# N303FE: 1973 Mcdonnell Douglas MD-10-30F

- Status: Valid registration
- Airframe: [Mcdonnell Douglas MD-10-30F](https://openairdocs.org/model/mcdonnell-douglas-md-10-30f) (registry code 3024020, 385 seats)
- Engine: [GE CF6-50 series](https://openairdocs.org/engine/ge-cf6-50-series) (registry code 30018)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE) (The Boeing Company), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (General Electric Company) (OpenAirDocs)
- Serial number: 46802
- Year built: 1973
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 4, 2002
- Certificate issued: April 3, 1984
- Expires: April 30, 2030
- Mode S code: A32AF9
- Registered owner: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION)
- 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=303FE
- Page: https://openairdocs.org/aircraft/N303FE

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 CF6-50 model are included.

## ADs that may apply (OpenAirDocs): 99 in force

### Matched by airframe (Mcdonnell Douglas MD-10-30F)

- [AD 2026-13-15](https://openairdocs.org/ad/2026-13-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jul 1, 2026
- [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 2025-23-53](https://openairdocs.org/ad/2025-23-53): Nacelles/pylons · Boeing MD-11, MD-11F, MD-10-10F and 8 more. Effective Dec 1, 2025
- [AD 2023-12-15](https://openairdocs.org/ad/2023-12-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jun 21, 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 2021-08-10](https://openairdocs.org/ad/2021-08-10): Nacelles/pylons · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective May 25, 2021
- [AD 2020-22-15](https://openairdocs.org/ad/2020-22-15): Fuselage · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Dec 18, 2020
- [AD 2018-22-10](https://openairdocs.org/ad/2018-22-10): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Dec 12, 2018
- [AD 2015-02-05](https://openairdocs.org/ad/2015-02-05): Navigation · Boeing 717-200, DC-10-10, DC-10-10F and 13 more. Effective Mar 5, 2015
- [AD 2014-21-05](https://openairdocs.org/ad/2014-21-05): Fuselage · Boeing DC-10-10, DC-10-10F, DC-10-30 and 4 more. Effective Dec 2, 2014
- [AD 2012-19-03](https://openairdocs.org/ad/2012-19-03): Fuselage · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Nov 5, 2012
- [AD 2011-12-01](https://openairdocs.org/ad/2011-12-01): Equipment/Furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 268 more. Effective Aug 1, 2011
- [AD 2011-11-05](https://openairdocs.org/ad/2011-11-05): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 10 more. Effective Jul 6, 2011
- [AD 2010-20-13](https://openairdocs.org/ad/2010-20-13): Fuel · Boeing DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40 and 2 more. Effective Nov 9, 2010
- [AD 2010-20-14](https://openairdocs.org/ad/2010-20-14): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Nov 5, 2010
- [AD 2010-09-12](https://openairdocs.org/ad/2010-09-12): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Jun 8, 2010
- [AD 2009-21-10 R1](https://openairdocs.org/ad/2009-21-10-R1): Oxygen · Airbus A300 B4-605R, A300 B4-620, A300 B4-622 and 138 more. Effective Feb 4, 2010
- [AD 2008-06-21 R1](https://openairdocs.org/ad/2008-06-21-R1): Fuel tank systems · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Dec 10, 2009
- [AD 2009-03-02](https://openairdocs.org/ad/2009-03-02): Auxiliary hydraulic pumps · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 31, 2009
- [AD 2008-17-16](https://openairdocs.org/ad/2008-17-16): Fuel boost pump · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Oct 2, 2008
- [AD 2008-11-14](https://openairdocs.org/ad/2008-11-14): Horizontal pressure panel · Boeing DC-10-10F, DC-10-30F (KC-10A, KDC-10), DC-10-40F and 4 more. Effective Jul 3, 2008
- [AD 2007-19-17](https://openairdocs.org/ad/2007-19-17): System 3 hydraulic piping · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Oct 26, 2007
- [AD 2007-19-15](https://openairdocs.org/ad/2007-19-15): Flight management system (FMS) · Boeing 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Oct 26, 2007
- [AD 2007-19-02](https://openairdocs.org/ad/2007-19-02): Fuel tank and the fuel transfer pump housing flange · Boeing DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40 and 4 more. Effective Oct 17, 2007
- [AD 2007-11-15](https://openairdocs.org/ad/2007-11-15): Center main wheel well · Boeing DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40 and 2 more. Effective Jul 5, 2007
- [AD 2007-10-12](https://openairdocs.org/ad/2007-10-12): Reinforced flight deck door · Reinforced cockpit door (Safran Cabin STC ST01335LA or 2 others). Effective Jun 27, 2007
- [AD 2007-04-17](https://openairdocs.org/ad/2007-04-17): Control modules of the fire detection systems · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Mar 23, 2007
- [AD 2006-19-03](https://openairdocs.org/ad/2006-19-03): Fabrication and installation of a wire harness guard in the right wheel well of the main  
 landing gear (MLG) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Oct 17, 2006
- [AD 2006-16-15](https://openairdocs.org/ad/2006-16-15): Airplane flight manual (AFM) · Boeing MD-10-10F, MD-10-30F, MD-11 and 1 more. Effective Sep 22, 2006
- [AD 2006-04-04](https://openairdocs.org/ad/2006-04-04): Smoke detectors · ATR - GIE Avions de Transport Régional ATR42-200, ATR42-300, ATR42-320 and 37 more. Effective Mar 24, 2006
- [AD 2006-03-13](https://openairdocs.org/ad/2006-03-13): Inboard and outboard hinge fittings · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 16, 2006
- [AD 2006-02-11](https://openairdocs.org/ad/2006-02-11): Drain holes of the pitot tubes · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 3, 2006
- [AD 2005-20-15](https://openairdocs.org/ad/2005-20-15): Rudder pedal torque tube assembly · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Nov 10, 2005
- [AD 2005-17-04](https://openairdocs.org/ad/2005-17-04): Fire extinguishing system · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Sep 26, 2005
- [AD 2005-15-12](https://openairdocs.org/ad/2005-15-12): Exterior emergency control handle assemblies of the forward passenger doors · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Aug 30, 2005
- [AD 2005-15-03](https://openairdocs.org/ad/2005-15-03): Exterior emergency control handle assemblies · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Aug 25, 2005
- [AD 2005-02-04](https://openairdocs.org/ad/2005-02-04): Cargo compartment smoke detectors · Boeing DC-10-10F, DC-10-30F (KC-10A, KDC-10), MD-10-10F and 2 more. Effective Feb 8, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-18-15](https://openairdocs.org/ad/2004-18-15): Flight engineer's station · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Oct 19, 2004
- [AD 2001-14-08 R1](https://openairdocs.org/ad/2001-14-08-R1): Auxiliary hydraulic pump · McDonnell Douglas DC-10 Series (all), MD-10-10F and MD-10-30F. Effective Sep 1, 2004
- [AD 2004-05-06](https://openairdocs.org/ad/2004-05-06): Number one passenger door slide · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Apr 7, 2004
- [AD 2004-02-06](https://openairdocs.org/ad/2004-02-06): Forward aft bracket · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 5, 2004
- [AD 2003-24-10](https://openairdocs.org/ad/2003-24-10): Rudder pedal arm assembly · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Jan 8, 2004
- [AD 2003-03-15 R1](https://openairdocs.org/ad/2003-03-15-R1): Airplane Flight Manual (AFM) - oxygen masks · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 90 more. Effective Dec 22, 2003
- [AD 2003-19-05](https://openairdocs.org/ad/2003-19-05): Inboard and outboard flaps · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Oct 27, 2003
- [AD 2003-16-02](https://openairdocs.org/ad/2003-16-02): Fuel Boost/Transfer Pumps · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Aug 25, 2003
- [AD 2003-08-03](https://openairdocs.org/ad/2003-08-03): Throttle control module (TCM) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective May 22, 2003
- [AD 2003-08-14](https://openairdocs.org/ad/2003-08-14): Airplane Flight Manual (AFM) - Fuel Tank · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective May 12, 2003
- [AD 2002-13-10](https://openairdocs.org/ad/2002-13-10): Fuel boost/transfer pump connectors · Boeing DC-10-10, DC-10-10F, DC-10-15 and 10 more. Effective Aug 12, 2002
- [AD 2002-06-14](https://openairdocs.org/ad/2002-06-14): Parallel Power Feeder Cables of the Number 2 Generator · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective May 7, 2002

