# N320FE: 1980 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 CF6-50C](https://openairdocs.org/engine/ge-cf6-50c) (registry code 30082)
- 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: 47835
- Year built: 1980
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 17, 2010
- Certificate issued: January 13, 2012
- Expires: January 31, 2028
- Mode S code: A36ED2
- 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=320FE
- Page: https://openairdocs.org/aircraft/N320FE

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): 99 in force

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

- [AD 2026-13-15](https://openairdocs.org/ad/2026-13-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jul 1, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-23-53](https://openairdocs.org/ad/2025-23-53): Nacelles/pylons · Boeing MD-11, MD-11F, MD-10-10F and 8 more. Effective Dec 1, 2025
- [AD 2023-12-15](https://openairdocs.org/ad/2023-12-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jun 21, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2021-08-10](https://openairdocs.org/ad/2021-08-10): Nacelles/pylons · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective May 25, 2021
- [AD 2020-22-15](https://openairdocs.org/ad/2020-22-15): Fuselage · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Dec 18, 2020
- [AD 2018-22-10](https://openairdocs.org/ad/2018-22-10): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Dec 12, 2018
- [AD 2015-02-05](https://openairdocs.org/ad/2015-02-05): Navigation · Boeing 717-200, DC-10-10, DC-10-10F and 13 more. Effective Mar 5, 2015
- [AD 2014-21-05](https://openairdocs.org/ad/2014-21-05): Fuselage · Boeing DC-10-10, DC-10-10F, DC-10-30 and 4 more. Effective Dec 2, 2014
- [AD 2012-19-03](https://openairdocs.org/ad/2012-19-03): Fuselage · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Nov 5, 2012
- [AD 2011-12-01](https://openairdocs.org/ad/2011-12-01): Equipment/Furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 268 more. Effective Aug 1, 2011
- [AD 2011-11-05](https://openairdocs.org/ad/2011-11-05): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 10 more. Effective Jul 6, 2011
- [AD 2010-20-13](https://openairdocs.org/ad/2010-20-13): Fuel · Boeing DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40 and 2 more. Effective Nov 9, 2010
- [AD 2010-20-14](https://openairdocs.org/ad/2010-20-14): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Nov 5, 2010
- [AD 2010-09-12](https://openairdocs.org/ad/2010-09-12): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Jun 8, 2010
- [AD 2009-21-10 R1](https://openairdocs.org/ad/2009-21-10-R1): Oxygen · Airbus A300 B4-605R, A300 B4-620, A300 B4-622 and 138 more. Effective Feb 4, 2010
- [AD 2008-06-21 R1](https://openairdocs.org/ad/2008-06-21-R1): Fuel tank systems · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Dec 10, 2009
- [AD 2009-03-02](https://openairdocs.org/ad/2009-03-02): Auxiliary hydraulic pumps · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 31, 2009
- [AD 2008-17-16](https://openairdocs.org/ad/2008-17-16): Fuel boost pump · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Oct 2, 2008
- [AD 2008-11-14](https://openairdocs.org/ad/2008-11-14): Horizontal pressure panel · Boeing DC-10-10F, DC-10-30F (KC-10A, KDC-10), DC-10-40F and 4 more. Effective Jul 3, 2008
- [AD 2007-19-17](https://openairdocs.org/ad/2007-19-17): System 3 hydraulic piping · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Oct 26, 2007
- [AD 2007-19-15](https://openairdocs.org/ad/2007-19-15): Flight management system (FMS) · Boeing 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Oct 26, 2007
- [AD 2007-19-02](https://openairdocs.org/ad/2007-19-02): Fuel tank and the fuel transfer pump housing flange · Boeing DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40 and 4 more. Effective Oct 17, 2007
- [AD 2007-11-15](https://openairdocs.org/ad/2007-11-15): Center main wheel well · Boeing DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40 and 2 more. Effective Jul 5, 2007
- [AD 2007-10-12](https://openairdocs.org/ad/2007-10-12): Reinforced flight deck door · Reinforced cockpit door (Safran Cabin STC ST01335LA or 2 others). Effective Jun 27, 2007
- [AD 2007-04-17](https://openairdocs.org/ad/2007-04-17): Control modules of the fire detection systems · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Mar 23, 2007
- [AD 2006-19-03](https://openairdocs.org/ad/2006-19-03): Fabrication and installation of a wire harness guard in the right wheel well of the main  
 landing gear (MLG) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Oct 17, 2006
- [AD 2006-16-15](https://openairdocs.org/ad/2006-16-15): Airplane flight manual (AFM) · Boeing MD-10-10F, MD-10-30F, MD-11 and 1 more. Effective Sep 22, 2006
- [AD 2006-04-04](https://openairdocs.org/ad/2006-04-04): Smoke detectors · ATR - GIE Avions de Transport Régional ATR42-200, ATR42-300, ATR42-320 and 37 more. Effective Mar 24, 2006
- [AD 2006-03-13](https://openairdocs.org/ad/2006-03-13): Inboard and outboard hinge fittings · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 16, 2006
- [AD 2006-02-11](https://openairdocs.org/ad/2006-02-11): Drain holes of the pitot tubes · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 3, 2006
- [AD 2005-20-15](https://openairdocs.org/ad/2005-20-15): Rudder pedal torque tube assembly · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Nov 10, 2005
- [AD 2005-17-04](https://openairdocs.org/ad/2005-17-04): Fire extinguishing system · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Sep 26, 2005
- [AD 2005-15-12](https://openairdocs.org/ad/2005-15-12): Exterior emergency control handle assemblies of the forward passenger doors · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Aug 30, 2005
- [AD 2005-15-03](https://openairdocs.org/ad/2005-15-03): Exterior emergency control handle assemblies · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Aug 25, 2005
- [AD 2005-02-04](https://openairdocs.org/ad/2005-02-04): Cargo compartment smoke detectors · Boeing DC-10-10F, DC-10-30F (KC-10A, KDC-10), MD-10-10F and 2 more. Effective Feb 8, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-18-15](https://openairdocs.org/ad/2004-18-15): Flight engineer's station · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Oct 19, 2004
- [AD 2001-14-08 R1](https://openairdocs.org/ad/2001-14-08-R1): Auxiliary hydraulic pump · McDonnell Douglas DC-10 Series (all), MD-10-10F and MD-10-30F. Effective Sep 1, 2004
- [AD 2004-05-06](https://openairdocs.org/ad/2004-05-06): Number one passenger door slide · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Apr 7, 2004
- [AD 2004-02-06](https://openairdocs.org/ad/2004-02-06): Forward aft bracket · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 5, 2004
- [AD 2003-24-10](https://openairdocs.org/ad/2003-24-10): Rudder pedal arm assembly · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Jan 8, 2004
- [AD 2003-03-15 R1](https://openairdocs.org/ad/2003-03-15-R1): Airplane Flight Manual (AFM) - oxygen masks · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 90 more. Effective Dec 22, 2003
- [AD 2003-19-05](https://openairdocs.org/ad/2003-19-05): Inboard and outboard flaps · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Oct 27, 2003
- [AD 2003-16-02](https://openairdocs.org/ad/2003-16-02): Fuel Boost/Transfer Pumps · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Aug 25, 2003
- [AD 2003-08-03](https://openairdocs.org/ad/2003-08-03): Throttle control module (TCM) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective May 22, 2003
- [AD 2003-08-14](https://openairdocs.org/ad/2003-08-14): Airplane Flight Manual (AFM) - Fuel Tank · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective May 12, 2003
- [AD 2002-13-10](https://openairdocs.org/ad/2002-13-10): Fuel boost/transfer pump connectors · Boeing DC-10-10, DC-10-10F, DC-10-15 and 10 more. Effective Aug 12, 2002
- [AD 2002-06-14](https://openairdocs.org/ad/2002-06-14): Parallel Power Feeder Cables of the Number 2 Generator · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective May 7, 2002

