# N308FE: 1986 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: 48297 - Year built: 1986 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 20, 1986 - Certificate issued: August 12, 2004 - Expires: February 29, 2028 - Mode S code: A33D8C - 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=308FE - Page: https://openairdocs.org/aircraft/N308FE 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/N308FE/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 N308FE. ## FAA accident and incident reports None matched to N308FE. ## Service difficulty reports (98, 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 FDEA202105041096](https://openairdocs.org/sdr/FDEA202105041096), May 4, 2021: O-RING. FAILED. ON CLIMB OUT, #2 ENGINE OIL QUANTITY WENT TO 1 QT. SUBSEQUENTLY OIL PRESSURE BEGAN TO DROP BELOW THE GREEN BAND. FOLLOWED QRH TO SHUT DOWN #2 ENGINE AND LAND AT - [SDR FDEA202103210738](https://openairdocs.org/sdr/FDEA202103210738), Mar 21, 2021: UNKNOWN. SMOKE. PDIS 308 21-50 7643 21MAR21 IND FACT U LOGPAGES:3203672 NOTE: AFTER STARTING APU AND TURNING ON PACKS AN ODD SMELL EMINATED FROM THE AIR VENTS. SMELLED LIKE TUR - [SDR FDEA2020011310110](https://openairdocs.org/sdr/FDEA2020011310110), Jan 11, 2020: PSEU. MALFUNCTIONED. ON FINAL FOR KMEM 18L AT 3000 FT, WE PUT THE GEAR HANDLE DOWN AND RECEIVED 4 RED GEAR UNSAFE INDICATIONS. WE EXECUTED A GO AROUND TO REENTER THE PATTERN AND RAN - [SDR FDEA2019082652015](https://openairdocs.org/sdr/FDEA2019082652015), Aug 25, 2019: FITTING. CRACKED. CENTER LANDING GEAR LT AFT DOOR, AFT LOWER SUPPORT WAS CRACKED AT LOWER ATTACH LUG HOLE. REMOVED AND REPLACEED LT MLG DOOR LOWER AFT LINK FITTING IAW DRAWING AB - [SDR FDEA2019082101972](https://openairdocs.org/sdr/FDEA2019082101972), Aug 20, 2019: HINGE FITTING. CRACKED. CENTER LANDING GEAR LH AFT DOOR IS LOOSE AT FWD AND AFT HINGES. REMOVED AND REPLACED FITTING IAW DAC DWG ANB7451. - [SDR FDEA201908091824](https://openairdocs.org/sdr/FDEA201908091824), Aug 9, 2019: VANE. WORN. LEFT WING INBOARD FLAP VANE WORN ON TOP INB INLINE WITH BUB STRIP APPROX. 4 INCHES. REPAIRED WORN AREA ON L/H I/B FLAP VANE AS REQUIRED REF. SRM 57-00-01 VOL.I - [SDR FDEA2019082181989](https://openairdocs.org/sdr/FDEA2019082181989), Aug 8, 2019: RIB. CRACKED. CENTER CARGO DOOR FWD RIB LOWER END IS CRACKED AND PIECE MISSING. REMOVED DAMAGED SECTION OF CENTER CARGO DOOR FWD RIB LOWER END AND INSTALLED REPAIR ANGLE AND - [SDR FDEA2019081281833](https://openairdocs.org/sdr/FDEA2019081281833), Aug 8, 2019: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR AT STA 1845 RBL 7 UNDER FLOOR BOARD SUPPORT IS CORRODED AT NUT PLATE HOLE. (MKD) REPLACED PER DAC DWG AGA3814 - [SDR FDEA2019081571858](https://openairdocs.org/sdr/FDEA2019081571858), Aug 7, 2019: FLOOR SUPPORT. CORRODED. INSIDE MAIN CABIN, AT BS 1885, RBL 20, UNDER FLOOR PANEL SUPPORT IS CORRODED AT NUT PLATE HOLES. