# N321FE: 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 CF6-50C2](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: 47836
- Year built: 1980
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 29, 2010
- Certificate issued: June 28, 2012
- Expires: June 30, 2028
- Mode S code: A37289
- 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=321FE
- Page: https://openairdocs.org/aircraft/N321FE

From the FAA registry file of October 22, 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/N321FE/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 N321FE.

## 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 19950125003389I](https://openairdocs.org/incident/19950125003389I), Jan 25, 1995: Doug DC1030 (N321FE), Philadelphia, PA, Minor damage. Narrative: during takeoff out of Philadelphia, captain observed deer crossing runway at V1 speeds. Continued takeoff and landed at ewr. Maintenance inspected…

## Service difficulty reports (193, 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 FDEA202211182822](https://openairdocs.org/sdr/FDEA202211182822), Nov 18, 2022: VANE. DELAMINATED. L/H O/B FLAP VANE #5 RUBSTRIP DELAM ( POS INTERIOR DELAM) REPAIRED L/H O/B FLAP VANE AT #5 RUBSTRIP AS REQUIRED PER SRM 51-71-00, VOL.II, PARA. #17 PG. 75-80, I
- [SDR FDEA202211172813](https://openairdocs.org/sdr/FDEA202211172813), Nov 17, 2022: RUB STRIP. DELAMINATED. DELAMINATED RUBSTRIP. R & R THE RUB STRIP IAW DWG ARC1455.
- [SDR FDEA202211162828](https://openairdocs.org/sdr/FDEA202211162828), Nov 16, 2022: VANE. DELAMINATED. LH OUTBD FLAP VANE #5 RUBSTRIP DELAM ( POS INTERIOR DELAM) REPAIRED PER SRM 57-00-01 FIG.4, SHEET 1
- [SDR FDEA2021083062136](https://openairdocs.org/sdr/FDEA2021083062136), Aug 26, 2021: FRAME. CORRODED. INSIDE AIR CONDITIONING COMPARTMENT BETWEEN #1 & # 2 ACM AT STATION 541.667 BOTTOM OF ACA3348-3 FRAME HAS CORROSION AT LOWER FLANGE. REPAIRED INBOARD LOWER FLAN
- [SDR FDEA202108252115](https://openairdocs.org/sdr/FDEA202108252115), Aug 25, 2021: ANGLE. CORRODED. INSIDE AIR CONDITIONING COMPARTMENT BETWEEN #1 & #2 ACM APPROX. STA 540 AT BOTTOM OF BULKHEAD VERTICAL FLANGE OF CHORD ANGLE HAS EXFOLIATION CORROSION APPROX. F
- [SDR FDEA2021083042114](https://openairdocs.org/sdr/FDEA2021083042114), Aug 24, 2021: RIB. CRACKED. VERTICAL STAB L/E - PNL #371CLE HAS CRACKED RIB - 7TH FROM BOTTOM L/H SIDE TRIMMED OUT DAMAGE AND INSTALLED REPAIR ANGLE AND FILLER REFERENCE SRM 55-00-01 FIG. 