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

- [AD 2023-04-11](https://openairdocs.org/ad/2023-04-11): Turbine Section · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 28, 2023
- [AD 2011-23-04](https://openairdocs.org/ad/2011-23-04): Forward engine mount assembly side links · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Dec 12, 2011
- [AD 2011-07-01](https://openairdocs.org/ad/2011-07-01): Forward and aft centerbodies · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 22, 2011
- [AD 2007-11-18 R1](https://openairdocs.org/ad/2007-11-18-R1): Forward fan stator cases · General Electric CF6-50C, CF6-50C1 and CF6-50C2. Effective Jan 4, 2010
- [AD 2008-02-17](https://openairdocs.org/ad/2008-02-17): Thrust reverser actuation systems · General Electric CF6-50A, CF6-50C, CF6-50C1 and 16 more. Effective Feb 28, 2008
- [AD 2007-19-06](https://openairdocs.org/ad/2007-19-06): Compressor discharge pressure (CDP) · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Oct 23, 2007
- [AD 2005-26-06](https://openairdocs.org/ad/2005-26-06): Low pressure turbine (LPT) stage 2 interstage seal assemblies · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jan 26, 2006
- [AD 2005-07-05](https://openairdocs.org/ad/2005-07-05): Low pressure turbine (LPT) · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective May 4, 2005
- [AD 2005-08-04](https://openairdocs.org/ad/2005-08-04): Low-cycle-fatigue (LCF) · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 28, 2005
- [AD 2003-09-06](https://openairdocs.org/ad/2003-09-06): Low pressure turbine (LPT) · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more. Effective Jun 3, 2003
- [AD 2003-02-07](https://openairdocs.org/ad/2003-02-07): Low pressure turbine (LPT) shrouds · General Electric CF6-50A, CF6-50C, CF6-50C1 and 30 more. Effective Mar 3, 2003
- [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08): High pressure compressor rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Jan 23, 2003
- [AD 2002-05-03](https://openairdocs.org/ad/2002-05-03): Life-Limited Rotating Parts · General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective Apr 12, 2002
- [AD 2002-02-09](https://openairdocs.org/ad/2002-02-09): Low Pressure Turbine Rotor (LPTR) Stage 2 Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Mar 15, 2002
- [AD 2001-12-20](https://openairdocs.org/ad/2001-12-20): Air Ducts and Reworked Mating Hardware · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more. Effective Jul 26, 2001
- [AD 2001-04-16](https://openairdocs.org/ad/2001-04-16): Low Pressure Turbine (LPT) Nozzle Lock Assembly Studs · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more. Effective Mar 21, 2001
- [AD 2000-11-12](https://openairdocs.org/ad/2000-11-12): High Pressure Compressor Disk Lock Slots · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Aug 14, 2000
- [AD 98-22-06](https://openairdocs.org/ad/98-22-06): Fan Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 41 more. Effective Nov 23, 1998
- [AD 97-22-14](https://openairdocs.org/ad/97-22-14): (HPCR) 3-9 Spool · General Electric CF6-50A, CF6-50C, CF6-50C1 and 29 more. Effective Nov 17, 1997
- [AD 95-08-03](https://openairdocs.org/ad/95-08-03): High Pressure Turbine Rotor Stage 2 Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jun 12, 1995
- [AD 91-10-03 R1](https://openairdocs.org/ad/91-10-03-R1): High Pressure Compressor · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 28, 1995
- [AD 94-08-05](https://openairdocs.org/ad/94-08-05): Fan Stator Case · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jul 5, 1994
- [AD 94-09-18](https://openairdocs.org/ad/94-09-18): High Pressure Turbine Disk · General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective Jun 6, 1994
- [AD 93-14-18](https://openairdocs.org/ad/93-14-18): High pressure turbine (HPT) thermal shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Oct 4, 1993
- [AD 93-13-10](https://openairdocs.org/ad/93-13-10): Compressor Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Sep 21, 1993
- [AD 91-23-13](https://openairdocs.org/ad/91-23-13): Fan Disks · General Electric CF6-50A, CF6-50C, CF6-50C1 and 12 more. Effective Nov 22, 1991
- [AD 91-15-16](https://openairdocs.org/ad/91-15-16): High Pressure Turbine Thermal Shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Sep 4, 1991
- [AD 91-01-04](https://openairdocs.org/ad/91-01-04): Fan Disk · General Electric CF6-45A, CF6-45A2, CF6-50A and 19 more. Effective Jan 22, 1991
- [AD 90-23-15](https://openairdocs.org/ad/90-23-15): Turbine Mid-frame · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Dec 6, 1990
- [AD 90-19-09](https://openairdocs.org/ad/90-19-09): High Pressure Turbine Stage One Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Oct 1, 1990
- [AD 90-12-06](https://openairdocs.org/ad/90-12-06): Low Pressure Turbine · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jun 25, 1990
- [AD 89-01-02](https://openairdocs.org/ad/89-01-02): High Pressure Turbine Stage 2 Disks · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more. Effective Dec 29, 1988
- [AD 87-23-06](https://openairdocs.org/ad/87-23-06): High Pressure Turbine Impeller Spacer · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Nov 5, 1987
- [AD 86-12-03](https://openairdocs.org/ad/86-12-03): High Pressure Turbine Rotor (HPTR) Stage 1 Disk · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jun 29, 1986
- [AD 84-01-01](https://openairdocs.org/ad/84-01-01): Compressor Assemblies · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Feb 10, 1984
- [AD 82-25-08](https://openairdocs.org/ad/82-25-08): HPT Spacer/Impeller · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Dec 30, 1982
- [AD 82-20-03](https://openairdocs.org/ad/82-20-03): Inspect First Stage HPT Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Oct 31, 1982
- [AD 77-08-08](https://openairdocs.org/ad/77-08-08): Compressor · General Electric CF6-50A, CF6-50C, CF6-50C1 and 2 more. Effective Feb 14, 1980
- [AD 76-17-01](https://openairdocs.org/ad/76-17-01): High Pressure Compressor · General Electric CF6-50A, CF6-50C, CF6-50E and 1 more. Effective Aug 20, 1976
- [AD 76-05-10](https://openairdocs.org/ad/76-05-10): Turbofan Engines · General Electric CF6-50A, CF6-50C, CF6-50E and 3 more. Effective Mar 24, 1976
- [AD 85-25-56 R1](https://openairdocs.org/ad/85-25-56-R1): Seventh Stage Low Pressure Turbine (LPT) Cooling Air Manifold Tube · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more
- [AD 79-13-09](https://openairdocs.org/ad/79-13-09): Compressor Rotor Spools · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more

