# Mcdonnell Douglas MD-10-10F

- Type: Aircraft model (FAA registry)
- Registry code: 3022112
- Manufacturer (registry): MCDONNELL DOUGLAS
- Model: MD-10-10F
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 3 · Turbo-fan
- Seats: 6
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Data sheet: [TCDS A22WE](https://openairdocs.org/tcds/A22WE) (OpenAirDocs)
- Holder: The Boeing Company
- Registered aircraft: 2
- Page: https://openairdocs.org/model/mcdonnell-douglas-md-10-10f

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [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

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

All 73: https://openairdocs.org/model/mcdonnell-douglas-md-10-10f/ads.md

## Information bulletins (advisory) (3)

- [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

## Registered aircraft (2)

- [N367FE](https://openairdocs.org/aircraft/N367FE): [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1971, S/N 46605
- [N369FE](https://openairdocs.org/aircraft/N369FE): [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1972, S/N 46607

## NTSB investigations (14)

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

- [NTSB DCA17MA022](https://openairdocs.org/ntsb/DCA17MA022), Oct 28, 2016: Mcdonnell Douglas MD 10-10F (N370FE), Fort Lauderdale, FL, substantial damage. Probable cause: The failure of the left main landing gear (MLG) due to fatigue cracking that initiated at a corrosion pit. The pit formed in the absence of a required protective cadmium coating the cause of which…
- [NTSB DCA08FA075](https://openairdocs.org/ntsb/DCA08FA075), Jun 14, 2008: Douglas MD-10 (N554FE), Raymond, PA, substantial damage. Probable cause: The flight crew's failure to adequately monitor the airplane's airspeed during the holding pattern, leading to the onset of an aerodynamic stall and subsequent structural damage to the tail from…
- [NTSB DCA06FA058](https://openairdocs.org/ntsb/DCA06FA058), Jul 28, 2006: Boeing MD-10-10F (N391FE), Memphis, TN, substantial damage. Probable cause: the failure of the left main landing gear due to fatigue cracking in the air filler valve hole on the aft side of the landing gear. The fatigue cracking occurred due to the presence of stray nickel…
- [NTSB DCA06FA033](https://openairdocs.org/ntsb/DCA06FA033), Apr 4, 2006: Mcdonnell Douglas DC10 (N386FE), Memphis, TN, substantial damage. Probable cause: The rupture of a fatigue crack in the forward air seal tooth serration of the No. 3 engine low pressure turbine stage 1 disk that initiated due to an improper weld repair performed during original…
- [NTSB CHI06LA038](https://openairdocs.org/ntsb/CHI06LA038), Nov 29, 2005: McDonnell Douglas MD-10 (N359FE), Chicago, IL, substantial damage. Probable cause: The failure of the flight crew to see and avoid the crew stairs and the failure of unknown persons to properly secure the stairs after use. Factors associated with the accident were the dark light…
- [NTSB DCA04MA011](https://openairdocs.org/ntsb/DCA04MA011), Dec 18, 2003: McDonnell Douglas MD-10-10F (N364FE), Memphis, TN, destroyed. Probable cause: 1) the first officer's failure to properly apply crosswind landing techniques to align the airplane with the runway centerline and to properly arrest the airplane's descent rate (flare) before the…
- [NTSB DEN04IA012](https://openairdocs.org/ntsb/DEN04IA012), Oct 12, 2003: McDonnell Douglas DC-10-10 (N375FE), Denver, CO, incident, minor damage. Probable cause: the manufacturer's improper installation of the inboard slat drive mechanism's lower left hand anti-torque strut, which resulted in the axial migration of the rod-end bearing, the binding of the…
- [NTSB ATL02IA155](https://openairdocs.org/ntsb/ATL02IA155), Aug 10, 2002: McDonnell Douglas DC-10-10 (N388FE), Tampa, FL, incident, minor damage. Probable cause: The failure of the left main landing gear retract cylinder support frame due to fatigue.
- [NTSB IAD01IA034](https://openairdocs.org/ntsb/IAD01IA034), Mar 6, 2001: McDonnell Douglas DC-10 (N375FE), Boston, MA, incident, minor damage. Probable cause: The inadequate de-ice and preflight inspection procedure of the #2 engine inlet and bellmouth area by company maintenance personnel that resulted in ice ingestion and foreign object damage of the #2…
- [NTSB CHI99IA100](https://openairdocs.org/ntsb/CHI99IA100), Mar 2, 1999: McDonnell Douglas DC-10 (N40061), Salina, KS, incident, no damage. Probable cause: The ARTCC personnel failed to maintain radio communications with both airplanes and failed to maintain IFR separation standards. Factors relating to the incident were the FAA does not require cargo…
- [NTSB MIA98LA124](https://openairdocs.org/ntsb/MIA98LA124), Apr 4, 1998: Douglas DC-10-10F (N68053), Memphis, TN, substantial damage. Probable cause: The tug operator's (maintenance representative) inadequate visual lookout during pushback.
- [NTSB LAX90FA148](https://openairdocs.org/ntsb/LAX90FA148), Apr 18, 1990: McDonnell Douglas DC-10-10F (N68056), Los Angeles, CA, substantial damage. Probable cause: PILOT FAILED TO ADHERE TO ESTABLISHED LANDING PROCEDURES, MAINTAIN A STABILIZED APPROACH, AND ALLOWED THE AIRSPEED TO GO BELOW THE PREDICTED V.
- [NTSB DEN83FA021](https://openairdocs.org/ntsb/DEN83FA021), Nov 19, 1982: Mcdonald Douglas DC-10 (N68056), Denver, CO, substantial damage
- [NTSB ANC78IA036](https://openairdocs.org/ntsb/ANC78IA036), May 9, 1978: Douglas DC-10 (N68054), Anchorage, AK, incident, minor damage

