# N733FD: 1993 Airbus Industrie A300 B4-605R

- Status: Valid registration
- Airframe: [Airbus Industrie A300 B4-605R](https://openairdocs.org/model/airbus-industrie-a300-b4-605r) (registry code 3930308, 380 seats)
- Engine: [GE CF6-80C2A5](https://openairdocs.org/engine/ge-cf6-80c2a5) (registry code 30104)
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) (Airbus SAS), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 715
- Year built: 1993
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 27, 2007
- Certificate issued: December 13, 2006
- Expires: February 28, 2029
- Mode S code: A9D6B1
- 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=733FD
- Page: https://openairdocs.org/aircraft/N733FD

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

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

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

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-23-02](https://openairdocs.org/ad/2025-23-02): Wings · Airbus A300 B4-603, A300 B4-605R, A300 B4-622 and 4 more. Effective Jan 13, 2026
- [AD 2025-19-09](https://openairdocs.org/ad/2025-19-09): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Dec 22, 2025
- [AD 2025-19-06](https://openairdocs.org/ad/2025-19-06): Doors · Conversion of Passenger to Freighter configuration (Airbus Deutschland STC ST00100NY or 3 others). Effective Oct 31, 2025
- [AD 2025-18-07](https://openairdocs.org/ad/2025-18-07): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Oct 23, 2025
- [AD 2025-16-05](https://openairdocs.org/ad/2025-16-05): Wings · Airbus A300 B4-2C, A300 B4-203, A300 B4-603 and 4 more. Effective Sep 22, 2025
- [AD 2025-05-01](https://openairdocs.org/ad/2025-05-01): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Apr 15, 2025
- [AD 2025-01-07](https://openairdocs.org/ad/2025-01-07): Wings · Airbus A300 B4-2C, A300 B4-103, A300 B4-203 and 9 more. Effective Mar 11, 2025
- [AD 2024-26-05](https://openairdocs.org/ad/2024-26-05): Oxygen · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 87 more. Effective Mar 11, 2025
- [AD 2024-19-15](https://openairdocs.org/ad/2024-19-15): Oxygen · Safran Aerosystems Oxygen Cylinder, Valve Assembly, Oxygen Valve and 103 more. Effective Nov 26, 2024
- [AD 2024-16-02](https://openairdocs.org/ad/2024-16-02): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Oct 21, 2024
- [AD 2024-14-07](https://openairdocs.org/ad/2024-14-07): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Sep 25, 2024
- [AD 2024-11-01](https://openairdocs.org/ad/2024-11-01): Electrical Power · Airbus A300 B4-2C, A300 B4-103, A300 B4-203 and 94 more. Effective Jul 3, 2024
- [AD 2024-08-08](https://openairdocs.org/ad/2024-08-08): Electrical Power · Airbus A300 B4-2C, A300 B4-103, A300 B4-203 and 94 more. Effective Jun 6, 2024
- [AD 2023-12-07](https://openairdocs.org/ad/2023-12-07): Time Limits/Maintenance Checks · Airbus A300 C4-605R Variant F, A300 F4-605R, A300 F4-622R and 6 more. Effective Aug 7, 2023
- [AD 2023-11-02](https://openairdocs.org/ad/2023-11-02): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Jul 11, 2023
- [AD 2016-15-01 R1](https://openairdocs.org/ad/2016-15-01-R1): Flight controls · Airbus A300 B2-1A, A300 B2-1C, A300 B2K-3C and 21 more. Effective Jun 23, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2022-21-09](https://openairdocs.org/ad/2022-21-09): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 13 more. Effective Mar 14, 2023
- [AD 2022-25-03](https://openairdocs.org/ad/2022-25-03): Fuselage · Airbus A300 B4-603, A300 B4-622, A300 B4-605R and 7 more. Effective Jan 23, 2023
- [AD 2022-25-08](https://openairdocs.org/ad/2022-25-08): Windows · Airbus A300 B2-1A, A300 B2-1C, A300 B2K-3C and 21 more. Effective Jan 20, 2023
- [AD 2022-21-02](https://openairdocs.org/ad/2022-21-02): Fuselage · Airbus A300 B2-1C, A300 B2K-3C, A300 B2-203 and 8 more. Effective Dec 14, 2022
- [AD 2022-01-08](https://openairdocs.org/ad/2022-01-08): Hydraulic power · Airbus A300 B2-1A, A300 B2K-3C, A300 B2-1C and 21 more. Effective Mar 8, 2022
- [AD 2021-11-18](https://openairdocs.org/ad/2021-11-18): Landing Gear · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Jul 16, 2021
- [AD 2020-22-11](https://openairdocs.org/ad/2020-22-11): Fuselage · Airbus A300 B4-603, A300 B4-605R, A300 B4-620 and 5 more. Effective Dec 14, 2020
- [AD 2020-02-22](https://openairdocs.org/ad/2020-02-22): Hydraulic power · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Mar 19, 2020
- [AD 2020-01-15](https://openairdocs.org/ad/2020-01-15): Fuel · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 9 more. Effective Mar 17, 2020
- [AD 2019-19-17](https://openairdocs.org/ad/2019-19-17): Wings · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 5 more. Effective Nov 14, 2019
- [AD 2019-19-07](https://openairdocs.org/ad/2019-19-07): Flight controls · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Nov 5, 2019
- [AD 2019-18-04](https://openairdocs.org/ad/2019-18-04): Stabilizers · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Oct 30, 2019
- [AD 2019-14-08](https://openairdocs.org/ad/2019-14-08): Electrical power · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Oct 2, 2019
- [AD 2019-15-08](https://openairdocs.org/ad/2019-15-08): Fuselage · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Sep 19, 2019
- [AD 2019-14-14](https://openairdocs.org/ad/2019-14-14): Stabilizers · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Sep 19, 2019
- [AD 2019-12-04](https://openairdocs.org/ad/2019-12-04): Wings · Airbus A300 B4-603, A300 B4-605R, A300 B4-620 and 5 more. Effective Aug 7, 2019
- [AD 2019-05-13](https://openairdocs.org/ad/2019-05-13): Removal of AD 2007-22-05 and AD 2013-13-13 · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Mar 21, 2019
- [AD 2018-23-12](https://openairdocs.org/ad/2018-23-12): Equipment/furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 180 more. Effective Dec 28, 2018
- [AD 2018-19-07](https://openairdocs.org/ad/2018-19-07): Landing Gear · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Nov 13, 2018
- [AD 2018-18-21](https://openairdocs.org/ad/2018-18-21): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Oct 23, 2018
- [AD 2018-18-20](https://openairdocs.org/ad/2018-18-20): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Oct 23, 2018
- [AD 2018-18-19](https://openairdocs.org/ad/2018-18-19): Time limits/maintenance checks · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Oct 23, 2018
- [AD 2018-17-16](https://openairdocs.org/ad/2018-17-16): Wings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Oct 2, 2018
- [AD 2018-17-10](https://openairdocs.org/ad/2018-17-10): Wings · Airbus A300 B4-605R, A300 B4-622R, A300 C4-605R Variant F and 2 more. Effective Sep 24, 2018
- [AD 2018-01-03](https://openairdocs.org/ad/2018-01-03): Equipment/furnishings · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Jan 18, 2018
- [AD 2017-25-09](https://openairdocs.org/ad/2017-25-09): Fuel · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Jan 18, 2018
- [AD 2017-24-09](https://openairdocs.org/ad/2017-24-09): Fuselage · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Jan 5, 2018
- [AD 2017-21-02](https://openairdocs.org/ad/2017-21-02): Fuselage · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Nov 27, 2017
- [AD 2017-20-04](https://openairdocs.org/ad/2017-20-04): Instruments · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Nov 15, 2017
- [AD 2017-19-12](https://openairdocs.org/ad/2017-19-12): Fuel · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Oct 24, 2017
- [AD 2017-18-15](https://openairdocs.org/ad/2017-18-15): Fuselage · Airbus A300 B4-603, A300 B4-605R, A300 B4-622 and 11 more. Effective Oct 19, 2017
- [AD 2017-17-05](https://openairdocs.org/ad/2017-17-05): Fuselage · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Sep 25, 2017

