# N318FE: 1979 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: 46837
- Year built: 1979
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 29, 1979
- Certificate issued: April 27, 2007
- Expires: April 30, 2030
- Mode S code: A3650B
- 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=318FE
- Page: https://openairdocs.org/aircraft/N318FE

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/N318FE/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

None matched to N318FE.

## 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 20091129052032I](https://openairdocs.org/incident/20091129052032I), Nov 29, 2009: Douglas DC-10-30F (N318FE), Salt Lake City, UT, Minor damage. On 11/29/09, at approximately 07:09 MST, a fedx DC-10 taxiing north on h clipped the right winglet of a swaa B-737. The top half of the winglet was severed off…

## Service difficulty reports (311, 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 FDEA202103170686](https://openairdocs.org/sdr/FDEA202103170686), Mar 17, 2021: FLOORBEAM. CORRODED. CENTER CARGO COMPT CEILING STA 1661 LBL 50-60 MAIN DECK FLOORBOARD CORRODED AT NUTCLIPS REMOVED AND REPLACED FLOORBOARD SUPPORT AT STA 1661 LBL50-60 PER DWG 385
- [SDR FDEA202103170685](https://openairdocs.org/sdr/FDEA202103170685), Mar 17, 2021: BEAM. BROKEN. UPON REMOVAL OF R-3 DOOR PLUG, FOUND LOWER BEAM BROKEN R&R BEAM PER DWG ADA0007
- [SDR FDEA202103140703](https://openairdocs.org/sdr/FDEA202103140703), Mar 14, 2021: SKIN. DENTED. RIGHT WING INBOARD AILERON UPPER SKIN HAS DAMAGE.(MARKED) TRIMMED OUT DAMAGE AND INSTALLED REPAIR DOUBLER. REFERENCE SRM 57-10-00 FIG.85 SH.1 VOL1. REFERENCE E.
- [SDR FDEA202103090612](https://openairdocs.org/sdr/FDEA202103090612), Mar 9, 2021: STRUCTURE. CRACKED. #2 ENGINE R/H CORE COWL HAS A CRACK @ RIB (MARKED). REMOVED AND REPLACED R/H #2 CORE COWL REF AMM 71-13-01-2.
- [SDR FDEA202103090697](https://openairdocs.org/sdr/FDEA202103090697), Mar 9, 2021: ANGLE. DAMAGED. CENTER CARGO STA. 1781 LOWER ANGLE -19 DAMAGE REF DWG AFA3871 REMOVED AND REPLACED FABRICATED ANGLE -19 REF DAC DWG AFA3871 ALODINE AND PRIME PRIME REF SRM 51-2
- [SDR FDEA202103090674](https://openairdocs.org/sdr/FDEA202103090674), Mar 9, 2021: ANGLE. CRACKED. RIGHT WING OUTBOARD FLAP INBOARD HINGE UPPER INBOARD SUPPORT IS CRACKED.(FLAP SIDE) REMOVED AND REPLACED R/H WING OUTB FLAP INB HINGE ANGLE ARC2149-5 PER DAC AR
- [SDR FDEA202103090610](https://openairdocs.org/sdr/FDEA202103090610), Mar 9, 2021: FLOOR PANEL. DAMAGED. CABIN FLOOR PANEL AFA3203-19 (281CF) HAS MISSING INSERTS AND DAMAGED CORNER AND REQUIRES REPLACEMENT FABRICATED CABIN FLOOR PANEL AFA3203-19 (281CF) PER DWG SRZ
- [SDR FDEA202103080599](https://openairdocs.org/sdr/FDEA202103080599), Mar 8, 2021: DOUBLER. CRACKED. RH WING AT APPROX XORS 906-INTERNAL BEADED DOUBLER HAS 1.00 INCH CRACK. CONFIRMED CRACK AND MARKED ENDS USING NDT HFEC. REPAIRED R/H WING AT STA XORS 906 WITH I
- [SDR FDEA202103060595](https://openairdocs.org/sdr/FDEA202103060595), Mar 6, 2021: DOME NUT. BROKEN. MAIN CABIN STA 1900 LBL55 BROKEN DOME NUT AND CORROSION ON BOTTOM OF FLOOR SUPPORT AT DOME NUT LOCATION REMOVED AND INSTALLED NEW FLOOR SUPPORT P/N:ACA3118-1 ON
- [SDR FDEA202103050700](https://openairdocs.org/sdr/FDEA202103050700), Mar 5, 2021: SEAT TRACK. CORRODED. MAIN CABIN AFT O/B L/H SEAT TRACK STA 1921 TO 1954 LBL81 CORROSION ON SEAT TRACK NUT CLIP LOBES BOTTOM SIDE REMOVED CORROSION FROM MAIN CABIN AFT O/B L/H SEAT T
- [SDR FDEA202103050575](https://openairdocs.org/sdr/FDEA202103050575), Mar 5, 2021: BEAM. CRACKED. R3 DOOR, TOP AFT DOOR STOP BRACKET IS CRACKED. LOCATED AND INSTALLED NEW UPPER DOOR BEAM PER DWG ADA0006.