### Matched by engine (GE CF6-50 series)

- [AD 2023-04-11](https://openairdocs.org/ad/2023-04-11): Turbine Section · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 28, 2023
- [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 2011-07-01](https://openairdocs.org/ad/2011-07-01): Forward and aft centerbodies · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 22, 2011
- [AD 2007-11-18 R1](https://openairdocs.org/ad/2007-11-18-R1): Forward fan stator cases · General Electric CF6-50C, CF6-50C1 and CF6-50C2. Effective Jan 4, 2010
- [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 2007-19-06](https://openairdocs.org/ad/2007-19-06): Compressor discharge pressure (CDP) · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Oct 23, 2007
- [AD 2005-26-06](https://openairdocs.org/ad/2005-26-06): Low pressure turbine (LPT) stage 2 interstage seal assemblies · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jan 26, 2006
- [AD 2005-07-05](https://openairdocs.org/ad/2005-07-05): Low pressure turbine (LPT) · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective May 4, 2005
- [AD 2005-08-04](https://openairdocs.org/ad/2005-08-04): Low-cycle-fatigue (LCF) · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 28, 2005
- [AD 2003-09-06](https://openairdocs.org/ad/2003-09-06): Low pressure turbine (LPT) · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more. Effective Jun 3, 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 2002-05-03](https://openairdocs.org/ad/2002-05-03): Life-Limited Rotating Parts · General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective Apr 12, 2002
- [AD 2002-02-09](https://openairdocs.org/ad/2002-02-09): Low Pressure Turbine Rotor (LPTR) Stage 2 Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Mar 15, 2002
- [AD 2001-12-20](https://openairdocs.org/ad/2001-12-20): Air Ducts and Reworked Mating Hardware · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more. Effective Jul 26, 2001
- [AD 2001-04-16](https://openairdocs.org/ad/2001-04-16): Low Pressure Turbine (LPT) Nozzle Lock Assembly Studs · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more. Effective Mar 21, 2001
- [AD 2000-11-12](https://openairdocs.org/ad/2000-11-12): High Pressure Compressor Disk Lock Slots · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Aug 14, 2000
- [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 95-08-03](https://openairdocs.org/ad/95-08-03): High Pressure Turbine Rotor Stage 2 Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jun 12, 1995
- [AD 91-10-03 R1](https://openairdocs.org/ad/91-10-03-R1): High Pressure Compressor · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 28, 1995
- [AD 94-08-05](https://openairdocs.org/ad/94-08-05): Fan Stator Case · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jul 5, 1994
- [AD 94-09-18](https://openairdocs.org/ad/94-09-18): High Pressure Turbine Disk · General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective Jun 6, 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 93-13-10](https://openairdocs.org/ad/93-13-10): Compressor Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Sep 21, 1993
- [AD 91-23-13](https://openairdocs.org/ad/91-23-13): Fan Disks · General Electric CF6-50A, CF6-50C, CF6-50C1 and 12 more. Effective Nov 22, 1991
- [AD 91-15-16](https://openairdocs.org/ad/91-15-16): High Pressure Turbine Thermal Shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Sep 4, 1991
- [AD 91-01-04](https://openairdocs.org/ad/91-01-04): Fan Disk · General Electric CF6-45A, CF6-45A2, CF6-50A and 19 more. Effective Jan 22, 1991
- [AD 90-23-15](https://openairdocs.org/ad/90-23-15): Turbine Mid-frame · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Dec 6, 1990
- [AD 90-19-09](https://openairdocs.org/ad/90-19-09): High Pressure Turbine Stage One Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Oct 1, 1990
- [AD 90-12-06](https://openairdocs.org/ad/90-12-06): Low Pressure Turbine · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jun 25, 1990
- [AD 89-01-02](https://openairdocs.org/ad/89-01-02): High Pressure Turbine Stage 2 Disks · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more. Effective Dec 29, 1988
- [AD 87-23-06](https://openairdocs.org/ad/87-23-06): High Pressure Turbine Impeller Spacer · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Nov 5, 1987
- [AD 86-12-03](https://openairdocs.org/ad/86-12-03): High Pressure Turbine Rotor (HPTR) Stage 1 Disk · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jun 29, 1986
- [AD 84-01-01](https://openairdocs.org/ad/84-01-01): Compressor Assemblies · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Feb 10, 1984
- [AD 82-25-08](https://openairdocs.org/ad/82-25-08): HPT Spacer/Impeller · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Dec 30, 1982
- [AD 82-20-03](https://openairdocs.org/ad/82-20-03): Inspect First Stage HPT Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Oct 31, 1982
- [AD 77-08-08](https://openairdocs.org/ad/77-08-08): Compressor · General Electric CF6-50A, CF6-50C, CF6-50C1 and 2 more. Effective Feb 14, 1980
- [AD 76-17-01](https://openairdocs.org/ad/76-17-01): High Pressure Compressor · General Electric CF6-50A, CF6-50C, CF6-50E and 1 more. Effective Aug 20, 1976
- [AD 76-05-10](https://openairdocs.org/ad/76-05-10): Turbofan Engines · General Electric CF6-50A, CF6-50C, CF6-50E and 3 more. Effective Mar 24, 1976
- [AD 85-25-56 R1](https://openairdocs.org/ad/85-25-56-R1): Seventh Stage Low Pressure Turbine (LPT) Cooling Air Manifold Tube · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more
- [AD 79-13-09](https://openairdocs.org/ad/79-13-09): Compressor Rotor Spools · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more