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

- [AD 2021-26-22](https://openairdocs.org/ad/2021-26-22): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 14, 2022
- [AD 2022-02-18](https://openairdocs.org/ad/2022-02-18): Engine Mount Section · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 3 more. Effective Feb 25, 2022
- [AD 2021-14-11](https://openairdocs.org/ad/2021-14-11): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 25 more. Effective Aug 27, 2021
- [AD 2021-03-02](https://openairdocs.org/ad/2021-03-02): Fuel Control/Turbine Engines · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Mar 31, 2021
- [AD 2016-08-10](https://openairdocs.org/ad/2016-08-10): Accessory heat shield · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Jun 1, 2016
- [AD 2014-21-01](https://openairdocs.org/ad/2014-21-01): Fuel manifold · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Nov 28, 2014
- [AD 2013-08-20](https://openairdocs.org/ad/2013-08-20): Fuel tube · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 14 more. Effective May 31, 2013
- [AD 2012-03-12](https://openairdocs.org/ad/2012-03-12): No. 3 bearing packing · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Apr 5, 2012
- [AD 2009-21-07](https://openairdocs.org/ad/2009-21-07): Thrust and thrust control · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Dec 1, 2009
- [AD 2009-07-03](https://openairdocs.org/ad/2009-07-03): Eddy current inspection (ECI) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Apr 30, 2009
- [AD 2009-04-10](https://openairdocs.org/ad/2009-04-10): Critical life-limited parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 30 more. Effective Mar 30, 2009
- [AD 2008-21-11](https://openairdocs.org/ad/2008-21-11): Low-pressure turbine (LPT) cases · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Nov 28, 2008
- [AD 2008-02-17](https://openairdocs.org/ad/2008-02-17): Thrust reverser actuation systems · General Electric CF6-50A, CF6-50C, CF6-50C1 and 16 more. Effective Feb 28, 2008
- [AD 2007-11-20](https://openairdocs.org/ad/2007-11-20): Fuel shroud retaining rings · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 22 more. Effective Jul 10, 2007
- [AD 2007-05-14](https://openairdocs.org/ad/2007-05-14): Cast titanium weld- repaired forward engine mount platforms · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 9, 2007
- [AD 2006-16-06](https://openairdocs.org/ad/2006-16-06): Certain stage 1 high- pressure turbine (HPT) rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Sep 5, 2006
- [AD 2005-17-05](https://openairdocs.org/ad/2005-17-05): High pressure compressor rotor (HPCR) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Sep 27, 2005
- [AD 2005-06-07](https://openairdocs.org/ad/2005-06-07): Directional pilot valve (DPV) assembly · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Apr 25, 2005
- [AD 2004-22-07](https://openairdocs.org/ad/2004-22-07): Stage 2 nozzle guide vanes (HPT S2 NGVs) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 1, 2004
- [AD 2003-12-08](https://openairdocs.org/ad/2003-12-08): Directional pilot valve · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Jul 23, 2003
- [AD 2003-02-07](https://openairdocs.org/ad/2003-02-07): Low pressure turbine (LPT) shrouds · General Electric CF6-50A, CF6-50C, CF6-50C1 and 30 more. Effective Mar 3, 2003
- [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08): High pressure compressor rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Jan 23, 2003
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2000-12-08](https://openairdocs.org/ad/2000-12-08): Mount Link Assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 4 more. Effective Aug 28, 2000
- [AD 2000-03-04](https://openairdocs.org/ad/2000-03-04): General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Apr 10, 2000
- [AD 99-01-01](https://openairdocs.org/ad/99-01-01): Accessory Gearbox (AGB) idler adapters · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jan 21, 1999
- [AD 98-22-06](https://openairdocs.org/ad/98-22-06): Fan Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 41 more. Effective Nov 23, 1998
- [AD 97-22-14](https://openairdocs.org/ad/97-22-14): (HPCR) 3-9 Spool · General Electric CF6-50A, CF6-50C, CF6-50C1 and 29 more. Effective Nov 17, 1997
- [AD 96-16-07](https://openairdocs.org/ad/96-16-07): Rear Right Hand Mount Link · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective Aug 28, 1996
- [AD 95-10-11](https://openairdocs.org/ad/95-10-11): Fan Reversers · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective May 31, 1995
- [AD 94-20-06](https://openairdocs.org/ad/94-20-06): Oil System · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 27, 1994
- [AD 94-06-03](https://openairdocs.org/ad/94-06-03): High Pressure Turbine Disk · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 29, 1994
- [AD 93-14-18](https://openairdocs.org/ad/93-14-18): High pressure turbine (HPT) thermal shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Oct 4, 1993
- [AD 91-15-25](https://openairdocs.org/ad/91-15-25): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Sep 6, 1991
- [AD 91-11-05](https://openairdocs.org/ad/91-11-05): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Jul 5, 1991
- [AD 91-05-21](https://openairdocs.org/ad/91-05-21): High Pressure Turbine · General Electric CF6-80C2A5, CF6-80C2B6, CF6-80C2B6F and 1 more. Effective Mar 27, 1991

