# N369FE: 1972 Mcdonnell Douglas MD-10-10F

- Status: Valid registration
- Airframe: [Mcdonnell Douglas MD-10-10F](https://openairdocs.org/model/mcdonnell-douglas-md-10-10f) (registry code 3022112, 6 seats)
- Engine: [GE CF6-6D](https://openairdocs.org/engine/ge-cf6-6d) (registry code 30076)
- 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: 46607
- Year built: 1972
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 23, 2008
- Certificate issued: October 25, 1997
- Expires: August 31, 2028
- Mode S code: A42E3D
- Registered owner: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION)
- 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=369FE
- Page: https://openairdocs.org/aircraft/N369FE

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): 81 in force

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

- [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 2013-19-20](https://openairdocs.org/ad/2013-19-20): JASC Code 32, Landing Gear · Boeing DC-10-10 and MD-10-10F. Effective Nov 7, 2013
- [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 2011-24-04](https://openairdocs.org/ad/2011-24-04): Wings · Boeing DC-10-10, DC-10-10F and MD-10-10F. Effective Jan 3, 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 2010-20-14](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 2010-13-06](https://openairdocs.org/ad/2010-13-06): Wings · Boeing DC-10-10, DC-10-10F and MD-10-10F. Effective Jul 28, 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 2008-09-17](https://openairdocs.org/ad/2008-09-17): Stray nickel or chrome plating deposits · Boeing DC-10-10, DC-10-10F, DC-10-15 and 1 more. Effective Jun 6, 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 2007-04-17](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 2006-17-15](https://openairdocs.org/ad/2006-17-15): Replacing the clamp bases for the fuel vent pipe with improved clamp bases · Boeing DC-10-10, DC-10-10F and MD-10-10F. Effective Sep 29, 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

### Matched by engine (GE CF6-6D)

- [AD 2003-10-01](https://openairdocs.org/ad/2003-10-01): High pressure turbine rotor (HPTR) rear shafts · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Jun 17, 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 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 98-18-10](https://openairdocs.org/ad/98-18-10): Low Pressure Turbine Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Sep 30, 1998
- [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 91-24-01](https://openairdocs.org/ad/91-24-01): Compressor Rear Frame Casing · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective May 26, 1992
- [AD 91-15-03](https://openairdocs.org/ad/91-15-03): Fan Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Aug 5, 1991
- [AD 91-12-09](https://openairdocs.org/ad/91-12-09): Fan Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Jun 27, 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 90-19-08](https://openairdocs.org/ad/90-19-08): Low Pressure Turbine Rotor Stage One Disk · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Oct 15, 1990
- [AD 89-20-01 R1](https://openairdocs.org/ad/89-20-01-R1): Fan Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Dec 12, 1989
- [AD 88-12-01](https://openairdocs.org/ad/88-12-01): High Pressure Compressor Rear Shafts · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Jun 6, 1988
- [AD 81-19-08](https://openairdocs.org/ad/81-19-08): Low Pressure Turbine Rotor Stage 2 Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Sep 21, 1981
- [AD 80-03-06](https://openairdocs.org/ad/80-03-06): Stage 2 HPT Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Feb 8, 1980
- [AD 78-07-03](https://openairdocs.org/ad/78-07-03): Compressor Spool · General Electric CF6-6D and CF6-6D1. Effective May 22, 1978
- [AD 76-21-04](https://openairdocs.org/ad/76-21-04): High Pressure Compressor · General Electric CF6-6D and CF6-6D1. Effective Nov 30, 1977
- [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 75-22-11](https://openairdocs.org/ad/75-22-11): High Pressure Turbine Thermal Shield · General Electric CF6-6D and CF6-6D1. Effective Oct 28, 1975
- [AD 74-14-08](https://openairdocs.org/ad/74-14-08): Turbine Blades · General Electric CF6-6D and CF6-6D1. Effective Jul 12, 1974
- [AD 72-16-03](https://openairdocs.org/ad/72-16-03): Turbine Discs · General Electric CF6-6D and CF6-6D1. Effective Aug 8, 1972

### 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 2003-03-15](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 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 95-18-14](https://openairdocs.org/ad/95-18-14) (historical): High Pressure Compressor Rotor · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Sep 21, 1995

All 96: https://openairdocs.org/aircraft/N369FE/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 N369FE.