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG AGA7091, AND SRM - [SDR FDEA2019081571857](https://openairdocs.org/sdr/FDEA2019081571857), Aug 7, 2019: FLOOR SUPPORT. CORRODED. INSIDE MAIN CABIN, AT BS 1885, LBL 20 UNDER FLOOR PANEL, HAT SECTION SUPPORT IS CORRODED AT NUT PLATE HOLES. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-35-01,V2 - [SDR FDEA2019080971826](https://openairdocs.org/sdr/FDEA2019080971826), Aug 7, 2019: FLOOR SUPPORT. CORRODED. INSIDE MAIN CABIN, AT STA 1885 LBL 44, UNDER FOOL SUPPORT HAT SECTION, IS CORRODED AT NUT PLATE HOLES. (MKD) AT STA. 1885, LBL 44, REMOVED AND REPLACED WITH NEW - [SDR FDEA2019080971825](https://openairdocs.org/sdr/FDEA2019080971825), Aug 7, 2019: FLOOR SUPPORT. CORRODED. INSIDE MAIN CABIN, AT STA 1885 LBL 36, UNDER FLOOR PANEL SMALL HAT SECTION IS CORRODED AT NUTPLATE HOLE. (MKD) AT STA. 1885, LBL 36, REMOVED AND REPLACED WITH N - [SDR FDEA201908062189](https://openairdocs.org/sdr/FDEA201908062189), Aug 6, 2019: FRAME. BENT. MAIN CARGO LT STA 1641 BETWEEN STR L13-L14. FRAME IS BENT. CUT OUT FRAME AND INSTALLED NEW FRAME SECTION PER SRM 53-30-00 FIG05 AND SRM 51- 38-01 VOL II. - [SDR FDEA2019080531794](https://openairdocs.org/sdr/FDEA2019080531794), Aug 3, 2019: SKIN. GOUGED. R/H WING, L/E, I/B FLAP, APPROX. STA. XIFH280 FOUND A GOUGE UNDERNEATH RUB STRIP. INSTALLED REPAIR DOUBLER I.A.W. SRM57-00-01 FIG. 4 SHT.2 VOL. I - [SDR FDEA2019100712483](https://openairdocs.org/sdr/FDEA2019100712483), Jul 31, 2019: SUPPORT. CRACKED. RIGHT WING, LOWER LEADING EDGE WAS CRACKED ON PANEL LAND, AFT OF NR 9 SLAT TRACK. REMOVED AND REPLACED DAMAGED SUPPORT ARB2933-50 IAW DWG ARB2933 AND SRM 51-33- - [SDR FDEA2019081531893](https://openairdocs.org/sdr/FDEA2019081531893), Jul 31, 2019: FLOOR SUPPORT. CORRODED. CENTER CARGO COMPARTMENT, FROM STATION 1541 TO STATION 1581, RBL-57 INTERCOSTALS CORRODED. REMOVED AND REPLACED CENTER CARGO COMPARTMENT INTERCOSTALS FROM STA.1 - [SDR FDEA2019081528856](https://openairdocs.org/sdr/FDEA2019081528856), Jul 28, 2019: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK BS 1975 RBL 35 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW DWG AGA7091, AND SRM 51-31-01,VOL 2. - [SDR FDEA2019080581795](https://openairdocs.org/sdr/FDEA2019080581795), Jul 28, 2019: FLOOR SUPPORT. CORRODED. MAIN CARGO DECK, STA1747 70RBL FLOOR SUPPORT HAS CORROSION (MARKED) REMOVED DAMAGED FLOOR SUPPORT AND REPLACED WITH NEW PER DWG AFA 3853 AND SRM 51-31-01,V2. - [SDR FDEA2019080281789](https://openairdocs.org/sdr/FDEA2019080281789), Jul 