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

- [AD 2023-26-06](https://openairdocs.org/ad/2023-26-06) (historical): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Mar 7, 2024
- [AD 2023-13-11](https://openairdocs.org/ad/2023-13-11) (historical): Oxygen · AVOX Systems Oxygen valve assemblies (body and gage assemblies), Oxygen cylinder and valve assemblies, A300 B2-1A and 102 more. Effective Sep 5, 2023
- [AD 2023-09-05](https://openairdocs.org/ad/2023-09-05) (historical): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Jul 11, 2023
- [AD 2023-05-13](https://openairdocs.org/ad/2023-05-13) (historical): Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective May 12, 2023
- [AD 2022-14-06](https://openairdocs.org/ad/2022-14-06) (historical): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-622 and 6 more. Effective Aug 19, 2022
- [AD 2022-13-09](https://openairdocs.org/ad/2022-13-09) (historical): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective Aug 9, 2022
- [AD 2022-11-01](https://openairdocs.org/ad/2022-11-01) (historical): Wings · Airbus A300 B2-1A, A300 B2-1C, A300 B2K-3C and 13 more. Effective Jul 5, 2022
- [AD 2021-26-20](https://openairdocs.org/ad/2021-26-20) (historical): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 6 more. Effective May 3, 2022
- [AD 2022-04-09](https://openairdocs.org/ad/2022-04-09) (historical): Oxygen System · Airbus A300 B2-1A, A300 B2-1C, A300 B2K-3C and 94 more. Effective Apr 4, 2022
- [AD 2020-23-11](https://openairdocs.org/ad/2020-23-11) (historical): Fuselage; Wings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Jan 4, 2021
- [AD 2019-21-01](https://openairdocs.org/ad/2019-21-01) (historical): Time Limits/ Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 more. Effective Nov 29, 2019
- [AD 2019-03-10](https://openairdocs.org/ad/2019-03-10) (historical): Landing Gear · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Mar 29, 2019
- [AD 2018-19-18](https://openairdocs.org/ad/2018-19-18) (historical): Wings · Airbus A300 B4-603, A300 B4-605R, A300 B4-620 and 4 more. Effective Nov 7, 2018
- [AD 2018-19-33](https://openairdocs.org/ad/2018-19-33) (historical): Time limits/maintenance checks · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 more. Effective Nov 2, 2018
- [AD 2018-01-07](https://openairdocs.org/ad/2018-01-07) (historical): Time limits/maintenance checks · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 more. Effective Feb 20, 2018
- [AD 2017-23-04](https://openairdocs.org/ad/2017-23-04) (historical): Wings · Airbus A300 B4-603, A300 B4-605R, A300 B4-620 and 4 more. Effective Dec 20, 2017
- [AD 2017-18-17](https://openairdocs.org/ad/2017-18-17) (historical): Fuselage · Airbus A300 B4-603, A300 B4-605R, A300 B4-620 and 5 more. Effective Oct 19, 2017
- [AD 2017-15-17](https://openairdocs.org/ad/2017-15-17) (historical): Wings · Airbus A300 B4-605R, A300 B4-622R, A300 C4-605R Variant F and 2 more. Effective Sep 5, 2017
- [AD 2017-07-05](https://openairdocs.org/ad/2017-07-05) (historical): Landing Gear · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Apr 17, 2017
- [AD 2016-20-11](https://openairdocs.org/ad/2016-20-11) (historical): Fuselage · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Jan 3, 2017
- [AD 2016-16-06](https://openairdocs.org/ad/2016-16-06) (historical): Fuslage · Airbus A300 B4-603, A300 B4-605R, A300 B4-622R and 3 more. Effective Sep 8, 2016
- [AD 2016-15-01](https://openairdocs.org/ad/2016-15-01) (historical): Flight controls · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Aug 26, 2016
- [AD 2016-07-22](https://openairdocs.org/ad/2016-07-22) (historical): Electrical Power · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective May 16, 2016
- [AD 2013-13-13](https://openairdocs.org/ad/2013-13-13) (historical): Wings · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Sep 23, 2014
- [AD 2014-13-17](https://openairdocs.org/ad/2014-13-17) (historical): Fuel · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Aug 19, 2014