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

- [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022
- [AD 2016-04-16](https://openairdocs.org/ad/2016-04-16) (historical): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Apr 15, 2016
- [AD 2013-08-23](https://openairdocs.org/ad/2013-08-23) (historical): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective May 29, 2013
- [AD 2009-26-17](https://openairdocs.org/ad/2009-26-17) (historical): Fuselage · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Feb 4, 2010
- [AD 2009-21-10](https://openairdocs.org/ad/2009-21-10) (historical): Oxygen · Airbus A300, Model B4-605R, A300, Model B4-620, A300, Model B4-622 and 138 more. Effective Dec 17, 2009
- [AD 2008-06-21](https://openairdocs.org/ad/2008-06-21) (historical): Fuel tank systems · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Apr 23, 2008
- [AD 2007-15-05](https://openairdocs.org/ad/2007-15-05) (historical): Fuel pump housing electrical connector · Boeing DC-10-10, DC-10-10F, DC-10-15 and 9 more. Effective Aug 8, 2007
- [AD 2005-12-05](https://openairdocs.org/ad/2005-12-05) (historical): Flight deck door · Reinforced cockpit door (Safran Cabin STC ST01335LA or 2 others). Effective Jul 19, 2005
- [AD 2004-18-04](https://openairdocs.org/ad/2004-18-04) (historical): Airplane Flight Manual (AFM) · McDonnell Douglas 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Sep 20, 2004
- [AD 2004-05-20](https://openairdocs.org/ad/2004-05-20) (historical): Electric motor operated auxiliary hydraulic pumps · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 9 more. Effective Apr 15, 2004
- [AD 2003-17-07](https://openairdocs.org/ad/2003-17-07) (historical): Fire Extinguishers for the Engine and Auxiliary Power Unit (APU) · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 60 more. Effective Sep 24, 2003
- [AD 2003-14-04](https://openairdocs.org/ad/2003-14-04) (historical): Flight Deck Door Pressure Relief Latch Assemblies · Boeing 737-200 Series, 737-300 Series, 737-400 Series and 14 more. Effective Jul 25, 2003
- [AD 2003-03-15](https://openairdocs.org/ad/2003-03-15) (historical): Airplane Flight Manual (AFM) - Oxygen Masks · Boeing 707 Series (all), 720 Series (all), 727 Series (all) and 75 more. Effective Mar 7, 2003
- [AD 2001-14-08](https://openairdocs.org/ad/2001-14-08) (historical): Electric Motors of the Auxiliary Hydraulic Pump · McDonnell Douglas DC-10 Series (all), MD-10-10F, MD-10-30F and 1 more. Effective Aug 16, 2001
- [AD 2012-02-07](https://openairdocs.org/ad/2012-02-07) (historical): LPT rotor stage 3 disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Mar 6, 2012
- [AD 2011-18-01](https://openairdocs.org/ad/2011-18-01) (historical): LPT rotor stage 3 disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Sep 26, 2011
- [AD 2011-02-07](https://openairdocs.org/ad/2011-02-07) (historical): Rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Feb 22, 2011
- [AD 2010-12-10](https://openairdocs.org/ad/2010-12-10) (historical): High-pressure turbine (HPT) · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Jun 24, 2010
- [AD 2010-06-15](https://openairdocs.org/ad/2010-06-15) (historical): Low-pressure turbine (LPT) stage 3 disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Apr 1, 2010
- [AD 2009-04-17](https://openairdocs.org/ad/2009-04-17) (historical): Long fixed core exhaust nozzle (LFCEN) assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 2, 2009
- [AD 2007-11-18](https://openairdocs.org/ad/2007-11-18) (historical): Forward fan stator cases · General Electric CF6-50C, CF6-50C1, CF6-50C2 and 1 more. Effective Jul 5, 2007
- [AD 2006-12-24](https://openairdocs.org/ad/2006-12-24) (historical): Five-link forward mount assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Jul 21, 2006
- [AD 2000-20-02](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 125: https://openairdocs.org/aircraft/N320FE/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 N320FE.

