# N658FE: 1995 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: 752 - Year built: 1995 - Type: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: July 24, 1995 - Certificate issued: July 31, 2019 - Expires: July 31, 2029 - Mode S code: A8AAF4 - 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=658FE - Page: https://openairdocs.org/aircraft/N658FE 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/N658FE/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 N658FE. ## FAA accident and incident reports None matched to N658FE. ## Service difficulty reports (352, 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 FDEA202607220984](https://openairdocs.org/sdr/FDEA202607220984), Jul 22, 2026: POWER SUPPLY. INOPERATIVE. RIGHT FORWARD DOOR SLIDE WILL NOT ARM. RELEASED FOR SERVICE PER MEL. ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE V - [SDR FDEA202603240368](https://openairdocs.org/sdr/FDEA202603240368), Mar 24, 2026: SDAC. INOPERATIVE. R1 DOOR WILL NOT ARM. AMM 52-10-00-00-02, DURING T/S FOUND THAT ARMING LEVER MOVED TO ARMED POSITION BUT ECAM INDICATION DID NOT SHOW (SLIDE) INDICATION. AMM: 3 - [SDR FDEA202603210362](https://openairdocs.org/sdr/FDEA202603210362), Mar 21, 2026: BATTERY. FAILED. BOTH L1 & R1 DOOR SLIDE WARNING LIGHTS INOP. BUZZERS WORK NORMALLY. MEL 20MAR26 19:20 PDX RELEASED FOR SERVICE PER MEL : 52-73-01-01 CATEGORY : C EXPIRATION : 3 - [SDR FDEA202603060322](https://openairdocs.org/sdr/FDEA202603060322), Mar 6, 2026: POWER SUPPLY. FAULTED. CHECK FOUND BOTH L & R FWD DOOR ESCAPE SLIDE WARNING LIGHT INOP, BUZZER WORK NORMAL. RELEASED FOR SERVICE PER MEL 52-73-01-01, CATEGORY C. REPLACED THE AUTONOMO - [SDR FDEA202603060321](https://openairdocs.org/sdr/FDEA202603060321), Mar 6, 2026: POWER SUPPLY. FAILED. R1 SLIDE INDICATION ON ECAM WILL NOT DISPLAY WHEN SLIDE IS ARMED. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. MEL: - [SDR FDEA202603040312](https://openairdocs.org/sdr/FDEA202603040312), Mar 4, 2026: POWER SUPPLY. INOPERATIVE. CHECK FOUND BOTH L & R FWD DOOR ESCAPE SLIDE WARNING LIGHT INOP, BUZZER WORK NORMAL. RELEASED FOR SERVICE IAW MEL 52-73-01-01, CATEGORY C. . L1 & R1 CREW ENTRY - [SDR FDEA202603030309](https://openairdocs.org/sdr/FDEA202603030309), Mar 3, 2026: SLIDE. OUT OF POSITION. FINISHED CHECK THAT L1 ESCAPE SLIDE PRESSURE INDICATOR IN GREEN BAND. THE ESCAPE SLIDE BUT THE NEW L1 ESCAPE SLIDE PRESSURE GAUGE NOT ALIGNED WITH VIEW PORT. ME - [SDR FDEA202602070142](https://openairdocs.org/sdr/FDEA202602070142), Feb 7, 2026: SKIN. DAMAGED. EXISTING REPAIR ON FUSELAGE SKIN AT FRS 19 - 20A, S38R - 42R REQUIRES EVALUATION FOR CONFORMITY. EVALUATED & FOUND NOT IN CONFORMITY WITH SRM 53-13-13 FIG.201. - [SDR FDEA202602050135](https://openairdocs.org/sdr/FDEA202602050135), Feb 5, 2026: FRAME. UNKNOWN. EXISTING REPAIR ON FUSELAGE FRAME AT FR28 BETWEEN STGR8LH AND STGR12LH REQUIRES EVALUATION FOR CONFORMITY. EVALUATED AND NO RECORD FOUND. REMOVED THE EXISTING R - [SDR FDEA202602100160](https://openairdocs.org/sdr/FDEA202602100160), Feb 4, 2026: CREASE BEAM. CORRODED. EXISTING REPAIR ON MDCC CROSSBEAM AT FR55 BETWEEN Y1456 AND Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM AT FR55 BETWEEN Y1456 - [SDR FDEA202602040132](https://openairdocs.org/sdr/FDEA202602040132), Feb 4, 2026: REPAIR. NO DISCREPANCY. EXISTING REPAIR ON MDCC CROSSBEAM AT FR55 BETWEEN Y1456 AND Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM AT FR55 BETWEEN Y1456 - [SDR FDEA202602010112](https://openairdocs.org/sdr/FDEA202602010112), Feb 1, 2026: FRAME. DAMAGED. EXISTING REPAIR ON FUSELAGE FRAME AT FR20A STGR39R-STGR42R REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE FRAME AT FR20A STGR39R-STGR42R WAS - [SDR FDEA202601290157](https://openairdocs.org/sdr/FDEA202601290157), Jan 29, 2026: FRAME. CRACKED. CENTER BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "H" HOLE FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T038 - [SDR FDEA202601280097](https://openairdocs.org/sdr/FDEA202601280097), Jan 28, 2026: CROSSBEAM. MISREPAIRED. EXISTING REPAIR ON MDCC CROSSBEAM LOWER FLANGE AT FR60 BETWEEN -Y1456 AND -Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM LOWER - [SDR FDEA202601210089](https://openairdocs.org/sdr/FDEA202601210089), Jan 21, 2026: REPAIR. OUT OF LIMITS. EXISTING REPAIR ON FUSELAGE SKIN AT FR22-FR23 STGR51L-STGR53L REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE SKIN AT FR22 - FR23 STGR51L-STG - [SDR FDEA202601160061](https://openairdocs.org/sdr/FDEA202601160061), Jan 16, 2026: FASTENER. MISSING. EXISTING REPAIR ON MDCC CROSSBEAM AT FR65 BETWEEN Y953 AND Y1456 REQUIRES EVALUATION FOR CONFORMITY. EVALUATED AND FOUND NOT IN CONFORMITY WITH EA 6-5310-160172 - [SDR FDEA202601160060](https://openairdocs.org/sdr/FDEA202601160060), Jan 16, 2026: SEAT TRACK. DAMAGED. EXISTING REPAIR ON MDCC SEAT TRACK AT Y0 BETWEEN FR71 AND FR73 REQUIRES EVALUATION FOR CONFORMITY. EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM 53-1 - [SDR FDEA202601160050](https://openairdocs.org/sdr/FDEA202601160050), Jan 16, 2026: SEAT TRACK. NO DISCREPANCY. EXISTING REPAIR ON MDCC SEAT TRACK AT -Y1456 BETWEEN FR26 AND FR31 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MDCC SEAT TRACK AT -Y1456 BETWEEN - [SDR FDEA202601160049](https://openairdocs.org/sdr/FDEA202601160049), Jan 16, 2026: SEAT TRACK. NO DISCREPANCY. EXISTING REPAIR ON MDCC SEAT TRACK AT Y450 BETWEEN FR32 AND FR34 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MDCC SEAT TRACK AT Y450 BETWEEN FR32 - [SDR FDEA202601150066](https://openairdocs.org/sdr/FDEA202601150066), Jan 