# N664FE: 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: 768 - Year built: 1995 - Type: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: April 10, 1996 - Certificate issued: September 28, 2020 - Expires: September 30, 2027 - Mode S code: A8C397 - 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=664FE - Page: https://openairdocs.org/aircraft/N664FE 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/N664FE/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 N664FE. ## FAA accident and incident reports None matched to N664FE. ## Service difficulty reports (307, 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 FDEA202602040125](https://openairdocs.org/sdr/FDEA202602040125), Feb 4, 2026: CONTROLLER. FAULTED. AT FLIGHT LEVEL 370 GOT AN ECAM DUE TO HIGH CABIN PRESSURE, SHORTLY AFTER THAT THE NR 2 PRESSURE REGULATOR FAULTED, DONED OXYGEN MASKS STARTED A DECENT AND RAN - [SDR FDEA202512092225](https://openairdocs.org/sdr/FDEA202512092225), Dec 9, 2025: BATTERY PACK. NO TEST. COURIER COMPARTMENT EXIT DOORS EMERGENCY LIGHTS NOT TESTING. RELEASED FOR SERVICE PER MEL 33-51-05-01. COURIER COMPARTMENT INTERIOR EMERGENCY LIGHTS, DOORS EXIT - [SDR FDEA202502260297](https://openairdocs.org/sdr/FDEA202502260297), Feb 26, 2025: SPCC. FAILED. FLAPS WOULD NOT RETRACT FROM INITIAL 15/15 POSITION USED ON TAKEOFF. CYCLED FLAP HANDLE AND FLAPS WOULD NOT MOVE - POSSIBLE FLAP OVER SPEED DURING CYCLE OF 1-2 - [SDR FDEA202412111793](https://openairdocs.org/sdr/FDEA202412111793), Dec 11, 2024: FITTING. NOT REPORTED. REPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 24 PER EO NO:E6- 5230-E0378588 A P5 REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRA - [SDR FDEA202412111792](https://openairdocs.org/sdr/FDEA202412111792), Dec 11, 2024: FITTING. NOT REPORTED. REPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23 PER EO NO:E6- 5230-E0378588 A P5 REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRA - [SDR FDEA202411201704](https://openairdocs.org/sdr/FDEA202411201704), Nov 20, 2024: SKIN. DAMAGED. 1EA WATER TRAPPED AREA (60MM*65MM) WAS FOUND AT L/H ELEVATOR TOP SKIN PANEL, ER2 210MM, 730MM FROM T/E. REPAIRED THE DAMAGE AREA WITH CORE AND PLIES AT L/H ELEV - [SDR FDEA202411201703](https://openairdocs.org/sdr/FDEA202411201703), Nov 20, 2024: SKIN. CRACKED. 1EA CRACK (5MM) WAS FOUND AT R/H WING CENTER FLAP RIB27 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RIB27 - [SDR FDEA202411201702](https://openairdocs.org/sdr/FDEA202411201702), Nov 20, 2024: SKIN. CRACKED. 1EA CRACK (25MM) WAS FOUND AT R/H WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RIB2 - [SDR FDEA202411201701](https://openairdocs.org/sdr/FDEA202411201701), Nov 20, 2024: SKIN. CRACKED. 1EA CRACK (25MM) WAS FOUND AT R/H WING CENTER FLAP RIB18 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RIB1 - [SDR FDEA202411201700](https://openairdocs.org/sdr/FDEA202411201700), Nov 20, 2024: SKIN. CRACKED. 1EA CRACK (25MM) WAS FOUND AT R/H WING CENTER FLAP RIB12 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RIB1 - [SDR FDEA202411201699](https://openairdocs.org/sdr/FDEA202411201699), Nov 20, 2024: SKIN. CRACKED. 