# N367FE: 1971 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: 46605
- Year built: 1971
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 15, 2006
- Certificate issued: October 7, 1997
- Expires: August 31, 2028
- Mode S code: A426CF
- 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=367FE
- Page: https://openairdocs.org/aircraft/N367FE

From the FAA registry file of October 22, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 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/N367FE/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 N367FE.

## FAA accident and incident reports

None matched to N367FE.

## Service difficulty reports (138, 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 FDEA201306021348](https://openairdocs.org/sdr/FDEA201306021348), Jun 2, 2013: WEB. CRACKED. THREE CRACKS LT MLG WW INBD BULKHEAD 25 INCHES AND 27 INCHES AFT OF FWD BULKHEAD AND BOTH 4 INCHES DOWN FROM UPPER BULKHEAD. LAST CRACK IS 23 INCHES AFT OF FWD 
- [SDR FDEA201306021347](https://openairdocs.org/sdr/FDEA201306021347), Jun 2, 2013: BULKHEAD. CRACKED. TWO CRACKS CENTER MLG WW LT BULKHEAD 25 INCHES AFT OF FWD BULKHEAD AND 4 INCHES AND 5.5 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED IAW EA 8-5310-T0300629.
- [SDR FDEA201301270199](https://openairdocs.org/sdr/FDEA201301270199), Jan 27, 2013: LINE. CLOGGED. ENGINE FAIL WARNING ILLUMINATED ON GLARESHIELD ON TAKEOFF, NR 1 ENG N1 DID NOT ACCELERATE PAST 87 PERCENT. ENG DID NOT FAIL. DISCONNECTED NR 1 ENG CDP LINE. BLE
- [SDR FDEA201202230648](https://openairdocs.org/sdr/FDEA201202230648), Feb 23, 2012: BOLT. CORRODED. FOUND TRUNNION BOLT CORRODED. REMOVED AND INSTALLED NEW FWD TRUNNION BOLT ON RT MLG. IAW E.O 8-3210-7-5004 PT 2.
- [SDR FDEA201202190620](https://openairdocs.org/sdr/FDEA201202190620), Feb 19, 2012: SHEAR TIE. CORRODED. AFT CARGO COMPARTMENT WASTE TANK AREA HAS 2 EA CORRODED SHEAR TIES AT STA. 1997 BETWEEN LONGERON L51-52 AND R50-51. REMOVED AND REPLACED SHEAR TIES AT STA 1997 
- [SDR FDEA201202100544](https://openairdocs.org/sdr/FDEA201202100544), Feb 10, 2012: ANGLE. CORRODED. AFT CARGO BAY ANGLE COMMON TO FRAME AND SKIN AT BS 1964 BETWEEN R51L AND L51L IS SHOWING EVIDENCE OF EXFOLIATION. REMOVE AND REPLACE WITH NEW ANGLE. LOCATED, DR
- [SDR FDEA201202100545](https://openairdocs.org/sdr/FDEA201202100545), Feb 10, 2012: SHEAR TIE. CORRODED. AFT CARGO BAY ANGLE COMMON TO FRAME AND SKIN AT STA.1975 BETWEEN R51L AND L51L HAS EVIDENCE OF CORROSION. LOCATED, DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40
- [SDR FDEA201202090539](https://openairdocs.org/sdr/FDEA201202090539), Feb 9, 2012: BEAM. CRACKED. R3 DOOR BEAM IS CRACKED. R & R CRACKED DOOR BEAM, REF SRM 51-35-01, VOL II.
- [SDR FDEA201202090536](https://openairdocs.org/sdr/FDEA201202090536), Feb 9, 2012: STRUCTURE. GOUGED. LT WING NR 3 SLAT TRACK IS RIDING/CUTTING INTO L/E SUPPORT STRUCTURE. FWD UPPER TRACK CORNERS. CLEARANCE CHECKED GOOD.