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

- [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022
- [AD 2016-04-16](https://openairdocs.org/ad/2016-04-16) (historical): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Apr 15, 2016
- [AD 2013-08-23](https://openairdocs.org/ad/2013-08-23) (historical): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective May 29, 2013
- [AD 2009-26-17](https://openairdocs.org/ad/2009-26-17) (historical): Fuselage · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Feb 4, 2010
- [AD 2009-21-10](https://openairdocs.org/ad/2009-21-10) (historical): Oxygen · Airbus A300, Model B4-605R, A300, Model B4-620, A300, Model B4-622 and 138 more. Effective Dec 17, 2009
- [AD 2008-06-21](https://openairdocs.org/ad/2008-06-21) (historical): Fuel tank systems · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Apr 23, 2008
- [AD 2007-15-05](https://openairdocs.org/ad/2007-15-05) (historical): Fuel pump housing electrical connector · Boeing DC-10-10, DC-10-10F, DC-10-15 and 9 more. Effective Aug 8, 2007
- [AD 2005-12-05](https://openairdocs.org/ad/2005-12-05) (historical): Flight deck door · Reinforced cockpit door (Safran Cabin STC ST01335LA or 2 others). Effective Jul 19, 2005
- [AD 2004-18-04](https://openairdocs.org/ad/2004-18-04) (historical): Airplane Flight Manual (AFM) · McDonnell Douglas 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Sep 20, 2004
- [AD 2004-05-20](https://openairdocs.org/ad/2004-05-20) (historical): Electric motor operated auxiliary hydraulic pumps · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 9 more. Effective Apr 15, 2004
- [AD 2003-17-07](https://openairdocs.org/ad/2003-17-07) (historical): Fire Extinguishers for the Engine and Auxiliary Power Unit (APU) · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 60 more. Effective Sep 24, 2003
- [AD 2003-14-04](https://openairdocs.org/ad/2003-14-04) (historical): Flight Deck Door Pressure Relief Latch Assemblies · Boeing 737-200 Series, 737-300 Series, 737-400 Series and 14 more. Effective Jul 25, 2003
- [AD 2003-03-15](https://openairdocs.org/ad/2003-03-15) (historical): Airplane Flight Manual (AFM) - Oxygen Masks · Boeing 707 Series (all), 720 Series (all), 727 Series (all) and 75 more. Effective Mar 7, 2003
- [AD 2001-14-08](https://openairdocs.org/ad/2001-14-08) (historical): Electric Motors of the Auxiliary Hydraulic Pump · McDonnell Douglas DC-10 Series (all), MD-10-10F, MD-10-30F and 1 more. Effective Aug 16, 2001
- [AD 2012-02-07](https://openairdocs.org/ad/2012-02-07) (historical): LPT rotor stage 3 disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Mar 6, 2012
- [AD 2011-18-01](https://openairdocs.org/ad/2011-18-01) (historical): LPT rotor stage 3 disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Sep 26, 2011
- [AD 2011-02-07](https://openairdocs.org/ad/2011-02-07) (historical): Rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Feb 22, 2011
- [AD 2010-12-10](https://openairdocs.org/ad/2010-12-10) (historical): High-pressure turbine (HPT) · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Jun 24, 2010
- [AD 2010-06-15](https://openairdocs.org/ad/2010-06-15) (historical): Low-pressure turbine (LPT) stage 3 disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Apr 1, 2010
- [AD 2009-04-17](https://openairdocs.org/ad/2009-04-17) (historical): Long fixed core exhaust nozzle (LFCEN) assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 2, 2009
- [AD 2007-11-18](https://openairdocs.org/ad/2007-11-18) (historical): Forward fan stator cases · General Electric CF6-50C, CF6-50C1, CF6-50C2 and 1 more. Effective Jul 5, 2007
- [AD 2006-12-24](https://openairdocs.org/ad/2006-12-24) (historical): Five-link forward mount assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Jul 21, 2006
- [AD 2000-08-11](https://openairdocs.org/ad/2000-08-11) (historical): Life-limited Parts · General Electric Aircraft Engines CF6-45 Series (all), CF6-50 Series (all) and CF6-6 Series (all). Effective Oct 23, 2000
- [AD 2000-20-02](https://openairdocs.org/ad/2000-20-02) (historical): Turbine Nozzle Lock Assemblies · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more. Effective Oct 17, 2000
- [AD 2000-16-12](https://openairdocs.org/ad/2000-16-12) (historical): High Pressure Compressor Rotor Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Sep 5, 2000
- [AD 99-24-15](https://openairdocs.org/ad/99-24-15) (historical): High Pressure Compressor Rotor (HPCR) Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Jan 28, 2000
- [AD 99-18-20](https://openairdocs.org/ad/99-18-20) (historical): Inadvertent In-flight Thrust Reverser · General Electric Aircraft Engines CF6-50 Series (all), CF6-80A1, CF6-80A3 and 6 more. Effective Nov 2, 1999
- [AD 99-08-18](https://openairdocs.org/ad/99-08-18) (historical): General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective May 13, 1999
- [AD 95-17-15](https://openairdocs.org/ad/95-17-15) (historical): Engine Mount Pylon · General Electric Aircraft Engines CF6-45 Series (all) and CF6-50 Series (all). Effective Oct 10, 1995