## FAA accident and incident reports (2)

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

- [Incident 20070811016529I](https://openairdocs.org/incident/20070811016529I), Aug 11, 2007: Doug DC1030F (N320FE), Boston, MA, No damage. (-23) Returned to ramp from position and hold due to an odor in the cockpit. Crew decided to stop on taxiway and request fire equipment as a fire was…
- [Incident 19980523043309I](https://openairdocs.org/incident/19980523043309I), May 23, 1998: Doug DC1030F (N320FE), Albuquerque, NM. (-5)Fire warning light for #1 engine illuminated in cruise. Shut down engine and diverted to abq. Discharged a&b fire bottles maintenance found low pressure…

## Service difficulty reports (183, 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 FDEA202110062471](https://openairdocs.org/sdr/FDEA202110062471), Oct 6, 2021: FUSE. LEAKING. ON SHORT FINAL AT KIND WITH SLATS EXTENDED AND FLAPS 22 DEG WE EXTENDED THE LANDING GEAR. VERY SOON AFTER EXTENDING THE LANDING WHILE PERFORMING THE BEFORE LAND
- [SDR FDEA202007311734](https://openairdocs.org/sdr/FDEA202007311734), Jul 31, 2020: WARNING MESSAGE. ILLUMINATED. LEVEL 1 AIR SYS 3 OFF ILLUMINATED FOURTEEN MINUTES INTO FLIGHT AT FL 280. ASSOCIATED BLEED (3) AND PACK (3) OFF. RED DUCT LINE ILLUMINATED ON AIR SYNOPTIC. COMP
- [SDR FDEA2020071091474](https://openairdocs.org/sdr/FDEA2020071091474), Jul 9, 2020: WARNING LIGHT. FALSE ACTIVATION. LVL 1 AIR SYS OFF ALERT. AIR SYS AUTOMATICALLY SHUT OFF NR 3 BLEED AND NR 3 PACK. NR 3 DUCT WENT MOMENTARILY RED PRIOR TO AUTO SHUTDOWN OF NR 3 AIR SYS. CHECKED
- [SDR FDEA202006201300](https://openairdocs.org/sdr/FDEA202006201300), Jun 20, 2020: WARNING MESSAGE. FALSE ACTIVATION. EMER LT BAT 1 LOW ON PREFLIGHT PERFORMED OPS CHECK OF EMERGENCY LIGHTS REF MD-10-30 AMM 33-50-00-5-0. OPS CHECK GOOD; OK FOR SERVICE.
- [SDR FDEA2020062301300](https://openairdocs.org/sdr/FDEA2020062301300), Jun 20, 2020: BATTERY. LOW VOLTAGE. EMER LIGHT BAT 1 LOW ON PREFLIGHT.
- [SDR FDEA202006161253](https://openairdocs.org/sdr/FDEA202006161253), Jun 16, 2020: CONTROL MODULE. FAILED. ON APPROACH SLATS EXTENDED, FLAPS WOULD NOT MOVE, HANDLE STUCK. EXECUTED A GO AROUND. SPENT SOME TIME WIGGLING THE HANDLE AND DIAL- AND-FLAP AND FINALLY GOT THE
- [SDR FDEA2019112633066](https://openairdocs.org/sdr/FDEA2019112633066), Nov 23, 2019: BEAM. CORRODED. CORROSION ON NUT PLATES FOR FLOOR ATTACHMENTS, AFT CARGO COMPARTMENT AT STA 1902. REMOVED CORROSION IAW SRM 53-00-01 VOL II. ORIG THICKNESS 0.063". AFTER REWORK
- [SDR FDEA2019111542960](https://openairdocs.org/sdr/FDEA2019111542960), Nov 14, 2019: LANDING. CRACKED. H-STAB ACCESS PANEL 311AB LANDING ON LH HAS A CRACK REMOVED DAMAGE IAW SRM 53-00-01 FIG 4 SHT 2. PERFORMED HFEC IAW SOPM 06-10-01-001. NO FURTHER CRACKS REMAIN.
- [SDR FDEA2019111542959](https://openairdocs.org/sdr/FDEA2019111542959), Nov 14, 2019: STOP. WORN. LATCH STOPS WORN ACCESS PANEL 311AB RH SIDE. TITLE: FUSELAGE - PLATES AND SKINS - 311AB ACCESS DOOR CUTOUT LANDING SKIN RH FWD DAMAGE REPAIR WAS ACCOMPLISHED ON
- [SDR FDEA2019111522935](https://openairdocs.org/sdr/FDEA2019111522935), Nov 12, 2019: NUT PLATE. DAMAGED. LT I/B FLAP INBOARD HOIST FITTING HAS 2 EACH NUT PLATES STRIPPED OUT. REMOVED AND REPLACED 2 EA NUT PLATES ON LT I/B FLAP I/B HOIST FITTING IAW DWG ARC2369 AND 
