# N316FE: 1988 Mcdonnell Douglas MD-10-30F

- Status: Valid registration
- Airframe: [Mcdonnell Douglas MD-10-30F](https://openairdocs.org/model/mcdonnell-douglas-md-10-30f) (registry code 3024020, 385 seats)
- Engine: [GE CF6-50 series](https://openairdocs.org/engine/ge-cf6-50-series) (registry code 30018)
- 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: 48314
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 9, 2000
- Certificate issued: December 5, 2013
- Expires: December 31, 2029
- Mode S code: A35D9D
- 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=316FE
- Page: https://openairdocs.org/aircraft/N316FE

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. The registry lists only the engine series, so ADs for every GE CF6-50 model are included.

## ADs that may apply (OpenAirDocs): 99 in force

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

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

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

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

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

- [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022
- [AD 2016-04-16](https://openairdocs.org/ad/2016-04-16) (historical): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Apr 15, 2016
- [AD 2013-08-23](https://openairdocs.org/ad/2013-08-23) (historical): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective May 29, 2013
- [AD 2009-26-17](https://openairdocs.org/ad/2009-26-17) (historical): Fuselage · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Feb 4, 2010
- [AD 2009-21-10](https://openairdocs.org/ad/2009-21-10) (historical): Oxygen · Airbus A300, Model B4-605R, A300, Model B4-620, A300, Model B4-622 and 138 more. Effective Dec 17, 2009
- [AD 2008-06-21](https://openairdocs.org/ad/2008-06-21) (historical): Fuel tank systems · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Apr 23, 2008
- [AD 2007-15-05](https://openairdocs.org/ad/2007-15-05) (historical): Fuel pump housing electrical connector · Boeing DC-10-10, DC-10-10F, DC-10-15 and 9 more. Effective Aug 8, 2007
- [AD 2005-12-05](https://openairdocs.org/ad/2005-12-05) (historical): Flight deck door · Reinforced cockpit door (Safran Cabin STC ST01335LA or 2 others). Effective Jul 19, 2005
- [AD 2004-18-04](https://openairdocs.org/ad/2004-18-04) (historical): Airplane Flight Manual (AFM) · McDonnell Douglas 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Sep 20, 2004
- [AD 2004-05-20](https://openairdocs.org/ad/2004-05-20) (historical): Electric motor operated auxiliary hydraulic pumps · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 9 more. Effective Apr 15, 2004
- [AD 2003-17-07](https://openairdocs.org/ad/2003-17-07) (historical): Fire Extinguishers for the Engine and Auxiliary Power Unit (APU) · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 60 more. Effective Sep 24, 2003
- [AD 2003-14-04](https://openairdocs.org/ad/2003-14-04) (historical): Flight Deck Door Pressure Relief Latch Assemblies · Boeing 737-200 Series, 737-300 Series, 737-400 Series and 14 more. Effective Jul 25, 2003
- [AD 2003-03-15](https://openairdocs.org/ad/2003-03-15) (historical): Airplane Flight Manual (AFM) - Oxygen Masks · Boeing 707 Series (all), 720 Series (all), 727 Series (all) and 75 more. Effective Mar 7, 2003
- [AD 2001-14-08](https://openairdocs.org/ad/2001-14-08) (historical): Electric Motors of the Auxiliary Hydraulic Pump · McDonnell Douglas DC-10 Series (all), MD-10-10F, MD-10-30F and 1 more. Effective Aug 16, 2001
- [AD 2012-02-07](https://openairdocs.org/ad/2012-02-07) (historical): LPT rotor stage 3 disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Mar 6, 2012
- [AD 2011-18-01](https://openairdocs.org/ad/2011-18-01) (historical): LPT rotor stage 3 disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Sep 26, 2011
- [AD 2011-02-07](https://openairdocs.org/ad/2011-02-07) (historical): Rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Feb 22, 2011
- [AD 2010-12-10](https://openairdocs.org/ad/2010-12-10) (historical): High-pressure turbine (HPT) · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Jun 24, 2010
- [AD 2010-06-15](https://openairdocs.org/ad/2010-06-15) (historical): Low-pressure turbine (LPT) stage 3 disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Apr 1, 2010
- [AD 2009-04-17](https://openairdocs.org/ad/2009-04-17) (historical): Long fixed core exhaust nozzle (LFCEN) assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 2, 2009
- [AD 2007-11-18](https://openairdocs.org/ad/2007-11-18) (historical): Forward fan stator cases · General Electric CF6-50C, CF6-50C1, CF6-50C2 and 1 more. Effective Jul 5, 2007
- [AD 2006-12-24](https://openairdocs.org/ad/2006-12-24) (historical): Five-link forward mount assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Jul 21, 2006
- [AD 2000-08-11](https://openairdocs.org/ad/2000-08-11) (historical): Life-limited Parts · General Electric Aircraft Engines CF6-45 Series (all), CF6-50 Series (all) and CF6-6 Series (all). Effective Oct 23, 2000
- [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 99-18-20](https://openairdocs.org/ad/99-18-20) (historical): Inadvertent In-flight Thrust Reverser · General Electric Aircraft Engines CF6-50 Series (all), CF6-80A1, CF6-80A3 and 6 more. Effective Nov 2, 1999
- [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
- [AD 95-17-15](https://openairdocs.org/ad/95-17-15) (historical): Engine Mount Pylon · General Electric Aircraft Engines CF6-45 Series (all) and CF6-50 Series (all). Effective Oct 10, 1995