All 128: https://openairdocs.org/aircraft/N303FE/ads.md

## Information bulletins (advisory) (3 in force)

- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [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-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

## NTSB investigations (1)

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

- [NTSB MIA98LA096](https://openairdocs.org/ntsb/MIA98LA096), Mar 6, 1998: Douglas DC-10-30F (N303FE), Memphis, TN, no damage. Probable cause: ground personnel (an equipment loader) failed to follow established written procedures (ramp safety policy), resulting in a pressurized entry door being opened before it was fully depressurized,…

## FAA accident and incident reports (2)

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

- [Incident 19990629019399I](https://openairdocs.org/incident/19990629019399I), Jun 29, 1999: Doug DC1010 (N303FE), Los Angeles, CA, Minor damage. (-5)On Tuesday 6/29/99, during test flight of a/c N303FE, flight crew heard a loud noise followed by airframe vibration. During post flight inspecti on, found…
- [Accident 19980306010419A](https://openairdocs.org/incident/19980306010419A), Mar 6, 1998: Doug DC1030F (N303FE), Memphis, TN. Arrived at gate not fully depressurized. Ground crew opened cargo door. Blown off lift. Depressure not full open. (.4)an equipment loader attempted to activate…

## Service difficulty reports (207, 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 FDEA202203120491](https://openairdocs.org/sdr/FDEA202203120491), Mar 12, 2022: NONE. NONE. UNSAFE GEAR WARNING DURING EXTENSION FOR ALL 4 GEAR ON PRIMARY AND SECONDARY INDICATORS. AIRSPEED AT APPROXIMATELY 190 KNOTS. RETRACTED AND FOLLOWED QRH. RECEIV
- [SDR FDEA202108212054](https://openairdocs.org/sdr/FDEA202108212054), Aug 21, 2021: O-RING. DAMAGED. PDIS 303 28-40 7724 21AUG21 IND OPEN U APPROXIMATELY 30 MIN INTO CRUISE TNK 1 FUEL QTY LO, TNK 1 TIP TRAPPED ALERTS ILLUMINATED. APPROXIMATELY 7700 LBS OF FUEL 
- [SDR FDEA202102070298](https://openairdocs.org/sdr/FDEA202102070298), Feb 7, 2021: CONNECTOR. DAMAGED. DURING COCKPIT SET UP/PREFLIGHT & AFTER APU STARTED RECIEVED FIRE WARNING TONE, LWR CARGO FIRE, FLASHING DISCHARGE LIGHTS, PUSHED DISCHARGE, AFTER 2 MIN, STILL 
- [SDR FDEA2020063081381](https://openairdocs.org/sdr/FDEA2020063081381), Jun 28, 2020: VIA. FAILED. ON TAKE OFF ROLL AT APPROX 120 KTS ALL DISPLAYS (DV'S) STARTED FLASHING EXCEPT FOR DV NR 1 (CAPTS ). TAKEOFF WAS CONTINUED & WE HAD NUMEROUS ALERTS THAT FLASHED
- [SDR FDEA202004160754](https://openairdocs.org/sdr/FDEA202004160754), Apr 16, 2020: SEAT TRACK. CORRODED. SEAT TRACK AT 1290 LBL100 HAS CORROSION REQ REPAIR. REPLACED CORRODED SEAT TRACK AT STA 1290 LBL 100 REF SRM 53-70-00 FIG 1 VOL 1.
- [SDR FDEA2020041730746](https://openairdocs.org/sdr/FDEA2020041730746), Apr 13, 2020: STRUCTURE. DAMAGED. DURING BOAT TAIL INSTALLATION, AFT SLING ATTACHMENT TO SKIN FAIRING CAP IS DAMAGED. REPAIRED DAMAGED AREA REFERENCE SRM 54-00-01 FIG. 11 SHT.1 VOL. 1 AND SRM 54
- [SDR FDEA2020041310732](https://openairdocs.org/sdr/FDEA2020041310732), Apr 11, 2020: FLOORBOARD. GOUGED. MAIN CARGO - FLOOR BOARD 233FF - GOUGE. REPAIRED FLOOR BOARD 233 FF. REF. FEDEX DRAWING SRZ-25-005
- [SDR FDEA2020040870704](https://openairdocs.org/sdr/FDEA2020040870704), Apr 7, 2020: SEAT TRACK. DAMAGED. MAIN CARGO -SEAT TRACK DAMAGED AT STA. 798 LBL 8. PERFORMED REPAIR TO SEAT TRACK REF. SRM 53-70-00 FIG. 1 SHEET 1 .VOL.1 FOR DAMAGED LOCATED AT STA 798 LBL 8 MA