15, 2026: FITTING. CRACKED. NDT INSPECTION, MAIN DECK DOOR ACTUATOR BEARING FITTINGS 3EA HOLES FOUND CRACK SIGNAL AT FRAME 23 AND 24. COMPLIED WITH EA 6-5230-T0386195 REPAIRED THE CRACKED - [SDR FDEA202601150045](https://openairdocs.org/sdr/FDEA202601150045), Jan 15, 2026: REPAIR. NO DISCREPANCY. EXISTING REPAIR ON FWD CARGO DOOR INNER SKIN FR 23A-24A BETWEEN BEAM 1 AND BEAM 2 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON FWD CARGO DOOR INNE - [SDR FDEA202601140034](https://openairdocs.org/sdr/FDEA202601140034), Jan 14, 2026: REPAIR. NO DISCREPANCY. EXISTING REPAIR ON MDCC FLOOR SUPPORT AT -Y1959 BETWEEN FR12A AND FR18 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MDCC FLOOR SUPPORT AT -Y1959 B - [SDR FDEA202601140033](https://openairdocs.org/sdr/FDEA202601140033), Jan 14, 2026: REPAIR. NO DISCREPANCY. EXISTING REPAIR ON MDCC FLOOR SUPPORT AT Y0 BETWEEN FR11 AND FR19 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MDCC FLOOR SUPPORT AT Y0 BETWEEN FR - [SDR FDEA202601140032](https://openairdocs.org/sdr/FDEA202601140032), Jan 14, 2026: REPAIR. NO DISCREPANCY. EXISITING REPAIR ON MDCC FLOOR SUPPORT AT Y450 BETWEEN FR11 AND FR15A REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MDCC FLOOR SUPPORT AT Y450 BETW - [SDR FDEA202601130031](https://openairdocs.org/sdr/FDEA202601130031), Jan 13, 2026: THRUST BRACKET. DAMAGED. EXISTING REPAIR ON FUSELAGE MAIN DECK CARGO COMPARTMENT FR 26 - FR 27 THRUST BRACKET WEB BETWEEN -Y450 AND -Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING - [SDR FDEA202601120290](https://openairdocs.org/sdr/FDEA202601120290), Jan 12, 2026: FITTING. DAMAGED. DOORS - CARGO DOOR, HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24. COMPL - [SDR FDEA202601120064](https://openairdocs.org/sdr/FDEA202601120064), Jan 12, 2026: PANEL. CRACKED. NDT INSP, LT CENTER BOX REAR SPAR FR47 FWD FITTING RIB 1 HOLE G FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0386165 REPAIRED THE CRACKED HOLE "G" AT LH CENTE - [SDR FDEA202601120048](https://openairdocs.org/sdr/FDEA202601120048), Jan 12, 2026: FRAME. CRACKED. NDT INSP - RT CENTER BOX REAR SPAR FR47 FWD FITTING RIB1 HOLE "C" FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0386164 REPAIRED THE CRACKED CENTER WING BOX REAR - [SDR FDEA202601100086](https://openairdocs.org/sdr/FDEA202601100086), Jan 10, 2026: CROSSBEAM. CORRODED. MDCC CROSSBEAM, LWR SURFACE AT FR54.2 CORRODED. COMPLIED WITH EA 6-5310-T0386271 REPAIRED THE CORRODED CROSSBEAM LOWER FLANGE AT FR54.2 BETWEEN Y1456 AND -Y1456 - [SDR FDEA202601100042](https://openairdocs.org/sdr/FDEA202601100042), Jan 10, 2026: HINGE ARM. DELAMINATED. LEFT WING SPOILER NR 3 CENTER INBD HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 55MM - 25MM, DEPTH: 0.91MM COMPLIED WITH EA 