# N315FE: 1988 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: 48313
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 30, 2010
- Certificate issued: November 12, 2013
- Expires: November 30, 2029
- Mode S code: A359E6
- 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=315FE
- Page: https://openairdocs.org/aircraft/N315FE

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/N315FE/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 N315FE.

## FAA accident and incident reports

None matched to N315FE.

## Service difficulty reports (212, 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 FDEA202107181804](https://openairdocs.org/sdr/FDEA202107181804), Jul 18, 2021: SEAL. TORN. PASSING APROX. 15,000 FT WE HAD A LEVEL 2 ALERT "CABIN INFLO LO" THIS ALERT ONLY REMAINED FOR A FEW SECONDS, BUT WAS FOLLOWED BY LEVEL 1 ALERT "CABIN RATE". THE
- [SDR FDEA202103290791](https://openairdocs.org/sdr/FDEA202103290791), Mar 29, 2021: AUTOPILOT SYS. FAILED. LOGPAGES:373542 AFTER T/O A/P WOULD NOT ENGAGE STUCK IN [NAV2 AP/OFF BOXED IN AMBER] CYCLED LANDING GEAR THINKING GROUND SENSE NO HELP CYCLED A/P PADDLES NUMERO
- [SDR FDEA202102160373](https://openairdocs.org/sdr/FDEA202102160373), Feb 16, 2021: PRESSURE SWITCH. FAILED. MDIS 315 25-60 8087 15FEB21 MCO OPEN U DURING PRE-DISPATCH CHECK FOUND THE L/H DOOR EVACTUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST LIGHT INDICATING SYSTEM INOP
- [SDR FDEA202102150359](https://openairdocs.org/sdr/FDEA202102150359), Feb 15, 2021: INDICATOR. INOPERATIVE. DURING PRE-DISPATCH CHECK, FOUND THE L1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST LIGHT INDICATING SYSTEM INOP REPLACED L1 REMOTE SLIDE PACK PRESSURE 
- [SDR FDEA2020090842124](https://openairdocs.org/sdr/FDEA2020090842124), Sep 4, 2020: SLIDE. UNKNOWN. RECEIVED CALL FROM RAMP THAT L-1 DOOR WAS ARMED. UPON ENTRY FROM MEC BAY FOUND SLIDE ON FLOOR NOT DEPLOYED. L-1 MAIN ENTRY SLIDE/RAFT REMOVED-EXTENDED OVERWATER
- [SDR FDEA202002270433](https://openairdocs.org/sdr/FDEA202002270433), Feb 27, 2020: SKIN. CRACKED. L/H WING TIP AFT - LOWER SURFACE BETWEEN ACCESS PANEL#528CB AND AFT POSITION LIGHT - 2 CRACKS EMINATING FROM FASTENER HOLE, CRACKS CONFIRMED AND ENDS. PERFORMED
- [SDR FDEA2020022870433](https://openairdocs.org/sdr/FDEA2020022870433), Feb 27, 2020: SKIN. CRACKED. L/H WING TIP AFT - LOWER SURFACE BETWEEN ACCESS PANEL#528CB AND AFT POSITION LIGHT - 2 CRACKS EMINATING FROM FASTENER HOLE, CRACKS CONFIRMED AND ENDS. PERFORMED
- [SDR FDEA202002130367](https://openairdocs.org/sdr/FDEA202002130367), Feb 13, 2020: CAP. CORRODED. CTR W/W CAP P/N AYB7080-7 REQ TO BE FABRICATED FABRICATED NEW CAP SECTIONS A AND B OF AYB7080-7 REF. E.A 8-5310- T0352380 "FUSELAGE-MAINFRAME-BLKHD INST'L AFT P