## FAA accident and incident reports

None matched to N369FE.

## Service difficulty reports (63, 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 FDEA201609093158](https://openairdocs.org/sdr/FDEA201609093158), Sep 9, 2016: CHANNEL. CORRODED. FORWARD CARGO COMPARTMENT FRAME DOUBLER AT STA 979 AT LONG 52, 51R AND 51L. FRAME MOUNT DOUBLER CHANNEL POSSIBLE CORROSION. FABRICATED AND INSTALLED J-CHANNEL I
- [SDR FDEA200911194048](https://openairdocs.org/sdr/FDEA200911194048), Nov 19, 2009: FIRE BOTTLE. LOW. ENG FIRE AGNT LO ALERT AND ENG 2 AGT 1 LOW LIGHT DURING CRUISE FOUND NR 2 ENG 1 FIRE BOTTLE LOW PRESS SWITCH BAD, REPLACED NR 2 ENG NR1 FIRE BOTTLE, LIGHT EXT. 
- [SDR FDEA200910203620](https://openairdocs.org/sdr/FDEA200910203620), Oct 20, 2009: VALVE. ACTIVATED. "AIR SYS 1 OFF" ANNUNCIATED. AFTER ABOUT A MINUTE GOT "AIR MANF 1 FAIL" LEVEL 3 ALERT. COMPLIED WITH QRH. DIVERTED, DURING DECENT, AIR MANF 1 FAIL ALERT CAME ON
- [SDR FDEA200902100502](https://openairdocs.org/sdr/FDEA200902100502), Feb 10, 2009: RELIEF VALVE. FAILED. AT FL 310 RECEIVED LEVEL 3 "CABIN ALTITUDE" ALERT WITH NO OTHER NOISE OR INDICATIONS. ENG A/I WAS ON. FOLLOWED QRH AND COULD NOT (WITH 3 PACKS) MAINTAIN INDICAT
- [SDR FDEA200801070057](https://openairdocs.org/sdr/FDEA200801070057), Jan 7, 2008: SKIN. CRACKED. FROM J/C SP10270016-7000-10J OTBD ELEVATOR LT T/E TIP WITH CRACK DUE ACCIDENTAL CONTACT AGAINST CRADLE. REPAIRED AREA IAW SRM 55-10-00 FIG 7 VOL I AND SRM 55-20
- [SDR 08FDEA00057](https://openairdocs.org/sdr/08FDEA00057), Jan 7, 2008: SKIN. CRACKED. OUTBD ELEVATOR LT T/E TIP WITH CRACK DUE ACCIDENTAL CONTACT AGAINST CRADLE.
- [SDR 07FDEA05046](https://openairdocs.org/sdr/07FDEA05046), Dec 13, 2007: NONE. NONE. MAIN CABIN L4 PASSENGER DOOR UPPER INTERNAL JAMB EXISTING DOUBLER. ACCOMPLISHED EA NR 8-5310-115295A.
- [SDR 07FDEA04985](https://openairdocs.org/sdr/07FDEA04985), Dec 3, 2007: LONGERON. CORRODED. FWD CARGO COMPT BILGE AREA FOUND CORROSION WITH EXFOLIATION ON LONGERON, REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 5.
- [SDR 07FDEA04982](https://openairdocs.org/sdr/07FDEA04982), Dec 3, 2007: LONGERON. CORRODED. FWD CARGO COMPT BILGE AREA FOUND SEVERE CORROSION ON LONGERON. REPAIRED AREA IAW SRM 53-30-00 FIG 10 VOL I.
- [SDR 07FDEA04981](https://openairdocs.org/sdr/07FDEA04981), Dec 3, 2007: LONGERON. CORRODED. FWD CARGO COMPT SUMP AREA FOUND CORROSION WITH EXFOLIATION, SEE NRC N00315, N00316, N00294, N00253. REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 5 SHEET 1.
- [SDR 07FDEA04977](https://openairdocs.org/sdr/07FDEA04977), Dec 3, 2007: BEAM. CRACKED. FWD CARGO COMPT BILGE AREA FOUND CRACK ON BEAM. REPAIRED BEAM IAW SRM 53-60-01 VOL I FIG 3.