- [SDR FDEA2020040100640](https://openairdocs.org/sdr/FDEA2020040100640), Mar 30, 2020: SKIN. CORRODED. MAIN CARGO DECK, STA 1241 102LBL TO 110LBL, CENTER WING UPPER SKIN CORROSION CENTRE WING TOP SKIN AT STRINGER 13, BETWEEN XCW 102 TO XCW110, CORROSION REWORK PE
- [SDR FDEA2020032760608](https://openairdocs.org/sdr/FDEA2020032760608), Mar 26, 2020: SKIN. CORRODED. SMIS 303 57-30 6345 25MAR20 MEM OPEN U MOD TYPE T MOD NO. 8-5730-T0353169 REV NO. PS P1 WING, SKIN AND PLATES: CENTER WING UPPER, CENTER SKIN PANEL, STR 14 TO S
- [SDR FDEA2020032760607](https://openairdocs.org/sdr/FDEA2020032760607), Mar 26, 2020: SKIN. CORRODED. SMIS 303 57-30 6346 25MAR20 MEM OPEN U MOD TYPE T MOD NO. 8-5730-T0353174 REV NO. PS P1 WING, SKIN AND PLATES: CENTER WING UPPER, FWD AND CENTER SKIN PANELS, ST
- [SDR FDEA2020032530602](https://openairdocs.org/sdr/FDEA2020032530602), Mar 23, 2020: SKIN. CRACKED. RIGHT CENTER LANDING GEAR DOOR AFT DOOR HAS INNER SKIN CRACK APPROX .5" JUST FWD OF THE FWD HINGE. NDT VERIFIED AND MARKED END OF THE CRACK. REMOVED AND REPLACE
- [SDR FDEA2020040890717](https://openairdocs.org/sdr/FDEA2020040890717), Mar 19, 2020: SKIN. CORRODED. MAIN CARGO DECK, CENTER WING UPPER SKIN, STA 1229 100RBL HAS CORROSION ALONG EDGE (MARKED) CENTRE WING UPPER SKIN, STRINGER 15, XCW -89 TO XCW -105, CORROSION A
- [SDR FDEA2020040890716](https://openairdocs.org/sdr/FDEA2020040890716), Mar 19, 2020: SKIN. CORRODED. MAIN CARGO DECK, CENTER WING UPPER SKIN, STA1229 88RBL TO 100RBL HAS CORROSION AROUND MARKED FASTENERS CENTRE WING UPPER SKIN, STRINGER 15, XCW -89 TO XCW -105,
- [SDR FDEA2020032980613](https://openairdocs.org/sdr/FDEA2020032980613), Mar 18, 2020: CAP. CORRODED. MAIN CARGO AFT PRESSURE BULKHEAD TEE CAP HAS A CONFIRMED CRACKED ON RADIOUS STA 2007 APPROX BETWEEN X23-X25 REMOVED AND REPLACED DAMAGED SECTION OF TEE CAP REF.
- [SDR FDEA202003270605](https://openairdocs.org/sdr/FDEA202003270605), Mar 17, 2020: FITTING. CRACKED. NLG WW RH SIDE BLKHD FITTING PN# ACA3837-2 REQUIRES FABRICATION DUE TO SHEET METAL REPAIR. REF NR# (225). INSTALLED ACA3837-2 FITTING I.A.W DWG. ACA3837. REF. N
- [SDR FDEA2020040350654](https://openairdocs.org/sdr/FDEA2020040350654), Mar 15, 2020: STRUCTURE. CORRODED. MAIN CARGO DECK, STA1227 83LBL TO 94LBL, CENTER UPPER WING SKIN HAS CORROSION (MARKED) CENTRE WING UPPER SKIN CORROSION AT STRINGER 15 BETWEEN XCW 83 TO XCW 94,
- [SDR FDEA2020040850724](https://openairdocs.org/sdr/FDEA2020040850724), Mar 15, 2020: INTERCOSTAL. CORRODED. AVIONICS COMPARTMENT AT STA 464 LBL 28. LONGITUDIONAL STIFENNER, AND WEB AATACH ANGLE CORRODED (MARKED) FABRICATED AND INSTALLED -59 INTERCOSTAL PER DWG NBA6074
- [SDR FDEA2020040840723](https://openairdocs.org/sdr/FDEA2020040840723), Mar 14, 2020: INTERCOSTAL. CORRODED. AFT AVIONIC COMPARTMENT, STA.475, LOOKING IN THRU REFRIGERATOR DOOR, L/H BILGE AREA FLOOR SUPPORT ANGLE SHOWING CORROSION.(MARKED) FABRICATED AND INSTALLED -59 
- [SDR FDEA2020040840708](https://openairdocs.org/sdr/FDEA2020040840708), Mar 14, 2020: ATTACH FITTING. CHAFED. R/H WING OUTBD SLAT #6 SLAT TRACK INBD ATTACHED FITTING IS WORN DUE TO EXCESSIVE CHAFING OF SLAT TRACK LOWER INBD RAIL. REPAIRED DAMAGED AREA BY BLENDING OUT AR
- [SDR FDEA2020040340660](https://openairdocs.org/sdr/FDEA2020040340660), Mar 14, 2020: FLOOR SUPPORT. CORRODED. MAIN CARGO COMPARTMENT UNDER FLOOR AREA, FLOOR SUPPORT BEAM CORRODED AT STATION 2006 RBL 23, VIEWED FROM AFT WASTE TANK COMPARTMENT. MARKED DOT #1. REAMOVED AND
- [SDR FDEA2020040340589](https://openairdocs.org/sdr/FDEA2020040340589), Mar 14, 2020: WEB. CRACKED. L/H NLG WHEEL WELL WEB HAS 2 EA. CRACKS AT FASTENER HOLES AT STA. 495 AND Z= -73. (MARKED) INSTALLED REPAIR DOUBLERS, FILLERS I.A.W SRM 53-30-00 FIG. 6.
