# N304FE: 1978 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 CF6-50C2](https://openairdocs.org/engine/ge-cf6-50c2) (registry code 30085)
- 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: 46992
- Year built: 1978
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 28, 2007
- Certificate issued: July 2, 1984
- Expires: November 30, 2027
- Mode S code: A32EB0
- 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=304FE
- Page: https://openairdocs.org/aircraft/N304FE

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): 96 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 CF6-50C2)

- [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 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 2000-20-02](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 99-08-18](https://openairdocs.org/ad/99-08-18) (historical): General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective May 13, 1999

All 122: https://openairdocs.org/aircraft/N304FE/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 ENG12IA012](https://openairdocs.org/ntsb/ENG12IA012), Feb 13, 2012: Mcdonnell Douglas MD-10-30F (N304FE), Portland, OR, incident, minor damage. Probable cause: The fracture of the fan mid shaft due to a stress corrosion cracking initiated by local regions of corrosion pitting, which resulted from oil migration within the shaft and its subsequent degradation.

## FAA accident and incident reports (1)

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 20060328008509I](https://openairdocs.org/incident/20060328008509I), Mar 28, 2006: Doug DC1030F (N304FE), Newark, NJ, Minor damage. (-23) Operator maintenance control center at oak, notified the FAA that upon landing, maintenance personnel performing their post flight walk-around…