All 128: https://openairdocs.org/aircraft/N316FE/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 N316FE.

## FAA accident and incident reports

None matched to N316FE.

## Service difficulty reports (107, 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 FDEA202211102747](https://openairdocs.org/sdr/FDEA202211102747), Nov 10, 2022: LINE. SPLIT. ON CLIMB OUT, RECEIVED A HYD 3 OFF LEVEL 1 ALERT, FOLLOWED BY A LOSS OF HYD FLUID LEADING TO A HYD 3 FAIL LVL 2 ALERT. A COMPLETE LOSS OF HYD FLUID & PRESSURE. 
- [SDR FDEA202204301098](https://openairdocs.org/sdr/FDEA202204301098), Apr 30, 2022: NONE. NONE. PDIS 316 27-50 7006 30APR22 SLC OPEN U UPON FLAPS 35 SELECTION, RECEIVED LEVEL 2 SLAT DISAG. ALERT. INITIATED GO AROUND, AND THEN RECEIVED LEVEL 2 FLAP DISAG. A
- [SDR FDEA202201220117](https://openairdocs.org/sdr/FDEA202201220117), Jan 22, 2022: SKIN. DAMAGED. INDY LINE FOUND ON NRC6053-509 TOP SKIN OF WEDGE ARC1953-503 (ARC1953-4, 2024-T3 0.025 TH, AND THE ARC1953-7 DOUBLER 0.016 TH ) PULLING BACK FROM IB EDGE (XOF 5
- [SDR FDEA202105291419](https://openairdocs.org/sdr/FDEA202105291419), May 29, 2021: DOOR SILL. CRACKED. CENTER CARGO DOOR SILL, LOWER AFT SECTION HAS A CRACK REPAIRED PER SRM MD10 53-00-01 VOL I P40
- [SDR FDEA202105211357](https://openairdocs.org/sdr/FDEA202105211357), May 21, 2021: FLOOR PANEL. DELAMINATED. MAIN DECK L-1 DOOR AREA FLOOR PANEL, RIGHT NEXT TO MAIN CARGO DOOR CONT, SHOWING SPONGY AND SUSPECTING DELAM. R/R THE FLOOR PANEL#223AF WITH SCREW PER SRM
- [SDR FDEA202105201408](https://openairdocs.org/sdr/FDEA202105201408), May 20, 2021: SKIN. DENTED. REWORK: REFERENCE SNRM 467..L/H WING UPPER SURFACE-L/E SKIN DENTED AT APPROX. STA. XDLE 309,INBD OF #3 SLAT FIXED WING LEADING EDGE IS PRIMARY STRUCTURE. "MAJOR
- [SDR FDEA202105171412](https://openairdocs.org/sdr/FDEA202105171412), May 17, 2021: DOUBLER. DAMAGED. RH WING INTERNAL LE - ABOVE ANTI-ICE TELESCOPE DUCT(ACCESS, PANEL 613AB)- BEADED DOUBLER IS DAMAGED. 0000575467 : WRAY, BASIL P. B. - 03-JUN-2021 13:20 TRIMMED 
- [SDR FDEA202105171261](https://openairdocs.org/sdr/FDEA202105171261), May 17, 2021: FILLET. GOUGED. LH WING # 1 SLAT FILLET ASSY LOWER SURFACE TRAILING EDGE GOUGE REPAIRED # 1 SLAT FILLET ASSY LOWER SURFACE TRAILING EDGE DAMAGED PER SRM 51-43- 01 VOL 2 PARAGRA
- [SDR FDEA202105151228](https://openairdocs.org/sdr/FDEA202105151228), May 15, 2021: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL FROM STA 1561 TO 1650 AT LBL 107 TO LBL 75 HAS GOUGES IN SEVERAL AREAS (MARKED) FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202105131214](https://openairdocs.org/sdr/FDEA202105131214), May 13, 2021: FLOOR PANEL. DELAMINATED. MAIN DECK FLOOR PANEL FROM STA 1099 TO 1029 AT LBL 107 TO LBL 75 POSSIBLY DELAMED (MARKED) FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202105121207](https://openairdocs.org/sdr/FDEA202105121207), May 12, 2021: FLOOR PANEL. DAMAGED. MAIN DECK: FLOOR PANEL AT APPROX STA 1503 BETWEEN RBL 8 AND LBL 8 IS DAMAGED (MARKED AND DOT 44 IN 2 PLACES) REPAIRED MAIN DECK: FLOOR PANEL AT APPROX STA 1503 