- [SDR FDEA202108232076](https://openairdocs.org/sdr/FDEA202108232076), Aug 23, 2021: SKIN. CRACKED. LOWER AFT RUDDER, BOTTOM RHS AFT SECTION HAS AN APPROX 1" CRACK, MARKED. REMOVED AND REPLACED LOWER AFT RUDDER. REF AMM 27-20-01-4 INSTALLED P/N: NMC6015- 505 S
- [SDR FDEA202108212055](https://openairdocs.org/sdr/FDEA202108212055), Aug 21, 2021: SKIN. DELAMINATED. R/H O/B ELEVATOR TRAILING EDGE DELAM. (MARKED) REPAIRED O/B TRAILING EDGE ELEVATOR ENVELOPE PER SRM 55-30-00 VOL.1 PGS 1-9. "MAJOR REPAIR"
- [SDR FDEA202108092002](https://openairdocs.org/sdr/FDEA202108092002), Aug 9, 2021: SKIN. DENTED. FUSELAGE EXTERIOR SKIN DENT/CREASE - AFT OF CENTER CARGO AT APPROX STA.1850 BETWEEN LONGS 38-39. CUT OUT DAMAGED SKIN AT STA. 1850 BETWEEN LONGERONS 38R AND 39R
- [SDR FDEA202107241851](https://openairdocs.org/sdr/FDEA202107241851), Jul 24, 2021: SKIN. DAMAGED. LEFT WING O/B FLAP UPPER I/B T/E SPLIT AT CONNECTION AND DAMAGED AT CORNER. (DOT 6) REMOVED, FABRICATED AND INSTALLED L/H WING O/B FLAP UPPER I/B T/E DAMAGED SE
- [SDR FDEA202107211829](https://openairdocs.org/sdr/FDEA202107211829), Jul 21, 2021: FLOORBOARD. DAMAGED. FWD CARGO FLOOR PANEL ADA0241-51(127WF) FABRICATED NEW FLOOR REF FEDEX DWG SRZ-25-005
- [SDR FDEA202107131969](https://openairdocs.org/sdr/FDEA202107131969), Jul 13, 2021: LOCK. SHEARED. L/H WING TOP SURFACE - TAPER LOCK STICKING UP FROM TOP SURFACE OF WING - APPROXIMATE STA XORS 275 ON GROSS WEIGHT MOD DOUBLER AFT OF REAR SPARE 0003748737 : KOT
- [SDR FDEA202107131848](https://openairdocs.org/sdr/FDEA202107131848), Jul 13, 2021: FRAME. WORN. CENTER CARGO COMPT FUSE FRAM SECTION REMOVED TO FOM STA 1787 L47R-L49R. INSTALLED STA. 1787 FRAME SECTION FROM LONGERON 47R TO 49R REF DOUGLAS DRAWING AFA 7112.
- [SDR FDEA202107131919](https://openairdocs.org/sdr/FDEA202107131919), Jul 13, 2021: FRAME. DAMAGED. CENTER CARGO COMPT FUSE FRAME SECTION REMOVED TO FOM STA 1801 L47L-L45R. INSTALLED STA. 1801 FRAME SECTION FROM LONGERON 47L AT B/P SPLICE TO 45R REF.DOUGLAS DR
- [SDR FDEA202107131847](https://openairdocs.org/sdr/FDEA202107131847), Jul 13, 2021: LONGERON. WORN. CENTER CARGO COMPT L47R HAS EXFOLITATION CORROSION ON INBOARD SIDE STA 1775. INSTALLED NEW SECTION OF LONGERON 47R FROM EXISTING SPLICE LOCATION AT STA. 1775 TO
- [SDR FDEA202107131772](https://openairdocs.org/sdr/FDEA202107131772), Jul 13, 2021: FLOOR PANEL. DELAMINATED. MAIN DECK FLOOR BOARD AT STATION 1039 L/H SIDE WITH 5/L MARKING FOUND TO BE SPONGE/SOFT FABRICATED NEW FLOOR PANEL MAIN DECK AT STATION 1039 L/H SIDE WITH 5/L M
- [SDR FDEA202107101939](https://openairdocs.org/sdr/FDEA202107101939), Jul 10, 2021: SUPPORT. CORRODED. MAIN CABIN AFT LAV SUPPORT AGA7087-504 STATION 1891-2007 RBL-24 EXFOLIATION CORROSION EXISTS UNDER DOME NUTS. INSTALLED NEW/FABRICATED AFT LAV SUPPORT ON MAIN C