28, 2019: SEAT TRACK. CRACKED. CTR. CARGO COMPT CEILING: STA. 1701 - 27.50 RBL, SEAT TRACK HAT SPLICE CRACKED (VIEWED LOOKING UP FROM CTR. CARGO COMPT.) MRKD. FABRICATED AND INSTALLED -20 SPL - [SDR FDEA201907272231](https://openairdocs.org/sdr/FDEA201907272231), Jul 27, 2019: CHANNEL. CORRODED. CENTER CARGO COMPT: APPROX STA 1521 X=56.19. RT O/B CARGO RAIL. REF FWD ATTACH FASTENERS. (UNDERSIDE IN CHANNEL) FASTENER NUTS, WASHERS AND STRUCTURE CHANNEL CO - [SDR FDEA2019081671902](https://openairdocs.org/sdr/FDEA2019081671902), Jul 27, 2019: SUPPORT WEB. CRACKED. CTR CARGO COMPT: STA 1701 APPROX LONGERON 44L-47L - LOWER SUPPORT WEB CRACKED BELOW ROLLER TRAYS. (MRKD) REMOVED AND REPLACED CRACKED SECTION OF FLOOR BEAM IN C - [SDR FDEA2019080871808](https://openairdocs.org/sdr/FDEA2019080871808), Jul 27, 2019: FLOORBEAM. CORRODED. CENTER CARGO COMPT: APPROX STA 1781, X=-16.5 FLOOR BOARD SUPPORT EXTRUSTION. 1 CLIPNUT HOLE SHOWS CORROSION. (UNDERSIDE) MARKED. INSTALLED FLOOR BOARD SUPPORT P - [SDR FDEA201907261894](https://openairdocs.org/sdr/FDEA201907261894), Jul 26, 2019: FLOORBEAM. CORRODED. AFT CARGO COMPT: APPROX STA 1841, FLOOR SUPPORT ANGLE HAS CORROSION AT NUT PLATES. (UNDERSIDE OF ANGLE). HEAVY AND LIGHT FROM RIGHT TO LEFT SIDE OF A/C. REMOVED - [SDR FDEA2019080861806](https://openairdocs.org/sdr/FDEA2019080861806), Jul 26, 2019: SKIN. GOUGED. LT WING FIXED LEADING EDGE - REPAIR DOUBLER INBD SIDE OF ANTI-ICE DUCT HAS GOUGE CAUSED BY CONTACT WITH SLAT. REPAIRED L/H WING SKIN ATSLAT ANTI-ICE TELESCOPING - [SDR FDEA2019080861805](https://openairdocs.org/sdr/FDEA2019080861805), Jul 26, 2019: SKIN. CRACKED. LT WING FIXED LEADING EDGE - REPAIR DOUBLER OUTBD SIDE OF ANTI-ICE DUCT HAS GOUGE CAUSED BY CONTACT WITH SLAT. (MARKED) REPAIRED L/H WING SKIN AT SLAT ANTI-CE T - [SDR FDEA2019101052497](https://openairdocs.org/sdr/FDEA2019101052497), Jul 25, 2019: BULKHEAD. CRACKED. FUSELAGE AFT PRESSURE BULKHEAD, FWD SIDE, AT UPPER CANTED AREA, PREVIOUS REPAIR BLEND OUT HAS A "1/2" INCH CRACK INDICATION. INSTALLED A REPAIR IAW EA 8-5310-T0 - [SDR FDEA2019081501851](https://openairdocs.org/sdr/FDEA2019081501851), Jul 25, 2019: SKIN. CRACKED. LEFT WING NR 8 SLAT, INBD LOWER SKIN WAS CRACKED. REMOVED AND REPLACED THE LT WING NR 8 SLAT, ADJUSTED AND OPS CHECKED GOOD IAW AMM 27-80-01-4, AND AMM 27-80-00 - [SDR FDEA2019080721799](https://openairdocs.org/sdr/FDEA2019080721799), Jul 25, 2019: FRAME SPLICE. CRACKED. MAIN DECK STA 1741 FRAME SPLICE DOUBLER CRACKED. MRKD LH SIDEWALL BETWEEN L13L- L14L REMOVED AND REPLACED PER DWG AFA 0018 - [SDR FDEA2019080841804](https://openairdocs.org/sdr/FDEA2019080841804), Jul 24, 2019: SKIN. WORN. RT WING DROOP L/E, INBD SIDE OF DROOP L/E SKIN