- [SDR 07FDEA04902](https://openairdocs.org/sdr/07FDEA04902), Nov 23, 2007: FRAME. CRACKED. INT CAC CRACK ON FRAME. PERFORMED FRAME REPAIR IAW SRM 53-30-00 VOL I FIG 7.
- [SDR 07FDEA04901](https://openairdocs.org/sdr/07FDEA04901), Nov 23, 2007: INTERCOSTAL. DAMAGED. LT WING L/E INTERNAL STRUCTURE ON HORIZONTAL INTERCOSTAL EXISTING ANGLE REPAIR. REPLACED INTERCOSTAL IAW DWG ARB2408 AND ARB1333.
- [SDR 07FDEA04900](https://openairdocs.org/sdr/07FDEA04900), Nov 22, 2007: LONGERON. CRACKED. FWD CARGO COMPT BILGE AREA FOUND CRACK ON LONGERON, SEE NRC N00293, N00294, N00295, N00297. REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 1-2.
- [SDR 07FDEA04856](https://openairdocs.org/sdr/07FDEA04856), Nov 19, 2007: SKIN PANEL. CRACKED. DURING STB INSP FOUND PANEL P/N 7206-1 AND P/N 7207-1 OF CONSTANT SECTION SKIN PANEL PLANKS, SEE ATTACHED SHEET FOR BEST DETAIL. CRACK IS IN FLYABLE LIMITS. ACC
- [SDR 07FDEA04716](https://openairdocs.org/sdr/07FDEA04716), Nov 2, 2007: DOOR FRAME. CRACKED. MAIN CABIN R1 DOOR FWD JAMB DURING PERFORM OAN J/C SP10240272-7001-2J FOUND CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-00-01 VOL I FIG 8.
- [SDR FDEA200710174625](https://openairdocs.org/sdr/FDEA200710174625), Oct 17, 2007: SILL. CORRODED. FWD CARGO COMPT FOUND CORROSION WITH EXFOLIATION ON FITTING SILL DOOR INSIDE JAMB FWD. REPAIRED AREA IAW SRM 53-50-00 FIG 1 VOL I.
- [SDR 07FDEA04628](https://openairdocs.org/sdr/07FDEA04628), Oct 17, 2007: LONGERON. CRACKED. CTR CARGO COMPT CRACK ON LONGERON. REPAIRED LONGERON IAW SRM 53-10-00 FIG 1-2 VOL I.
- [SDR 07FDEA04627](https://openairdocs.org/sdr/07FDEA04627), Oct 17, 2007: LONGERON. CRACKED. CTR CARGO COMPT CRACK ON LONGERON. REPAIRED LONGERON IAW SRM 53-10-00 FIG 1-2 VOL I.
- [SDR 07FDEA04625](https://openairdocs.org/sdr/07FDEA04625), Oct 17, 2007: SILL. CORRODED. FWD CARGO COMPT FOUND CORROSION WITH EXFOLIATION ON FITTING SILL DOOR INSIDE JAMB FWD.
- [SDR 07FDEA04550](https://openairdocs.org/sdr/07FDEA04550), Oct 10, 2007: SEAT TRACK. CORRODED. ENTRY WAY, DURING REMOVAL FLOOR PANELS WITH OAN J/C MD10-0600C220-1JR FOUND SEVERE EXFOLIATION CORROSION INTERNAL SEAT TRACK. REPAIRED SEAT TRACK IAW SRM 53-70-
- [SDR 07FDEA04417](https://openairdocs.org/sdr/07FDEA04417), Oct 1, 2007: DOUBLER. DAMAGED. RT WING NR 1 SLAT EXTERNAL SKIN EXISTING DOUBLER. REPAIRED AREA IAW SRM 57-10-00 FIG 84 VOL I.
- [SDR 07FDEA04169](https://openairdocs.org/sdr/07FDEA04169), Sep 21, 2007: SKIN. CORRODED. LT WING INBD AILERON CORROSION BOTTOM UPPER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 86 VOL I.
- [SDR 07FDEA04167](https://openairdocs.org/sdr/07FDEA04167), Sep 21, 2007: WEB. CORRODED. PERFORMED INSPECTION AFTER REMOVAL FLOOR PANEL IN COCKPIT WITH OAN J/C SP10530208-2JR, FOUND SEVERE CORROSION WITH EXFOLIATION ON MEMBRANE AND CRACK 2" LONG. RE