- [SDR FDEA201202090535](https://openairdocs.org/sdr/FDEA201202090535), Feb 9, 2012: STRUCTURE. GOUGED. LEFT WING NR 1 SLAT TRACK IS RIDING AND CUTTING INTO L/E SUPPORT STRUCTURE. FWD UPPER TRACK CORNERS. BURNISHED THE SLAT TRACK IAW CMM 57-55-04. ALODINE AND PAIN
- [SDR FDEA201202090533](https://openairdocs.org/sdr/FDEA201202090533), Feb 9, 2012: SLAT TRACK. GOUGED. LEFT WING NR 16 SLAT TRACK INBD SIDE IS RIDING INTO L/E STRUCTURE. L/E STRUCTURE HAS DAMAGE DUE TO THIS RIDING CONDITION. BLENDED DAMAGE AREA IAW SRM 57-00-01, 
- [SDR FDEA201201100064](https://openairdocs.org/sdr/FDEA201201100064), Jan 10, 2012: LENS. MISSING. RT DOOR DISARMED LIGHT LENS IS MISSING. FOUND LENS ON FLOOR. REINSTALLED LENS. LIGHTS WORK OK.
- [SDR FDEA201105282016](https://openairdocs.org/sdr/FDEA201105282016), May 28, 2011: BATTERY. INOPERATIVE. R1 DOOR CIRCUITRY TEST LIGHT INOPERATIVE. REMOVED AND REPLACED THE R1 DOOR REMOTE SLIDE PRESSURE INDICATOR AND REPLACED BATTERIES. OPS CK GOOD.
- [SDR FDEA201012044578](https://openairdocs.org/sdr/FDEA201012044578), Dec 4, 2010: CONTROLLER. FAILED. AT CRUISE FL330, AIR MANF 2 FAIL. COMPLIED WITH QRH AND DIVERTED. RELEASED FOR SERVICE IAW MEL: 36-23-01-02, CATEGORY: C EXPIRATION: 13DEC10 "MEL 36-23-01-02: N
- [SDR FDEA201004281382](https://openairdocs.org/sdr/FDEA201004281382), Apr 28, 2010: SKIN. DENTED. RT WING INBD FLAP UPPER SURFACE AT APPROX XIFH 215 FOUND 1 EACH DENT WITH DEEP NICK DURING BLEND OUT. DENT WITH DEEP NICK AT RT WING INBD FLAP UPPER SURFACE AT 
- [SDR FDEA201004261365](https://openairdocs.org/sdr/FDEA201004261365), Apr 26, 2010: SEAT TRACK. CORRODED. AFT CABIN AT STA 1963, X= -107.25 RT CURVE SEAT TRACK FOUND CORROSION. FT CABIN AT STA 1963, X= -107.25 RT CURVE SEAT TRACK R & R IAW SRM 51-31-01, VOL II REV 9
- [SDR FDEA201004261360](https://openairdocs.org/sdr/FDEA201004261360), Apr 26, 2010: SKIN. DEFORMED. LT WING INBD FLAP LOWER L/E INBD OF OTBD HINGE, FOUND SKIN DEFORMED. LT WING INBD FLAP LOWER L/E INBD OF OTBD HINGE DEFORMED SKIN EVALUATED AND FOUND WITHIN LIM
- [SDR FDEA201004251359](https://openairdocs.org/sdr/FDEA201004251359), Apr 25, 2010: SKIN. DENTED. EMPENNAGE- RT HORIZONTAL STABILIZER NR3 L/E (FROM INBD) FOUND DENTED. DENT AREA TRIMMED OUT AND FABRICATED REPAIR DOUBLER, REPAIR SKIN AND REPAIR CARRRIED OUT I
- [SDR FDEA201004241347](https://openairdocs.org/sdr/FDEA201004241347), Apr 24, 2010: SKIN. DENTED. DENT - RT WING INBD FLAP LOWER SURFACE. REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 3, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.