- [AD 2014-12-06](https://openairdocs.org/ad/2014-12-06) (historical): Fuselage · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Jul 2, 2014
- [AD 2014-08-02](https://openairdocs.org/ad/2014-08-02) (historical): Wings · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 3 more. Effective May 21, 2014
- [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013
- [AD 2012-21-04](https://openairdocs.org/ad/2012-21-04) (historical): Fuel · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Nov 27, 2012
- [AD 2012-15-14](https://openairdocs.org/ad/2012-15-14) (historical): Wings · Airbus A300 B4-103, A300 B4-203, A300 B4-2C and 9 more. Effective Sep 11, 2012
- [AD 2012-13-06](https://openairdocs.org/ad/2012-13-06) (historical): Electrical Power · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Aug 14, 2012
- [AD 2012-08-03](https://openairdocs.org/ad/2012-08-03) (historical): Wings · Airbus A300 B4-103, A300 B4-203, A300 B4-2C and 17 more. Effective May 29, 2012
- [AD 2011-10-17](https://openairdocs.org/ad/2011-10-17) (historical): Doors, Fuselage, Nacelles/pylons, Stabilizers, Wings, and Powerplant · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Jun 17, 2011
- [AD 2010-23-26](https://openairdocs.org/ad/2010-23-26) (historical): Wings · Airbus A300 B2-1C, A300 B2-203, A300 B2K-3C and 10 more. Effective Jan 5, 2011
- [AD 2010-06-05](https://openairdocs.org/ad/2010-06-05) (historical): Fuselage · Airbus A300 B4-103, A300 B4-203, A300 B4-2C and 6 more. Effective Apr 15, 2010
- [AD 2010-06-04](https://openairdocs.org/ad/2010-06-04) (historical): Nacelles/Pylons · Airbus A300 B2-1C, A300 B2-203, A300 B2K-3C and 17 more. Effective Apr 15, 2010
- [AD 2007-10-10 R1](https://openairdocs.org/ad/2007-10-10-R1) (historical): Fuel tank systems · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 more. Effective Dec 28, 2009
- [AD 2009-18-15](https://openairdocs.org/ad/2009-18-15) (historical): Landing gear · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 21 more. Effective Oct 27, 2009
- [AD 2009-11-09](https://openairdocs.org/ad/2009-11-09) (historical): Equipment/Furnishings · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Jun 12, 2009
- [AD 2009-06-06](https://openairdocs.org/ad/2009-06-06) (historical): Transmission shafts · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Apr 28, 2009
- [AD 2009-02-04](https://openairdocs.org/ad/2009-02-04) (historical): Fuel level sensor-amplifier (FLSA) · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 more. Effective Mar 27, 2009
- [AD 2008-06-18](https://openairdocs.org/ad/2008-06-18) (historical): Lower skin panel · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Apr 23, 2008
- [AD 2008-03-04](https://openairdocs.org/ad/2008-03-04) (historical): P-clips · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 more. Effective Mar 6, 2008
- [AD 2007-25-15](https://openairdocs.org/ad/2007-25-15) (historical): Main landing gear (MLG) · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Jan 14, 2008
- [AD 2007-22-05](https://openairdocs.org/ad/2007-22-05) (historical): Center box assembly · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 more. Effective Nov 28, 2007
- [AD 2007-20-03](https://openairdocs.org/ad/2007-20-03) (historical): Time Limits/Maintenance Checks · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 more. Effective Oct 31, 2007
- [AD 2007-18-02](https://openairdocs.org/ad/2007-18-02) (historical): Fuel pump cables · Airbus A300 Model B2-1A, A300 Model B2-1C, A300 Model B2-203 and 13 more. Effective Oct 2, 2007
- [AD 2007-14-05](https://openairdocs.org/ad/2007-14-05) (historical): Airworthiness Limitations · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 14 more. Effective Aug 22, 2007
- [AD 2007-03-09](https://openairdocs.org/ad/2007-03-09) (historical): Ram air turbine (RAT) · Airbus A300B4-601, A300B4-603, A300B4-605R and 6 more. Effective Mar 12, 2007
- [AD 2007-03-18](https://openairdocs.org/ad/2007-03-18) (historical): Wing main landing gear (MLG) · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 13 more. Effective Feb 23, 2007

