# N306FE: 1985 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: 48287
- Year built: 1985
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 24, 1986
- Certificate issued: February 10, 2005
- Expires: August 31, 2029
- Mode S code: A3361E
- 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=306FE
- Page: https://openairdocs.org/aircraft/N306FE

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/N306FE/ads.md

## Information bulletins (advisory) (3 in force)

- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008
- [SAIB NM-06-57](https://openairdocs.org/saib/NM-06-57): Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.. Issued Jul 27, 2006

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ATL94LA077](https://openairdocs.org/ntsb/ATL94LA077), Apr 7, 1994: McDonnell Douglas DC-10-30 (N306FE), Memphis, TN, minor damage. Probable cause: Not Determined.

## FAA accident and incident reports

None matched to N306FE.

## Service difficulty reports (167, 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 FDEA202211292851](https://openairdocs.org/sdr/FDEA202211292851), Nov 29, 2022: ENGINE. FIRE. DURING ENGINE 1 START SEQUENCE, ENGINE TOOK LONGER THAN NORMAL TO START. IGNITER USED WAS B, SWITCHED TO A DURING START. ENGINE APPEARED TO START NORMALLY, BUT 
- [SDR FDEA202209222357](https://openairdocs.org/sdr/FDEA202209222357), Sep 22, 2022: BULB. NO TEST. ON ARRIVAL EVACUATE SLIDE REMOTE PRESS TO TEST INDICATION SWITCH L1 DOOR LIGHT INOP. REPLACED BULBS IN L1 DOOR INDICATOR PRESS TO TEST SWITCH IN REF TO AMM 25-6
- [SDR FDEA202206071399](https://openairdocs.org/sdr/FDEA202206071399), Jun 7, 2022: WARNING MESSAGE. ILLUMINATED. UNEVENTFUL FLIGHT FROM SMF UNTIL ALERT. LEVEL AT FL310 APROX 2 30 INTO FLIGHT. COST INDEX 200 GAVE US .837MACH. GOT TRI-TONE AND MASTER WARNING LIGHT, WITH "LWR
- [SDR FDEA202202180321](https://openairdocs.org/sdr/FDEA202202180321), Feb 18, 2022: NONE. NONE. DESCENDING INTO KMEM WITH FSC IN MANUAL, WE RECIEVED LEVEL 1 ALERT, TANK 3 QTY LO. FUEL WAS 7.1/6.2/5.2. THE QRH SAID TO TREAT AS REAL SO WE DECLARED AN EMERGEN
- [SDR FDEA202111282943](https://openairdocs.org/sdr/FDEA202111282943), Nov 28, 2021: NONE. NONE. THIS CARD IS CREATED FOR TRACKING PURPOSES TO CREATE A RDR/SDR FOR THE REPAIR DONE TO MCD LOWER JAMB AT STA. 697.87 UNDER E.A.8-5330-T0365660 B PART 2 CREATED R
- [SDR FDEA202107291917](https://openairdocs.org/sdr/FDEA202107291917), Jul 29, 2021: RIB. CRACKED. RIGHT HAND WING - LOWER SURFACE - SECONDARY STRUCTURE IS CRACKED AFT/OUTBOARD OF FUELING PANEL (MARKED). REPAIRED RIB PER EA.8-5710-T0363338
- [SDR FDEA202107191817](https://openairdocs.org/sdr/FDEA202107191817), Jul 19, 2021: PANEL. CORRODED. L/H WING PANEL 541LB L/E LAND CORROSION AROUND SCREW HOLE.(MARKED) REMOVED CORROSION , .118 REMAINING THICKNESS, .132 ORIGINAL THICKNESS, .012 MATERIAL REMOVED 
- [SDR FDEA202107031710](https://openairdocs.org/sdr/FDEA202107031710), Jul 3, 2021: SUPPORT. WORN. RIGHT WING L/E #6 SLAT TRACK SUPPORT STRUCTURE GOUGED BY FWD O/B RUB BLOCK. (DOT 4) ACCOMPLISHED EA 8-5710-T0362811 WINGS - BASIC WING STRUCTURE - RH WING SLAT 
- [SDR FDEA202107011645](https://openairdocs.org/sdr/FDEA202107011645), Jul 1, 2021: PANEL. CRACKED. PANEL ACA3213 (231LF) CRACK ALONG ONE OF THE HOLES. FABRICATED A NEW PANEL.