- [SDR FDEA2020021430336](https://openairdocs.org/sdr/FDEA2020021430336), Feb 13, 2020: SUPPORT BRACKET. WORN. R/H I/B FLAP ACTUATOR SUPPORT BRACKET LOWER END HAS LOOSE HI LOKS BRACKET. REFER TO N/R 797 FOR ANB7394-502 BUSHING REPAIR PER EA T 8-5340-T0352193 P1. RH INBD 
- [SDR FDEA2020021430334](https://openairdocs.org/sdr/FDEA2020021430334), Feb 13, 2020: SKIN. GOUGED. DEEP GOUGE FOUND ON WING TIP L/E PANEL REPAIR PER E.A. 8-5720-T0352117
- [SDR FDEA20200130231](https://openairdocs.org/sdr/FDEA20200130231), Jan 28, 2020: SEAT TRACK. CORRODED. MAIN DECK- SEAT TRACK- CORROSION FOUND FROM STATION 1089 TO STATION 1229, RBL9. REPAIRED DAMAGED SEAT TRACK FROM STATION 1089 TO STATION 1229, RBL9 PER SRM 53- 
- [SDR FDEA2020013070245](https://openairdocs.org/sdr/FDEA2020013070245), Jan 17, 2020: FLOORBEAM. CORRODED. MAIN CAGO DECK AT STA1741 L/H SIDE FLOOR BOAED SUPPORTS AGAINTS WALL HAS CORROSION REMOVED AND REPLACED FLOOR SIPPORT AT STATION 1741, LBL 80 TO 108 PER DAC DWG
- [SDR FDEA2020020650274](https://openairdocs.org/sdr/FDEA2020020650274), Jan 15, 2020: FLOORBEAM. CORRODED. MAIN CARGO DECK AT APPROX STA 1481 RBL 100 FLOOR SUPPORT HAS EXFOLIATION CORROSION. MARKED #4 REMOVED AND REPLACED CORRODED FLOOR SUPPORT REF DAC DWG NEA6018 AN
- [SDR FDEA2020020650273](https://openairdocs.org/sdr/FDEA2020020650273), Jan 15, 2020: FLOORBEAM. CORRODED. MAIN CARGO DECK AT APPROX STA 1501 LBL 9 FLOOR SUPPORT HAS EXFOLIATION CORROSION. MARKED #7 REMOVED AND REPLACED CORRODED FLOOR SUPPORT REF DAC DWG NEA6018 AND 
- [SDR FDEA2020020650271](https://openairdocs.org/sdr/FDEA2020020650271), Jan 15, 2020: FLOORBEAM. CORRODED. MAIN CARGO DECK AT APPROX STA 1381 LBL 9 FLOOR SUPPORT HAS EXFOLIATION CORROSION. MARKED #6 REMOVED AND REPLACED CORRODED FLOOR SUPPORT REF DAC DWG NEA6018 AND 
- [SDR FDEA2020020415256](https://openairdocs.org/sdr/FDEA2020020415256), Jan 15, 2020: FLOORBEAM. CORRODED. MAIN CARGO DECK AT APPROX STA 1361 LBL 100 FLOOR SUPPORT HAS EXFOLIATION CORROSION. MARKED #8 REMOVED AND REPLACED CORRODED FLOOR SUPPORT AEA0394-1 REF DAC DWG 
- [SDR FDEA2020013050249](https://openairdocs.org/sdr/FDEA2020013050249), Jan 15, 2020: FLOORBEAM. CORRODED. UPPER CARGO, SEAT TRACK APROX STATION 1741 RBL 100 SHOW SIGNS OF CORROSION AROUND SEVERAL NUT PLATES (VIEWED FROM CTR CARGO) REMOVED AND REPLACED FLOOR SIPPORT 
- [SDR FDEA202002040255](https://openairdocs.org/sdr/FDEA202002040255), Jan 14, 2020: FLOOR SUPPORT. CORRODED. MAIN CARGO DECK AT APPROX STA 1361 RBL 100 FLOOR SUPPORT HAS EXFOLIATION CORROSION. MARKED #3 REMOVED AND REPLACED CORRODED FLOOR SUPPORT AEA0394-1 REF DAC DWG 
- [SDR FDEA2020013040246](https://openairdocs.org/sdr/FDEA2020013040246), Jan 14, 2020: FLOORBEAM. CORRODED. UPPER CARGO- APROX STATION 1741 RBL 118, FLOOR BOARD SUPPORT SHOWS SIGNS OF CORROSION (VIEWED FROM CTR CARGO) REMOVED AND REPLACED FLOOR SIPPORT AT STATION 1741