All 468: https://openairdocs.org/aircraft/N733FD/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 N733FD.

## FAA accident and incident reports

None matched to N733FD.

## Service difficulty reports (203, 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 FDEA202609161354](https://openairdocs.org/sdr/FDEA202609161354), Sep 16, 2026: SEAT TRACK. DAMAGED. SEAT TRACK LOBE DAMAGED UNDER MDC LOCK ML1080. AMM 53-10-16-06 SEAT TRACK LOBE DAMAGED UNDER MDC LOCK ML1080 MEL: 25-50-02-01-J LOCKED REMOVED AND PLACED IN CLO
- [SDR FDEA202608071099](https://openairdocs.org/sdr/FDEA202608071099), Aug 7, 2026: SKIN. CRACKED. MAIN DECK CARGO DOOR UPPER EDGE AT PT1 BETWEEN FR22 AND FR25 FOUND CRACK SIGNAL ON 4 EA FASTENER HOLES. REPAIRED THE FASTENER HOLES ON THE MAIN DECK CARGO DOOR 
- [SDR FDEA202608051111](https://openairdocs.org/sdr/FDEA202608051111), Aug 5, 2026: SKIN PANEL. CRACKED. FUSELAGE FRAME, FR 54 LATERAL PANEL THREE HOLES CRACKED AT STRINGER 36L, 44L - 44R. COMPLIED WITH EA 6-5330-T0388383 P1 REPAIRED THE FUSELAGE FRAME FR54 LATERAL
- [SDR FDEA202608021117](https://openairdocs.org/sdr/FDEA202608021117), Aug 2, 2026: FITTING. DAMAGED. CARGO DOOR, HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24. COMPLIED WITH
- [SDR FDEA202608011089](https://openairdocs.org/sdr/FDEA202608011089), Aug 1, 2026: SKIN. CONTAMINATED. LEFT ELEVATOR LOWER SURFACE HAS 1EA TRAPPED WATER AT ER5. REPAIRED LH ELEVATOR LOWER SURFACE ER5 TRAPPED WATER IAW SRM 55-21-12-201-2, PARA.5.J & SRM 51-77-12-2
- [SDR FDEA202608011088](https://openairdocs.org/sdr/FDEA202608011088), Aug 1, 2026: SKIN. CONTAMINATED. LEFT ELEVATOR UPPER SURFACE HAS 3EA TRAPPED WATER AT ER10. REPAIRED LT ELEVATOR UPPER ER10 TRAPPED WATER IAW SRM55-21-12-201-2 PARA.5.J & SRM 51-77-12-201. THIS
- [SDR FDEA202608011087](https://openairdocs.org/sdr/FDEA202608011087), Aug 1, 2026: FLOORBEAM. CORRODED. FUSELAGE SKIN INTERNAL BEAM CORRODED AT FR39 S50L - S54L. COMPLIED WITH EA 6-5310-T0388500 P1 REPAIRED THE FWD CARGO COMPARTMENT FR39 LOWER TEE BEAM CORROSION B
- [SDR FDEA202607311110](https://openairdocs.org/sdr/FDEA202607311110), Jul 31, 2026: REINFORCEMENT. CORRODED. AFT CARGO COMPARTMENT LOWER INTERNAL REINFORCING RING AND STRINGER FITTING CORRODED AT FR 54, STRINGERS 44R - 45R. FUSELAGE - MAINFRAME - FR54 TEE SECTION CORRO
- [SDR FDEA202607291098](https://openairdocs.org/sdr/FDEA202607291098), Jul 29, 2026: DOOR FRAME. CRACKED. RT PAX DOOR FRAME SEGMENT AT FR14C FOUND 2EA CRACKS. REPLACED THE CRACKED SEGMENT ON RH PAX DOOR FRAME AT FR14C IAW SRM 51-40-21 AND DWG F52181299(ISSUE: G). RS
- [SDR FDEA202607291079](https://openairdocs.org/sdr/FDEA202607291079), Jul 29, 2026: CARGO TRACK. CORRODED. MDC LOADING SYS TRACK Y450 CORRODED AT FR18 - FR19. REPLACED THE MDC CORRODED LOADING SYS TRACK AT FR18 - FR19 Y450 PER SRM 51-40-21 & DWG A53612518 (ISSUE.A00)
- [SDR FDEA202607291078](https://openairdocs.org/sdr/FDEA202607291078), Jul 29, 2026: CARGO TRACK. CORRODED. MDC LOADING SYS TRACK Y953 CORRODED AT FR18 - FR19. REPLACED THE MDC CORRODED LOADING SYS TRACK AT FR18 - FR19 Y953 IAW SRM 51-40-21 & DWG: A53615224 (ISSUE.A00
- [SDR FDEA202607251077](https://openairdocs.org/sdr/FDEA202607251077), Jul 25, 2026: SEAT TRACK. DAMAGED. SEAT TRACK LOBE DAMAGED UNDER MDC LOCK ML1080. REPLACED THE MDC CORRODED LOADING SYS TRACK AT FR40 - FR45 -Y450 PER A300-600 SRM51-40-21 & DWG A53832020, ISSUE:
- [SDR FDEA202602130218](https://openairdocs.org/sdr/FDEA202602130218), Feb 13, 2026: MOUNT. CORRODED. WHILE WORKING WRI 25-60/9552 FOR R1 FEA SLIDE INSPECTION, THE AMTS FOUND CORROSION AND 2 SCREWS BROKEN. REMOVED R1 SLIDE PER REF ABOVE.
- [SDR FDEA202502140227](https://openairdocs.org/sdr/FDEA202502140227), Feb 14, 2025: BUTTON. JAMMED. UPON TROUBLESHOOTING OF WRI 33-20/8722 FOUND THAT COURIER EMERGENCY TEST BUTTON JAMMED TOO AND NOT WORKING. CLEANED SWITCH REF ESPM 20-55-50-0 , OPS CKS OK M/M 
- [SDR FDEA202410231576](https://openairdocs.org/sdr/FDEA202410231576), Oct 23, 2024: SWITCH. FAILED. PDIS 733 52-70 8386 23OCT24 05:16 MEM OPEN PASSING FL230, RECEIVED A FLASHING RED LIGHT AND ALARM FOR THE R ENTRY DOOR. ALARM AND LIGHT STOPPED BELOW FL190 ON D
- [SDR FDEA202408161130](https://openairdocs.org/sdr/FDEA202408161130), Aug 16, 2024: CONTACTOR. FAILED. RIGHT AFTER TAKING THE RUNWAY FOR TAKEOFF, PRIOR TO ENGINE RUN UP, GOT A GEN 1 FAULT. ATTEMPTED ONE RESET IAW QRH/ECAM, BUT FAULTED AGAIN. AMM: 24-22-18-04 ESPM