- [SDR FDEA201004231316](https://openairdocs.org/sdr/FDEA201004231316), Apr 23, 2010: STRUCTURE. CRACKED. LT WING - NR 1 SLAT LOWER SIDE BETWEEN NR 1 AND NR 2 TRACK FOUND EXTRUSION WITH CRACK. REPAIR CARRIED OUT IAW EA 8-5750-137977: REPAIR CLASSIFIED AS MAJOR IAW G
- [SDR FDEA201004231315](https://openairdocs.org/sdr/FDEA201004231315), Apr 23, 2010: PANEL. BULGED. LT WING T/E UPPER PANEL AT REAR SPAR APPROX XORS 860 FOUND WITH BULGING. CORROSION FOUND AT BULGING AREA REMOVED AND REPROTECTED IAW SRM 51-21-01 VOL II, REV 96
- [SDR FDEA201004231314](https://openairdocs.org/sdr/FDEA201004231314), Apr 23, 2010: DOOR FRAME. DAMAGED. FWD CARGO DOOR JAMB-UPON REMOVAL OF AFT LOWER DOOR JAMB SEAL RETAINER, RIVET HOLES ON WEB STRUCTURE FOUND ELONGATED. REPAIR CARRIED OUT IAW EA NR 8-5310-137983,
- [SDR FDEA201004231313](https://openairdocs.org/sdr/FDEA201004231313), Apr 23, 2010: ANGLE. CRACKED. FWD CARGO BILGE AREA - APPROX STA 899 FRAME 'L' CLIP FOUND CRACKED. FWD CARGO BILGE AREA STA 899 FRAME 'L' CLIP REPAIR CARRIED OUT IAW SRM 53-30-00, FIG.10, VOL
- [SDR FDEA201004231312](https://openairdocs.org/sdr/FDEA201004231312), Apr 23, 2010: BEAM. CRACKED. CRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 7 LOWER JAMB FITTING AT HOLES B AND D. REPAIR C
- [SDR FDEA201004231311](https://openairdocs.org/sdr/FDEA201004231311), Apr 23, 2010: BEAM. CRACKED. CRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" HOLE AT MAIN CARGO DOOR NR 7 LOWER JAMB FITTING AT HOLE B. REPAIR CA
- [SDR FDEA201004231310](https://openairdocs.org/sdr/FDEA201004231310), Apr 23, 2010: BEAM. CRACKED. CRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 6 LOWER JAMB FITTING AT HOLE C. REPAIR CARRIED 
- [SDR FDEA201004231309](https://openairdocs.org/sdr/FDEA201004231309), Apr 23, 2010: BEAM. CRACKED. CRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 6 LOWER JAMB FITTING AT HOLES C. REPAIR CARRIED
- [SDR FDEA201004231308](https://openairdocs.org/sdr/FDEA201004231308), Apr 23, 2010: BEAM. CRACKED. CRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 1 LOWER JAMB FITTING AT HOLES A, B AND D. REPAI
- [SDR FDEA201004231307](https://openairdocs.org/sdr/FDEA201004231307), Apr 23, 2010: RIB. CRACKED. RT WING FIXED L/E LOWER FOUND CRACKED ON SLAT TRACK NR 16 INBD FWD RIB. CRACKED AT RT WING FIXED L/E LOWER ON SLAT TRACK NR 16 INBD FWD RIB REPLACED IAW SRM 51-
- [SDR FDEA201004231306](https://openairdocs.org/sdr/FDEA201004231306), Apr 23, 2010: BEAM. CRACKED. CRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 1, LOWER JAMB FITTING AT HOLES A, B, C AND D. R
