABOUT AN HOUR AFTER TAKEOFF WE GOT ECAM WARNING OF ENG #1 FUEL FILTER CLOG. WE ALSO GOT THE FUE
- [SDR FDEA202109142301](https://openairdocs.org/sdr/FDEA202109142301), Sep 14, 2021: HANDLE. FAILED. PDIS 676 32-30 0707 14SEP21 AFW OPEN U GEAR WOULD NOT RETRACT AFTER TAKEOFF (GEAR HANDLE STOPPED IN MIDDLE POSITION) - TRIED POS 1 AND 2 WITH NO DIFFERENCE. PLA
- [SDR FDEA2020072431636](https://openairdocs.org/sdr/FDEA2020072431636), Jul 23, 2020: FLOOR PANEL. CRACKED. AFT CARGO FLOOR PANEL 152PF CRACKED AND DELAMINATED.(PANEL RACK) FABRICATED NEW FLOOR PANEL 152PF ON VTMAE TRAVELER # T20/1503455 IAW FEDEX DWG SRZ-25-005R, MAJ
- [SDR FDEA2020072311613](https://openairdocs.org/sdr/FDEA2020072311613), Jul 21, 2020: FLOOR PANEL. CRACKED. FLOOR PANEL 151PF CRACKED, FABRICATED FLOOR PANEL 151PF FROM TRAVELER TD/000437 IAW DWG SRZ-25-005R, CATEGORY "A" AND MAJOR REPAIR.
- [SDR FDEA202007211609](https://openairdocs.org/sdr/FDEA202007211609), Jul 21, 2020: SKIN. CRACKED. FOUND RH CENTER FLAP CRACKED AT RIB 17 APPROX 5" AFT OF FRONT SPAR LOWER SKIN. AFTER FURTHER INVESTIGATIONI OF X-RAY FILM AND BORESCOPE OF THE SUSPECTED AREA AR
- [SDR FDEA202007171575](https://openairdocs.org/sdr/FDEA202007171575), Jul 17, 2020: SKIN. DELAMINATED. LEFT ELEVATOR HAD WATER ENTRAPMENT 30 7/8 INCHES FROM THE OTBD EDGE OF ER13, APPROXIMATELY 21 INCHES FROM THE TRALING EDGE AND MEASURES 1 X 1 INCH IN SIZE. REPA
- [SDR FDEA202007171574](https://openairdocs.org/sdr/FDEA202007171574), Jul 17, 2020: SKIN. DELAMINATED. LEFT ELEVATOR HAD WATER ENTRAPMENT 12 INCHES FROM THE OUTBD EDGE OF ER2, APPROXIMATELY 21 1/4 INCHES FROM THE TRALING EDGE AND MEASURES 1 1/4 X 1 3/8 INCHES IN 
- [SDR FDEA202007171573](https://openairdocs.org/sdr/FDEA202007171573), Jul 17, 2020: SKIN. DELAMINATED. LEFT ELEVATOR HAD WATER ENTRAPMENT 19 1/2 INCHES FROM THE OUTBD EDGE OF ER2, APPROXIMATELY 21 3/8 INCHES FROM THE TRAILING EDGE AND MEASURES 5/8 X 3/4 INCH IN S
- [SDR FDEA202007171572](https://openairdocs.org/sdr/FDEA202007171572), Jul 17, 2020: SKIN. DELAMINATED. RIGHT ELEVATOR HAD WATER ENTRAPMENT ON THE LT EDGE OF ER13 APPROIMATELY 12 3/4 INCHES FROM THE TRAILING EDGE AND MEASURES 1 5/8 INCHES X 2 INCHES IN SIZE. REPAI
- [SDR FDEA2020072361546](https://openairdocs.org/sdr/FDEA2020072361546), Jul 16, 2020: FLOOR PANEL. DELAMINATED. BULK CARGO FLOOR PANEL 161GF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R. CAT A MAJOR REPAIR.
- [SDR FDEA2020071761552](https://openairdocs.org/sdr/FDEA2020071761552), Jul 16, 2020: SKIN. CRACKED. FOUND A CRACK ON THE RT CENTER FLAP AT RIB 18, APPROX 5 INCHES FWD OF REAR SPAR ON UPPER SKIN. CUT THE SKIN ON LOWER SURFACE FOR ACCESS AND REPAIRED THE CRACK I
- [SDR FDEA2020071761551](https://openairdocs.org/sdr/FDEA2020071761551), Jul 16, 2020: SKIN. CRACKED. FOUND A CRACK ON THE RT CENTER FLAP, AT RIB 16 APPROX 4.8 INCHES FWD OF REAR SPAR UPPER SKIN. CUT THE SKIN ON LOWER SURFACE FOR ACCESS AND REPAIRED THE CRACK IA
- [SDR FDEA2020071761550](https://openairdocs.org/sdr/FDEA2020071761550), Jul 16, 2020: SKIN. CRACKED. FOUND A CRACK ON THE RT CENTER FLAP AT RIB 12, APPROX 5.1 INCHES FWD OF REAR SPAR, ON UPPER SKIN. ACCESSED AND REPAIRED THE DAMAGE IAW SRM 57-50-00, FIG 201. IN
- [SDR FDEA2020071761549](https://openairdocs.org/sdr/FDEA2020071761549), Jul 16, 2020: SKIN. CRACKED. FOUND A CRACK ON THE RT CENTER FLAP AT RIB 11, LOCATED APPROX 5 INCHES FWD OF REAR SPAR IN THE UPPER SKIN. ACCESSED AND REPAIRED THE DAMAGE IAW SRM 57-50-00, FI
- [SDR FDEA2020071761548](https://openairdocs.org/sdr/FDEA2020071761548), Jul 16, 2020: FLOOR PANEL. DELAMINATED. BULK CARGO FLOOR PANEL 161AF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R. CATAGOY -A- MAJOR REPAIR.

All 178: https://openairdocs.org/aircraft/N676FE/reports.md

## STCs that may be installed (OpenAirDocs) (133, 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 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 133: https://openairdocs.org/aircraft/N676FE/stcs.md

## Related

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

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