- [SDR 07FDEA04165](https://openairdocs.org/sdr/07FDEA04165), Sep 21, 2007: FLOOR PANEL. CRACKED. PERFORMED INSPECTION AFTER REMOVAL FLOOR PANEL IN COCKPIT WITH OAN JC SP10530208-2JR, FOUND CRACK ON MEMBRANE. REPAIRED WEB IAW SRM 53-00-01 VOL I FIG 10.
- [SDR 07FDEA04008](https://openairdocs.org/sdr/07FDEA04008), Sep 19, 2007: WEB. CORRODED. PERFORMED INSPECTION AFTER REMOVAL FLOOR PANEL IN COCKPIT WITH OAN J/C SP10530208-2JR, FOUND MODERATE CORROSION AND CRACK 2" LONG ON MEMBRANE. REPLACED WEB SECT
- [SDR 07FDEA03818](https://openairdocs.org/sdr/07FDEA03818), Sep 17, 2007: STRUCTURE. CRACKED. FWD CARGO COMPT BILGE AREA HAS CRACK ON CAP TEE OF BULKHEAD. REPAIRED AREA IAW EA 8-5310-99388.
- [SDR 07FDEA03590](https://openairdocs.org/sdr/07FDEA03590), Sep 12, 2007: SKIN. CRACKED. PYLON NR 1 EXT SKIN FOUND CRACK ON SKIN UPPER SIDE RT. 10-25-07 REPAIRED PYLON SKIN IAW SRM 51-00-01 VOL I FIG 100 & SRM 54-00-01 VOL I FIG 2B.
- [SDR 07FDEA03369](https://openairdocs.org/sdr/07FDEA03369), Sep 5, 2007: FLOOR PANEL. CORRODED. PERFORMED INSPECTION AFTER REMOVAL FLOOR PANEL IN COCKPIT WITH OAN J/C SP10530208-2JR, FOUND SEVERE CORROSION WITH EXFOLIATION (OUT OF LIMIT) ON MEMBRANE AND CR
- [SDR 07FDEA03336](https://openairdocs.org/sdr/07FDEA03336), Sep 4, 2007: RIB. CRACKED. RT WING TIP CRACKS, 1.5" LONG ON EXTERNAL SKIN XW 928, YW 799. CONTINUED CRACK ON INT OLD REPAIR ON FRAME XW 928, YW 799. REPAIRED AREA IAW SRM 57-00-01 FIG 10 
- [SDR 07FDEA03335](https://openairdocs.org/sdr/07FDEA03335), Sep 4, 2007: BULKHEAD. CRACKED. NLG W/W FOUND CRACK ON LT VERTICAL BULKHEAD. REPAIRED WEB IAW SRM 53-40-00 FIG 34 VOL I.
- [SDR 07FDEA03319](https://openairdocs.org/sdr/07FDEA03319), Sep 3, 2007: SKIN. DAMAGED. R1 PASSENGERS DOOR DEFORMATION OLD REPAIR ON UPPER FWD CORNER EXTERNAL SKIN. REPAIRED AREA IAW SRM 52-10-00 FIG 12A VOL I.
- [SDR 07FDEA03318](https://openairdocs.org/sdr/07FDEA03318), Sep 3, 2007: PAN. CRACKED. LOWER CENTER CARGO DOOR CRACK LONG .250" AND DEFORMATION ON LWR FORWARD CORNER. 11-07-07 REPAIRED AREA IAW SRM 52-10-00 FIG 17 VOL I.
- [SDR 07FDEA03217](https://openairdocs.org/sdr/07FDEA03217), Aug 29, 2007: LONGERON. CORRODED. FWD CARGO COMPT BILGE AREA FOUND SEVERE CORROSION ON LONGERON. REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 1& 2.
- [SDR 07FDEA03216](https://openairdocs.org/sdr/07FDEA03216), Aug 29, 2007: BULKHEAD. CRACKED. RT W/W CRACK 0.5" LONG ON VERTICAL BULKHEAD. REPAIRED BULKHEAD IAW SRM 53-00-01 VOL I FIG 10.
- [SDR 07FDEA03215](https://openairdocs.org/sdr/07FDEA03215), Aug 29, 2007: BULKHEAD. CRACKED. CTR W/W SPACE CRACK ON VERTICAL BULKHEAD. PERFORMED REPAIR IAW SRM 53-00-01 VOL I FIG 4.