- [SDR FDEA2019102412717](https://openairdocs.org/sdr/FDEA2019102412717), Oct 21, 2019: FLOOR PANEL. DAMAGED. MAIN CARGO FLOOR PANEL BETWEEN STA 595 AND STA 675 BETWEEN X27.5 AND X47.5 IS DAMAGED. MAIN CARGO FLOOR PANEL AT STA 595 TO STA 675 BETWEEN X27.5 AND X47.5 FABR
- [SDR FDEA2019102412716](https://openairdocs.org/sdr/FDEA2019102412716), Oct 21, 2019: FLOOR PANEL. DAMAGED. MAIN CARGO FLOOR PANEL BETWEEN STA 765 AND STA 795 BETWEEN X91.5 AND X107.5 IS DAMAGED. MAIN CARGO FLOOR PANEL BETWEEN STA 765 TO 795 BEWTEEN X91.5 AND X107.5 F
- [SDR FDEA2019102412715](https://openairdocs.org/sdr/FDEA2019102412715), Oct 21, 2019: FLOOR PANEL. DAMAGED. MAIN CARGO FLOOR PANEL BETWEEN STA 495 AND STA 595 BETWEEN X27.5 AND X47.5 IS DAMAGED. MAIN CARGO FLOOR PANEL BETWEEN STA 495 AND STA 595 BETWEEN X27.5 AND X47.
- [SDR FDEA2019102412714](https://openairdocs.org/sdr/FDEA2019102412714), Oct 21, 2019: FLOOR PANEL. DAMAGED. MAIN CARGO FLOOR PANEL BETWEEN STA 675 AND STA 735 BETWEEN X27.5 AND X47.5 IS DAMAGED. MAIN CARGO FLOOR PANEL AT STA 675 - STA 735 BETWEEN X27.5 TO X47.5 FABRIC
- [SDR FDEA2019102412713](https://openairdocs.org/sdr/FDEA2019102412713), Oct 21, 2019: FLOOR PANEL. DAMAGED. MAIN CARGO FLOOR PANEL BWTWEEN STA 595 AND STA 675 BETWEEN -X75.5 AND -X107.5 IS DAMAGED. MAIN CARGO FLOOR PANEL BETWEEN STA 595-675 AND BETWEEN -X75.5 AND -X10
- [SDR FDEA2018042601108](https://openairdocs.org/sdr/FDEA2018042601108), Apr 24, 2018: LIGHT. MALFUNCTIONED. DURING PREFLIGHT, WHEN SELECTING EMERGENCY PWR SWITCH TO ARM, THE ON LIGHT REMAINED ILLUMINATED. RESET FUEL LEVERS. ACFT HAD POWER DROP OFF DURING PREFLIGHT. CO
- [SDR FDEA201712283460](https://openairdocs.org/sdr/FDEA201712283460), Dec 28, 2017: TRANSMITTER. OUT OF ADJUST. AT 121 KNOTS DURING TAKEOFF, RECEIVED AN AUDIBLE WARNING FOR THE FLAPS, FOLLOWED BY A WARNING FOR THE SLATS. . REJECTED TAKEOFF AT 130 KNOTS. PERFORMED A FLAP I
- [SDR FDEA201711043166](https://openairdocs.org/sdr/FDEA201711043166), Nov 4, 2017: BULKHEAD. CRACKED. NR 3 AC PACK COMPARTMENT STA 475 BULKHEAD WEB, A/C CHECK VALVE FASTENER HOLE AT 4:30 POSITION HAS A .5 INCH CRACK PROPAGATING THROUGH HOLE. REPAIRED PER EA 8-53
- [SDR FDEA201710102886](https://openairdocs.org/sdr/FDEA201710102886), Oct 10, 2017: PANEL. DELAMINATED. LT WING, PANEL 541 LB IS DELAMINATED/SPLIT. REPAIRED LT WING, PANEL 541 LB AT THE DELAMINATED/SPLIT AREA REF SRM 51-71-00 VOL 2 PG 1-47 AND DRAWING NUMBER ARC03
- [SDR FDEA201710042856](https://openairdocs.org/sdr/FDEA201710042856), Oct 4, 2017: SEAT TRACK. WORN. MAIN DECK APPROX STA 1265, CENTER LINE X.8.5 SEAT TRACK IS DAMAGED. REPAIRED SEAT TRACK PER SRM 53-70-00 FIG 1.
- [SDR FDEA201710042855](https://openairdocs.org/sdr/FDEA201710042855), Oct 4, 2017: SEAT TRACK. WORN. SEAT TRACK AT BS 625, RBL 27.5 IS DAMAGED. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 1.
- [SDR FDEA201710042854](https://openairdocs.org/sdr/FDEA201710042854), Oct 4, 2017: SEAT TRACK. DAMAGED. SEAT TRACK BS 1581, LBL 75 DAMAGED. REPAIRED IAW SRM 53-70-00, FIG 1.
- [SDR FDEA201710042853](https://openairdocs.org/sdr/FDEA201710042853), Oct 4, 2017: SEAT TRACK. DAMAGED. MAIN DECK SEAT TRACK BS 565, LBL 8.5 SHOWS DAMAGE. REPAIRED IAW SRM 53-70-00, FIG 1.
- [SDR FDEA201710033020](https://openairdocs.org/sdr/FDEA201710033020), Oct 3, 2017: CHANNEL. CRACKED. NR 3 A/C COMPARTMENT BS 555, LONGERON 34R FRAME J-CHANNEL HAS A 1.5 INCH CRACK. INSTALLED A TYPICAL FORMED CHANNEL REPAIR IAW SRM 53-00-01, FIG.8, SHEET 2, PAGE