HAS WEAR GROOVE/MARKS (MARKED AND DOT 4) PERFORMED DLE SKIN REPAIR I.A.W. SRM 57-10-00 , PARA. 95 AND FIG. 97 VOL - [SDR FDEA2019081231832](https://openairdocs.org/sdr/FDEA2019081231832), Jul 23, 2019: FRAME. CRACKED. LH WHEEL WELL FRAME STA. 1501 APPROX STRINGER 33 - 1 INCH CRACK EMANATING FROM FASTENER HOLE AT FRAME. CRACK WAS CONFIRMED USING NDT HFEC. REPAIRED CRACKED FRAM - [SDR FDEA2019081523876](https://openairdocs.org/sdr/FDEA2019081523876), Jul 23, 2019: SEAT TRACK. WORN. MAIN DECK: SEAT TRACK WORN NEAR STA. 1122 AT RBL X=8.50. AREA MARKED RED REPLACED PER SRM CH 53-70-00,FIG 1,VOL 1. - [SDR FDEA201903190684](https://openairdocs.org/sdr/FDEA201903190684), Mar 19, 2019: UNKNOWN. ODOR. FUME EVENT. ON TAKEOFF FROM CYMY WITH ENGINES SET TO TAKEOFF POWER AND ABOVE 80KNOTS, BOTH CREW MEMBERS SMELLED A MODERATELY INTENSE BURNED OIL ODOR. THE ODOR D - [SDR FDEA201901100081](https://openairdocs.org/sdr/FDEA201901100081), Jan 10, 2019: LANDING GEAR. DAMAGED. AFTER TAKEOFF FROM 36L WITH GEAR HANDLE UP WE RECEIVED A UNSAFE CENTER GEAR INDICATION IN BOTH THE PRIMARY AND SECONDARY INDICATORS. CYCLED GEAR HANDLE PER QRH - [SDR FDEA201801060034](https://openairdocs.org/sdr/FDEA201801060034), Jan 6, 2018: DOOR. INOPERATIVE. L1 DOOR DID NOT WORK ELECTRICALLY. - [SDR FDEA201709212666](https://openairdocs.org/sdr/FDEA201709212666), Sep 21, 2017: SKIN. DELAMINATED. RIGHT WING NR 1 SPOILER OTBD TOP SECTION HAS A 2.75 X 3.5 INCHES OF DELAMINATION AT XORS 346. REPAIRED THE SPOILER IAW SRM 71-00-01, FIG 4, SHEET 1, VOL I. - [SDR FDEA201709212665](https://openairdocs.org/sdr/FDEA201709212665), Sep 21, 2017: PANEL. DELAMINATED. RIGHT WING TO FUSELAGE FIXED FAIRING, T/E AT INBD FLAP, PANEL ARC0288-504 R2, PREVIOUS REPAIR HAS COME OFF AND BOTTOM SIDE IS DELAMINATED. REPAIRED. - [SDR FDEA201709192871](https://openairdocs.org/sdr/FDEA201709192871), Sep 19, 2017: DOUBLER. CRACKED. RT WING LE XORS 562 INNER BEADED DOUBLER IS CRACKED. CONDITION CONFIRMED WITH HFEC. REPAIRED PER SRM 57-10-T0335748. - [SDR FDEA201709132849](https://openairdocs.org/sdr/FDEA201709132849), Sep 13, 2017: FITTING. CRACKED. MAIN CARGO DOOR FRAME NR 7 LATCH SPOOL LOWER SUPPORT FITTING HAS A ONE INCH CRACK EMANATING FROM RETAINER HOLE AT THE FWD INBD SIDE OF FITTING. INSTALLED A NEW - [SDR FDEA201709112862](https://openairdocs.org/sdr/FDEA201709112862), Sep 11, 2017: FRAME. CRACKED. RT WING LEADING EDGE FRAME ARB1161-15 AT STA XRS 269 IS CRACKED. RT LEADING EDGE FORMER REPAIRED PER EA 8-5710-T0335774. - [SDR FDEA201709112861](https://openairdocs.org/sdr/FDEA201709112861), Sep 11, 2017: FLOOR SUPPORT. CORRODED. AFT WASTE COMPT STA 2007 APPROX 24LBL UNDERSIDE OF FLOOR SUPPORT TRACK CORROSION. REMOVED AND INSTALLED NEW