- [SDR FDEA202407191035](https://openairdocs.org/sdr/FDEA202407191035), Jul 19, 2024: SLIDE. MALFUNCTIONED. DURING CRUISE R1 ENTRY DOOR, ARMING LEVER, RED ALARM, AUDIBLE AND VISUAL ALARM WENT OFF. PLND: DATE: 22JUL24 ENT BY: 779762 ON: 19JUL24 14:30 Z AT: LCK-LINE MEL
- [SDR FDEA202407171026](https://openairdocs.org/sdr/FDEA202407171026), Jul 17, 2024: TIRE. LOW PRESSURE. NO.1 MAIN TIRE TO BE REPLACED DUE TO LOW TIRE PRESSURE OF NO.2 MAIN TIRE AND KNOWN TO HAVE ROLLED DURING EVENT.
- [SDR FDEA202411200816](https://openairdocs.org/sdr/FDEA202411200816), May 11, 2024: SWITCH. FAULTED. AT TOP OF CLIMB, JUMPSEATER HEARD RI ALARM RINGING & NOTICED SLIDE ARM WARNING LIGHT FLASHING. COMPLIED WITH QRH WITH NO RELIEF OF ALARM OR LIGHT. ALARM QUIT ON
- [SDR FDEA202404090451](https://openairdocs.org/sdr/FDEA202404090451), Apr 9, 2024: FITTING. CRACKED. RH WING - BASIC WING STRUCTURE FR40 STGR32R - STGR33R I/B HOLE FOUND CRACK COMPLIED WITH FEDEX EA 6-5710-T0378762 REPAIRED THE RH WING BASIC WING STRUCTURE RH F
- [SDR FDEA202404090450](https://openairdocs.org/sdr/FDEA202404090450), Apr 9, 2024: RIB SPLICE. CRACKED. RH WING - CENTER SPAR RIB1 SPLICE TYPE 5 MIDDLE HOLE FOUND CRACK. COMPLIED WITH FEDEX EA 6-5710-T0378735 P1 REPAIRED THE RH WING CENTER SPAR RIB1 SPLICE TYPE 5 
- [SDR FDEA202404080449](https://openairdocs.org/sdr/FDEA202404080449), Apr 8, 2024: NONE. NONE. EXISTING REPAIR ON AFT CARGO DOOR INNER SURFACE BETWEEN FR62A AND FR63, BEAM 4 - BEAM 5 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON AFT CARGO DOOR
- [SDR FDEA202404080448](https://openairdocs.org/sdr/FDEA202404080448), Apr 8, 2024: NONE. NONE. EXISTING REPAIR ON AFT CARGO DOOR INNER SURFACE BETWEEN FR60A AND FR61, BEAM 4 - BEAM 5 REQUIRES EVALUATION FOR CONFORMITY. EXISTING REPAIR ON AFT CARGO DOOR IN
- [SDR FDEA202403300416](https://openairdocs.org/sdr/FDEA202403300416), Mar 30, 2024: BEAM. CRACKED. WINGS - CENTER WING JOINT - FR40 STGR27L - STGR28L LH HOLE C FOUND CRACK REPAIRED CENTER WING JOINT FR40 STGR27L - STGR28L CRACKED LH HOLE C PER A300-600 SRM57-
- [SDR FDEA202403300415](https://openairdocs.org/sdr/FDEA202403300415), Mar 30, 2024: STRUCTURE. CRACKED. CENTER WING BOX - FR47 LHS REAR SPAR DATUM HOLE C FOUND CRACK COMPLIED WITH FEDEX EA 6-5710-T0378646 REPAIRED THE FR47 LHS REAR SPAR DATUM CRACKED HOLE C. TITLE
- [SDR FDEA202403290404](https://openairdocs.org/sdr/FDEA202403290404), Mar 29, 2024: RIB. CRACKED. RH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB18 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH FEDEX EA 6-5750-T0378628 P1 REPAIRED THE RH WING CENTE
- [SDR FDEA202403290403](https://openairdocs.org/sdr/FDEA202403290403), Mar 29, 2024: RIB. CRACKED. RH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB21 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH FEDEX EA 6-5750-T0378628 P1 REPAIRED THE RH WING CENTER 
- [SDR FDEA202403290402](https://openairdocs.org/sdr/FDEA202403290402), Mar 29, 2024: RIB. CRACKED. RH WING CENTER FLAP RIB UPPER FLANGE FOUND 5EA CRACKS AT RIB25, RIB26, RIB27 BETWEEN STGR2.7 AND REAR SPAR COMPLIED WITH FEDEX EA 6-5750-T0378628 P1 REPAIRED TH
- [SDR FDEA202403290401](https://openairdocs.org/sdr/FDEA202403290401), Mar 29, 2024: RIB. CRACKED. LH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB26, RIB27 BETWEEN STGR2.6 AND REAR SPAR COMPLIED WITH FEDEX EA 6-5750-T0378625 P1 REPAIRED THE LH WI
- [SDR FDEA202403290400](https://openairdocs.org/sdr/FDEA202403290400), Mar 29, 2024: RIB. CRACKED. LH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH FEDEX EA 6-5750-T0378625 P1 REPAIRED THE LH WING CENTE
- [SDR FDEA202403260374](https://openairdocs.org/sdr/FDEA202403260374), Mar 26, 2024: NONE. NONE. EXISTING REPAIR ON FUSELAGE STRINGER AT S-56R BETWEEN FR62 AND FR63 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT S-56R BETWEEN
- [SDR FDEA202403260373](https://openairdocs.org/sdr/FDEA202403260373), Mar 26, 2024: NONE. NONE. EXISTING REPAIR ON FUSELAGE STRINGER AT S-56R BETWEEN FR63 AND FR64 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT S-56R BETWEEN
- [SDR FDEA202403220342](https://openairdocs.org/sdr/FDEA202403220342), Mar 22, 2024: CROSSBEAM. CORRODED. AFT CARGO COMPARTMENT CROSS BEAM FR60 CORRODED AT Y-140 ~ Y-805 REPAIRED THE AFT CARGO COMPARTMENT CORRODED CROSS BEAM FR60 AT Y-140 ~ Y-805 PER A300-600 SRM53-