- [SDR 07FDEA03146](https://openairdocs.org/sdr/07FDEA03146), Aug 27, 2007: INTERCOSTAL. CRACKED. LT WING L/E CRACK ON INTERNAL INTERCOSTAL. REPAIRED INTERCOSTAL IAW SRM 57-00-01 VOL I FIG 10.
- [SDR 07FDEA03145](https://openairdocs.org/sdr/07FDEA03145), Aug 27, 2007: INTERCOSTAL. CRACKED. LT WING L/E INTERNAL CRACK LONG 0.50" ON INTERCOSTAL. 10-10-07 REPAIRED INTERCOSTAL IAW SRM 57-00-01 VOL I FIG 10.
- [SDR 07FDEA03143](https://openairdocs.org/sdr/07FDEA03143), Aug 27, 2007: RIB. CRACKED. LT WING INTERNAL L/E ON UPPER RIB FOUND CRACK 0.70" LONG. REPAIRED RIB IAW SRM 57-20-00 FIG 1 VOL I.
- [SDR 07FDEA03088](https://openairdocs.org/sdr/07FDEA03088), Aug 24, 2007: BULKHEAD. CRACKED. CTR W/W SPACE: CRACKS ON VERTICAL BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 10 SHT 4 VOL I.
- [SDR 07FDEA03086](https://openairdocs.org/sdr/07FDEA03086), Aug 24, 2007: SKIN. CORRODED. LT WING OUTBOARD FLAP CORROSION UNDER UPPER SKIN. 10-11-07 REPAIRED AREA IAW SRM 57-10-00 VOL I FIG 85.
- [SDR FDEA200708223046](https://openairdocs.org/sdr/FDEA200708223046), Aug 22, 2007: SKIN. CRACKED. LT WING L/E CRACK ON EXTERNAL LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 VOL I.
- [SDR FDEA200708223034](https://openairdocs.org/sdr/FDEA200708223034), Aug 22, 2007: SKIN. CRACKED. L/E RT WING CRACK ON EXTERNAL SKIN L/E. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.
- [SDR 07FDEA03049](https://openairdocs.org/sdr/07FDEA03049), Aug 22, 2007: SKIN. DENTED. EXT SURFACE RT SIDE FOUND DENT 2" BY 1" DEEP 0.062" ON SKIN. 09-19-07 REPAIRED SKIN IAW SRM 53-20-00 FIG 13 SHT 3-5 VOL I.
- [SDR 07FDEA03048](https://openairdocs.org/sdr/07FDEA03048), Aug 22, 2007: SKIN. DENTED. EXT FUSELAGE RT SIDE FOUND DENT .45" BY .25" DEEP 0.027" ON SKIN. 09-19-07 REPAIRED SKIN IAW SRM 53-20-00 FIG 13 SHT 3-5 VOL I.
- [SDR 07FDEA03047](https://openairdocs.org/sdr/07FDEA03047), Aug 22, 2007: SKIN. CRACKED. LT WING LWR SURFACE FOUND CRACK ON SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.
- [SDR 07FDEA03046](https://openairdocs.org/sdr/07FDEA03046), Aug 22, 2007: SKIN. CRACKED. LT WING L/E CRACK ON EXTERNAL LOWER SKIN.
- [SDR 07FDEA03034](https://openairdocs.org/sdr/07FDEA03034), Aug 22, 2007: SKIN. CRACKED. L/E RT WING CRACK ON EXTERNAL SKIN L/E .
- [SDR 07FDEA03033](https://openairdocs.org/sdr/07FDEA03033), Aug 22, 2007: SCOOP. CRACKED. INT CAC CRACK ON SUGAR SCOOP. REPAIR AREA IAW SRM 53-40-00 VOL I FIG 8.
- [SDR 06FDEA00043](https://openairdocs.org/sdr/06FDEA00043), Jan 5, 2006: SENSOR. MALFUNCTIONED. PDIS: ON ROTATION FOR TAKEOFF BOTH STICK SHAKERS ACTIVATED AND REMAINED ON WITH NORMAL AIRCRAFT INDICATIONS, NORMAL FEEL, AIRSPEED INDICATORS ALL THE SAME & NOR