FLOORBOARD SUPPORT BEAM PER DRAWING AGA7087 AND SRM - [SDR FDEA201709082870](https://openairdocs.org/sdr/FDEA201709082870), Sep 8, 2017: DOOR FRAME. CRACKED. A/C COMPT PACK BAY NR 1, APPROX STA 553 LONG 36 REF PACK BAY DOOR (113DL). FWD FRAME OF DOOR CUTOUT. THE FRAME IS CRACKED. IT HAS APPROX A 2" CRACK NEAR TOP OF - [SDR FDEA201709082778](https://openairdocs.org/sdr/FDEA201709082778), Sep 8, 2017: SEAT TRACK. WORN. UPPER MAIN DECK SEAT TRACK WORN AT RBL 8.50 NEAR STA 675. REMOVED AND INSTALLED DAMAGED SEAT TRACK REF SRM 53-70-00 FIG 11 VOLUME 1. - [SDR FDEA201709082699](https://openairdocs.org/sdr/FDEA201709082699), Sep 8, 2017: SEAT TRACK. WORN. UPPER MAIN DECK, TWO SEAT TRACKS WORN AT LBL 47.50 NEAR BS 615. REPLACED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL I, SRM 51-4-01, VOL II, AND SR10-53-002A. M - [SDR FDEA201607182499](https://openairdocs.org/sdr/FDEA201607182499), Jul 18, 2016: WARNING LIGHT. ILLUMINATED. RECIEVED AN EMERGENCY LIGHT BATTERY 1 LOW, ALERT DURING EMERGENCY LIGHT TEST. - [SDR FDEA201604051144](https://openairdocs.org/sdr/FDEA201604051144), Apr 5, 2016: DOOR FRAME. CRACKED. DURING HYD LEAK CHECK INSPECTION, OPENED & CLOSED RT MAIN GEAR DOOR. WHEN CLOSING THE RT GEAR DOOR, THE DOOR WOULD NOT STAY UP. TROUBLE SHOT TO THE LATCH ACTUAT - [SDR FDEA201510203289](https://openairdocs.org/sdr/FDEA201510203289), Oct 20, 2015: SKIN. CRACKED. SIX INCH CRACK ON EXTERNAL SKIN OF NR 3 ACM ACCESS DOOR. REPAIRED THE CRACK SKIN IAW EA 8-5240-T0320735 A. - [SDR FDEA201510203287](https://openairdocs.org/sdr/FDEA201510203287), Oct 20, 2015: BULKHEAD. DENTED. CENTER CARGO STATION 1841, LBL 6, BULKHEAD WEB HAS LARGE DENT. CUT OUT DENTED WEB AS REQUIRED IAW SRM 51-00-01 FIG 10. INSTALLED REPAIR DOUBLER IAW EA 8-5310-T0 - [SDR FDEA201510203286](https://openairdocs.org/sdr/FDEA201510203286), Oct 20, 2015: BULKHEAD. DENTED. CENTER CARGO STATION 1841, RBL 6, BULKHEAD WEB HAS LARGE DENT. REPAIR DOUBLER IAW EA 8-5310-T0320825. - [SDR FDEA201510173268](https://openairdocs.org/sdr/FDEA201510173268), Oct 17, 2015: WEB. CRACKED. RIGHT MLG WW NR 3 RESERVOIR, LOWER ATTACH STRUCTURE WEB CRACKED. REMOVED LOWER ATTACH STRUCTURE WEB, RT MLG WW IAW SRM 51-31-01 VOL 2. INSTALLED & FABRICATED ST - [SDR FDEA201510123179](https://openairdocs.org/sdr/FDEA201510123179), Oct 12, 2015: STRUCTURE. CORRODED. CENTER WING LOWER BARREL, CTR AUXILIARY TANK, CORROSION UNDER RUB STRIPS OF UPPER INBD & OTBD STRIPS. STRUCTURE IS FOR CTR AUXILIARY FUEL TANK COVER. REMOVED LI All 98: https://openairdocs.org/aircraft/N308FE/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/N308FE/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 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.