- [SDR FDEA202107011646](https://openairdocs.org/sdr/FDEA202107011646), Jul 1, 2021: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL, MAIN UPPER CARGO [L/H, O/B ][STA 600-695]. REMOVED AND REPLACED DELAMINATED FLOOR PANEL REF SRM 51-31-01 VOL2
- [SDR FDEA202106291615](https://openairdocs.org/sdr/FDEA202106291615), Jun 29, 2021: RIB. CRACKED. RIB CRACKED REMOVED AND FABRICATED NEW RIB AND INSTALLED PER DOUGLAS DWG ANB7143 AND SRM 51-31-00 VOL 2
- [SDR FDEA202106281614](https://openairdocs.org/sdr/FDEA202106281614), Jun 28, 2021: SKIN. WORN. R/H WING FIX L/E O/B SIDE HAS WORN MARK FROM SLAT # 2 RUBBING AGAINST IT. LOCATION OF DAMAGE IS ON TOP I/B SIDE STA. XORS 160. REPAIRED PER SRM 57-10-00 VOL 1 F
- [SDR FDEA202106271609](https://openairdocs.org/sdr/FDEA202106271609), Jun 27, 2021: SKIN. CORRODED. CORROSION AT STA.1926-1942 L47-49 BELOW AFT CARGO DOOR. REPAIRED CORROSION AT STA.1926-1942 L47-49 PER EA #T 8-5310-T0362734 TITLED: FUSELAGE - MAINFRAME - SKIN
- [SDR FDEA202106251589](https://openairdocs.org/sdr/FDEA202106251589), Jun 25, 2021: FLOOR PANEL. DELAMINATED. LOWER FUSELAGE AFT CARGO PANEL 187FF DELAMINATED P/N AGA3877-15 FABRICATED NEW LOWER FUSELAGE AFT CARGO COMPARTMENT PANEL 187FF P/N AGA3877- 15 REF FEDEX DRAWIN
- [SDR FDEA202106211577](https://openairdocs.org/sdr/FDEA202106211577), Jun 21, 2021: FLOORBOARD. DAMAGED. FLOORBOARD SR84852-125 DAMAGED. FABRICATED FLOORBOARD SR84852-125 PER FEDEX DRW SRZ-25-001
- [SDR FDEA202106181625](https://openairdocs.org/sdr/FDEA202106181625), Jun 18, 2021: BRACKET. CRACKED. #3 ACM RAM AIR INLET SHELL BRACKET THAT IS MOUNTED BELOW THE AVIONINCS RACK IS BROKEN. REMOVED & REPLACED BRACKET REF ABA7221 & MD10-30 SRM 51-33-01 VOL II.
- [SDR FDEA202106171565](https://openairdocs.org/sdr/FDEA202106171565), Jun 17, 2021: FLOOR PANEL. DELAMINATED. LOWER FUSELAGE AFT CARGO PANEL 187CF DELAMINATED P/N AGA7429-9 FABRICATED LOWER FUSELAGE AFT CARGO COMPARTMENT PANEL 187CF P/N AGA7429-9 REF FEDEX DRAWING SRZ-2
- [SDR FDEA202106171560](https://openairdocs.org/sdr/FDEA202106171560), Jun 17, 2021: FLOOR PANEL. DELAMINATED. LOWER FUSELAGE AFT CARGO FLOOR BOARD PANEL 187BF P/N AGA7428-7 IS DELAMINATED AND MISSING INSERTS FABRICATED LOWER FUSELAGE AFT CARGO FLOOR PANEL 187BF P/N AGA7
- [SDR FDEA202106151549](https://openairdocs.org/sdr/FDEA202106151549), Jun 15, 2021: FLOORBOARD. DELAMINATED. LWR FWD PIT FLOOR BOARD 123KF DAMAGED FABRICATED PANEL PER FEDEX DRAWING SRZ-25-005
- [SDR FDEA202106141706](https://openairdocs.org/sdr/FDEA202106141706), Jun 14, 2021: SKIN. DENTED. AFT-INTERMEDIATE/CENTER CARGO - AT APX STA 1790 L34 AFT OF CTR CARGO DOOR, DENT IS PRESENT (TOP DENT). 0000098319 : NAVARRO, ENRIQUE S - 08-JUL-2021 18:25 REPAI
- [SDR FDEA202106121510](https://openairdocs.org/sdr/FDEA202106121510), Jun 12, 2021: FLOOR PANEL. DAMAGED. CENTER CARGO FLOOR BOARD 183YF IS DAMAGED FABRICATED CENTER CARGO FLOOR PANEL 183YF REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202106111505](https://openairdocs.org/sdr/FDEA202106111505), Jun 11, 2021: FLOORBOARD. DELAMINATED. DELAMINATION ADA0244-13 (127EF). FABRICATED PER FEDEX DRAWING SRZ-25-005.