- [SDR FDEA202103050574](https://openairdocs.org/sdr/FDEA202103050574), Mar 5, 2021: BEAM. CRACKED. R-3 DOOR PLUG, FOUND LOWER BEAM BROKEN LOCATED AND INSTALLED NEW LWR DOOR BEAM PER DWG ADA0007.
- [SDR FDEA202103030656](https://openairdocs.org/sdr/FDEA202103030656), Mar 3, 2021: SKIN. WORN. R/H WING, I/B AILERON, LOWER L/E SKIN, IS WORN THROUGH JUST O/B OF AILERON ACTUATOR ACTUATOR ATTACH POINT. INTIRE LENGHT HAS EXCESSIVE WEAR ASSOCIATED WITH WING
- [SDR FDEA202102280516](https://openairdocs.org/sdr/FDEA202102280516), Feb 28, 2021: SKIN. CORRODED. R/H WING TOP SURFACE AT STA XORS 77 STR 22, HAS CORROSION BLISTER REMOVED CORROSION, REMAINING THICKNESS VERIFIED TO BE WITHIN LIMTS PER SRM 57-10- 00 FIG61 SHT
- [SDR FDEA202102250451](https://openairdocs.org/sdr/FDEA202102250451), Feb 25, 2021: FLOORBEAM. CORRODED. FLOOR SUPPORT AT STA 1881 RBL 10-20 IS CORRODED MAIN DECK REMOVED AND REPLACED MAIN DECK FLOOR SUPPORT AT STA 1881 RBL 10-20. REF. SRM 51- 35-01, VOL II
- [SDR FDEA202102250449](https://openairdocs.org/sdr/FDEA202102250449), Feb 25, 2021: SEAT TRACK. CORRODED. MAIN DECK, SEAT TRACK AT STA 1881 RBL 8 IS CORRODED ON AFT END REPLACED DAMAGED SEAT TRACK FROM STA 1861-1887. REF SRM 53-70-00 FIG 1 VOL 1, 51-31- 01 VOL 2, DW
- [SDR FDEA202102240673](https://openairdocs.org/sdr/FDEA202102240673), Feb 24, 2021: BRACKET. CRACKED. R/H WING OUTB FLAP INB HINGE ARC2151-3 TEE BRACKET CRACKED. REMOVED AND REPLACED R/H WING OUTB FLAP INB HINGE ANGLE ARC2151-3 PER DAC ARC2151 AND SRM 51-31-01 V
- [SDR FDEA202102230437](https://openairdocs.org/sdr/FDEA202102230437), Feb 23, 2021: FLOORBOARD. DELAMINATED. MAIN CARGO FLOOR BOARD DAMAGED AT STA 879- STA 888 CENTERLINE, FEELS DELAMINATED. FABRICATED NEW FLOOR PANEL 253BF AS REQ'D REF FDX DWG SRZ-25-005.