- [SDR FDEA202403220343](https://openairdocs.org/sdr/FDEA202403220343), Mar 22, 2024: CROSSBEAM. CORRODED. AFT CARGO COMPARTMENT CROSS BEAM FR56 CORRODED AT Y140 - Y1470. REPAIRED THE AFT CARGO COMPARTMENT CORRODED CROSS BEAM FR56 AT Y-140 ~ Y1470 PER SRM53-10-15-201
- [SDR FDEA202403220341](https://openairdocs.org/sdr/FDEA202403220341), Mar 22, 2024: CROSSBEAM. CORRODED. AFT CARGO COMPARTMENT CROSS BEAM FR63 CORRODED AT Y-140 - Y1470. REPAIRED THE AFT CARGO COMPARTMENT CORRODED CROSS BEAM FR63 AT Y-140 ~ Y1470 PER A300-600 SRM53
- [SDR FDEA202402160164](https://openairdocs.org/sdr/FDEA202402160164), Feb 16, 2024: SWITCH. FAILED. DURING THE FLIGHT, THE DOOR ON THE RIGHT SIDE WAS ALARMING. INDICATIONS IN COCKPIT WERE NORMAL. T/S CARRIED OUT IAW ABOVE REF. OPS TEST OF R1 DOOR EMERGENCY ESC
- [SDR FDEA202310121881](https://openairdocs.org/sdr/FDEA202310121881), Oct 12, 2023: BATTERY. INOPERATIVE. EMERGENCY LIGHTS PUSH TO TEST SWITCH IN COURIER AREA DOES NOT ILLUMINATE DURING TEST. (EMERGENCY LIGHTS DO ILLUMINATE.) RED LED ON POWER SUPPLY UNIT IS ILLUMINA
- [SDR FDEA202302110248](https://openairdocs.org/sdr/FDEA202302110248), Feb 11, 2023: FRAME. DAMAGED. DURING ROTO INSP OF FR40 RHS UPPER AND LOWER HOLES NOTED WITH REJECTABLE DAMAGE INDICATIONS. WORK ACCOMPLISHED ON EA 6-5710-T0310489 REV E PT 5. EA TITLE WINGS 
- [SDR FDEA202301110098](https://openairdocs.org/sdr/FDEA202301110098), Jan 11, 2023: SLEEVE. CRACKED. T/R STRUCTURE/SLEEVE - RH ENGINE I/B UPPER ACTUATOR SUPPORT , COMPLY WITH E.A.6-7833-T0372382 REV.C P2 REPAIRED #2 ENGINE I/B T/R STRUCTURE/SLEEVE - RH ENGINE I
- [SDR FDEA202201060019](https://openairdocs.org/sdr/FDEA202201060019), Jan 6, 2022: PACKING. FAILED. PDIS 733 29-02 5545 06JAN22 IND OPEN U ON CLIMB OUT, HYDRAULIC GREEN SYSTEM LOW QUANTITY. COMPLIED WITH ECAM AND QRH AND SECURED GREEN SYSTEM HYDRAULIC PUMPS. D
- [SDR FDEA202111112818](https://openairdocs.org/sdr/FDEA202111112818), Nov 11, 2021: NONE. CRACKED. LOWER FUSELAGE LH SIDE OF R GANTRY #5 AT FR50B CRACKED PERFORMED THE REPAIR ON LH SIDE OF R GANTRY #5 AT FR50B PER FEDEX EO: 6-5310-7- 5021 F PT9 TITLE: FUSELAG
- [SDR FDEA202111112817](https://openairdocs.org/sdr/FDEA202111112817), Nov 11, 2021: SEAT TRACK. CRACKED. MDCC FR20-FR21, -Y450 SEAT TRACK CRACKED COMPLIED WITH FEDEX EA:6-5310-T0365152 P1, TITLE: FUSELAGE-MAINFRAME-MCD -Y450 SEAT SEAT TRACK BENT BETWEEN FR20 AND FR
- [SDR FDEA202111082793](https://openairdocs.org/sdr/FDEA202111082793), Nov 8, 2021: NONE. CRACKED. LOWER FUSELAGE LH SIDE OF R GANTRY #5 AT FR51A CRACKED PERFORMED THE REPAIR ON LH SIDE OF R GANTRY #5 AT FR51A PER FEDEX EO: 6-5310-7-5021 5021 F PT9 TITLE: FUS
- [SDR FDEA202111082792](https://openairdocs.org/sdr/FDEA202111082792), Nov 8, 2021: NONE. DELAMINATED. RH AILERRON UPPER SURFACE T/E AREA FOUND 1EA PUNCTURED COMPLIED WITH EA: 6-5750-T0365067 P1 TITLE: WING-FLIGHT SURFACES-RH AILERON TRAILING EDGE WEDGE UPPER SUR
- [SDR FDEA202103170684](https://openairdocs.org/sdr/FDEA202103170684), Mar 17, 2021: ACTUATOR. MALFUNCTIONED. PDIS 733 32-60 4477 17MAR21 IND FACT U ON DEPARTURE OUT OF IND GOT ECAM ALERT FOR L/G DOORS NOT CLOSED. NOSE GEAR AMBER DOOR LIGHT ILLUMINATED ON FORWARD AND OV
- [SDR FDEA202103160670](https://openairdocs.org/sdr/FDEA202103160670), Mar 16, 2021: SLIDE. DETACHED. RAMP REPORTED BEING UNABLE TO OPEN R1 ENTRY DOOR. UPON ARRIVAL TO AIRCRAFT FOUND R1 DOOR SLIDE SEPARATED FROM R1 DOOR WITH SLIDE MOUNTS STILL ATTACHED TO DOOR A
- [SDR FDEA202011182963](https://openairdocs.org/sdr/FDEA202011182963), Nov 18, 2020: TARGET. OUT OF POSITION. ON FINAL APPROACH IN KELP F/O PUT THE LANDING GEAR HANDLE TO THE DOWN POSITION, ONLY RECEIVED THE GEAR DOOR UNLOCK LIGHTS AND GEAR DID NOT EXTEND FOR 20 -30 SEC
- [SDR FDEA201907181626](https://openairdocs.org/sdr/FDEA201907181626), Jul 18, 2019: SPAR. CRACKED. CRACK SIGNAL WAS FOUND AT RH WING FRONT SPAR RIB9 "S" HOLE AFTER ROTO-TEST INSPECTION COMPLIED WITH FEDEX EA: 6-5710-T0347649 P1, TITLE: WINGS - BASIC WING STRU
- [SDR FDEA201906291427](https://openairdocs.org/sdr/FDEA201906291427), Jun 29, 2019: SKIN. DAMAGED. LT WING - INBD FLAP LWR SKIN WITH DEEP SCRATCH (LOCATION: 17 INCH FROM T/E, 34 INCH FROM I/B EDGE) REPAIRED THE LT WING INBD FLAP SCRATCHED SKIN (LOCATION: 17 I
- [SDR FDEA201906131281](https://openairdocs.org/sdr/FDEA201906131281), Jun 13, 2019: STIFFENER. CORRODED. REPLACED THE CORRODED STIFFENER ON TOILET SERVICE PANEL CUTOUT SKIN AT FR12- FR12A PER A300-600 SRM51-40-21. MAJOR REPAIR IAW GMM 6-2-100.