- [SDR FDEA202105121196](https://openairdocs.org/sdr/FDEA202105121196), May 12, 2021: FLOOR PANEL. DELAMINATED. MAIN DECK FLOOR PANEL FROM STA 600 TO STA 658 AT LBL 107 TO 75 DELAMED FABRICATED FLOOR PANEL REF. FEDEX DRAWING SRZ-25-005
- [SDR FDEA202105121195](https://openairdocs.org/sdr/FDEA202105121195), May 12, 2021: FLOOR PANEL. DELAMINATED. MAIN DECK FLOOR PANEL FROM STA 600 TO STA 658 AT LBL 47 TO LBL 75 HAS SEVERAL GOUGES - POSSIBLE DELAMED FABRICATED FLOOR PANEL REF. FEDEX DRAWING SRZ-25-005
- [SDR FDEA202105111194](https://openairdocs.org/sdr/FDEA202105111194), May 11, 2021: FLOOR PANEL. DELAMINATED. MAIN DECK FLOOR PANEL FROM APPROX STA 1481-1561 BETWEEN RBL 75-RBL107 IS WORN THROUGH TOP LAYER AT APPROX STA 1511 RBL 75 SIDE (MARKED AND DOT 41) FABRICATED NE
- [SDR FDEA202104281055](https://openairdocs.org/sdr/FDEA202104281055), Apr 28, 2021: FLOOR PANEL. DAMAGED. AFT CARGO PIT FLOOR PANEL 187EF HAS MINOR DAMAGES ON TOP SURFACE FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202104281054](https://openairdocs.org/sdr/FDEA202104281054), Apr 28, 2021: FLOOR PANEL. DAMAGED. AFT CARGO PIT FLOOR PANEL 187EF HAS MINOR DAMAGES ON TOP SURFACE FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202104261042](https://openairdocs.org/sdr/FDEA202104261042), Apr 26, 2021: FLOOR PANEL. DELAMINATED. AFT CARGO PIT FLOOR PANEL 187GF HAS MULTIPLE PUNCTURES AND SHOWS SIGNS OF DELAMINATION FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202104261041](https://openairdocs.org/sdr/FDEA202104261041), Apr 26, 2021: FLOOR PANEL. DELAMINATED. AFT CARGO PIT FLOOR PANEL 187CF HAS MULTIPLE PUNCTURES AND SHOWS SIGNS OF DELAMINATION FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202104261040](https://openairdocs.org/sdr/FDEA202104261040), Apr 26, 2021: FLOOR PANEL. DELAMINATED. AFT CARGO PIT FLOOR PANEL 187AF HAS MULTIPLE PUNCTURES AND SHOWS SIGNS OF DELAMINAION FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202104261039](https://openairdocs.org/sdr/FDEA202104261039), Apr 26, 2021: FLOOR PANEL. PUNCTURED. AFT CARGO PIT FLOOR PANEL 187BF HAS MULTIPLE PUNCTURES AND SHOWS SIGNS OF DEMLAMINATION FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202104241193](https://openairdocs.org/sdr/FDEA202104241193), Apr 24, 2021: SKIN. CRACKED. R/H WING ANTI ICE TELESCOPING DUCT CUT OUT, TOP O/B CORNER CRACKED (MARKED) REPAIRED CRACK ON CORNER OF SKIN CUT-OUT FOR ANTI-ICE DUCT PER SRM 57-10-00 VOL.1 FI