- [SDR FDEA201710032846](https://openairdocs.org/sdr/FDEA201710032846), Oct 3, 2017: SEAT TRACK. DAMAGED. MAIN CARGO COMPT APPROX STA 1601 RBL 75 SEAT TRACK IS DAMAGED. REPAIRED SEAT TRACK PER SRM 53-70-00 FIG 1.
- [SDR FDEA201710032844](https://openairdocs.org/sdr/FDEA201710032844), Oct 3, 2017: SEAT TRACK. WORN. MAIN DECK, APPROX STA 1039 LBL 75 GROOVE/ GOUGE WORN INTO TRACK. SEAT TRACK IS DAMAGED. REPAIRED PER SRM 53-70-00 FIG 1.
- [SDR FDEA201710012877](https://openairdocs.org/sdr/FDEA201710012877), Oct 1, 2017: FRAME. CRACKED. CENTER CARGO BAY, APPROXIMATELY BS 1841, LBL 6 AND RBL 6, FRAME WEB IS CRACKED. REPAIRED THE FRAME IAW SRM 51-00-01, FIG 10, SHT 5, VOL I.
- [SDR FDEA201709303046](https://openairdocs.org/sdr/FDEA201709303046), Sep 30, 2017: SKIN. CRACKED. LEFT OTBD FLAP UPPER SKIN HAS A .75 INCH CRACK AT XOF 572. 5 INCHES FWD OF TRAILING EDGE. REPAIRED IAW SRM 57-00-01, FIG 4, SHT 2.
- [SDR FDEA201709303045](https://openairdocs.org/sdr/FDEA201709303045), Sep 30, 2017: SKIN. CRACKED. LEFT OTBD FLAP UPPER SKIN HAS A 2.875 INCH CRACK AND A .4 INCH CRACK AT XOF 569. 8 INCHES FWD OF TRAILING EDGE. REPAIR IAW SRM 57-00-01, FIG 4, SHT 2.
- [SDR FDEA201709303044](https://openairdocs.org/sdr/FDEA201709303044), Sep 30, 2017: SKIN. CRACKED. LEFT OTBD FLAP UPPER SKIN HAS A 2.0 IN. CRACK AT XOF 563. 12 INCHES FWD OF TRAILING EDGE. REPAIR IAW SRM 57-00-01, FIG 4, SHT 2.
- [SDR FDEA201709283088](https://openairdocs.org/sdr/FDEA201709283088), Sep 28, 2017: SKIN. CRACKED. LOWER FUSELAGE NR 1 ACM EXHAUST DOOR CUT OUT UPPER AFT CORNER IS CRACKED FROM SKIN EDGE TO FASTENER HOLE. ACCOMPLISHED EA WORK CARD 8-5340-T0336191.
- [SDR FDEA201709283087](https://openairdocs.org/sdr/FDEA201709283087), Sep 28, 2017: SKIN. CRACKED. LOWER FUSELAGE NR 1 ACM EXHAUST DOOR CUT OUT, AFT LOWER CORNER IS CRACKED FROM SKIN EDGE TO FASTENER HOLE. ACCOMPLISHED EA WORK CARD 8-5340-0336191. MAJOR REPAI
- [SDR FDEA201709283028](https://openairdocs.org/sdr/FDEA201709283028), Sep 28, 2017: DOOR. CRACKED. LOWER FUSELAGE NR 3 ACM ACCESS DOOR UPPER FLANGE PREVIOUS REPAIR HAS CONTINUED TO CRACK. REPAIRED THE NR 3 ACM DOOR UPPER FLANGE CRACK IAW EA 8-5240-T0336127.
- [SDR FDEA201709273132](https://openairdocs.org/sdr/FDEA201709273132), Sep 27, 2017: TEE FITTING. CRACKED. BS 595, BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 39L HAS A 2 INCH. CRACK EXTENDED THROUGH THE RADIUS. REPAIED THE BULKHEAD TEE CAP IAW EA T 8-5310-T0335740, PA
- [SDR FDEA201709273003](https://openairdocs.org/sdr/FDEA201709273003), Sep 27, 2017: BULKHEAD WEB. CRACKED. NOSE WHEEL WELL RIGHT VERTICAL PANEL AT APPROX STA 480 HAS A CRACK APPROX 6 INCH LONG. INSTALLED WEB SECTION AND DOUBLERS REF. SRM 53-00-01 FIG.10 (SHEET 5) VOL
- [SDR FDEA201709272925](https://openairdocs.org/sdr/FDEA201709272925), Sep 27, 2017: WEB. CRACKED. NOSE WHEEL WELL LEFT VERTICAL WEB PANEL BS 315, HAS A CRACK BEHIND THE HYDRAULIC LINES. REMOVED AND REPLACED DAMAGED SECTION OF THE WEB IAW SRM 53-00-01, FIG 10
- [SDR FDEA201704201245](https://openairdocs.org/sdr/FDEA201704201245), Apr 20, 2017: WARNING MESSAGE. FALSE INDICATION. AT FL 350, HAD A LEVEL 3 AIR MANIFOLD 3 FAILURE. RAN QRH, ALERT WENT AWAY. DECLARED AN EMERGENCY AND DIVERTED TO NEAREST SUITABLE AIRPORT. CHECKED MANIFOLD FAIL