- [SDR FDEA202102180401](https://openairdocs.org/sdr/FDEA202102180401), Feb 18, 2021: FLOOR PANEL. DAMAGED. MAIN CARGO DECK FLOOR PANEL AT APPROX. STA.1437 RBL 60 HAS DAMAGE REQUIRE NEW STENCILING REPAIRED MAIN DECK PANEL (PN ADA 7556-16) AT ST 1437 RBL 60 REF SRM 53-
- [SDR FDEA202102180404](https://openairdocs.org/sdr/FDEA202102180404), Feb 18, 2021: FLOORBOARD. DAMAGED. UPPER FUSELAGE MAIN CABIN FLOORBOARD STA 1481 RBL 75 - 107 NEEDS 4 INSERTS, MARKED IN RED. 0000484495 : SKIATHITIS, GEORGE M - 18-FEB-2021 19:22 REPLACED MISSIN
- [SDR FDEA202102180400](https://openairdocs.org/sdr/FDEA202102180400), Feb 18, 2021: FLOOR PANEL. DAMAGED. MAIN CARGO COMPARTMENT FLOOR PANEL AT 8L STA1159-1219 HAS DAMAGE INSERTS REPLACED DAMAGED INSERTS FOR PANEL ADA3209-15 ON MAINDECK CARGO FLOOR PANEL 8L STAT-115
- [SDR FDEA202102160581](https://openairdocs.org/sdr/FDEA202102160581), Feb 16, 2021: SKIN. CORRODED. L/H WING TOP SURFACE AT STA XORS 106 STR 13, HAS CORROSION BLISTER. (MKD GREASE PENCIL) L/H WING TOP SURFACE CORROSION REPAIRED PER EA 8-5730-T0360256 WING - PL
- [SDR FDEA202102160452](https://openairdocs.org/sdr/FDEA202102160452), Feb 16, 2021: FLOORBEAM. CORRODED. CENTER CARGO COMPT CEILING STA 1761 LBL 18 MAIN DECT FLOORBOARD SUPPORT CORRODED AT NUT CLIPS. MRKD
- [SDR FDEA202102160450](https://openairdocs.org/sdr/FDEA202102160450), Feb 16, 2021: FLOORBEAM. CORRODED. CENTER CARGO COMPT CEILING STA 1661 RBL 65 MAIN DECK FLOORBOARD SUPPORT CORRODED. MRKD REMOVED AND REPLACED FLOOR SUPPORT, P/N: AFA 3853-21 AT STA 1661 @ RBL 62
- [SDR FDEA202102160409](https://openairdocs.org/sdr/FDEA202102160409), Feb 16, 2021: FLOOR SUPPORT. CORRODED. CENTER CARGO COMPT CEILING STA 1661 LBL 50/60 MAIN DECK FLOORBOARD SUPPORT CORRODED AT 2 NUTCLIPS. MRKD REMOVED AND REPLACED FLOORBOARD SUPPORT AT STA 1661 LBL 
- [SDR FDEA202102160605](https://openairdocs.org/sdr/FDEA202102160605), Feb 16, 2021: FLOORBEAM. CORRODED. CENTER CARGO COMPT CEILING STA 1561 RBL 60 MAIN DECK FLOORBOARD SUPPORT BRACKET CORRODED AT NUT CLIP. FABRICATED AND INSTALLED FLOOR BOARD SUPPORT P/N AFA3853-3
- [SDR FDEA202102160521](https://openairdocs.org/sdr/FDEA202102160521), Feb 16, 2021: ANGLE. CRACKED. RH WING PANEL MISSING FASTENER - PANEL IS BETWEEN ACCESS 651AB AND OUTBD FLAP INBD HINGE LOOKING UP. REMOVED CRACKED ANGLE ARC0744-14 AND REPLACED WITH NEW FABR
- [SDR FDEA202102160440](https://openairdocs.org/sdr/FDEA202102160440), Feb 16, 2021: FLOOR SUPPORT. CORRODED. CENTER CARGO COMPT CEILING STA 1561 LBL 76 MAIN DECK FLOORBOARD SUPPORT CORRODED AT 2 NUTCLIPS. MRKD REMOVED AND REPLACED FLOORBOARD SUPPORT AT STA. 1561 LBL 76
- [SDR FDEA202102160407](https://openairdocs.org/sdr/FDEA202102160407), Feb 16, 2021: SEAT TRACK. CORRODED. CENTER CARGO COMPT CEILING STA 1741 LBL 75 MAIN DECK SEAT TRACK CORRODED AT NUT CLIP. MRKD REMOVED AND REPLACED FLOOR BOARD SUPPORT AFA3853-9 AT STA 1741 LBL 75