- [SDR FDEA202104211215](https://openairdocs.org/sdr/FDEA202104211215), Apr 21, 2021: SKIN. CRACKED. LH WING TIP LOWER SURFACE, 1" CRACK IN SKIN - APPROX. XW987, OUTBD OF STROBE LIGHT CONTROLLER ACCESS DOOR. REPAIRED WINGTIP SKIN CRACK REF: SRM 57-00-01 VOL 1, 
- [SDR FDEA202104201259](https://openairdocs.org/sdr/FDEA202104201259), Apr 20, 2021: SEAL. CRACKED. RH WING OUTBD FLAP OUTBD HINGE XW638 - METAL SEAL CRACKED AT PANEL 636JL. REMOVED AND INSTALLED NEW METAL SEAL PN ARC2148-9 ON ARC2148-504(636JL)FAIRING REF SRM
- [SDR FDEA202104191354](https://openairdocs.org/sdr/FDEA202104191354), Apr 19, 2021: LONGERON. CORRODED. AFT CARGO COMPT BILGE STA 1854-1864 CORROSION AT L48R. MRKD 0003884010 : GUTZWEILER, JOHN - 22-MAY-2021 05:37 REMOVED AND REPLACED DISCREPANT LONGERON SPLICE AS
- [SDR FDEA202104171312](https://openairdocs.org/sdr/FDEA202104171312), Apr 17, 2021: DOOR FRAME. CHAFED. LOWER CENTER CARGO DOOR, LOWER AFT JAMB EDGE DAMAGED, MARKED. REMOVED DAMAGE AND COMPLIED WITH DOOR JAMB REPAR AT LOWER CENTER CARGO DOOR LOWER AFT EDGE PER MD1
- [SDR FDEA202104171133](https://openairdocs.org/sdr/FDEA202104171133), Apr 17, 2021: SKIN. DAMAGED. RIGHT WING #3 SLAT AFT SIDE HAS MANY DAMAGED, MISSING AND LOOSE RIVETS. 0000435071 : HARPER, RICHARD R - 05-MAY-2021 19:03 REMOVED AND REPLACED FASTNERS ON R/H 
- [SDR FDEA202104171132](https://openairdocs.org/sdr/FDEA202104171132), Apr 17, 2021: SKIN. DAMAGED. RIGHT WING #4 SLAT AFT SIDE HAS MANY DAMAGED, MISSING AND LOOSE RIVETS. 0000435071 : HARPER, RICHARD R - 05-MAY-2021 18:58 REMOVED AND REPLACED FASTNERS ON R/H 
- [SDR FDEA202104161355](https://openairdocs.org/sdr/FDEA202104161355), Apr 16, 2021: PANEL. CORRODED. L/H WING TRAPERZOID PANEL ARC0269-503 SHOWS SIGNS OF CORROSION AND DELAMINATION PERFORMED REPAIR BONDING ON PNL ARC0269-503 PER SRM 51-71-00 VII PARAGRAPH 18.
- [SDR FDEA202104161131](https://openairdocs.org/sdr/FDEA202104161131), Apr 16, 2021: SEAT TRACK. WORN. MAIN CARGO COMPT, APPROX STA 1199 X= 47.50, SEAT TRACK WORN. FOUND SEAT TRACK TO BE WORN OUT OF LIMITS. REPLACED SEAT TRACK SECTION AT APPROX STA 1213 TO 1261 X
- [SDR FDEA202104161050](https://openairdocs.org/sdr/FDEA202104161050), Apr 16, 2021: SEAT TRACK. DAMAGED. MAIN CARGO COMPT, APPROX STA 959-969 X= -27.50, SEAT TRACK WORN AT TWO LOCATIONS. REMOVED DAMAGE AND INSTALLED PLUG REPAIR. REF. SRM 53-70-00 FIG. 2 VOL.1 "MAJO
- [SDR FDEA202104151057](https://openairdocs.org/sdr/FDEA202104151057), Apr 15, 2021: SUPPORT. CORRODED. STRUCTURES - FUSELAGE SEALS AND DRAINS: DURING FUSELAGE PRESSURIZATION, AT R/H MAIN LANDING GEAR WHEEL WELL R/H UPPER T-CORD FWRD BULKKHEAD LEAKING, SHOWING SHO