- [SDR FDEA202107091846](https://openairdocs.org/sdr/FDEA202107091846), Jul 9, 2021: RIB. CRACKED. R/H WING UPPER FILLET PANEL SUPPORT RIB ANB7142-10 AT STATION 1341 CRACKED LOWER END. REMOVED AND REPLACED RIGHT HAND WING UPPER FILLET PANEL SUPPORT RIB ANB714
- [SDR FDEA202107082023](https://openairdocs.org/sdr/FDEA202107082023), Jul 8, 2021: BULKHEAD WEB. WORN. MAIN CARGO STATION 2007 LBL 30 HOLE DAMAGED ON PRESSURE BULKHEAD AT FLOOR BOARD SUPPORT TEE REPAIRED HOLE PER SRM 51-39-01 VOL II. REF. E.A # 8-5310-T0363077 TI
- [SDR FDEA202107061942](https://openairdocs.org/sdr/FDEA202107061942), Jul 6, 2021: SUPPORT. CORRODED. MAIN CABIN AFT LAV SUPPORT AGA7544-1 STATION 1891-2007 LBL 24 EXFOLIATION CORROSION EXISTS ON FOWARD END BEYOND LIMITS INSTALLED NEW/FABRICATED AFT LAV SUPPORT 
- [SDR FDEA202106301622](https://openairdocs.org/sdr/FDEA202106301622), Jun 30, 2021: VANE. WORN. R/H INB'D T/E FLAP VANE INB'D L/E AREA SHOWING RUBBING DAMAGE. REPAIRED R/H INB FLAP VANE I/B L/E PER SRM 51-71-00 VOL II PAR 16 PG 64. I.A.W. SRM 57-00-01 FIG 
- [SDR FDEA202106221811](https://openairdocs.org/sdr/FDEA202106221811), Jun 22, 2021: LONGERON. CORRODED. CENTER CARGO COMP. APPROX. STA 1750 TO 1781 LONG 46R FOUND SEVERAL AREAS OF CORROSION INSIDE HAT SECTION OF LONGERON. (MKD) REMOVED CORRODED SECTIONS AND INSTAL
- [SDR FDEA202106221647](https://openairdocs.org/sdr/FDEA202106221647), Jun 22, 2021: FRAME. CRACKED. LEFTHAND WING; XORS=570 LEADING EDGE INTERNAL FRAME STRAP HAS 6" CRACKS @ UPPER OUTBOARD SECTION. REMOVED AND REPLACED LEFT WING XORS 570 LEADING EDGE INTERNAL 
- [SDR FDEA202106221592](https://openairdocs.org/sdr/FDEA202106221592), Jun 22, 2021: ANGLE. CRACKED. L/H WING #2 SLAT OUTBOARD CAP CRACKED AT THE ANGLE #2 SLAT OUTBOARD CAP ANGLE REPAIR PER SRM 57-00-01 FIG 10 VOL 1 . "MAJOR REPAIR"
- [SDR FDEA202106211812](https://openairdocs.org/sdr/FDEA202106211812), Jun 21, 2021: LONGERON SPLICE. CORRODED. CENTER GARGO COMPARTMENT BILGE - APPROX STA.1808 46R - EXFOLIATION CORROSION ON LONG AND SPLICE. REMOVED CORRODED LONGERON SECTIONS AND INSTALLED NEW SECTIONS O
- [SDR FDEA202106211626](https://openairdocs.org/sdr/FDEA202106211626), Jun 21, 2021: WEB. DENTED. CENTER CARGO COMPT STA 1841 AT FLOOR LEVEL WEB IS DENTED FROM CONTAINER CONTACT. MRKD LBL 15 TO RBL 5. REMOVED AND REPLACED DAMAGED WEB AGA7170-3 IAW DAC DWG AG
- [SDR FDEA202106192025](https://openairdocs.org/sdr/FDEA202106192025), Jun 19, 2021: FLOOR SUPPORT. CORRODED. AFT FUSE WASTE TANK COMPT, CORROSION ON FLOOR SUPPORT FRAME AT STA 2007 APPROX. LBL24, (MARKED #13) PERFORMED "MAJOR REPAIR" PER SRM 53-40-00 FIG. 16 VOL. 1, SR