All 203: https://openairdocs.org/aircraft/N733FD/reports.md

## STCs that may be installed (OpenAirDocs) (168, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Airbus Industrie A300 B4-605R)

- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [STC SA5040NM](https://openairdocs.org/stc/SA5040NM): Installation of cargo pallet and net. Satco Inc
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC SA3400NM](https://openairdocs.org/stc/SA3400NM): Installation of floor proximity emergency escape path marking system. Bruce Aerospace Inc. Lists A300 Series
- [STC ST01999AT](https://openairdocs.org/stc/ST01999AT): This installation adds three recording parameters (pitch control, lateral control, and rudder) to the existing A300 and A310 Digital Flight Data Recorder (DFDR) to meet the requirements of 14 CFR 121.344. Acron Aviation Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST01694CH](https://openairdocs.org/stc/ST01694CH): Installation of Honeywell International Enhanced Ground Proximity Warning System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST02161CH](https://openairdocs.org/stc/ST02161CH): Installation of GPS wiring and antenna provisions. Amphenol Cable and Interconnect Technologies Inc
- [STC ST02169CH](https://openairdocs.org/stc/ST02169CH): Installation of elementary and enhanced Mode S transponders. Amphenol Cable and Interconnect Technologies Inc
- [STC ST02866CH](https://openairdocs.org/stc/ST02866CH): Upgrade of the internal core software of the ACARS Data Link Management Unit (DLM-900). Amphenol Cable and Interconnect Technologies Inc
- [STC ST11861AT](https://openairdocs.org/stc/ST11861AT): Installation of a new Control Wheel Push-to-Talk (PTT) switch with three positions and latchable in accordance with the MDL shown in the attached AML No. ST11861AT. FedEx Express
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST00691SE](https://openairdocs.org/stc/ST00691SE): Installation of lightweight window plugs. LiteAir Aviation Products Inc
- [STC ST02302CH](https://openairdocs.org/stc/ST02302CH): Install ERDA model 7004 HI-LO table with slide top. Collins Aerospace
- [STC ST01940CH](https://openairdocs.org/stc/ST01940CH): Installation of a Honeywell RESCU 406AF Emergency Locator Transmitter (ELT) System. Honeywell International Inc
- [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [STC ST00181SE](https://openairdocs.org/stc/ST00181SE): Installation of Model 4033, 4034 and 4038 Transient Suppression Units. Honeywell International Inc
- [STC ST00440SE](https://openairdocs.org/stc/ST00440SE): Installation of the Honeywelll Enhanced Ground Proximity Warning System. Honeywell International Inc
- [STC SA5672SW-D](https://openairdocs.org/stc/SA5672SW-D): Modification of air to air heat exchanger (P/N 187900-9). Honeywell International Inc
- [STC SA7565SW](https://openairdocs.org/stc/SA7565SW): Rebuild A300 Auxiliary Power Unit Oil Cooler Assembly by manufacturing a new core assembly. Honeywell International Inc. Lists A300 Series
- [STC SA4821NM](https://openairdocs.org/stc/SA4821NM): Installation of a Hughes-Avicom video entertainment system. Burrana Inc. Lists A300 Series
- [STC SA3483NM](https://openairdocs.org/stc/SA3483NM): Installation of Trans Com video projection system. Burrana Inc. Lists A300 Series
- [STC ST03574AT](https://openairdocs.org/stc/ST03574AT): Installation of a Talon Aerospace Anti-Collision Light. Aaxico Technical Services Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC SA6082NM](https://openairdocs.org/stc/SA6082NM): Installation of audio entertainment system. Burrana Inc. Lists A300 B4 Series
- [STC ST04092NY](https://openairdocs.org/stc/ST04092NY): Installation of Wireless PCMCIA for DFDAU. Delta Engineering Corporation
- [STC ST04511AT](https://openairdocs.org/stc/ST04511AT): Installation of Whelen LED logo lights. Avionics Support Group Inc
- [STC ST02686LA](https://openairdocs.org/stc/ST02686LA): Installation of an alternate part number. Honeywell International Inc
- [STC ST04049NY](https://openairdocs.org/stc/ST04049NY): Installation of a Hoffman Engineering LLC LED Landing Light to replace the OEM Q4559 Series Incandescent Lamp, used as a Landing/Takeoff Light. Hoffman Engineering LLC
- [STC ST00855LA](https://openairdocs.org/stc/ST00855LA): Installation of ANCRA main deck cargo handling system. Ancra International LLC. Lists A300 B4 Series
- [STC ST01644LA](https://openairdocs.org/stc/ST01644LA): Installation of Ancra cargo system. Ancra International LLC
- [STC ST02482LA](https://openairdocs.org/stc/ST02482LA): Installation of main deck cargo loading system. Ancra International LLC
- [STC ST04345NY](https://openairdocs.org/stc/ST04345NY): Upgrade from TCAS II software version 7.0 to 7.1. PMV Engineering
- [STC ST01891LA-D](https://openairdocs.org/stc/ST01891LA-D): Installation of a Commercial Medical Stretcher. LifePort LLC
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST09962SC](https://openairdocs.org/stc/ST09962SC): Installation of X-Band nose radome shell assembly. The NORDAM Group LLC
- [STC ST01215AT-D](https://openairdocs.org/stc/ST01215AT-D): Installation of Collins SAT-906 SATCOM System with Canadian Marconi CMA-2102 antenna system. TIMCO. Lists A300 Series
- [STC ST01223AT-D](https://openairdocs.org/stc/ST01223AT-D): Installation of Airshow 210 System with Dual RADVR and with Airshow Provisions. HAECO Cabin Solutions LLC
- [STC ST01361AT-D](https://openairdocs.org/stc/ST01361AT-D): Installation of Dual Mode "S" Transponders. HAECO Cabin Solutions LLC
- [STC ST03848NY](https://openairdocs.org/stc/ST03848NY): Installation of SuperSeal UltraLite (SSUL) PHOTOLUMINESCENT AISLE PATH MARKING SYSTEM. STG Aerospace Ltd
- [STC ST02639LA](https://openairdocs.org/stc/ST02639LA): Replace the existing Mode S Transponder system. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST04229NY](https://openairdocs.org/stc/ST04229NY): Introduction of a 16G New Generation Stretcher XL P/N 1120030-Series. Bucher Leichtbau AG
- [STC ST04309CH](https://openairdocs.org/stc/ST04309CH): Installation of ADS-B OUT Global Positioning Satellite System (GPSS)/Space-Based Augmentation System (SBAS) & ADS-B IN Flight Information Services-Broadcast (FIS-B) system. Innoviator LLC
- [STC ST04221AT](https://openairdocs.org/stc/ST04221AT): The installation of a Honeywell Enhanced Ground Proximity Warning System (EGPWS). United Parcel Service Company
- [STC SA3185SO](https://openairdocs.org/stc/SA3185SO): Installation of a replacement coalescer filter. Purolator Facet, Inc
- [STC ST04372AT](https://openairdocs.org/stc/ST04372AT): Installation of Wireless Data Loader Provisions. Chippewa Aerospace Inc
- [STC ST02406LA](https://openairdocs.org/stc/ST02406LA): Installation of TCAS version 7.1. Aviation Communication and Surveillance Systems (ACSS) LLC

All 168: https://openairdocs.org/aircraft/N733FD/stcs.md

## Earlier aircraft with N733FD

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N733FD before.

- [Cancelled 1977-03-21](https://openairdocs.org/deregistered/N733FD-1977-03-21): Cessna 172N, S/N 17268254. Exported to Canada. Owner: [Commander Aviation Corp](https://openairdocs.org/faa-owner/COMMANDER%20AVIATION%20CORP), [Bismarck, ND](https://openairdocs.org/faa-place/ND/Bismarck)

## Related

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

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