6-5750-T0386109 P1 TO REPAIR - [SDR FDEA202601100043](https://openairdocs.org/sdr/FDEA202601100043), Jan 10, 2026: HINGE ARM. DELAMINATED. RIGHT WING SPOILER NR 5 CENTER OTBD HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 90 MM-24MM, DEPTH: 1.25 MM. COMPLIED WITH EA 6-5750-T0386108 P1 TO REPAI - [SDR FDEA202601090044](https://openairdocs.org/sdr/FDEA202601090044), Jan 9, 2026: SKIN. CRACKED. FWD CARGO DOOR INNER SKIN AT FR22A, BEAM1-BEAM2 CRACKED. COMPLIED WITH EA 6-5230-T0386127 REPAIRED THE FWD CARGO DOOR FR22A BEAM1-BEAM2 CRACKED INNER SKIN. TITL - [SDR FDEA202601080041](https://openairdocs.org/sdr/FDEA202601080041), Jan 8, 2026: RIB. CRACKED. RIGHT CENTER FLAP RIB UPPER FLANGE FOUND 5EA CRACKS AT RIB 26 BETWEEN STGR2.6 AND REAR SPAR, RIB 27 BETWEEN STGR 2.7 AND REAR SPAR. RIB27 BETWEEN STGR2.7 AND RE - [SDR FDEA202601080040](https://openairdocs.org/sdr/FDEA202601080040), Jan 8, 2026: RIB. CRACKED. RIGHT CENTER FLAP RIB UPPER FLANGE FOUND CRACK AT RIB 11 BETWEEN S 2.7 AND S 2.8. COMPLIED WITH EA:6-5750-T0386104 P1 TO REPAIR RH CENTER FLAP RIB CRACKED UPPER - [SDR FDEA202601060047](https://openairdocs.org/sdr/FDEA202601060047), Jan 6, 2026: CROSSBEAM. CRACKED. MDCC CROSSBEAM AT FR64, BETWEEN -Y1456 AND -Y1959 CRACKED. REPAIRED THE MDCC CRACKED CROSSBEAM ON MDCC AT FR64 BETWEEN -Y1456 AND -Y1959 PER A300-600F SRM 53-10 - [SDR FDEA202505230795](https://openairdocs.org/sdr/FDEA202505230795), May 23, 2025: SLIDE. FAILED. AFTER CLOSING AND ARMING DOORS FOR DEPARTURE, F/O NOTICED THAT THE RAMP AGENT LEFT HER SCANNER. IN AN EFFORT TO RETURN IT TO HER, HE INADVERTENTLY OPENED THE DO - [SDR FDEA202406110790](https://openairdocs.org/sdr/FDEA202406110790), Jun 11, 2024: BOLT. MISSING. LEFT PASSENGER DOOR SLIDE MISSING SLIDE ATTACH BOLT REF IPC 25-61-21-01 ITEM 30-40. GMM: 7-1-100 AMM: 25-61-21-04, INSTALLED SLIDE ATTACHING SCREW PART NUMBER N - [SDR FDEA202403290409](https://openairdocs.org/sdr/FDEA202403290409), Mar 29, 2024: BOTTLE. LOW PRESSURE. MDIS 658 52-10 6061 29MAR24 12:02 LRD FACT L1 DOOR ASSIST BOTTLE PRESSURE LOW FACT 29MAR24 18:22 LRD AMM: 52_10_14_03_02 SERVICED L1 EMERGENCY OPERATION CYLINDE - [SDR FDEA202311261927](https://openairdocs.org/sdr/FDEA202311261927), Nov 26, 2023: PIN. LOOSE. THERE IS A RED FLAG PROTRUDING FROM UNDER THE R1 DOOR SLIDE. 26NOV23 - REMOVED RED TAG LABELED - REMOVE BEFOREINSTALLATION - ON R1 DOOR SLIDE REF ABOVE AMM REFE - [SDR FDEA202310091735](https://openairdocs.org/sdr/FDEA202310091735), Oct 9, 2023: CROSSBEAM. CRACKED. MDCC C59, Y650 CROSS BEAM CRACKED. REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CRACKED CROSSBEAM AT FR58 BETWEEN Y1456 AND Y1959 PER A300-600F SRM5 - [SDR FDEA202310091734](https://openairdocs.org/sdr/FDEA202310091734), Oct 9, 2023: SPOILER. DELAMINATED. RH WING #5 