- [SDR FDEA202104151136](https://openairdocs.org/sdr/FDEA202104151136), Apr 15, 2021: BULKHEAD. CRACKED. CENTER LANDING GEAR WHEEL WELL, L/H FWD VERTICAL BULKHEAD, AT TRANSITION HOLE FOR SPOILER/AILERON CONTROL RODS, STA 1381 Z=-76 TO -87. DOUBLER FITTING AEA0486 H
- [SDR FDEA202104150974](https://openairdocs.org/sdr/FDEA202104150974), Apr 15, 2021: SEAT TRACK. WORN. MAIN DECK SEAT TRACK AT APROX STA 1640 RBL 47.50 WORN (MARKED) REMOVED WORN SEAT TRACK SECTION AND SPLICED IN NEW SECTION OF SEAT TRACK . REF. SRM 53-70-00 FIG.
- [SDR FDEA202102240441](https://openairdocs.org/sdr/FDEA202102240441), Feb 24, 2021: LINE. LEAKING. PDIS 316 29-02 5970 23FEB21 MEM FACT U "ENROUTE TO KMEM LEVEL 1 "HYD 3 ELEV OFF" ALERT ILLUMINATED. HYD 3 WAS AT 4.3 AT THE TIME. HYD 3 CONTINUED TO DECREASE TO
- [SDR FDEA202101010001](https://openairdocs.org/sdr/FDEA202101010001), Jan 1, 2021: TEE FITTING. CRACKED. "HYD 3 ELEV OFF" ALERT CAME ON. WE NOTICED HYD 3 QUANTITY SLOWLY DECLINE. WE LATER HAD HYD QUANTITY LOW. WE EXTENDED THE LANDING GEAR NORMALLY. WE THEN HAD HYD 
- [SDR FDEA202011282986](https://openairdocs.org/sdr/FDEA202011282986), Nov 28, 2020: LAMP. INOPERATIVE. MDIS 316 25-60 5669 28NOV20 MEM OPEN U. L1 DOOR SLIDE PRESS TO TEST LIGHT INOPERABLE. RELAMPED AND R & R BATTERIES, PER AMM 25-61-03-2. TROUBLESHOOTING IS REQUI
- [SDR FDEA2019111542953](https://openairdocs.org/sdr/FDEA2019111542953), Nov 14, 2019: BATTERY PACK. NO TEST. L1 DOOR SLIDE LIGHT WILL NOT TEST. REPLACED SLIDE INDICATOR BATTERIES, OPS CHECKS GOOD. REF MD10MM 25-61-02-2.
- [SDR FDEA201906111271](https://openairdocs.org/sdr/FDEA201906111271), Jun 11, 2019: ENGINE. FLUCTUATES. CLIMBOUT OUT OFF FL230"ENG 3 EXCEEDANCE"LVL ALERT DISPLAYED.EGT OBSERVERED AT 964 WITH PWR EQUAL OTHER PARAMETERS EQUAL.DURING CRUISE HAD #3 ENG PULLED BACK 10-
- [SDR FDEA201905081015](https://openairdocs.org/sdr/FDEA201905081015), May 8, 2019: PANEL. CORRODED. AUX FUEL TANK PANEL AT REAR SPAR HAS CORROSION AT MANY LOCATIONS. FABRICATED FUEL TANK BULKHEAD PANEL ON T19/1410809. REINSTALLED 6EA STIFFNERS IAW SRM 51-31-01
- [SDR FDEA2019042290865](https://openairdocs.org/sdr/FDEA2019042290865), Apr 19, 2019: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK AT X8.5 STA 1601 TO STA 1661 HAS GOUGES AND SURFACE CORROSION AT 3EA LOCATIONS. REMOVED AND REINSTALLED 2EA FLOOR PANELS FOR ACCESS IAW MD1
- [SDR FDEA201811033089](https://openairdocs.org/sdr/FDEA201811033089), Nov 3, 2018: SWITCH. ACTIVATED. AT FL280 ABOUT TO DESCEND INTO ICING WE TURNED ON WING ANTI-ICE. RECEIVED LVL 1 AIR SYS 3 OFF WITH RED MANIFOLD NR 3 INDICATION BOTH ON SCHEMATIC AND AIR SYSTEM