2EA CRACKS (20MM) & (20MM) WERE FOUND AT R/H WING CENTER FLAP RIB11 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR AN - [SDR FDEA202411191684](https://openairdocs.org/sdr/FDEA202411191684), Nov 19, 2024: CROSSBEAM. CRACKED. FLOOR STRUCTURE CROSS BEAM FOUND CRACK AT FR 23, Y-450 9.5" CUT OUT THE DAMAGED AREA AND REWORKED THE REPAIR AREA. THEN INSTALLED REPAIR ANGLE AND FILLER WITH F - [SDR FDEA202411091755](https://openairdocs.org/sdr/FDEA202411091755), Nov 9, 2024: CROSSBEAM. CRACKED. UNDER M/D FLOOR PNL FOUND A CROSSBEAM CRACK AT FR54.1, Y953~Y1456. FABRICATED A CROSSBEAM AND INSTALLED. LOCATE AT MAIN DECK FLOOR PANEL FR54.1, Y953 ~ Y1456.I. - [SDR FDEA202411091697](https://openairdocs.org/sdr/FDEA202411091697), Nov 9, 2024: CROSSBEAM. CRACKED. UNDER M/D FLOOR PNL FOUND A CROSSBEAM CRACK AT FR54.1, Y953~Y1456. FABRICATED A CROSSBEAM AND INSTALLED. LOCATE AT MAIN DECK FLOOR PANEL FR54.1 Y953 ~ Y1456. I. - [SDR FDEA202411081743](https://openairdocs.org/sdr/FDEA202411081743), Nov 8, 2024: RIB. DAMAGED. RH WING #7 SPOILER O/B JACK RIB TO BEAM LOWER BORE WAS FOUND IRREGULAR ALUMINIUM REPAIN BUSHING ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #7 SPOILER OUTBD JAC - [SDR FDEA202411081740](https://openairdocs.org/sdr/FDEA202411081740), Nov 8, 2024: RIB. DAMAGED. RH WING #6 SPOILER O/B JACK RIB TO BEAM UPPER & LOWER BORES WAS FOUND IRREGULAR ALUMINIUM REPAIN BUSHING ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #6 SPOILER - [SDR FDEA202411081735](https://openairdocs.org/sdr/FDEA202411081735), Nov 8, 2024: RIB. DAMAGED. RH WING #6 SPOILER I/B JACK RIB TO BEAM LOWER BORE WAS FOUND IRREGULAR ALUMINIUM REPAIR BUSHING ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #6 SPOILER INBD JACK - [SDR FDEA202411081734](https://openairdocs.org/sdr/FDEA202411081734), Nov 8, 2024: RIB. CORRODED. RH SPOILER #6 INBD JACK RIB UPPER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #6 SPOILER INBD JACK RIB UPPER BORE. I.A.W FEDEX EA NO:T6-5740-T0381 - [SDR FDEA202411051742](https://openairdocs.org/sdr/FDEA202411051742), Nov 5, 2024: RIB. CORRODED. RH SPOILER #7 OUTBOARD JACK RIB UPPER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #7 SPOILER OUTBD JACK RIB UPPER BORE. I.A.W FEDEX EA NO:T6-5740- - [SDR FDEA202411051741](https://openairdocs.org/sdr/FDEA202411051741), Nov 5, 2024: RIB. CORRODED. N00595 LH WING #4 SPOILER O/B JACK RIB TO BEAM UPPER BORE GOT CORROSION ACCOMPLISHED THE REINFORCEMENT REPAIR AT LH #4 SPOILER OUTBD JACK RIB UPPER BORE. I.A.W - [SDR FDEA202411051736](https://openairdocs.org/sdr/FDEA202411051736), Nov 5, 2024: RIB. CORRODED. RH SPOILER #6 INBD JACK RIB UPPER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #6 SPOILER INBD JACK RIB UPPER BORE. I.A.W FEDEX EA NO:T6-5740-T0381 - [SDR FDEA202411051733](https://openairdocs.org/sdr/FDEA202411051733), Nov 5, 2024: RIB. CORRODED. RH SPOILER #5 OUTBOARD JACK RIB LOWER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #5 SPOILER OUTBD JACK RIB LOWER BORE. I.A.W FEDEX EA NO:T6-5740- - [SDR FDEA202411051732](https://openairdocs.org/sdr/FDEA202411051732), Nov 5, 2024: RIB. CORRODED. RH SPOILER #4 INBD JACK RIB UPPER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #4 SPOILER INBD JACK RIB UPPER BORE. I.A.W FEDEX EA NO:T6-5740-T0381 - [SDR FDEA202410311682](https://openairdocs.org/sdr/FDEA202410311682), Oct 31, 2024: SEAT TRACK. CORRODED. MAIN DECK FLOOR STRUCTURE SEAT TRACK FOUND CORROSION NEAR FR15A, Y450 CUT THE FLOOR STRUCTURE AND FABRICATED THE REPAIR ANGLE AND FLOOR SUPPORT. INSTALLED REPAI - [SDR FDEA202410291681](https://openairdocs.org/sdr/FDEA202410291681), Oct 29, 2024: CROSSBEAM. CORRODED. BULK CARGO COMPT REPAIR FLOOR BEAM UPPER SURFACE CORRODED AT FR66,-Y1117 POSITION. REPLACED CORRODED BEAM WITH NEW FASTENERS ON BULK CARGO COMPT AT FR66, -Y1117 - [SDR FDEA202410291650](https://openairdocs.org/sdr/FDEA202410291650), Oct 29, 2024: REPAIR. NONE. AIRCRAFT REPAIR ASSESSMENT : EXISTING FLUSH DOUBLER REPAIR FOUND ON LH I/B FLAP NOSE SKIN BTW RIB 12~14 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, - [SDR FDEA202410291635](https://openairdocs.org/sdr/FDEA202410291635), Oct 29, 2024: SKIN. NONE. AIRCRAFT REPAIR ASSESSMENT : EXISTING FLUSH DOUBLER REPAIR FOUND ON RH I/B FLAP NOSE SKIN BTW RIB 20D~24B COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT - [SDR FDEA202410281790](https://openairdocs.org/sdr/FDEA202410281790), Oct 28, 2024: FITTING. DAMAGED. SEQ0944, E6-5230-E0378588P5 DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND - [SDR FDEA202410281789](https://openairdocs.org/sdr/FDEA202410281789), Oct 28, 2024: FITTING. DAMAGED. CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 PERFORMED NEW BEARING FITTING IN - [SDR FDEA202410281729](https://openairdocs.org/sdr/FDEA202410281729), Oct 28, 2024: SKIN. DAMAGED. 1EA WATER TRAPPED AREA (90MM*340MM) WAS FOUND AT R/H ELEVATOR BOTTOM SKIN PANEL T/E AREA, BETWEEN FASTENER NO.10 TO NO.12. *COUNTING T/E FASTENER FROM I/B TO O/ - [SDR FDEA202410281728](https://openairdocs.org/sdr/FDEA202410281728), Oct 28, 2024: SKIN. DAMAGED. 2EA WATER TRAPPED AREAS (470MM*100MM, 50MM*80MM) WERE FOUND AT R/H ELEVATOR TOP SKIN PANEL T/E AREA, BETWEEN FASTENER NO.9 TO NO.11 *COUNTING T/E FASTENER FROM - [SDR FDEA202410271618](https://openairdocs.org/sdr/FDEA202410271618), Oct 27, 2024: PROFILE. CRACKED. MAIN DECK FLOOR STRUCTURE FOUND 1EA PROFILE-Z CRACK NEAR FR82, Y1450 REPLACED CRACK PROFILE-Z WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51- 40- - [SDR FDEA202410271617](https://openairdocs.org/sdr/FDEA202410271617), Oct 27, 2024: PROFILE. CRACKED. MAIN DECK FLOOR STRUCTURE FOUND 1 EA PROFILE-Z CRACK NEAR FR82, Y-1450 REPLACED CRACK PROFILE-Z WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001 PAGE.2 AND 51- 40 - [SDR FDEA202410261760](https://openairdocs.org/sdr/FDEA202410261760), Oct 26, 2024: SHEAR PANEL. CRACKED. WALL (SHEAR) CRACK AT FWD CARGO COMPT, POSITION FR38, -Y1410, -Z2090 SIDE. REPLACED CRACK WALL WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001, PAGE2 AND 51-40-2 - [SDR FDEA202410251616](https://openairdocs.org/sdr/FDEA202410251616), Oct 25, 2024: SHEAR PLATE. CRACKED. MAIN DECK FLOOR STRUCTURE 1 EA SHEAR PLATE CRACK NEAR FR79 PLUS 3", Y1600 REPLACED CRACK SHEAR PLATE WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND - [SDR FDEA202410251615](https://openairdocs.org/sdr/FDEA202410251615), Oct 25, 2024: SHEAR PLATE. CRACKED. MAIN DECK FLOOR STRUCTURE 1EA SHEAR PLATE CRACK NEAR FR79 PLUS 7", Y-1600 REPLACED CRACK SHEAR PLATE WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND - [SDR FDEA202410231632](https://openairdocs.org/sdr/FDEA202410231632), Oct 23, 2024: ANGLE. BENT. AFT CGO COMPT CEILING PLATE DEFORM NEAR LIFT ACTUATOR FWD SIDE AREA. REPLACED THE DAMAGE PLATE WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001, PAGE.2. LOCATION - [SDR FDEA202410221589](https://openairdocs.org/sdr/FDEA202410221589), Oct 22, 2024: FLOOR PANEL. NONE. AIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON BULK CARGO COMPARTMENT FLOOR PANEL 162DF COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, - [SDR FDEA202410211593](https://openairdocs.org/sdr/FDEA202410211593), Oct 21, 2024: FLOORBEAM. CRACKED. CABIN FLOOR STRUCTURE CROSSBEAM ANGLE FITTING CRACK AT -Y953 ON AVIONICS COMPT. CRACKED ANGLE FITTING REPLACED NEW PART AT AVIONICS COMPT -Y953. INSTALLED WITH - [SDR HNAA2024100101050](https://openairdocs.org/sdr/HNAA2024100101050), Oct 18, 2024: SKIN. NONE. EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR26~27, S-33R~35R COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, REPAIR IDENTIFICATION & TRACKING - [SDR FDEA202410181595](https://openairdocs.org/sdr/FDEA202410181595), Oct 18, 2024: SKIN. NONE. EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR26~27, S-33R~35R COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, REPAIR IDENTIFICATION & TRACKING - [SDR FDEA202308081391](https://openairdocs.org/sdr/FDEA202308081391), Aug 8, 2023: BUSHING. CORRODED. VERTICAL STABILIZER, #4 RUDDER ATTACH FORK FITTING BUSHINGS (UPPER AND LOWER) HAVE SURFACE CORROSION. 0000490349 : THOMAS, BILLY W - 09-AUG-2023 04:43 REMOVED A - [SDR FDEA202302240341](https://openairdocs.org/sdr/FDEA202302240341), Feb 24, 2023: VALVE. FAILED. PDIS 664 21-30 5359 24FEB23 ABQ OPEN U 2 HOURS INTO WHILE USING PRESS REG #1, PRESS REG ONE FAULTED. WE TURNED SYST #1 OFF PER ECAM. THE SYSTEM SWITCHED TO REG - [SDR FDEA202205221269](https://openairdocs.org/sdr/FDEA202205221269), May 22, 2022: NONE. NONE. FR54/54.2 LH NO.4 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) BUT LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.20MM. I.A.W A300- - [SDR FDEA202205201261](https://openairdocs.org/sdr/FDEA202205201261), May 20, 2022: SEAT TRACK. CORRODED. COURIER AREA FLOOR SEAT TRACK GOT CORROSION LOCATION AT FR15A 6" AND Y953 REMOVED CORROSION SEAT TRACK AND INSTALLED NEW SEAT TRACK I.A.W A300-600F SRM 51-72-10 - [SDR FDEA202205141216](https://openairdocs.org/sdr/FDEA202205141216), May 14, 2022: NONE. DAMAGED. THE #241RG FLOOR PANEL WAS FOUND INSERT DAMAGED WITH MARK REPLACED THE DAMAGED INSERT WITH NEW INSERT I.A.W A300-600F SRM 51-72-10-001, P.2 - [SDR FDEA202205141279](https://openairdocs.org/sdr/FDEA202205141279), May 14, 2022: FLOOR PANEL. DAMAGED. THE #131SG FLOOR PANEL WAS FOUND INSERT DAMAGED REPLACED THE DAMAGED INSERTS WITH NEW INSERTS I.A.W A300-600F SRM 51-72-10-001, P.2 AND FEDEX DRAWING NO: SRZ-25 - [SDR FDEA202205141215](https://openairdocs.org/sdr/FDEA202205141215), May 14, 2022: FLOOR PANEL. DAMAGED. THE #242NH FLOOR PANEL WAS FOUND INSERT DAMAGED WITH MARK REPLACED THE DAMAGED INSERT WITH NEW INSERT I.A.W A300-600F SRM 51-72-10-001, P.2 AND FEDEX DRAWING NO - [SDR FDEA202205141213](https://openairdocs.org/sdr/FDEA202205141213), May 14, 2022: FLOOR PANEL. DAMAGED. THE #241MF FLOOR PANEL WAS FOUND EDGE DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F SRM 53-10-20-201, PARA.8A, P.201-205, FIG.201 - [SDR FDEA202205081340](https://openairdocs.org/sdr/FDEA202205081340), May 8, 2022: HINGE ARM. CRACKED. VERTICAL STABILIZER TO RUDDER NO.4 HINGE ARM FOUND LOWER PART CRACK AT LH-FWD AREA (RIB 10). REPLACED THE LOWER HINGE ARM WITH NEW ONE I.A.W EA NO:6-5530-T03684 All 307: https://openairdocs.org/aircraft/N664FE/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/N664FE/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.