- [SDR FDEA2020022110366](https://openairdocs.org/sdr/FDEA2020022110366), Jan 11, 2020: ACCESS PANEL. CORRODED. CENTER WHEEL WELL - LOWER AUX TANK ACCESS PANEL LOWER LANDING (AIRCRAFT SIDE) HAS COROSSION IN NUMEROUS AREAS. (AREAS MARKED) REMOVED CORRODED LOWER CAP AYB7080
- [SDR FDEA2020022090354](https://openairdocs.org/sdr/FDEA2020022090354), Jan 9, 2020: FRAME. GOUGED. AVIONICS COMPARTMENT, NO. 1 RAM AIR DUCT RED COUPLING/BOOT, LOWER BOLT IS CONTACTING AND GOUGING AIRCRAFT FRAME. MARKED WITH DOT #20. LOCATED AFT OF THE MAIN AV
- [SDR FDEA2020012780225](https://openairdocs.org/sdr/FDEA2020012780225), Jan 8, 2020: FLOORBEAM. CORRODED. LOWER CTR CARGO PIT AT DOOR ENTRY STA. 1750 CEILING FLOOR BEAM HAS CORROSION ON LOWER LEG OF I-BEAM REMOVED & REPLACED CEILING FLOOR I-BEAM LOWER LEG AFA7509-5,
- [SDR FDEA2020013080237](https://openairdocs.org/sdr/FDEA2020013080237), Jan 8, 2020: SPAR. CRACKED. R/H WING REAR SPAR LOWER SURFACE, FILLER STRIP CRACKED AT STA XORS 408. MARKED DOT #1. REMOVED CRACKED FILER STRIP SILL FROM I/B END TO NEW CUT LOCATION BETWEEN
- [SDR FDEA2020011670139](https://openairdocs.org/sdr/FDEA2020011670139), Jan 7, 2020: BULKHEAD WEB. CORRODED. INSIDE CLG WW, AFT BULKHEAD STA 1521, L/H SIDE, ATTACHING HORIZONTAL CHANNEL SECTION IS CORRODED THROUGH. POSSIBLE CORROSION ON AREA OF BULKHEAD COVERED UP BY C
- [SDR FDEA2020011670149](https://openairdocs.org/sdr/FDEA2020011670149), Jan 7, 2020: DOUBLER. CRACKED. LH WING LEADING EDGE INTERNAL AT APPROX XORS 568 - INNER BEADED DOUBLER HAS SIX (6) CRACKS. DAMAGED CONFIRMED USING NDT HFEC. REPAIRED CRACKED ,(6)PLACES,INNER 
- [SDR FDEA2020020450264](https://openairdocs.org/sdr/FDEA2020020450264), Jan 5, 2020: SEAT TRACK. WORN. MAIN DECK: APPROX STA 795, RBL 28, SEAT TRACK LOBE WORN BEYOND LIMITS (MARKED AND DOT 62) REPLACED DAMAGED SECTION OF SEAT TRACK AT STA 795, RBL 28, REF SRM 53-
- [SDR FDEA2020013050244](https://openairdocs.org/sdr/FDEA2020013050244), Jan 5, 2020: SEAT TRACK. WORN. MAIN DECK: APPROX STA 635, RBL 8, SEAT TRACK LOBE WORN (IS CRESCENT SHAPED). (MARKED AND DOT 64) REPAIRED DAMAGED SEAT TRACK FROM STATION 635 TO STATION 659, RB
- [SDR FDEA2020012340208](https://openairdocs.org/sdr/FDEA2020012340208), Jan 4, 2020: SEAT TRACK. CORRODED. MAIN DECK - SEAT TRACK - AT STA 1200-1210, RBL 9 HAS SOMETHING SPILLED IN TRACK THAT REQUIRES REMOVAL, TO FACILITATE INSPECTION FOR CORROSION. (MARKED) REPAIRED
- [SDR FDEA2020012340207](https://openairdocs.org/sdr/FDEA2020012340207), Jan 4, 2020: SEAT TRACK. CORRODED. MAIN DECK - SEAT TRACK - AT STA 1180-1190, RBL 9 HAS SOMETHING SPILLED IN TRACK THAT REQUIRES REMOVAL, TO FACILITATE INSPECTION FOR CORROSION. (MARKED) REPAIRED