- [SDR FDEA201004231305](https://openairdocs.org/sdr/FDEA201004231305), Apr 23, 2010: SUPPORT FITTING. CRACKED. CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES A, B, C AND D. REPAIR CARRIED OUT 
- [SDR FDEA201004231304](https://openairdocs.org/sdr/FDEA201004231304), Apr 23, 2010: SUPPORT FITTING. CRACKED. CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES A, B, C AND D. REPAIR CARRIED OUT 
- [SDR FDEA201004231303](https://openairdocs.org/sdr/FDEA201004231303), Apr 23, 2010: SKIN. DAMAGED. FUSELAGE - FWD CARGO DOOR CUT-OUT LOWER AFT EXISTING DOUBLER FOUND DAMAGED. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 26 VOL. I REV. 96. REPAIR CLASSIFIED AS M
- [SDR FDEA201004231302](https://openairdocs.org/sdr/FDEA201004231302), Apr 23, 2010: SKIN. DENTED. FUSELAGE - AFT OF NOSE RADOME AT STA 305 LOWER CTR AREA WITH EXISTING BLEND OUT. EXISTING BLEND OUT AT FUSELAGE AFT OF NOSE RADOME AT STA 305, LOWER CTR AREA EV
- [SDR FDEA201004231301](https://openairdocs.org/sdr/FDEA201004231301), Apr 23, 2010: SKIN. DAMAGED. WHILE ACCOMPLISHING EA 8-5230-137737 PART 3 -TO REPAIR SKIN OF AFT LOWER CARGO DOOR OUTER SKIN, FOUND REPAIR AREA CLOSE TO COVER CUT-OUT AND PLACARD INSTALLATIO
- [SDR FDEA200912104402](https://openairdocs.org/sdr/FDEA200912104402), Dec 10, 2009: VALVE. LEAKING. AT FL 280 GOT LEVEL-1 "HYD 3 ELEV OFF" FLUID IN NR 3 3.5 GAL. SECURED HYD SYS NR 3 FOR LANDING. AFTER DIRTY UP LOST REMAINING FLUID FOLLOWED BY "HYD 3 FAIL" TOW
- [SDR FDEA200810224488](https://openairdocs.org/sdr/FDEA200810224488), Oct 22, 2008: LEAD. FAILED. WHEN DESCENDING OUT OF FL240 FOR LANDING, GOT "ENG 3 EGT HI" AND ENG 3 EXCEEDANCE ALERTS, EGT 3 INDICATIONS SEQUENCED BETWEEN HIGH INDICATIONS (1053) AND AMBER 
- [SDR 08FDEA04488](https://openairdocs.org/sdr/08FDEA04488), Oct 22, 2008: LEAD. MALFUNCTIONED. WHEN DESCENDING OUT OF FL240 FOR LANDING, GOT "ENG 3 EGT HI" AND ENG 3 EXCEEDANCE ALERTS EGT 3 INDICATION. SEQUENCED BETWEEN HIGH INDICATIONS (1053) AND AMBER "
- [SDR 08FDEA03717](https://openairdocs.org/sdr/08FDEA03717), Sep 3, 2008: PRESSURE SWITCH. FAILED. DURING CLIMB-OUT, ABOVE 10,000 FT, RECEIVED LEVEL 1 HYD 2 OFF ALERT WITH SUBSEQUENT SHUTDOWN OF LT AND RT NR 2 ENGINE DRIVEN PUMPS. DURING APPROACH AND LANDING 
- [SDR 08FDEA01954](https://openairdocs.org/sdr/08FDEA01954), May 22, 2008: PANEL. DELAMINATED. RIGHT WING PANEL 635 BL HAS DELAMINATION AND A PUNCTURE. REPAIRED PANEL BY FABRICATING A NEW INNER SKIN IAW E.A. 8-5720-118490 & TPS 1001, REV E. DURING POST CU
- [SDR 08FDEA01852](https://openairdocs.org/sdr/08FDEA01852), May 15, 2008: FITTING. CORRODED. THE CENTER CARGO COMPARTMENT, LEFT TRANSITION PANEL SUPPORT HAS CORROSION AT STATION 1601, STRINGER 43L. REMOVED CORROSION IAW SRM 51-21-01; VOL II. FOUND TO TO