## Service difficulty reports (283, 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 FDEA202206221509](https://openairdocs.org/sdr/FDEA202206221509), Jun 22, 2022: HYDRAULIC SYSTEM. FAILED. 2 00 INTO FLIGHT WE RECEIVED A LEVEL 1 HYD 3 ELEV OFF ALERT. COMPLIED WITH THE QRH AND NOTICED SYSTEM 3 QUANTITY DECREASING THROUGH 4.0. WE PREEMPTIVELY COMPLET
- [SDR FDEA2020090942146](https://openairdocs.org/sdr/FDEA2020090942146), Sep 4, 2020: SEAT TRACK. WORN. MAIN CABIN BETWEEN STATIONS 1441 AND 1561 AT LBL 42 SEAT TRACK NEEDS TO BE REPLACED DUE TO CARGO SYSTEM WILL NOT LINE UP. R & R SEAT TRACK SECTION, PER SRM 53-7
- [SDR FDEA2020090922123](https://openairdocs.org/sdr/FDEA2020090922123), Sep 4, 2020: SEAT TRACK. CRACKED. MAIN DECK STA: 1265 RBL 8 SEAT TRACK IS CRACKED, MARKED YELLOW DOT. R & R SEAT-TRACK SECTION, PER SRM 53-70-00 FIG 1A DWG SR10-53-010.
- [SDR FDEA202008192034](https://openairdocs.org/sdr/FDEA202008192034), Aug 19, 2020: WEB. CRACKED. LT OBSERVER'S SEAT FLOOR LIGHTNING HOLE HAS 1/2 INCH CRACK, MARKED. REPAIRED PER SRM 53-60-01 FIG 4 SHT 1 AND EA.8-5320-T0356129.
- [SDR FDEA2020082651894](https://openairdocs.org/sdr/FDEA2020082651894), Aug 14, 2020: SEAT TRACK. CORRODED. MAIN CARGO DECK, APPROX STA. 1210, RBL 10, SEAT TRACK FLOOR BOARD FASTENER HOLE LIGHT CORROSION. MARKED RED GREASE PENCIL. 0000309500 : BARNETT, HARRY H - 22-AU
- [SDR FDEA2020081851894](https://openairdocs.org/sdr/FDEA2020081851894), Aug 14, 2020: SEAT TRACK. CORRODED. MAIN CARGO DECK, APPROX STA. 1210, RBL 10, SEAT TRACK FLOOR BOARD FASTENER HOLE LIGHT CORROSION.
- [SDR FDEA2020082061945](https://openairdocs.org/sdr/FDEA2020082061945), Aug 6, 2020: SUPPORT ANGLE. DAMAGED. FORMER ANGLE P/N ARB1163-21 HAS (3) ELONGATED HOLES CLOSE TO RADIUS OF ANGLE. FS,LE @ STA. XOS 667.67. REF:NR00169 FOR MATING PARTS INSTALLATION. REPLACED DAMAG
- [SDR FDEA2020081041833](https://openairdocs.org/sdr/FDEA2020081041833), Aug 4, 2020: FLOORBEAM. CORRODED. BS 458, RBL 12 - 27, FLOORBEAM HAD CORROSION. REMOVED AND REPLACED IAW DWG ABA7425, AND NBA6018. MAJOR REPAIR.
- [SDR FDEA202007302007](https://openairdocs.org/sdr/FDEA202007302007), Jul 30, 2020: DOOR FRAME. CORRODED. FWD CARGO DOOR NR 1 LATCH SPOOL DOOR JAMB HOLES ARE CORROSION REPAIRED PER EA. 8-5350-T0356071.
- [SDR FDEA202007301730](https://openairdocs.org/sdr/FDEA202007301730), Jul 30, 2020: FLOOR PANEL. DAMAGED. FLOOR PANEL 283CF IN AFT PASSENGER COMPARTMENT AFT SECTION IS MISSING SEVERAL INSERTS. REPLACED THE MISSING INSERTS IAW DWG SRZ-25-005.
- [SDR FDEA2020081271716](https://openairdocs.org/sdr/FDEA2020081271716), Jul 25, 2020: FLOORBEAM. CRACKED. AFT CARGO BILGE, CRACK ON FLOOR SUPPORT ANGLE AT FWD BLKHD, STA 1786 APPROX LBL 10 REMOVED AND REPALCED FLOOR SUPPORT ANGLE AT STA 1786 LBL 10 REF SRM 51-35-01 
- [SDR FDEA2020073051716](https://openairdocs.org/sdr/FDEA2020073051716), Jul 25, 2020: ANGLE. CRACKED. AFT CARGO BILGE, CRACK ON FLOOR SUPPORT ANGLE AT FWD BULKHEAD, BS 1786, LBL 10.
- [SDR FDEA2020081271773](https://openairdocs.org/sdr/FDEA2020081271773), Jul 23, 2020: FLOORBEAM. CORRODED. MAIN DECK STA.421, RBL 6 TO RBL 24, FLOORBEAM HAD LIGHT SURFACE CORROSION AT SEVERAL AREA AROUND NUT PLATES REMOVED & REPLACED FLOOR SUPPORT IAW DWG NBA 6022.