- [SDR FDEA2020012340206](https://openairdocs.org/sdr/FDEA2020012340206), Jan 4, 2020: SEAT TRACK. CORRODED. MAIN DECK - SEAT TRACK - AT STA 1125-1140, RBL 9 HAS SOMETHING SPILLED IN TRACK THAT REQUIRES REMOVAL, TO FACILITATE INSPECTION FOR CORROSION. (MARKED) REPAIRED
- [SDR FDEA2020012340205](https://openairdocs.org/sdr/FDEA2020012340205), Jan 4, 2020: SEAT TRACK. CORRODED. MAIN DECK - SEAT TRACK - AT STA 1100-1129, RBL 9 HAS SOMETHING SPILLED IN TRACK THAT REQUIRES REMOVAL, TO FACILITATE INSPECTION FOR CORROSION. (MARKED) REPAIRED
- [SDR FDEA2020012340203](https://openairdocs.org/sdr/FDEA2020012340203), Jan 4, 2020: SEAT TRACK. WORN. MAIN DECK - SEAT TRACK - AT STA 1821, LBL 47 IS WORN. (MARKED) REPAIRED DAMAGED (WORN) SEAT TRACK , FROM STA. 1811 TO STA. 1831, LBL 47, PER SRM 53-70-00 FIG. 1
- [SDR FDEA2020012340200](https://openairdocs.org/sdr/FDEA2020012340200), Jan 4, 2020: SEAT TRACK. WORN. MAIN DECK - SEAT TRACK - AT STA 1721, LBL 47 IS WORN. (MARKED) REPAIRED DAMAGED (WORN) SEAT TRACK , FROM STA. 1721 TO STA. 1741, LBL 47, PER SRM 53-70-00 FIG. 1
- [SDR FDEA201810313064](https://openairdocs.org/sdr/FDEA201810313064), Oct 31, 2018: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHT TEST. EMER LT BAT 1 LO ALERT. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY POWER SUPPLY WITH CPN 3300197 S/N 1027 IAW AMM 33-51-01-4-1. OPS C
- [SDR FDEA2018082192125](https://openairdocs.org/sdr/FDEA2018082192125), Aug 19, 2018: CONNECTOR. DAMAGED. L1 DOOR EVAC SLIDE REMOTE PRESSURE PRESS TO TEST INDICATION SYSTEM INOP. FOUND BATTERY SOLDER CONNECTION TO BE DISCONNECTED. RE-SOLDERED CONNECTION SLIDE LIGHT 
- [SDR FDEA201802060310](https://openairdocs.org/sdr/FDEA201802060310), Feb 6, 2018: BOTTLE. LOW PRESSURE. DURING PREFLIGHT, DISCOVERED THE R1 DOOR SLIDE BOTTLE PRESSURE NOT IN THE GREEN BAND. SERVICED THE BOTTLE IAW AMM 52-11-07-2
- [SDR FDEA201801180120](https://openairdocs.org/sdr/FDEA201801180120), Jan 18, 2018: WIRE. BROKEN. LEVEL 1 BRAKE DIFFERENTAL TEMP AT 30 MINUTES INTO FLIGHT FL380 SAT -56 BRAKE TEMP WHEEL 6 FLUCTUATING RAPIDLY BTWN 330-375. AT 40 MIN INTO FLIGHT LVL 2 BRAKE OV
- [SDR FDEA201801020001](https://openairdocs.org/sdr/FDEA201801020001), Jan 2, 2018: SKIN. CRACKED. LEFT WING OTBD FLAP UPPER SURFACE SKIN XOF 563, HAS A 2.25 INCH CRACK. CONFIRMED BY HFEC. INSTALLED A FILLER AND DOUBLER IAW SRM 57-20-01, FIG 4, SHEET 2, VOL 1
- [SDR FDEA201712303474](https://openairdocs.org/sdr/FDEA201712303474), Dec 30, 2017: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AT BS 715 RBL 63 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-31-01 VOL II
- [SDR FDEA201712293476](https://openairdocs.org/sdr/FDEA201712293476), Dec 29, 2017: ROLLER TRAY. CORRODED. FWD CARGO BAY, BS 959 - 1099 ROLLER TRAY CORRODED AT THE LOCKS AND ROLLER AREAS. MAJOR REPAIR. REPAIRED IAW SRM 51-31-01, VOL.2, AND DWG NDJ6230.