- [SDR FDEA202106111503](https://openairdocs.org/sdr/FDEA202106111503), Jun 11, 2021: FLOORBOARD. DELAMINATED. DELAMINATION ADA0238-9 (127BF). FABRICATED PER FEDEX DRAWING SRZ-25-005.
- [SDR FDEA202106111502](https://openairdocs.org/sdr/FDEA202106111502), Jun 11, 2021: FLOORBOARD. DAMAGED. DAMAGED FLOORBOARD ADA8349-3 (242DF) FABRICATED PER FEDEX DRAWING SRZ-25-005.
- [SDR FDEA202106091623](https://openairdocs.org/sdr/FDEA202106091623), Jun 9, 2021: NUT PLATE. DAMAGED. NUMEROUS NUT PLATES DAMAGED INSIDE ZONE 316 R/H UPPER SIDE. AFTER FURTHER INSPECTION CORROSION WAS FOUND AND DETERMINED OUT OF LIMITS. INSTALLED REPAIR DOUBLER 
- [SDR FDEA202106091478](https://openairdocs.org/sdr/FDEA202106091478), Jun 9, 2021: FLOORBOARD. DAMAGED. DAMAGE FLOOR BOARD AGA7078-70(292EF). FABRICATED NEW FLOOR BOARD PER FEDEX DRAWING SRZ-25-005.
- [SDR FDEA202106091475](https://openairdocs.org/sdr/FDEA202106091475), Jun 9, 2021: SKIN. DELAMINATED. R/H TRAILING EDGE PANEL 641HB FOUND TO HAVE DELAMINATION AFTER REMOVAL, MARKED AREA IN RED REPAIRED R/H TRAILING EDGE PANEL 641HB AT THE MARKED DELAMINATED AREA
- [SDR FDEA202106081619](https://openairdocs.org/sdr/FDEA202106081619), Jun 8, 2021: BRACKET. CRACKED. LH WING UPPER SURFACE, FUSELAGE STA.1341 - LOWER BRACKET FOR FAIRING SUPPORT/FRAME CRACKED. BRACKET UNDER PANEL 151FT. REMOVED & REPLACED BRACKET REF DAC DWG AN
- [SDR FDEA202106081599](https://openairdocs.org/sdr/FDEA202106081599), Jun 8, 2021: BRACKET. CRACKED. LH WING UPPER SURFACE, FUSELAGE STA.1298 - LOWER BRACKET FOR FAIRING SUPPORT/FRAME CRACKED. BRACKET UNDER PANEL 151ET. REMOVED AND REPLACED BRACKET REF DAC DWG 
- [SDR FDEA202106081598](https://openairdocs.org/sdr/FDEA202106081598), Jun 8, 2021: BRACKET. CRACKED. LH WING UPPER SURFACE, FUSELAGE STA.1321 - LOWER BRACKET FOR FAIRING SUPPORT/FRAME CRACKED. BRACKET UNDER PANEL 151FT. REMOVED & REPLACED BRACKET REF DAC DWG AN
- [SDR FDEA202106081597](https://openairdocs.org/sdr/FDEA202106081597), Jun 8, 2021: BRACKET. CRACKED. LH WING UPPER SURFACE, FUSELAGE STA.1273 - LOWER BRACKET FOR FAIRING SUPPORT/FRAME CRACKED. BRACKET UNDER PANEL 151ET. REMOVED AND REPLACED BRACKET REF ANB7138 
- [SDR FDEA202106081588](https://openairdocs.org/sdr/FDEA202106081588), Jun 8, 2021: FLOOR SUPPORT. CORRODED. AFT CARGO COMPT RH TUNNEL STA 1853 RBL 85 MAIN DECK FLOORBOARD SUPPORT CORRODED. MRKD REMOVED, FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT AGA3814-34 REF