- [SDR FDEA2020081271715](https://openairdocs.org/sdr/FDEA2020081271715), Jul 23, 2020: FLOORBEAM. CRACKED. AFT CARGO BILGE, CRACK AND CORROSION ON FLOOR SUPPORT ANGLE AT FWD BLKHD STA 1786 RBL 24. REMOVED AND REPALCED FLOOR SUPPORT ANGLE AT STA 1786 RBL 24 REF SRM 51
- [SDR FDEA2020081271714](https://openairdocs.org/sdr/FDEA2020081271714), Jul 23, 2020: FLOORBEAM. CRACKED. AFT CARGO BILGE, CRACK AND CORROSION ON FLOOR SUPPORT ANGLE AT FWD BLKHD STA 1786 LBL 12. REMOVED AND REPALCED FLOOR SUPPORT ANGLE AT STA 1786 LBL 12 REF SRM 51
- [SDR FDEA2020081271713](https://openairdocs.org/sdr/FDEA2020081271713), Jul 23, 2020: ANGLE. CRACKED. AFT CARGO BILGE, CRACK ON FLOOR SUPPORT ANGLE AT FWD BLKHD STA 1786 LBL24. REMOVED AND REPALCED FLOOR SUPPORT ANGLE AT BS 1786 LBL 24 IAW SRM 51-35-01 VOL 2, DW
- [SDR FDEA2020080721773](https://openairdocs.org/sdr/FDEA2020080721773), Jul 23, 2020: FLOORBEAM. CORRODED. MAIN DECK STA.421, RBL 6 TO RBL 24, FLOOR SUPPORT, LIGHT SURFACE CORROSION AT SEVERAL AREA AROUND NUT PLATES REMOVED AND REPLACED SEAT-TRACK SRM 53-70-00 FIG 1A
- [SDR FDEA2020073001715](https://openairdocs.org/sdr/FDEA2020073001715), Jul 23, 2020: ANGLE. CRACKED. AFT CARGO BILGE, CRACK AND CORROSION ON FLOOR SUPPORT ANGLE AT FWD BULKHEAD BS 1786, RBL 24.
- [SDR FDEA2020073031714](https://openairdocs.org/sdr/FDEA2020073031714), Jul 23, 2020: ANGLE. CRACKED. AFT CARGO BILGE, CRACK AND CORROSION ON FLOOR SUPPORT ANGLE AT FWD BULKHEAD BS 1786, LBL 12.
- [SDR FDEA2020073031713](https://openairdocs.org/sdr/FDEA2020073031713), Jul 23, 2020: ANGLE. CRACKED. AFT CARGO BILGE, CRACKED FLOOR SUPPORT ANGLE AT FWD BULKHEAD, BS 1786, LBL24.
- [SDR FDEA2020073021698](https://openairdocs.org/sdr/FDEA2020073021698), Jul 22, 2020: FLOORBEAM. CRACKED. CENTER CARGO COMPT FLOORBOARD SUPPORT BRACKET CRACKED AT FASTENER HOLE. MRKD STA 1601 RBL 18. REMOVED DAMAGED FLOOR BOARD SUPPORT & REPLACED WITH FAB FLOOR BEAM
- [SDR FDEA202008101644](https://openairdocs.org/sdr/FDEA202008101644), Jul 21, 2020: FLOOR PANEL. DELAMINATED. MAIN DECK, BS 799 - 840, FLOOR PANEL WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. MAJOR REPAIR
- [SDR FDEA202007211645](https://openairdocs.org/sdr/FDEA202007211645), Jul 21, 2020: FLOOR PANEL. DELAMINATED. MAIN DECK, FLOOR PANEL WAS DELAMINATED BS 840 - 879. FABRICATED A NEW MAIN DECK FLOOR PANEL IAW DWG SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA2020072411644](https://openairdocs.org/sdr/FDEA2020072411644), Jul 21, 2020: FLOOR PANEL. DELAMINATED. MAINDECK, APPROX STA. 799 THRU 840 CTR PANEL IS DELAM. FABRICATED NEW CENTER FLOOR PANEL, STA 799 - STA 840, REF DWG SRZ-25-005.
- [SDR FDEA2020081201865](https://openairdocs.org/sdr/FDEA2020081201865), Jul 20, 2020: SKIN. DAMAGED. UPPER CARGO DOOR JAMB, FUSELAGE SKIN DAMAGED AT FWD LWR AREA REAIRED PER SRM 53-50-00 FIG.026
- [SDR FDEA202007191774](https://openairdocs.org/sdr/FDEA202007191774), Jul 19, 2020: RIB. CRACKED. LT WING FIXED LEADING EDGE RIB CRACKED. MARKED 3 RIBS OUTBOARD OF SLAT TRACK NR 14. REPAIRED CRACKS AT NLG WHEEL WELL LT FWD UPPER BULKHEAD ON UPPER CAP AREA BE