- [SDR FDEA202102160474](https://openairdocs.org/sdr/FDEA202102160474), Feb 16, 2021: FLOORBEAM. CORRODED. CENTER CARGO COMPT CEILING STA 1561 RBL 10 MAIN DECK FLOORBOARD SUPPORT CORRODED AT NUT CLIP. MRKD MAIN CARGO AT STA 1561 RBL 10 REMOVED AND REPLACED FLOOR SUPP
- [SDR FDEA202102160462](https://openairdocs.org/sdr/FDEA202102160462), Feb 16, 2021: FLOORBEAM. CORRODED. CENTER CARGO COMPT CEILING STA 1821 RBL 10-20 MAIN DECK FLOORBOARD SUPPORT HAS CORROSION AT 3 NUTCLIPS. MRKD REMOVED AND REPLACED FLOOR BOARD SUPPORT CENTER CAR
- [SDR FDEA202102160482](https://openairdocs.org/sdr/FDEA202102160482), Feb 16, 2021: CAP. CRACKED. R/H HORIZONTAL LEADING EDGE (# 2 FROM INBOARD) ALC7272-502, UPPER OUTBOARD CAP ALC7052-20 CRACKED. REMOVED AND REPLACED O/B UPPER CAP ALC7052-20 OF # 2 O/B HORI
- [SDR FDEA202102160453](https://openairdocs.org/sdr/FDEA202102160453), Feb 16, 2021: FLOORBEAM. CORRODED. CENTER CARGO COMPT CEILING STA 1741 LBL 35 MAIN DECK FLOORBOARD SUPPORT CORRODED AT NUT CLIPS. MRKD REMOVED CORRODED SUPPORT & INSTALLED NEW FABRICATED FLOOR SU
- [SDR FDEA202102160408](https://openairdocs.org/sdr/FDEA202102160408), Feb 16, 2021: FLOOR SUPPORT. CORRODED. CENTER CARGO COMPT CEILING STA 1561 LBL 10 MAIN DECK FLOORBOARD SUPPORT CORRODED AT NUT CLIP. MRKD REMOVED AND REPLACED CORRODED FLOOR SUPPORT WITH FABRICATED F
- [SDR FDEA202102160463](https://openairdocs.org/sdr/FDEA202102160463), Feb 16, 2021: FLOORBEAM. CORRODED. CENTER CARGO COMPT CEILING STA 1761 RBL 10-20 MAIN DECK FLOORBOARD SUPPORT CORRODED AT NUT CLIPS. MRKD REMOVED AND REPLACED FLOOR SUPPORT AT STA. 1761 RBL 10-20
- [SDR FDEA202102160376](https://openairdocs.org/sdr/FDEA202102160376), Feb 16, 2021: DOUBLER. DAMAGED. FWD CARGO DOOR LOWER AFT EDGE, FUSE SKIN DOUBLER NOT PER SRM (MARKED 24) REMOVE AND REPLACE PER SRM CH 53-50-00 FIG 27
- [SDR FDEA202102140672](https://openairdocs.org/sdr/FDEA202102140672), Feb 14, 2021: SUPPORT BEAM. CORRODED. AFT CARGO COMPT FWD BLKHD, CORROSION ON SUPPORT BEAM AND ANGLE AT STA 1841 RBL RBL 24 (MARKED #44) REPAIRED SUPPORT AT STATION 1841 RBL 24, Z-92 REF SRM 53-00-0
- [SDR FDEA202102140639](https://openairdocs.org/sdr/FDEA202102140639), Feb 14, 2021: SUPPORT ANGLE. CRACKED. AFT CARGO COMPT TUNNEL, L/H SIDEWALL SUPPORT ANGLE IS CRACKED AT STA 1915 L-42. REMOVED CRACKED SUPPORT, FABRICATED AND INSTALLED NEW SUPPORT ANGLE REF DWG AGA0
- [SDR FDEA202102140638](https://openairdocs.org/sdr/FDEA202102140638), Feb 14, 2021: SUPPORT ANGLE. CRACKED. AFT CARGO COMPT TUNNEL, L/H SIDEWALL SUPPORT ANGLE IS CRACKED AT STA 1853 L-42. REMOVED CRACKED SUPPORT, FABRICATED AND INSTALLED NEW SUPPORT ANGLE REF DWG AGA0
- [SDR FDEA202102140637](https://openairdocs.org/sdr/FDEA202102140637), Feb 14, 2021: SUPPORT ANGLE. CRACKED. AFT CARGO COMPT TUNNEL, L/H SIDEWALL SUPPORT ANGLE IS CRACKED AT STA 1901 L-42 (MARKED #42) REMOVED CRACKED SUPPORT, FABRICATED AND INSTALLED NEW SUPPORT ANGLE 