- [SDR FDEA2020031940589](https://openairdocs.org/sdr/FDEA2020031940589), Mar 14, 2020: WEB. CRACKED. L/H NLG WHEEL WELL WEB HAS 2 EA. CRACKS AT FASTENER HOLES AT STA. 495 AND Z= -73. (MARKED) REPAIR CRACKED REF SRM 53-30-00 FIG. 6 VOL. 1, AND DAC DWG NCA6046.
- [SDR FDEA2020032730606](https://openairdocs.org/sdr/FDEA2020032730606), Mar 13, 2020: SUPPORT BRACKET. CRACKED. NOSE LANDING GEAR L/H RETRACT SUPPORT BRACKET LUG CRACKED. REMOVED AND REPLACED ACA007-1 FITTING REF. DAC DWG NCA6044 AND EO 8-5340-7-5000 D PT2.
- [SDR FDEA2023011620725](https://openairdocs.org/sdr/FDEA2023011620725), Mar 12, 2020: SEAT TRACK. DAMAGED. MAIN CARGO - SEAT TRACK DAMAGED AT STA.1661 LBL 106. REPAIRED SEAT TRACK DAMAGE REF: SRM 53-70-00 FIG.1 SHT.1 PG.3
- [SDR FDEA2020041020725](https://openairdocs.org/sdr/FDEA2020041020725), Mar 12, 2020: SEAT TRACK. DAMAGED. MAIN CARGO - SEAT TRACK DAMAGED AT STA.1661 LBL 106. REPAIRED SEAT TRACK DAMAGE REF: SRM 53-70-00 FIG.1 SHT.1 PG.3
- [SDR FDEA2020031920588](https://openairdocs.org/sdr/FDEA2020031920588), Mar 12, 2020: BULKHEAD. CRACKED. NOSE LANDING GEAR WHEELWELL; X= -24 Y= 494 Z= -58 HAS 2EA. 1" CRACKS @ ADJACENT FASTENERS ON BULKHEAD. REPAIR CRACKED REF SRM 53-30-00 FIG. 6 VOL. 1, AND DAC DW
- [SDR FDEA2020031920587](https://openairdocs.org/sdr/FDEA2020031920587), Mar 12, 2020: BULKHEAD. CRACKED. NOSE LANDING GEAR WHEELWELL; X= -24 Y= 486 Z= -48 2" CRACK ON BULKHEAD. REPAIR CRACKED REF SRM 53-30-00 FIG. 6 VOL. 1, AND DAC DWG NCA6046. INSTALLED REPAIR DOU
- [SDR FDEA2020040810713](https://openairdocs.org/sdr/FDEA2020040810713), Mar 11, 2020: WEB. CORRODED. LH WHEEL WELL - WEB (P/N AEA0026-5) BETWEEN STA 1501 - 1521 IS CORRODED. (AREA MARKED) REMOVED AND REPLACED WITH FABRICATED PART FX AEA0026-5 PER DWG AEA0026 AN
- [SDR FDEA2020031910585](https://openairdocs.org/sdr/FDEA2020031910585), Mar 11, 2020: BULKHEAD. CRACKED. NLG WHEEL WELL RH BULKHEAD -Y= 24, APPROX STA. 470 AND 476, -X= 41. TWO 6" INCH CRACKS. REPAIR CRACKED REF SRM 53-30-00 FIG. 6 VOL. 1. AND DAC DWG NCA6046. INST
- [SDR FDEA2020042390766](https://openairdocs.org/sdr/FDEA2020042390766), Mar 9, 2020: STIFFENER. CRACKED. AFT BULKHEAD TAIL CONE AT UPPER R/H SUPPORT STIFFNER (3RD FROM THE TOP, MARKED IN RED) O/B IS CRACKED. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR HAT CHANNEL 
- [SDR FDEA2020032590603](https://openairdocs.org/sdr/FDEA2020032590603), Mar 9, 2020: DOUBLER. GOUGED. FWD CARGO CUT-OUT - LOWER AFT CORNER - DOUBLER/TRIPLER GOUGED. REMOVED DAMAGED DOUBLERS AND REPLACED WITH NEW DOUBLERS,REF SRM 53-50- 00,FIG26.
- [SDR FDEA2020012750228](https://openairdocs.org/sdr/FDEA2020012750228), Jan 25, 2020: VALVE. MALFUNCTIONED. PDIS 303 28-43 6202 25JAN20 LIT OPEN U LOGPAGES:3213631 "TNK 1 TIP TRAPPED" AT FL350 FOR 3 MINUTS. ALERT CLEARED ITSELF, THEN RETURNED CAUSING DIVERT INTO KLIT 
- [SDR FDEA201910302785](https://openairdocs.org/sdr/FDEA201910302785), Oct 30, 2019: SWITCH. DEFECTIVE. IN CLT DURING TAXI "DOOR DISARMED" LIGHT ON PANEL TO THE RIGHT SIDE OF THE R1 DOOR ILLUMINATED. ALL DOORS SHOWED CLOSED IN COCKPIT, AND DOOR LEVER WAS IN THE "S
- [SDR FDEA201910212728](https://openairdocs.org/sdr/FDEA201910212728), Oct 21, 2019: SKIN. DAMAGED. AIRCRAFT FUSELAGE STRUCK BY CONTAINER DURING STORM, LEAVING HOLE IN SKIN JUST FORWARD AND BELOW BULK CARGO DOOR. INSTALLED REPAIR REF MD-10 SRM 53-20-00 FIG 6 A
- [SDR FDEA201907261702](https://openairdocs.org/sdr/FDEA201907261702), Jul 26, 2019: UNKNOWN. SMOKE. PDIS 303 21-10 5616 25JUL19 MCI OPEN U LOGPAGES:3142593 TURNED ON #2 PACK IN CRUISE. GOT SMOKE IN COCKPIT ONLY, TURNED #2 PACK OFF SMOKE DISSIPATED. MEL 26JUL19