- [SDR FDEA202106192024](https://openairdocs.org/sdr/FDEA202106192024), Jun 19, 2021: FLOOR SUPPORT. CORRODED. AFT FUSE WASTE TANK COMPT, CORROSION ON FLOOR SUPPORT FRAME AT STA 2007 APPROX. RBL24, (MARKED #12) PERFORMED "MAJOR REPAIR" PER SRM 53-40-00 FIG. 16 VOL. 1, SR
- [SDR FDEA202106191783](https://openairdocs.org/sdr/FDEA202106191783), Jun 19, 2021: FLOOR SUPPORT. CORRODED. CENTER CARGO COMPT MAIN DECK FLOORBOARD SUPPORT CORRODED STA 1741 RBL 55. MRKD REMOVED AND REPLACED FLOORBOARD SUPPORT AT STA. 1741 RBL 55 CTR CARGO COMPT. PER 
- [SDR FDEA202106181665](https://openairdocs.org/sdr/FDEA202106181665), Jun 18, 2021: SKIN. CORRODED. AFT FUSE WASTE TANK COMPT, CORROSION ON INTERIOR OF FUSELAGE SKIN, AT EXISTING EXTERIOR DOUBLER AREA, AT STA 2000 BETWEEEN L-45 AND L-45 R/H. (MARKED #11) REMOV
- [SDR FDEA202106171699](https://openairdocs.org/sdr/FDEA202106171699), Jun 17, 2021: DOOR FRAME. WORN. MAIN CARGO DECK, LH SIDE, STA. 535, LONG 23, FRAME GOUGED BY LOWER HINGE HARDWARE OF CARGO NET BRACKET. DOT #10. REMOVED DAMAGED PREVIOUS "L" ANGLE REPAIR AND I
- [SDR FDEA202106171698](https://openairdocs.org/sdr/FDEA202106171698), Jun 17, 2021: DOOR FRAME. DAMAGED. MAIN CARGO DECK, LH SIDE, STA. 535, LONG 20, FRAME GOUGED BY UPPER HINGE HARWARE OF CARGO NET BRACKET. DOT #9. REMOVED PREVIOUS "L" ANGLE REPAIR AND INSTALLED N
- [SDR FDEA202106161814](https://openairdocs.org/sdr/FDEA202106161814), Jun 16, 2021: SEAT TRACK. WORN. MAIN DECK: SEAT TRACK WORN, NEAR STA 1501 LBL 8.50 ON MAIN DECK: INSTALLED NEW SECTION OF SEAT TRACK AND SPLICE AT LBL 8.5 FROM STA 1501-1551 REF SRM 53-70-00 F
- [SDR FDEA202106161813](https://openairdocs.org/sdr/FDEA202106161813), Jun 16, 2021: SEAT TRACK. WORN. MAIN DECK: SEAT TRACK WORN, NEAR STA 1139 LBL 47.50 ON MAIN DECK: INSTALLED NEW SECTION OF SEAT TRACK AND SPLICE AT LBL 47.5 FROM STA 1129-1149 REF SRM 53-70-00
- [SDR FDEA202106161795](https://openairdocs.org/sdr/FDEA202106161795), Jun 16, 2021: SEAT TRACK. WORN. MAIN DECK: SEAT TRACK WORN, NEAR STA 1370 RBL 47.50 INSTALLED NEW SECTION OF SEAT TRACK ONLY WITH EXITING SPLICES AT RBL 47.5 FROM STA 1313-1411 REF SRM 53-70-0
- [SDR FDEA202106161794](https://openairdocs.org/sdr/FDEA202106161794), Jun 16, 2021: SEAT TRACK. WORN. MAIN DECK: SEAT TRACK WORN, NEAR STA 1139 RBL 8.50 INSTALLED NEW SECTION OF SEAT TRACK ONLY WITH EXITING SPLICES AT RBL 8.5 FROM STA 1129-1069 REF SRM 53-70-00 
- [SDR FDEA202106161792](https://openairdocs.org/sdr/FDEA202106161792), Jun 16, 2021: SEAT TRACK. WORN. MAIN DECK, GOUGES ON SEAT TRACK LOBES AT STA 1039 LBL 78 (MARKED #18) INSTALLED NEW SECTION OF SEAT TRACK AND SPLICE AT LBL 78 FROM STA 1009-1089 REF SRM 53-70-
- [SDR FDEA202106161713](https://openairdocs.org/sdr/FDEA202106161713), Jun 16, 2021: SKIN. DENTED. LH FUSELAGE APPROX STA.1894 BETWEEN L43-L44 - DENT ON SKIN. REPAIRED DAMAGED SKIN REF SRM 53-20-00 FIG.6 SHEETS 12-13 VOL. 1 AND SRM 51-31-01 VOL. 2.