SPOILER CENTER I/B HINGE O/B FOUND DELAMINATION. SIZE: 30MMX20MM, DEPTH: 1.80MM PERFORMED THE REPAIR ON RH WING #5 SPOILER CENTER I/B & O/B HINGE ARM - [SDR FDEA202310041699](https://openairdocs.org/sdr/FDEA202310041699), Oct 4, 2023: CROSSBEAM. CRACKED. MDCC FR30, Y650 CROSS BEAM CRACKED. REPAIRED THE MDCC CRACKED CROSSBEAM AT FR30 Y650 PER A300-600F SRM53-10-15-201 PARA.15 FIG.212 & EA:6-5310-T0376581 P1. THIS - [SDR FDEA202306280914](https://openairdocs.org/sdr/FDEA202306280914), Jun 28, 2023: POWER SUPPLY. DIRTY. R1 ENTRY DOOR NOT SHOWING ARMED ON ECAM WITH DOOR IN ARMED POSITION. RELEASED FOR SERVICE PER MEL : 52-30-04 CATEGORY : C EXPIRATION : 08JUL26 "MEL 52-30-04: EC - [SDR FDEA202207201787](https://openairdocs.org/sdr/FDEA202207201787), Jul 20, 2022: CONTROLLER. FAULTED. PDIS 658 36-10 4286 19JUL22 BOS FACT U DURING DEPARTURE PASSING 4,000 MSL IN HIGH THRUST SETTING, BLEED VALVE #1 FAULT. COMPLIED WITH ECAM WHICH TRIED RESETTING - [SDR FDEA202107091709](https://openairdocs.org/sdr/FDEA202107091709), Jul 9, 2021: SELECTOR VALVE. INOPERATIVE. GEAR WOULD NOT COME DOWN ON FINAL, ECAM DIRECTED MANUAL CRANK DOWN. WE COMPLIED WITH ECAM AND RAN THE CHECKLIST AND THE GEAR CAME DOWN WITH THE CRANK. GEAR DOOR - [SDR FDEA202104281065](https://openairdocs.org/sdr/FDEA202104281065), Apr 28, 2021: ATTACH FITTING. DAMAGED. WHILE ACCOMPLISHING STEP 9 OF E0 6-5710-7-3301 PT1 THE CUTTER INCREMENTS WERE NOT NOT FOLLOWED THEREFORE CUTTING MORE MATERIAL THAN REQUIRED ON ATTACHED FITTING - [SDR FDEA202102150358](https://openairdocs.org/sdr/FDEA202102150358), Feb 15, 2021: SKIN. DAMAGED. DURING INSTALL OF R/H WING CENTER FLAP FOUND SKIN PUNCTURED, LOWER SURFACE CENTER OF FLAP. REPAIRED DAMAGE/PUNCTURED ON LOWER SURFACE OF CENTER FLAP IAW A300 SR - [SDR FDEA202102030284](https://openairdocs.org/sdr/FDEA202102030284), Feb 3, 2021: ROLLER TRAY. CORRODED. AFT PIT ROLLER TRAY FR 56 RH (I/B OF PDU) CORRODED LWR SURFACE. DOT NO. 17-62 BLENDED ROLLER TRAY LOWER SURFACE AT FR 56 R/H SIDE IAW SRM 51-74-10. FOUND TO BE - [SDR FDEA202102010260](https://openairdocs.org/sdr/FDEA202102010260), Feb 1, 2021: CROSSBEAM. CORRODED. AFT PIT FLOOR STRUCTURE FR 56 RH END CORRODED. DOT NO. 17-59 REPAIRED FLOOR SUP. AFT PIT FR. 56 R.H. IAW A-300 SRM 53-10-15 FIG. 208, REMOVED CORROSION IAW SRM - [SDR FDEA202101300247](https://openairdocs.org/sdr/FDEA202101300247), Jan 30, 2021: FLOOR PANEL. DELAMINATED. COURIER FLOOR PANEL 221MF DELAMINATED FABRICATED COURIER FLOOR PANEL 221MF ON VTMAE TRAVELER T21/1531290 MAJOR REPAIR. REPAIR CAT A IAW DWG SRZ-25-005 REV R. All 352: https://openairdocs.org/aircraft/N658FE/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/N658FE/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 --- 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.