- [SDR FDEA201807061643](https://openairdocs.org/sdr/FDEA201807061643), Jul 6, 2018: PROBE. INOPERATIVE. 15 MIN ENROUTE. JUST LEVELED AT FL350. GOT LVL 2 FUEL QTY/USED CHK. COMPLIED WITH QRH. TOTAL QTY INDICATED. 9.0 LBS LESS THAN REQUIRED. ( SHOULD OF HAD 57.0, IN
- [SDR FDEA201803230766](https://openairdocs.org/sdr/FDEA201803230766), Mar 23, 2018: CONTROL MODULE. OUT OF ADJUST. DURING TAKEOFF THE FLAP/SLAT HANDLE WOULD NOT MOVE OUT OF TAKEOFF FLAP SETTING 15.5. INITIALLY COULD NOT MOVE FLAP SELECTOR WHEEL EITHER. EVENTUALLY USED THE FL
- [SDR FDEA201707192004](https://openairdocs.org/sdr/FDEA201707192004), Jul 19, 2017: WIRE. PULLED. EMERGENCY LIGHTS BATTERY 1 LOW ALERT. FOUND WIRE FOR PIN 8 OF P1-1756A PULLED OUT OF CONTACT. TERMINATED THE WIRE. EMERGENCY LIGHTS OPS CHECKED GOOD. PERFORMED 
- [SDR FDEA201703150897](https://openairdocs.org/sdr/FDEA201703150897), Mar 15, 2017: FITTING. CRACKED. RIGHT WING, OTBD FLAP INBD HINGE STRESS FITTING FOUND CRACKED. REMOVED AND REPLACED THE FITTING IAW EA 8-5740 -T0331942, AND DWG ARB0029.
- [SDR FDEA201703120855](https://openairdocs.org/sdr/FDEA201703120855), Mar 12, 2017: SKIN. CRACKED. RT WING, FWD OF FUEL ACCESS PANEL CUT OUT, L/E SKIN HAS A CRACKED .075 LENGTH. REMOVED CRACKED, INSTALLED FILLER AND DOUBLER PER SRM 57-10-00 VOL 1 FIGURE 106 S
- [SDR FDEA201703120854](https://openairdocs.org/sdr/FDEA201703120854), Mar 12, 2017: SKIN. CRACKED. RT WING, FWD OF FUEL ACCESS PANEL CUT OUT, L/E SKIN HAS A CRACKED .075 LENGTH. REMOVED CRACK AND INSTALLED DOUBLER AND FILLER PER SRM 57-10-00 FIG 106 VOL2 SHEE
- [SDR FDEA201703090827](https://openairdocs.org/sdr/FDEA201703090827), Mar 9, 2017: SUPPORT. CORRODED. AFT WASTE COMP STA 1967 LOWER CENTER SUPPORT STRUCTURE AFT SIDE HAS EXFOLIATION CORROSION AROUND SEVERAL NUTPLATES . REMOVED AND REPLACED SUPPORT PER DWG AGA 38
- [SDR FDEA201703080818](https://openairdocs.org/sdr/FDEA201703080818), Mar 8, 2017: SKIN. CRACKED. RT I/B FLAP VANE LOWER SURFACE HAS DEEP DENT, FOUND AN 3/8" CRACK. REPAIRED CRACK IAW SRM 51-71-00 VOL II PAGE 9 PAR 5 (A).
- [SDR FDEA201703020753](https://openairdocs.org/sdr/FDEA201703020753), Mar 2, 2017: SKIN. DELAMINATED. RIGHT OTBD FLAP VANE SKIN BENEATH NR 6 RUBSTRIP IS DELAMINATED. REPAIRED THE SKIN IAW SRM 51-71-00, VOL II, PAGE 9, PAR 5 (A), PAR 15.

All 107: https://openairdocs.org/aircraft/N316FE/reports.md

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

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

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

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

All 73: https://openairdocs.org/aircraft/N316FE/stcs.md

## Related

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

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