- [SDR 08FDEA01847](https://openairdocs.org/sdr/08FDEA01847), May 14, 2008: SKIN. CORRODED. RIGHT WING INBD FLAP; INBD UPPER AFT SKIN IS CORRODED. REMOVED AND REPLACED THE SKIN IAW DC/MD-10 SRM 51-35-01; VOL II. FABRICATED NEW PANEL IAW DAC DWG NR ARC 
- [SDR 08FDEA01841](https://openairdocs.org/sdr/08FDEA01841), May 13, 2008: BRACKET. GOUGED. RIGHT WING INBD FLAP, INBD HINGE POINT IS GOUGED. BLENDED AREA. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01 AND DWG ARC 2518. REMOVED DAMAGED FAIL SAFE STRAP AND
- [SDR 08FDEA01827](https://openairdocs.org/sdr/08FDEA01827), May 12, 2008: FITTING. CORRODED. CENTER CARGO COMPARTMENT LT TRANSITION PANEL SUPPORT FITTING HAS CORROSION; MOUNTED ON THE FRAME AT FS 1661 LBL 43. REMOVED CORROSION IAW 51-21-01; VOL II. FOUN
- [SDR 08FDEA01832](https://openairdocs.org/sdr/08FDEA01832), May 12, 2008: HINGE. CORRODED. RIGHT WING OUTBD FLAP, OUTBD HINGE LOCATION NR 3 OUTBD BORE IS CORRODED. REMOVED CORROSION FROM THE OUTBD BORE OF THEN 3 LUG IAW CMM 57-44-01. MACHINED BUSHING 
- [SDR 08FDEA01831](https://openairdocs.org/sdr/08FDEA01831), May 12, 2008: HINGE. CORRODED. RIGHT WING OUTBD FLAP, OUTBD HINGE LOCATION NR 3 INBD BORE IS CORRODED. REMOVED THE CORROSION FROM THE INBD BORE IAW CMM 57-44-01. MACHINED NEW BUSHINGS FOR THE
- [SDR 08FDEA01830](https://openairdocs.org/sdr/08FDEA01830), May 12, 2008: HINGE. CORRODED. RIGHT WING OUTBD FLAP, INBD HINGE LOCATION NR 3 OUTBD LUG FACE OUTER SURFACE IS CORRODED. LUG THICKNESS VERIFIED TO BE .421 IAW BAC CMM 57-44-01. CORROSION FOUN
- [SDR 08FDEA01829](https://openairdocs.org/sdr/08FDEA01829), May 12, 2008: HINGE. CORRODED. RIGHT WING OUTBD FLAP, INBD HINGE, LOCATION NR 3 INBD LUG FACE OUTER SURFACE IS CORRODED. LUG THICKNESS VERIFIED TO BE .421 IAW BAC CMM 57-44-01. CORROSION FOUN
- [SDR 08FDEA01828](https://openairdocs.org/sdr/08FDEA01828), May 12, 2008: HINGE. CORRODED. RIGHT WING OUTBD FLAP, INBD HINGE LOCATION NR 3 MOUNTING SURFACE IS CORRODED. REMOVED THE CORROSION FROM THE NR 3 LUG FACE IAW CMM 57-44-08. FABRICATED SHIMS IA
- [SDR 08FDEA01795](https://openairdocs.org/sdr/08FDEA01795), May 8, 2008: SKIN. DENTED. RIGHT WING FIXED LEADING EDGE SKIN IS DENTED IN 4 PLACES AT STA XFS 627 TO XFS 653. DEPTH OF THE DENTS ARE0.045 TO 0.120. DENTS ARE OUT OF LIMITS IAW SRM 57-00-

All 138: https://openairdocs.org/aircraft/N367FE/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/N367FE/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

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