- [SDR FDEA201701030027](https://openairdocs.org/sdr/FDEA201701030027), Jan 3, 2017: WARNING LIGHT. FALSE ACTIVATION. R1 DOOR SLIDE LIGHT ILLUMITATED. PERFORMED OPERATIONAL CHECK OF THE R1 DOOR SLIDE BOTTLE PRESSURE LIGHT IAW AMM 25-61-03-5-0. TESTED GOOD SEVERAL TIMES. OK FOR 
- [SDR FDEA201602140557](https://openairdocs.org/sdr/FDEA201602140557), Feb 14, 2016: TEST SWITCH. FAULTY. R1 DOOR EVAC SLIDE, REMOTE PRESSURE PRESS TO TEST INDICATING SYS INOPERATIVE. RELEASED FOR SERVICE IAW MEL 25-61-01, CATEGORY C, EXPIRATION 24 FEB 16. EVAC SLID
- [SDR FDEA201510263375](https://openairdocs.org/sdr/FDEA201510263375), Oct 26, 2015: SKIN PANEL. CRACKED. LEFT HORIZONTAL STABILIZER SKIN PANEL 7281-1, HAS A .700" CRACK JUST FWD OF REAR SPAR CAP, FWD BARREL NUT HOLE. R & R SECTION OF SKIN PANEL, PLANK, IAW EA 8-551
- [SDR FDEA201510263374](https://openairdocs.org/sdr/FDEA201510263374), Oct 26, 2015: SPAR CAP. CRACKED. LEFT HORIZONTAL STABILIZER, UPPER OUTER REAR SPAR CAP, FWD BARREL NUT HOLE HAS A .400" VERTICAL CRACK EXTENDING FROM BELOW THE BARREL NUT AT THE 5:00 POSITION. 
- [SDR FDEA201510233327](https://openairdocs.org/sdr/FDEA201510233327), Oct 23, 2015: PANEL. DELAMINATED. LEFT WING HINGE PANEL 551DB HAS DELAMINATION. REPAIRED THE HINGE PANEL IAW SRM 51-71-00 VOL II. PREPPED & PAINTED IAW SRM 51-21-02 VOL II.
- [SDR FDEA201510223316](https://openairdocs.org/sdr/FDEA201510223316), Oct 22, 2015: PANEL. DELAMINATED. AFT ENG INLET DUCT, RT SIDE PANEL 364JR, LOWER SFT DELAMINATED. REPAIRED PANEL 364JR IAW SRM 51-71-00 VOL II. PREPPED & PAINTED IAW SRM 51-21-02 VOL II.
- [SDR FDEA201510223315](https://openairdocs.org/sdr/FDEA201510223315), Oct 22, 2015: PANEL. DELAMINATED. AFT ENG INLET DUCT, RT SIDE PANEL 364JR DELAMINATED, LOWER FWD. REPAIRED PANEL 364JR IAW SRM 51-71-00 VOL. II. PREPPED & PAINTED IAW SRM 51-21-02 VOL II.
- [SDR FDEA201510203292](https://openairdocs.org/sdr/FDEA201510203292), Oct 20, 2015: FUEL DOOR. DAMAGED. RIGHT WING REFUEL & DEFUEL DOOR, PUNCTURED ON UPPER MID SURFACE. REPAIR IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-02 VOL II.
- [SDR FDEA201510203291](https://openairdocs.org/sdr/FDEA201510203291), Oct 20, 2015: PANEL. DELAMINATED. LEFT WING NR 5 SPOILER PANEL HAS DELAMINATION, UPPER SURFACE. REPAIR SPOILER IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-02 VOL II.
- [SDR FDEA201510203285](https://openairdocs.org/sdr/FDEA201510203285), Oct 20, 2015: WIRE. DAMAGED. FOUND WIRE DAMAGED, LOCATED AT BS 1346, RT OF CENTERLINE OF ACFT. SPLICED IN A NEW WIRE IAW SWPM 20-10-03, 20-00-16, WDM 29-12-01, AND E8-2810-7-5002 PT 1.
- [SDR FDEA201510203284](https://openairdocs.org/sdr/FDEA201510203284), Oct 20, 2015: WIRE. DAMAGED. FOUND DAMAGED WIRE LOCATED AT BS 1346, RT SIDE OF CENTERLINE. SPLICED IN NEW WIRE IAW SWPM 20-10-03, 20-00-16, WDM 33-32-02, AND E8-2810-7-5002 PT1.
- [SDR FDEA201510203283](https://openairdocs.org/sdr/FDEA201510203283), Oct 20, 2015: WIRE. DAMAGED. FOUND WIRE DAMAGED, LOCATED AT BS 1240, RT SIDE OF CENTERLINE OF ACFT. REPLACED WIRE IAW SWPM 20-10-03, 20-00-16, WDM 28-21-03, AND E8-2810-7-5002 PT1.
- [SDR FDEA201510203282](https://openairdocs.org/sdr/FDEA201510203282), Oct 20, 2015: WIRE. DAMAGED. FOUND WIRE DAMAGED, LOCATED AT BS 1346, RT OF CENTERLINE. SPLICED IN NEW WIRE IAW SWPM 20-10-03, 20-00- 16, WDM 52-33-01 AND E8-7-2810-5002 PT1.