- [SDR FDEA202106151769](https://openairdocs.org/sdr/FDEA202106151769), Jun 15, 2021: FLOORBOARD. DAMAGED. MAIN DECK, PUNTURE ON FLOOR BOARD STA 775 BL 0 (MARKED #16) FABRICATED NEW FLOOR BOARD PER SRZ-25-005
- [SDR FDEA202106151768](https://openairdocs.org/sdr/FDEA202106151768), Jun 15, 2021: FLOORBOARD. DAMAGED. MAIN DECK, PUNTURE ON FLOOR BOARD STA 775 BL 0 (MARKED #16) FABRICATED NEW FLOOR BOARD PER SRZ-25-005
- [SDR FDEA202106151770](https://openairdocs.org/sdr/FDEA202106151770), Jun 15, 2021: FLOORBOARD. DAMAGED. MAIN DECK, PUNTURE ON FLOOR BOARD STA 775 BL 0 (MARKED #16) FABRICATED NEW FLOOR BOARD PER SRZ-25-005
- [SDR FDEA202103160657](https://openairdocs.org/sdr/FDEA202103160657), Mar 16, 2021: ENGINE. FAILED. APPROXIMENTELY 30 MINUTES IN TO FLIGHT (FL350) CREW HEARD A VERY LOUD BANG WITH SIGNIFICANT AIRCRAFT YAW. OBSERVED ENGINE NO 1 N1 ROLL BACK WITH CONFIRM ENG OUT
- [SDR FDEA2020050860906](https://openairdocs.org/sdr/FDEA2020050860906), May 6, 2020: BOOT. DEFECTIVE. JUST AS BEGAIN DESCENT ONTO MEM RECEIVED LEVEL ONE AIR SYST 3 OFF ALERT AT APPROX IMATELY FL370 ASSOCIATED RED MANF LT NEXT TO #3 BLEED ALSO ILLUMINATED CORRESP
- [SDR FDEA2020043090841](https://openairdocs.org/sdr/FDEA2020043090841), Apr 29, 2020: ADIRU. FAILED. AT FL340 GOT IAS DISPLAYED ON PFD'S AS WELL AS WSHEAR DET FAIL SEL ELEV FEEL MAN AND SEL FLAP LIMIT OVED DISPLAY. COMPLIED WITH AIRSPEED UNRELIABLE CHECKLIST IN
- [SDR FDEA2020043090840](https://openairdocs.org/sdr/FDEA2020043090840), Apr 29, 2020: ADC. FAILED. AT FL340 GOT IAS DISPLAYED ON PFD'S AS WELL AS WSHEAR DET FAIL SEL ELEV FEEL MAN AND SEL FLAP LIMIT OVED DISPLAY. COMPLIED WITH AIRSPEED UNRELIABLE CHECKLIST IN
- [SDR FDEA2020010640019](https://openairdocs.org/sdr/FDEA2020010640019), Jan 4, 2020: POWER SUPPLY. FAILED. MDIS 321 33-50 6660 04JAN20 MEM OPEN U LOGPAGES:3133468 EMERGENCY LT BATT 1 LOW VOLTS FACT 05JAN20 22:09 MEM REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPLY O
- [SDR FDEA201910142639](https://openairdocs.org/sdr/FDEA201910142639), Oct 14, 2019: DIMMER. FAILED. DURING CLIMB ABOVE 18,000 FT, OVERHEAD PANEL WENT COMPLETELY DARK. NO INDICATION LIGHTS OF ANY KIND EXCEPT ENGINE IGNITION WERE ILLUMINATED. ON PREFLIGHT THE NR
- [SDR FDEA201909162254](https://openairdocs.org/sdr/FDEA201909162254), Sep 16, 2019: SEAT. FAULTY. CREW REPORTS CAPTAINS SEAT WILL NOT MOVE AFT MANUALLY WHEN POSITIONED FWD ALL THE WAY. REMOVED AND REPLACED CAPTAINS SEAT PER AMM 25-11-01-4, FUNCTION CHECK GOO
- [SDR FDEA201906301468](https://openairdocs.org/sdr/FDEA201906301468), Jun 30, 2019: SEAT TRACK. DAMAGED. UPPER MAIN DECK SEAT TRACK STA 735 LBL 110 CRACKED. REPAIRED DAMAGED SEAT TRACK FROM STATION 705 TO 725 REF. SRM 53-70-00 FIG. 1 VOL. 1, SRM 51-31-01 VOL. 2 AND
- [SDR FDEA201906301467](https://openairdocs.org/sdr/FDEA201906301467), Jun 30, 2019: SEAT TRACK. DAMAGED. UPPER MAIN DECK SEAT TRACK STA 645, LBL 110 CRACKED. REPAIRED DAMAGED SEAT TRACK FROM STATION 645 TO STATION 664, LBL 107 REF. SRM 53-70-00 FIG. 1 VOL. 1. AND D

All 193: https://openairdocs.org/aircraft/N321FE/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/N321FE/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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