- [SDR FDEA202007191944](https://openairdocs.org/sdr/FDEA202007191944), Jul 19, 2020: DOUBLER. CRACKED. LH WING FIXED L/E RIB CRACKED. MRKD O/B OF SLAT TRACK #10. REPLACED/FABRICATED ARB3954-5 DOUBLER. DOUBLER REF: ARB3954 DAC DRAWING. REF. PART MATES WITH ARB2930
- [SDR FDEA2020080791774](https://openairdocs.org/sdr/FDEA2020080791774), Jul 19, 2020: WEB. CRACKED. CRACKS AT NLG WHEEL WELL LT FWD UPPER BULKHEAD ON UPPER CAP AREA BEHIND THE HYD LINES AT APPROX STA 490. REPAIRED IAW SRM 53-30-00, VOL 1, FIG 6, SHEET 2, PAGE 
- [SDR FDEA2020080591737](https://openairdocs.org/sdr/FDEA2020080591737), Jul 19, 2020: SKIN. CRACKED. R/H LOWER WING SKIN AT #12 SLAT TRACK AFT OUTBOARD CORNER HAS A .100 IN. CRACK. (MARKED) 0000721523 : COLON, LUIS R - 31-JUL-2020 18:44 REPAIRED R/H LOWER WING 
- [SDR FDEA2020080391737](https://openairdocs.org/sdr/FDEA2020080391737), Jul 19, 2020: SKIN. CRACKED. RIGHT LOWER WING SKIN AT THE NR 12 SLAT TRACK, AFT OUTBOARD CORNER HAD A .100 IN. CRACK. REPAIRED THE RT LOWER WING SKIN IAW SRM 57-10-00, VOLUME 1, FIGURE 68, 
- [SDR FDEA202007181590](https://openairdocs.org/sdr/FDEA202007181590), Jul 18, 2020: FLOORBOARD. GOUGED. MAIN CARGO DECK FLOOR BOARD AT APPROX STA 680 & CENTER PANEL BETWEEN LBL 8.50-RBL 8.50 TOP SURFACE HAS SEVERAL GOUGES, MARKED. FABRICATED FLOORBOARD, PER SRZ 25
- [SDR FDEA202007181691](https://openairdocs.org/sdr/FDEA202007181691), Jul 18, 2020: SEAT TRACK. WORN. MAIN CARGO DECK AT APPROX STA 640 & RBL 47.50 SEAT TRACK WORN. THE SEAT TRACK WAS REPAIRED IAW SRM 53-70-00.FIG.1,VOL.1.
- [SDR FDEA202008120621](https://openairdocs.org/sdr/FDEA202008120621), Jul 18, 2020: SEAT TRACK. WORN. MAIN CARGO DECK AT APPROX STA 1633 & RBL 47 SEAT TRACK WORN (MARKED) INSTALLED SPLICE SEAT-TRACK PER SRM 53-42-01 FIG 4
- [SDR FDEA2020081011711](https://openairdocs.org/sdr/FDEA2020081011711), Jul 18, 2020: FLOORBOARD. GOUGED. MAIN CARGO DECK FLOORBOARD AT BS 755 & BETWEEN LBL 8.50 - RBL 8.50, TOP SURFACE WAS GOUGED. REPAIRED THE FLOORBOARD IAW SRM 53-60-00, FIG. 6, PG. 6. MAJOR REPAI
- [SDR FDEA2020081081710](https://openairdocs.org/sdr/FDEA2020081081710), Jul 18, 2020: FLOOR PANEL. DAMAGED. MAIN CARGO DECK FLOOR BOARD PANEL AT BS 790 & BETWEEN LBL 107.25 - LBL 75.25, TOP SURFACE WAS GOUGED. REPAIRED THE FLOOR PANEL IAW SRM 53-60-00, FIG 6, PG 6. MA
- [SDR FDEA2020080701781](https://openairdocs.org/sdr/FDEA2020080701781), Jul 18, 2020: BULKHEAD WEB. CRACKED. NLG WHEEL WELL L/H FWD UPPER BULKHEAD CRACKED ON UPPER CAP AREA JUST BHIND THE HYDRO LINES AT APPROX. STA 490. (DOT 5) 0005082863 : ROBLES, VICTOR R - 06-AUG-20
- [SDR FDEA202008071772](https://openairdocs.org/sdr/FDEA202008071772), Jul 18, 2020: SEAT TRACK. WORN. MAIN CARGO DECK AT APPROX STA 1780 & LBL 28 SEAT TRACK WORN (MARKED) REPAIRED SEAT TRACK REF. SRM53-70-00 VOL.1
- [SDR FDEA2020080581768](https://openairdocs.org/sdr/FDEA2020080581768), Jul 18, 2020: SEAT TRACK. CORRODED. MAIN CARGO DECK AT APPROX STA 930-920 & RBL 47.50 SEVERAL SEAT TRACK WORN (MARKED) 0000456493 : DEMARTI, SEAN E - 29-JUL-2020 19:19 REMOVED DAMAGED SEAT TRACK S
- [SDR FDEA2020080581767](https://openairdocs.org/sdr/FDEA2020080581767), Jul 18, 2020: SEAT TRACK. WORN. MAIN CARGO DECK AT APPROX STA 1465 & LBL 47.50 SEAT TRACK WORN (MARKED) REPAIRED SEAT-TRACK PER SRM 53-70-00 FIG 1A