All 183: https://openairdocs.org/aircraft/N320FE/reports.md

## STCs that may be installed (OpenAirDocs) (73, first 50)

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

### Approved for the airframe (Mcdonnell Douglas MD-10-30F)

- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST01391LA](https://openairdocs.org/stc/ST01391LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST02184CH](https://openairdocs.org/stc/ST02184CH): Installation of elementary or enhanced surveillance Mode S transponders. Amphenol Cable and Interconnect Technologies Inc
- [STC ST02002WI](https://openairdocs.org/stc/ST02002WI): Replacement of Rockwell Collins LRA-900 Low Range Radio Altimeters with upgraded LRA-900 units for improved RF immunity to 5G cellular data interference. Rockwell Collins, Inc
- [STC ST03367AT](https://openairdocs.org/stc/ST03367AT): Installation of dual Artex Model C406-N Emergency Locator Transmitters (ELT). Woven Electronics LLC
- [STC ST00536SE](https://openairdocs.org/stc/ST00536SE): Installation of the Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS). Honeywell International Inc
- [STC ST02126AT](https://openairdocs.org/stc/ST02126AT): Courier seat installation. GDC Technics LLC
- [STC ST03879AT](https://openairdocs.org/stc/ST03879AT): Installation of Talon Aerospace Cargo Lights. Aaxico Technical Services Inc
- [STC ST03574AT](https://openairdocs.org/stc/ST03574AT): Installation of a Talon Aerospace Anti-Collision Light. Aaxico Technical Services Inc
- [STC ST04002AT](https://openairdocs.org/stc/ST04002AT): Installation of a Talon LED Replacement Wing and Tail Mounted Anti-Collision Lights. Aaxico Technical Services Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST04092NY](https://openairdocs.org/stc/ST04092NY): Installation of Wireless PCMCIA for DFDAU. Delta Engineering Corporation
- [STC ST02532LA](https://openairdocs.org/stc/ST02532LA): Modify the wing fuel tanks access cover installation by replacing the existing rubstrip and seal with a new encapsulated wire mesh gasket and a new seal. Aviation Devices & Electronic Components LLC
- [STC ST02669LA](https://openairdocs.org/stc/ST02669LA): Installation of Honeywell MKV EGPWS with Landing Performance Enhancement (LPE) functionality. Honeywell International Inc
- [STC ST00349LA](https://openairdocs.org/stc/ST00349LA): Installation of cargo handling system. Ancra International LLC
- [STC ST01805WI](https://openairdocs.org/stc/ST01805WI): Modification of Rockwell Collins TCAS II System Installation with DC powered TCAS Transmitter Receiver Processor. Rockwell Collins Inc
- [STC ST00399DE](https://openairdocs.org/stc/ST00399DE): Installation of nose radome shell assembly. The NORDAM Group LLC
- [STC ST00687AT-D](https://openairdocs.org/stc/ST00687AT-D): Interior Reconfiguration. HAECO Cabin Solutions LLC
- [STC ST02639LA](https://openairdocs.org/stc/ST02639LA): Replace the existing Mode S Transponder system. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST04323CH](https://openairdocs.org/stc/ST04323CH): Installation of ADS-B OUT Global Positioning Satellite System (GPSS)/Space-Based Augmentation System (SBAS) & ADS-B IN Flight Information Services-Broadcast (FIS-B) system. Innoviator LLC
- [STC ST03967AT](https://openairdocs.org/stc/ST03967AT): Installation of an Avionica, Inc. avWiFi wireless router system. Archeion Holdings LLC
- [STC ST04376AT](https://openairdocs.org/stc/ST04376AT): Installation of a Cobham INMARSAT/SwiftBroadband SATCOM System. Avionics Support Group Inc
- [STC ST01289LA](https://openairdocs.org/stc/ST01289LA): Insulation Blankets Installation. Lamart California Inc
- [STC ST02406LA](https://openairdocs.org/stc/ST02406LA): Installation of TCAS version 7.1. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST02599LA](https://openairdocs.org/stc/ST02599LA): Installation of Oxygen Aneroid Switch P/N 44A3-4 for aircraft to be used for high altitude airports. AeroSys Inc
- [STC ST02580LA](https://openairdocs.org/stc/ST02580LA): Reconfigure an MD-10-30F to support a modular eye hospital with 48 supernumeries. ORBIS International Inc
- [STC ST02589LA](https://openairdocs.org/stc/ST02589LA): Installation of main deck cargo loading system. Ancra International LLC
- [STC ST00864LA](https://openairdocs.org/stc/ST00864LA): Modification of existing Litton LTN-72R Inertial navigation system to include VOR/DME RNAV updating. Northrop Grumman Systems Corporation
- [STC ST02540LA](https://openairdocs.org/stc/ST02540LA): Installation of Telair International LLC light weight P/Ns PMC100 and PAG100 series cargo pallets. Telair International LLC
- [STC SA5466NM](https://openairdocs.org/stc/SA5466NM): Installation of Telair International cargo loading systems. Telair International LLC
- [STC ST01347LA](https://openairdocs.org/stc/ST01347LA): Installation of a lower lobe anti-rollout latch Telair part number 92036-1, -2. Telair International LLC
- [STC ST02489LA](https://openairdocs.org/stc/ST02489LA): Installation of Telair International Inc. light weight LD3 (NAS3610 / SAE36100 - 2K2) cargo container P/N LD3100-31000ZZZ. Telair International LLC
- [STC ST04214AT](https://openairdocs.org/stc/ST04214AT): Installs a standalone Astronics AES 110V AC 60 Hz and 5V DC power system with two outlets in the cockpit. FedEx Express
- [STC SA3892WE](https://openairdocs.org/stc/SA3892WE): Installation of Stowe Corp. service carts. Driessen Aircraft Interior Systems, Inc DBA Zodiac Galleys USA Inc
- [STC ST03327AT](https://openairdocs.org/stc/ST03327AT): Installation of a Dual NavAero Class 2 Electronic Flight Bags (EFB) . Avionics Support Group Inc
- [STC ST03483AT](https://openairdocs.org/stc/ST03483AT): Installation of a Portable Beverage Dispensing System, P/N B43-FA-001. Dynamo Beverage Company, USA, L.L.C
- [STC ST00503LA](https://openairdocs.org/stc/ST00503LA): Installation of Securaplane Model No. BC-1302 Battery Charger, Battery Temperature Sensor Model No. BTS-1302 and Remote Display Unit Model No. DU-1302 as a form, fit, and functional replacement for the existing General Electric Battery Charger System. Securaplane Technologies
- [STC ST02050LA](https://openairdocs.org/stc/ST02050LA): Installation of Goodrich-Hella Anticollision Recognition Lighting System (ARLS). Goodrich
- [STC SA5016NM](https://openairdocs.org/stc/SA5016NM): Installation of cargo containers. Satco Inc
- [STC ST03557AT](https://openairdocs.org/stc/ST03557AT): Installation of a Honeywell head up display and a Kollsman infrared enhanced flight vision system (HUD/EFVS). Federal Express Corp
- [STC ST09368SC](https://openairdocs.org/stc/ST09368SC): Installation of a supplemental crew oxygen system. Schwartz Aviation LLC
- [STC SA3415NM](https://openairdocs.org/stc/SA3415NM): Installation of a main cabin cargo handling system. Ancra International LLC
- [STC SA5003NM](https://openairdocs.org/stc/SA5003NM): Installation of a cabin cargo handling system. Ancra International LLC
- [STC ST03944AT](https://openairdocs.org/stc/ST03944AT): Installation of Avionica, Inc. satLINK System to provide voice and short burst data communications over the Iridium satellite Communications network (SATCOM), with Wi-Fi voice over IP (VoIP) cordless phone in accordance with Archeion Holdings LLC Master Data List 102810-MDL, Revision D, Dated January 17, 2012, or later FAA approved revisions. Archeion Holdings LLC
- [STC ST01338CH](https://openairdocs.org/stc/ST01338CH): Installation of an Auxiliary Power Unit Door Actuator System. Woodward MPC
- [STC ST02540AT-D](https://openairdocs.org/stc/ST02540AT-D): Installation of replacement fuel tank sealant system. FFC Manufacturing
- [STC ST00688AT-D](https://openairdocs.org/stc/ST00688AT-D): Sony Transcom Video Monitor Installation. TIMCO
- [STC ST03662AT](https://openairdocs.org/stc/ST03662AT): Installation of an L-3 Communications FA2100CVR Cockpit Voice Recorder. Chippewa Aerospace, Inc

All 73: https://openairdocs.org/aircraft/N320FE/stcs.md

## Related

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

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