## FAA accident and incident reports (45)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20161028023139A](https://openairdocs.org/incident/20161028023139A), Oct 28, 2016: Douglas Acft Co Inc DC10 (N370FE), Fort Lauderdale, FL, Destroyed. Aircraft experienced left main landing gear collapse and subsequent fire in the left wing 12 seconds after landing on runway 10L at Fort Lauderdale?Hollywood…
- [Incident 20150716013019I](https://openairdocs.org/incident/20150716013019I), Jul 16, 2015: Mcdonnell Douglas MD-10-10F (N68049), Newark, NJ, No damage. Fedex 1607 reported being illuminated by a broad green laser pulse while climbing out of 1500? Six miles southwest of the Newark airport. Pulse was reported to…
- [Incident 20110201001209I](https://openairdocs.org/incident/20110201001209I), Feb 1, 2011: Mcdonnell D MD-10-10F (N567FE), Newark, NJ, Minor damage. At 0923 local time in ewr, N567FE an MD10 was parked on fedx spot 1 at ewr. N399FE another MD10 was parked on the center line and being deiced by a bucket…
- [Accident 20080614839519A](https://openairdocs.org/incident/20080614839519A), Jun 14, 2008: Doug MD1010F (N554FE), Elmira, NY, Substantial damage. (-23) While holding on J-106 at hoxie intersection the flightcrew allowed the aircraft airspeed to detiorate to the point that they could no longer maintain…
- [Incident 20070530011439I](https://openairdocs.org/incident/20070530011439I), May 30, 2007: Doug MD1010F (N566FE), Fort Worth, TX, Minor damage. (-23) Upon landing at afw, crew deployed thrust reversers. After deployment, thrust reverser #2 would restow. When aircraft arrived at ramp, it was discovered…
- [Incident 20060927027339I](https://openairdocs.org/incident/20060927027339I), Sep 27, 2006: Doug MD1010F (N388FE), Oakland, CA. (-23) Investigation revealed: flt crew executed a missed approach due to an unsafe gear indication, then landed oak without further incident. Three unsafe gear…
- [Incident 20060925027409I](https://openairdocs.org/incident/20060925027409I), Sep 25, 2006: Doug MD1010F (N68057), Oakland, CA. (-23) Investigation revealed: rt main gear down on retraction after t/o. light went red and stayed red until gear handle placed down again. Crew recycled gear…
- [Accident 20060728014379A](https://openairdocs.org/incident/20060728014379A), Jul 28, 2006: Doug MD1010F (N391FE), Memphis, TN, Substantial damage. (-23) On July 28, 2006 at 1125 CDT, federal express corporation flight 680 (FDX630), a MD10-10F, N391FE, crashed on landing at Memphis International Airport,…
- [Accident 20060404004029A](https://openairdocs.org/incident/20060404004029A), Apr 4, 2006: Doug MD1010F (N386FE), Jonesboro, AR, Substantial damage. (-23) On 4 April 2006 at approximately 1550 hours fedex flight #597, N386FE, an MD-10-10, was enroute from memphis to seattle when the crew experienced engine…
- [Incident 20060205002429I](https://openairdocs.org/incident/20060205002429I), Feb 5, 2006: Doug MD1010F (N571FE), Austin, TX. (-23) A ballast cargo can container was loaded on an all cargo aircraft and the container locks were not set. The aircraft was flown from kelp to kaus with…
- [Accident 20051128032179A](https://openairdocs.org/incident/20051128032179A), Nov 28, 2005: Doug MD1010F (N359FE), Chicago, IL, Substantial damage. (-23) On 11-28-05 fedx 1205 taxied out of ord enroute to mem, struck an airstair that was too close to the l taxiway at ord. Crew did not notice the aircraft…
- [Incident 20050727025569I](https://openairdocs.org/incident/20050727025569I), Jul 27, 2005: Doug DC1010 (N397FE), Newark, NJ, Substantial damage. (-23) Crew reported no. one engine fire, after hearing a loud bang. Engine was shut down and one fire bottle discharged that extinguished the fire. The fire…