- [SDR FDEA2020073081711](https://openairdocs.org/sdr/FDEA2020073081711), Jul 18, 2020: FLOOR PANEL. WORN. MAIN CARGO DECK FLOOR BOARD PANEL AT APPROX STA 755 & (CNTR PANEL) BTWN LBL 8.50 - RBL 8.50 TOP SURFACE HAS SEVERAL GOUGES. REPAIRED DAMAGE TO MAIN CARGO DECK C
- [SDR FDEA2020073081710](https://openairdocs.org/sdr/FDEA2020073081710), Jul 18, 2020: FLOORBOARD. DAMAGED. MAIN CARGO DECK FLOORBOARD AT APPROX STA 790 & (LH OUTBOARD PANEL) BTWN LBL 107.25 - LBL 75.25 TOP SURFACE HAS A GOUGE. REPAIRED MAIN CARGO DECK FLOOR PANEL GOU
- [SDR FDEA2020073081709](https://openairdocs.org/sdr/FDEA2020073081709), Jul 18, 2020: SEAT TRACK. WORN. MAIN DECK SEAT TRACK WORN BEYOND LIMITS @ STA-959 LBL-47...(MRK) REPAIRED DAMAGED SECTION OF SEAT TRACK LBL 47, STA 949 TO 1159 REF SRM 53-70-00 FIG 1 SHT 1 VOL
- [SDR FDEA2020073081695](https://openairdocs.org/sdr/FDEA2020073081695), Jul 18, 2020: SEAT TRACK. WORN. MAIN CARGO DECK AT APPROX STA 1653 & LBL 8.50 SEAT TRACK WORN (MARKED) REPAIRED SEAT TRACK AT STA 1641-1661 LBL 8.5 PER SRM 53-70-00 FIG 1 SHT 1 VOL1.
- [SDR FDEA2020073081693](https://openairdocs.org/sdr/FDEA2020073081693), Jul 18, 2020: SEAT TRACK. WORN. MAIN CARGO DECK AT APPROX STA 1360 & LBL 47.50 SEAT TRACK WORN (MARKED) REMOVED AND REPLACED DAMAGE SECTION OF SEAT FROM STA 1360 THRU 1440 AT LBL 47.5, PER SRM
- [SDR FDEA2020073081691](https://openairdocs.org/sdr/FDEA2020073081691), Jul 18, 2020: SEAT TRACK. WORN. MAIN CARGO DECK AT APPROX STA 640 & RBL 47.50 SEAT TRACK WORN. INSTALLED SEAT-TRACK SPLICE PER SRM 53-70-00 FIG 1A.
- [SDR FDEA2020072781675](https://openairdocs.org/sdr/FDEA2020072781675), Jul 18, 2020: SEAT TRACK. WORN. MAIN CARGO DECK AT APPROX BS 700 & RBL 47.50, SEAT TRACK WORN. INSTALLED SPLICE SEAT TRACK IAW SRM 53-70-00, FIG 1A.
- [SDR FDEA202007181595](https://openairdocs.org/sdr/FDEA202007181595), Jul 18, 2020: FLOORBOARD. DELAMINATED. MAIN DECK FLOOR PANELS, FLOORBOARD 231HF IS DELAMINATED AND HAS ANTI-SKID TAPE MISSING. FABRICATED NEW MAIN DECK FLOOR PANEL 231HF, REF DWG SRZ-25-005. MAJOR RE
- [SDR FDEA202007181593](https://openairdocs.org/sdr/FDEA202007181593), Jul 18, 2020: FLOORBOARD. DELAMINATED. MAIN CARGO DECK FLOORBOARD AT APPROX BS 780 & (CNTR PANEL) BETWEEN LBL 8.50 - RBL 8.50, THE TOP SURFACE HAD SEVERAL GOUGES. REPAIRED THE MAIN DECK FLOOR PANEL I
- [SDR FDEA2020072381590](https://openairdocs.org/sdr/FDEA2020072381590), Jul 18, 2020: FLOORBOARD. GOUGED. MAIN CARGO DECK FLOOR BOARD AT APPROX STA 680 & (CNTR PANEL) BTWN LBL 8.50 - RBL 8.50 TOP SURFACE HAS SEVERAL GOUGES (MARKED)
- [SDR FDEA2020072381634](https://openairdocs.org/sdr/FDEA2020072381634), Jul 18, 2020: SEAT TRACK. WORN. MAIN CARGO DECK AT APPROX BS 1360 & LBL 8.50, SEAT TRACK WORN. REMOVED AND REPLACED THE SEAT TRACK SECTION FROM BS 1370 TO 1410 IAW SRM 53-70-00, FIG 1, SHT 1, 

All 283: https://openairdocs.org/aircraft/N304FE/reports.md

## STCs that may be installed (OpenAirDocs) (72, 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 72: https://openairdocs.org/aircraft/N304FE/stcs.md

## Related

- Other Mcdonnell Douglas MD-10-30F aircraft: https://openairdocs.org/model/mcdonnell-douglas-md-10-30f/aircraft.md
- The GE CF6-50C2 engine: https://openairdocs.org/engine/ge-cf6-50c2.md

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