- [SDR FDEA201907211649](https://openairdocs.org/sdr/FDEA201907211649), Jul 21, 2019: POWER SUPPLY. FAILED. MDIS 303 33-50 5599 21JUL19 JFK OPEN U ON PRE-FLIGHT CHKS "EMER LT BAT 1 LO" DISPLAYED DURING EMERGENCY LIGHT TEST. MEL 21JUL19 10:27 JFK U RELEASED FOR SERVICE
- [SDR FDEA201902120413](https://openairdocs.org/sdr/FDEA201902120413), Feb 12, 2019: HINGE. CRACKED. RIGHT MAIN GEAR DOOR CENTER HINGE CRACKED. REMOVED AND RE3PLACED DOOR HINGE AND INTERNAL TEE FITTINGS AND INSTALLED GEAR DOOR PAN REPAIR UISNG REF MD10 SRM 52-1
- [SDR FDEA201806201548](https://openairdocs.org/sdr/FDEA201806201548), Jun 20, 2018: WIRE. DAMAGED. EMER LIGHTS BAT 1 LO ALERT. FOUND DAMAGED WIRE AT P1-1756A PIN 1 GND CAUSING ONLY 64 VAC TO PIN 6 CHARGING POWER. REPAIRED WIRE GND AT PIN 1 CKS GOOD AS WELL AS
- [SDR FDEA2018052301266](https://openairdocs.org/sdr/FDEA2018052301266), May 20, 2018: POWER SUPPLY. FAILED. EMERGENCY LIGHT BATTERY 1 LOW ALERT. REPLACED THE POWER SUPPLY. OPS CHECKED GOOD.
- [SDR FDEA2018042601111](https://openairdocs.org/sdr/FDEA2018042601111), Apr 24, 2018: SKIN. CRACKED. LEFT INBD UPPER SURFACE CRACKED ON OTBD TRIM AT XIFH 310. REMOVED AND REPLACED THE SKIN IAW DWG ARC 2443, ZONE 8.
- [SDR FDEA201804171037](https://openairdocs.org/sdr/FDEA201804171037), Apr 17, 2018: SKIN. CRACKED. LEFT INBD FLAP UPPER SKIN CRACKED ON OUTBD TRIM AT XIFH 310. REMOVED & INSTALLED A FABRICATED OUTBD TRIM SKIN IAW SRM 57-52-01, FIG 1, PAGE 1 VOL I, DRAWINGS AR
- [SDR FDEA2018042601102](https://openairdocs.org/sdr/FDEA2018042601102), Apr 12, 2018: SEAT TRACK. CORRODED. MAIN DECK BS 1753, RBL 107 SEAT TRACK FLANGE HAS CORROSION. INSTALLED A NEW SEAT TRACK AND SPLICES IAW SRM 53-70-00, FIG 1, SHEET 1, VOL 1, DWG SR10-53-002, SRM
- [SDR FDEA201804121076](https://openairdocs.org/sdr/FDEA201804121076), Apr 12, 2018: SEAT TRACK. CORRODED. MAIN DECK, BS 1759, RBL 107 SEAT TRACK FLANGE HAS CORROSION. INSTALLED A NEW SEAT TRACK AND SPLICE IAW SRM 53-70-00, FIG 1, SHEET 1, VOL 1, DWG SR10-53-002, SRM
- [SDR FDEA201804121075](https://openairdocs.org/sdr/FDEA201804121075), Apr 12, 2018: SEAT TRACK. CORRODED. MAIN DECK, BS 1738, RBL 107 SEAT TRACK FLANGE HAS CORROSION. INSTALLED A NEW SEAT TRACK AND SPLICE IAW SRM 53-70-00, FIG 1, SHEET 1, VOL 1, DWG SR10-53-002, SRM
- [SDR FDEA201804111074](https://openairdocs.org/sdr/FDEA201804111074), Apr 11, 2018: SEAT TRACK. CORRODED. MAIN DECK, BS 1681, RBL 107 SEAT TRACK FLANGE HAS CORROSION. INSTALLED A NEW SEAT TRACK AND SPLICES IAW SRM 53-70-00, FIG 1, SHEET 1, VOL 1, DWG SR10-53-002, SR
- [SDR FDEA201804080998](https://openairdocs.org/sdr/FDEA201804080998), Apr 8, 2018: STOP FITTING. CRACKED. NR 3 ACM DOOR FRAME STOP FITTING HAS A .250 INCH CRACK. REPAIRED STOP FITTING IAW SRM 53-00-01, FIG 2, SHEET 2, VOL 1, AND EA.
- [SDR FDEA201804070997](https://openairdocs.org/sdr/FDEA201804070997), Apr 7, 2018: HINGE. CRACKED. NR 3 PACK DOOR AFT HINGE CRACKED. REPAIRED IAW SRM 53-00-01, FIG 2, PAGE 15, VOL 1, AND EA.
- [SDR FDEA201804070918](https://openairdocs.org/sdr/FDEA201804070918), Apr 7, 2018: SHEAR TIE. CORRODED. AFT CARGO BAY, BS 1967, LONGERON 48L SHEAR TIE CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW DWG AGA7058.
- [SDR FDEA201804051100](https://openairdocs.org/sdr/FDEA201804051100), Apr 5, 2018: SEAT TRACK. CORRODED. MAIN CABIN BS 1761 - 1741 BETWEEN RBL 47 - 74, CORROSION FOUND ON THE SEAT TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-70-00, VOL 1, FIG 1, PAGE 3.