All 63: https://openairdocs.org/aircraft/N369FE/reports.md

## STCs that may be installed (OpenAirDocs) (63, 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-10-10F)

- [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 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 ST00536SE](https://openairdocs.org/stc/ST00536SE): Installation of the Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS). Honeywell International Inc
- [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 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 ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) 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 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 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 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
- [STC ST01874LA](https://openairdocs.org/stc/ST01874LA): Installation of a main deck cargo container fire suppression system. Federal Express Corp
- [STC ST01919SE](https://openairdocs.org/stc/ST01919SE): Installation of a coffee maker conversion kit on an aircraft. Radford and Associates Inc
- [STC ST01989NY-D](https://openairdocs.org/stc/ST01989NY-D): Installation of ELS/EHS. Delta Engineering Corporation
- [STC ST00800CH](https://openairdocs.org/stc/ST00800CH): Installation of an On-Board Maintenance Terminal System. Canard Aerospace Corporation
- [STC ST01166CH](https://openairdocs.org/stc/ST01166CH): Installation of provisions for a pilot access terminal (PAT). Canard Aerospace Corporation
- [STC ST01307CH](https://openairdocs.org/stc/ST01307CH): Installation of Gatelink Radio System. Canard Aerospace Corporation
- [STC ST01900LA](https://openairdocs.org/stc/ST01900LA): Installation of Meggitt Safety Systems, Inc. Engine and APU Fire Detection System Control Module Modification Kit P/N 904738. Meggitt Safety Systems, Inc
- [STC ST02249CH](https://openairdocs.org/stc/ST02249CH): Installation of an ELTA ADT 406 AF Emergency Locator Transmitter (ELT). Armstrong Aerospace
- [STC ST01185WI-D](https://openairdocs.org/stc/ST01185WI-D): Modification of an existing FAA approved Collins HF Communication System with HFS-900D Receiver/Transmitter. Rockwell Collins Inc
- [STC ST01667NY](https://openairdocs.org/stc/ST01667NY): Modification of existing Mode S Transponders and TCAS by installation of HOneywell/ACSS P/N 7517800-10005, ATDL transponders and 7517900-10004 TCAS. Approval is only for replacement of transponder units and TCAS unit. Does not include installation of transponder or TCAS system, wiring, trays, antennas, etc. Delta Engineering

All 63: https://openairdocs.org/aircraft/N369FE/stcs.md

## Related

- Other Mcdonnell Douglas MD-10-10F aircraft: https://openairdocs.org/model/mcdonnell-douglas-md-10-10f/aircraft.md
- The GE CF6-6D engine: https://openairdocs.org/engine/ge-cf6-6d.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.