- [SDR FDEA202106081550](https://openairdocs.org/sdr/FDEA202106081550), Jun 8, 2021: SKIN. WORN. R/H WING DROOP LEADING EDGE FLEX SKIN ASSY (PN:ARB2404-3) HAS WORN SLOT HOLE ON SKIN (MARKED). 0004002945 : FICKES, KYLE S - 15-JUN-2021 23:15 REMOVED DAMAGED S
- [SDR FDEA202106071774](https://openairdocs.org/sdr/FDEA202106071774), Jun 7, 2021: STRIKER. WORN. AFT FUSELAGE COMPT DOOR, LATCH INNER STRIKER SURFACE WORN AT MARKED POSITIONS. REPAIRED PER REF E.A 8-5330-T-0362904 :FUSELAGE- PLATES & SKINS - ACCESS DOOR 311
- [SDR FDEA202106071865](https://openairdocs.org/sdr/FDEA202106071865), Jun 7, 2021: SKIN. WORN. LH FUSELAGE STA 695 SKIN HAS GOUGE AT MAIN CARGO DOOR CUTOUT. MRKD AT LWR JAMB AFT OF LATCH SPOOL #4 REPAIRED PER EA # 8-5330-T0362732 P1
- [SDR FDEA202106071591](https://openairdocs.org/sdr/FDEA202106071591), Jun 7, 2021: DOUBLER. CRACKED. RH WING LE INTERNAL STRUCTURE AT APPROX XORS 555 - BEADED DOUBLER IS CRACKED AT SEVERAL LOCATIONS. CRACKS HAVE BEEN CONFIRMED WITH NDT HFEC AND ENDS MARKED. INS
- [SDR FDEA202106071509](https://openairdocs.org/sdr/FDEA202106071509), Jun 7, 2021: SKIN. CRACKED. L/H WING SKIN AT THE SLAT ANTI-ICE DUCT CUT OUT UPPER INBOARD CORNER HAS A .400 IN. CRACK (MARKED) REPAIRED NOTED CRACK AS REQUIRED PER SRM REQUIREMENTS REF SRM
- [SDR FDEA202106071556](https://openairdocs.org/sdr/FDEA202106071556), Jun 7, 2021: DOUBLER. CRACKED. RH WING LE INTERNAL STRUCTURE AT XORS 683 - BEADED DOUBLER IS CRACKED AT TWO (2) LOCATIONS. CRACKS HAVE BEEN CONFIRMED WITH HFEC AND ENDS MARKED. INSTALLED REPA
- [SDR FDEA202106071461](https://openairdocs.org/sdr/FDEA202106071461), Jun 7, 2021: FLOORBOARD. DAMAGED. AFA3200-2 DAMAGED FABRICATED PER DRAWING SRZ-25-005
- [SDR FDEA202106061570](https://openairdocs.org/sdr/FDEA202106061570), Jun 6, 2021: FORMER. CRACKED. LH WING LE INTERNAL STRUCTURE AT XORS 562 AND APPROX 18" AFT OF LE - FORMER/FRAME IS CRACKED APPROX .750" IN LENGTH. CRACKED CONFIRMED WITH HFEC AND ENDS MARKED
- [SDR FDEA202106061541](https://openairdocs.org/sdr/FDEA202106061541), Jun 6, 2021: BEAM. CRACKED. FWD LWR CARGO COMPT STA 595 BULKHEAD BEAM NCA 6044 CRACKED 4 PLACES. MRKD X DIM -5 AND 5 TWO PLACES EACH. Z DIM -59.38 CORRECTION Z DIM SHOULD REA -80 REPAIRED 
- [SDR FDEA202106061566](https://openairdocs.org/sdr/FDEA202106061566), Jun 6, 2021: DOUBLER. CRACKED. LH WING LE INTERNAL STRUCTURE AT XORS 562 - BEADED DOUBLER IS CRACKED AT SEVERAL LOCATIONS. CRACKS HAVE BEEN CONFIRMED WITH HFEC AND ENDS MARKED. INSTALLED DOUB