- [SDR FDEA202102120348](https://openairdocs.org/sdr/FDEA202102120348), Feb 12, 2021: SEAT TRACK. DAMAGED. MAIN DECK SEAT RAIL LOCATED BTWN STA 1019 AND 1065 LBL 75 REQUIRES SPLICE REPAIR DUE TO DAMAGE BEING OUT OF LIMITS. 0000953084 : HANG, SEAN T - 02-MAR-2021 23:4
- [SDR FDEA202102110675](https://openairdocs.org/sdr/FDEA202102110675), Feb 11, 2021: HINGE FITTING. CRACKED. RIGHT OUTBOARD FLAP INBOARD HINGE INBOARD SIDE HAS 3 LOOSE SCREWS AND DAMAGED DAMAGED BRACKET. MARKED #36 REMOVED AND REPLACED R/H WING OUTB FLAP INB HINGE ANGL
- [SDR FDEA202102110412](https://openairdocs.org/sdr/FDEA202102110412), Feb 11, 2021: FORMER. CRACKED. R/H WING LEADING EDGE INT STRUCTURE, ZONE 626, UPPER RIB SUPPORT BRACKET IS CRACKED. (MKD WITH DOT #1, JUST INDB OF THE 13TH SLAT TRACK.) 0005202340 : LEMUS, JO
- [SDR FDEA202102100706](https://openairdocs.org/sdr/FDEA202102100706), Feb 10, 2021: STOP FITTING. CRACKED. R3 DOOR, TOP AFT DOOR STOP BRACKET IS CRACKED. (MARKED #5) 0000349196 : RAMOS, STEVEN - 19-MAR-2021 14:58 REMOVED AND REPLACED BEAM PER DWG ADAOOO6
- [SDR FDEA202102090391](https://openairdocs.org/sdr/FDEA202102090391), Feb 9, 2021: CARGO TRACK. DAMAGED. MAIN CARGO COMPARMENT SEAT TRACK, STA 615 RBL 24, LUG IS DAMAGED. (MKD) 0000953084 : HANG, SEAN T - 02-MAR-2021 03:37 MAIN CARGO, STA 585-625, RBL 24 REMOVED AN
- [SDR FDEA202102090424](https://openairdocs.org/sdr/FDEA202102090424), Feb 9, 2021: SEAT TRACK. WORN. MAIN DECK SEAT TRACK GOUGED AT APPROX STA. Y=919 X=107. REMOVE AND REPLACE SEAT TRACK AT STA 919 LBL 107 REF MD10-30 SRM 53-70-00 FIGURE 1 VOL 1, SRM 51-31-01 V
- [SDR FDEA202102080580](https://openairdocs.org/sdr/FDEA202102080580), Feb 8, 2021: SKIN. CORRODED. L/H WING TOP SURFACE AT STA XORS 110 STR 14, HAS CORROSION BLISTER. (MKD) L/H WING TOP SURFACE CORROSION REPAIRED PER EA 8-5730-T0360256 WING - PLATES AND SKINS
- [SDR FDEA202102080579](https://openairdocs.org/sdr/FDEA202102080579), Feb 8, 2021: SKIN. CORRODED. L/H WING TOP SURFACE AT STA XORS 110 STR 11, HAS CORROSION BLISTER. (MKD) L/H WING TOP SURFACE CORROSION REPAIRED PER EA 8-5730-T0360256 WING - PLATES AND SKINS
- [SDR FDEA202002180350](https://openairdocs.org/sdr/FDEA202002180350), Feb 18, 2020: WARNING MESSAGE. FALSE ACTIVATION. PDIS 318 28-40 7406 18FEB20 MEM FACT U LOGPAGES:3248935 LVL 2 FUEL QTY/USED CHK" ALERT- QRH PROCEDURES FOLLOWED. ALERT WENT OUT. REOCCURED AFTER ABOUT 5 MINS. U
- [SDR FDEA2019060321208](https://openairdocs.org/sdr/FDEA2019060321208), Jun 2, 2019: COMPARATOR. MALFUNCTIONED. IAS COMPARATOR AND "SEL ELEV FEEL MAN" AND "SEL FLAP LIM OVRD". CAPTAIN AIRSPEED 9 KNOTS SLOWER THAN F/O AND SBY. CAPTAIN SHOWED 35 KNOT TAILWIND WITH A 3 KNOT 

All 311: https://openairdocs.org/aircraft/N318FE/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/N318FE/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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