- [SDR FDEA201712293464](https://openairdocs.org/sdr/FDEA201712293464), Dec 29, 2017: FLOOR SUPPORT. CORRODED. MAIN CARGO FLOOR SUPPORT AT BS 715, RBL 63 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-31-01, VOL II
- [SDR FDEA201712283463](https://openairdocs.org/sdr/FDEA201712283463), Dec 28, 2017: CARGO TRACK. WORN. MAIN CARGO BAY, BS 1640, RBL 47.50, CARGO TRACK WORN BEYOND LIMITS. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 53-70-00, FIG 1 VOL. 1, SHEET 1, AND SRM 51-31-
- [SDR FDEA201712233433](https://openairdocs.org/sdr/FDEA201712233433), Dec 23, 2017: SEAT TRACK. WORN. MAIN DECK LBL 75.25 NEAR STA 740 SEAT TRACK WORN. REPAIRED DAMAGE SEAT TRACK AT LBL75.25 STA 740 REFERENCE SRM 53-70-00 FIGURE 2A PAGE II VOL I.
- [SDR FDEA201712203424](https://openairdocs.org/sdr/FDEA201712203424), Dec 20, 2017: SKIN. GOUGED. TWO GOUGES IN SKIN UNDER HORIZONTAL STABILIZER, BS 2139. BLENDED GOUGES AND INSTALLED A REPAIR DOUBLER IAW SRM 53-20-00, FIG 22, VOL 1.
- [SDR FDEA201712143392](https://openairdocs.org/sdr/FDEA201712143392), Dec 14, 2017: SEAT TRACK. WORN. MAIN CABIN APPRO. STA. 1240 X-= 47.50, SEAT TRACK UPPER SURFACE , NICKED /GOUGED PAINT PEELNG REMOVED AND REPLACED SEAT TRACK REF. SRM 53-70-00 FIG 1 VOL 1 AND 
- [SDR FDEA201712143384](https://openairdocs.org/sdr/FDEA201712143384), Dec 14, 2017: SEAT TRACK. WORN. MAIN DECK SEAT TRACK STA791 RBL47.50 WORN BEYOND LIMITS REPAIRED SEAT TRACK @ STA791 RBL47.50 PER SR10-53-501
- [SDR FDEA201712133426](https://openairdocs.org/sdr/FDEA201712133426), Dec 13, 2017: SEAT TRACK. DAMAGED. UPPER MAIN DECK SEAT TRACK RBL 27.50 NEAR BS 1635 TO 1650 DAMAGED. REPLACED THE SEAT TRACK SECTION IAW SRM 53-70-00, FIG 1, VOL 1. MAJOR REPAIR.,
- [SDR FDEA201712133379](https://openairdocs.org/sdr/FDEA201712133379), Dec 13, 2017: SEAT TRACK. DAMAGED. MAIN DECK SEAT TRACK LBL 47.50 NEAR STA. 1375 DAMAGED REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1
- [SDR FDEA201712133378](https://openairdocs.org/sdr/FDEA201712133378), Dec 13, 2017: SEAT TRACK. DAMAGED. MAIN DEACK SEAT TRACK LBL 47.50 NEAR STA. 1365 DMAGED REMOVED AND REPLACED DMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL. 1
- [SDR FDEA201712133377](https://openairdocs.org/sdr/FDEA201712133377), Dec 13, 2017: SEAT TRACK. DAMAGED. MAIN DECK SEAT TRACK LBL 47.50 NEAR STA 1380 DAMAGED REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1

All 212: https://openairdocs.org/aircraft/N315FE/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/N315FE/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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