- [SDR FDEA202106021450](https://openairdocs.org/sdr/FDEA202106021450), Jun 2, 2021: WEB. CRACKED. NOSE W/W, STA 472, RH WEB NCA6046-3 IS CRACKED JUST BELOW THE REPAIR DOUBLER / ABOVE HORIZONTAL STIFFENER(MARKED). THE CORRECT PART NUMBER FOR THE WEB IS NCA624
- [SDR FDEA202106021520](https://openairdocs.org/sdr/FDEA202106021520), Jun 2, 2021: SEAT TRACK. WORN. MAIN CARGO DECK, STA. 1265, LBL 27.50", SEAT TRACK APROX 16" SECTION WORN. DOT #79 REPLACED DAMAGED SEAT TRACK FROM STA 1255 TO 1310 LBL 27.5 REF SRM 53-70-00 F
- [SDR FDEA202106021477](https://openairdocs.org/sdr/FDEA202106021477), Jun 2, 2021: SEAT TRACK. WORN. MAIN CARGO DECK, STA. 1265, LBL 8.50", SEAT TRACK WORN. DOT #9 REPLACED DAMAGED SEAT TRACK FROM STA 1269 TO 1334 AT LBL 8.50 REF SRM 53-70-00 FIG 1 VOL 1, SRM 5
- [SDR FDEA202106021476](https://openairdocs.org/sdr/FDEA202106021476), Jun 2, 2021: SEAT TRACK. WORN. MAIN CARGO DECK, STA. 1255, LBL 8.50", SEAT TRACK WORN. DOT #67. REPLACED DAMAGED SEAT TRACK FROM STA 1269 TO 1334 AT LBL 8.50 REF SRM 53-70-00 FIG 1 VOL 1, SRM
- [SDR FDEA2020061641236](https://openairdocs.org/sdr/FDEA2020061641236), Jun 14, 2020: WIRE HARNESS. DEFECTIVE. ON DESCENT NR 2 ENGINE EGT EXCEEDANCE 1007*C, PRECAUTIONARY SHUT DOWN. NO OTHER EXCEEDANCES, EGT GAUGE "X'D" OUT SEVERAL TIMES. WHEN TROUBLESHOOTING EGT HARNESS
- [SDR FDEA2020062300884](https://openairdocs.org/sdr/FDEA2020062300884), May 3, 2020: SKIN. DENTED. ON WALK AROUND FOUND DENT ON R/H SIDE OF AIRCRAFT JUST AFT RADOME. FABRICATED DOUBLER, TRIPLER AND FILLER. DRILLED AND COUNTERSINK. ALODINED AND PRIMED IAW SRM 
- [SDR FDEA2020050430884](https://openairdocs.org/sdr/FDEA2020050430884), May 3, 2020: SKIN. DAMAGED. ON WALK AROUND FOUND DENT ON R/H SIDE OF AIRCRAFT JUST AFT RADOME. FABRICATED DOUBLER, TRIPLER AND FILLER. DRILLED AND COUNTERSINK. ALODINED AND PRIMED IN REF T
- [SDR FDEA201909072132](https://openairdocs.org/sdr/FDEA201909072132), Sep 7, 2019: SWITCH. FAULTY. UPON GEAR RETRACTION ALL THE PRIMARY GEAR AND SECONDARY LIGHTS ILLUMINATED WITH THE GEAR HANDLE UP. FOLLOWED QRH PROCEDURES AND THE GEAR RETRACTED. TROUBLESHOOT

All 167: https://openairdocs.org/aircraft/N306FE/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/N306FE/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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