All 207: https://openairdocs.org/aircraft/N303FE/reports.md

## STCs that may be installed (OpenAirDocs) (73, 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 (Mcdonnell Douglas MD-10-30F)

- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST01391LA](https://openairdocs.org/stc/ST01391LA): Installation of a reinforced cockpit door. Safran Cabin 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 ST02184CH](https://openairdocs.org/stc/ST02184CH): Installation of elementary or enhanced surveillance Mode S transponders. Amphenol Cable and Interconnect Technologies Inc
- [STC ST02002WI](https://openairdocs.org/stc/ST02002WI): Replacement of Rockwell Collins LRA-900 Low Range Radio Altimeters with upgraded LRA-900 units for improved RF immunity to 5G cellular data interference. Rockwell Collins, Inc
- [STC ST03367AT](https://openairdocs.org/stc/ST03367AT): Installation of dual Artex Model C406-N Emergency Locator Transmitters (ELT). Woven Electronics LLC
- [STC ST00536SE](https://openairdocs.org/stc/ST00536SE): Installation of the Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS). Honeywell International Inc
- [STC ST02126AT](https://openairdocs.org/stc/ST02126AT): Courier seat installation. GDC Technics LLC
- [STC ST03879AT](https://openairdocs.org/stc/ST03879AT): Installation of Talon Aerospace Cargo Lights. Aaxico Technical Services Inc
- [STC ST03574AT](https://openairdocs.org/stc/ST03574AT): Installation of a Talon Aerospace Anti-Collision Light. Aaxico Technical Services Inc
- [STC ST04002AT](https://openairdocs.org/stc/ST04002AT): Installation of a Talon LED Replacement Wing and Tail Mounted Anti-Collision Lights. 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 ST02532LA](https://openairdocs.org/stc/ST02532LA): Modify the wing fuel tanks access cover installation by replacing the existing rubstrip and seal with a new encapsulated wire mesh gasket and a new seal. Aviation Devices & Electronic Components LLC
- [STC ST02669LA](https://openairdocs.org/stc/ST02669LA): Installation of Honeywell MKV EGPWS with Landing Performance Enhancement (LPE) functionality. Honeywell International Inc
- [STC ST00349LA](https://openairdocs.org/stc/ST00349LA): Installation of cargo handling system. Ancra International LLC
- [STC ST01805WI](https://openairdocs.org/stc/ST01805WI): Modification of Rockwell Collins TCAS II System Installation with DC powered TCAS Transmitter Receiver Processor. Rockwell Collins Inc
- [STC ST00399DE](https://openairdocs.org/stc/ST00399DE): Installation of nose radome shell assembly. The NORDAM Group LLC
- [STC ST00687AT-D](https://openairdocs.org/stc/ST00687AT-D): Interior Reconfiguration. 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 ST04323CH](https://openairdocs.org/stc/ST04323CH): 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 ST03967AT](https://openairdocs.org/stc/ST03967AT): Installation of an Avionica, Inc. avWiFi wireless router system. Archeion Holdings LLC
- [STC ST04376AT](https://openairdocs.org/stc/ST04376AT): Installation of a Cobham INMARSAT/SwiftBroadband SATCOM System. Avionics Support Group Inc
- [STC ST01289LA](https://openairdocs.org/stc/ST01289LA): Insulation Blankets Installation. Lamart California Inc
- [STC ST02406LA](https://openairdocs.org/stc/ST02406LA): Installation of TCAS version 7.1. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST02599LA](https://openairdocs.org/stc/ST02599LA): Installation of Oxygen Aneroid Switch P/N 44A3-4 for aircraft to be used for high altitude airports. AeroSys Inc
- [STC ST02580LA](https://openairdocs.org/stc/ST02580LA): Reconfigure an MD-10-30F to support a modular eye hospital with 48 supernumeries. ORBIS International Inc
- [STC ST02589LA](https://openairdocs.org/stc/ST02589LA): Installation of main deck cargo loading system. Ancra International LLC
- [STC ST00864LA](https://openairdocs.org/stc/ST00864LA): Modification of existing Litton LTN-72R Inertial navigation system to include VOR/DME RNAV updating. Northrop Grumman Systems Corporation
- [STC ST02540LA](https://openairdocs.org/stc/ST02540LA): Installation of Telair International LLC light weight P/Ns PMC100 and PAG100 series cargo pallets. Telair International LLC
- [STC SA5466NM](https://openairdocs.org/stc/SA5466NM): Installation of Telair International cargo loading systems. Telair International LLC
- [STC ST01347LA](https://openairdocs.org/stc/ST01347LA): Installation of a lower lobe anti-rollout latch Telair part number 92036-1, -2. Telair International LLC
- [STC ST02489LA](https://openairdocs.org/stc/ST02489LA): Installation of Telair International Inc. light weight LD3 (NAS3610 / SAE36100 - 2K2) cargo container P/N LD3100-31000ZZZ. Telair International LLC
- [STC ST04214AT](https://openairdocs.org/stc/ST04214AT): Installs a standalone Astronics AES 110V AC 60 Hz and 5V DC power system with two outlets in the cockpit. FedEx Express
- [STC SA3892WE](https://openairdocs.org/stc/SA3892WE): Installation of Stowe Corp. service carts. Driessen Aircraft Interior Systems, Inc DBA Zodiac Galleys USA Inc
- [STC ST03327AT](https://openairdocs.org/stc/ST03327AT): Installation of a Dual NavAero Class 2 Electronic Flight Bags (EFB) . Avionics Support Group Inc
- [STC ST03483AT](https://openairdocs.org/stc/ST03483AT): Installation of a Portable Beverage Dispensing System, P/N B43-FA-001. Dynamo Beverage Company, USA, L.L.C
- [STC ST00503LA](https://openairdocs.org/stc/ST00503LA): Installation of Securaplane Model No. BC-1302 Battery Charger, Battery Temperature Sensor Model No. BTS-1302 and Remote Display Unit Model No. DU-1302 as a form, fit, and functional replacement for the existing General Electric Battery Charger System. Securaplane Technologies
- [STC ST02050LA](https://openairdocs.org/stc/ST02050LA): Installation of Goodrich-Hella Anticollision Recognition Lighting System (ARLS). Goodrich
- [STC SA5016NM](https://openairdocs.org/stc/SA5016NM): Installation of cargo containers. Satco Inc
- [STC ST03557AT](https://openairdocs.org/stc/ST03557AT): Installation of a Honeywell head up display and a Kollsman infrared enhanced flight vision system (HUD/EFVS). Federal Express Corp
- [STC ST09368SC](https://openairdocs.org/stc/ST09368SC): Installation of a supplemental crew oxygen system. Schwartz Aviation LLC
- [STC SA3415NM](https://openairdocs.org/stc/SA3415NM): Installation of a main cabin cargo handling system. Ancra International LLC
- [STC SA5003NM](https://openairdocs.org/stc/SA5003NM): Installation of a cabin cargo handling system. Ancra International LLC
- [STC ST03944AT](https://openairdocs.org/stc/ST03944AT): Installation of Avionica, Inc. satLINK System to provide voice and short burst data communications over the Iridium satellite Communications network (SATCOM), with Wi-Fi voice over IP (VoIP) cordless phone in accordance with Archeion Holdings LLC Master Data List 102810-MDL, Revision D, Dated January 17, 2012, or later FAA approved revisions. Archeion Holdings LLC
- [STC ST01338CH](https://openairdocs.org/stc/ST01338CH): Installation of an Auxiliary Power Unit Door Actuator System. Woodward MPC
- [STC ST02540AT-D](https://openairdocs.org/stc/ST02540AT-D): Installation of replacement fuel tank sealant system. FFC Manufacturing
- [STC ST00688AT-D](https://openairdocs.org/stc/ST00688AT-D): Sony Transcom Video Monitor Installation. TIMCO
- [STC ST03662AT](https://openairdocs.org/stc/ST03662AT): Installation of an L-3 Communications FA2100CVR Cockpit Voice Recorder. Chippewa Aerospace, Inc

All 73: https://openairdocs.org/aircraft/N303FE/stcs.md

## Related

- Other Mcdonnell Douglas MD-10-30F aircraft: https://openairdocs.org/model/mcdonnell-douglas-md-10-30f/aircraft.md
- The GE CF6-50 series engine: https://openairdocs.org/engine/ge-cf6-50-series.md

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