- [Incident 20050603012339I](https://openairdocs.org/incident/20050603012339I), Jun 3, 2005: Doug DC1010F (N68053), Kansas City, MO. (-23) See attached for flight engineer information. Facts given by the director of operations: aircraft was in cruise flight at FL350 and all indications were…
- [Accident 20031218037819A](https://openairdocs.org/incident/20031218037819A), Dec 18, 2003: Doug MD1010F (N364FE), Memphis, TN, Destroyed. (-23) The right main gear failed on landing.
- [Incident 20031012026399I](https://openairdocs.org/incident/20031012026399I), Oct 12, 2003: Doug DC1010 (N375FE), Denver, CO, Minor damage. (-23) During takeoff acceleration, the crew received a take-off warning horn and initiated a rejected take-off. During deceleration, the tower reported via…
- [Incident 20030524009299I](https://openairdocs.org/incident/20030524009299I), May 24, 2003: Doug DC1010F (N368FE), Oakland, CA, Substantial damage. (-23) Federal express aircraft N368FE, DC-10-10/87 serial number 46606, departed Oakland international at 0602PDT on 05/24/2003 for flt 3103 enroute to fort…
- [Incident 20021226034699I](https://openairdocs.org/incident/20021226034699I), Dec 26, 2002: Doug DC1010 (N375FE), Kansas City, MO. (-23) On December 26, 2002 federal express flight 3606 a DC-10 advised a.t.c. that the number one engine was out, an emergency was declared and the aircraft…
- [Incident 20020810020829I](https://openairdocs.org/incident/20020810020829I), Aug 10, 2002: Doug DC1010 (N388FE), Tampa, FL, Minor damage. (-23) On August 10, 2002, during the approach to landing at Tampa International Airport a federal express aircraft N388FE experienced a left main landing gear…
- [Incident 20020330006579I](https://openairdocs.org/incident/20020330006579I), Mar 30, 2002: Doug DC1010F (N383FE), Indianapolis, IN. (-23) On 03/30/2002 fdx flight 1605 took emergency action due to a fire warning at 300 feet. After landing attempted to fire #2 bottle. No indication that it…
- [Incident 20011222035539I](https://openairdocs.org/incident/20011222035539I), Dec 22, 2001: Doug DC1010 (N390FE), Pittsburgh, PA. (-23) On dec. 22, 2001, federal express flight #3186, a DC-10-10, tail number N390FE, diverted to pit due to #12 cabin smoke indication. The crew followed the…
- [Incident 20011113034209I](https://openairdocs.org/incident/20011113034209I), Nov 13, 2001: Doug DC1010F (N68059), Newark, NJ, Minor damage. (-23) Report from mem aod powerplant engineering senior engineer larry andrews attached. [privacy data omitted]
- [Incident 20010303003559I](https://openairdocs.org/incident/20010303003559I), Mar 3, 2001: Doug DC1010 (N375FE), Boston, MA, Substantial damage. (-23)Weather: snow and ice ref NE incidnet 2001-444, night IFR
- [Incident 20000819029279I](https://openairdocs.org/incident/20000819029279I), Aug 19, 2000: Doug DC1010F (N364FE), Mobile, AL, Minor damage. (-23)All (4) tires on right main landing gear truck blew during take-off and landing. Aircraft damages due to rubber debris are: 1)the #3 engine fan section…
- [Incident 19980909032699I](https://openairdocs.org/incident/19980909032699I), Sep 9, 1998: Doug DC1010 (N397FE), Indianapolis, IN. While on final approach for runway 5R, the outboard vane stop assemble for the right side inboard flap fell off of the aircraft. The stop assemble struck a…
- [Accident 19980404005999A](https://openairdocs.org/incident/19980404005999A), Apr 4, 1998: Doug DC1010F (N68053), Memphis, TN, Substantial damage. Collided with nose dock on pushback from gate. Tug driver cut it around too soon. (.4)the tug operator (maintenance representative) was pushing back an…
- [Incident 19920721033479I](https://openairdocs.org/incident/19920721033479I), Jul 21, 1992: Doug DC1010 (N68057), Los Angeles, CA. Avionics compartment exit door light on after rotation. Returned. Door was fully open and locked in place.
- [Accident 19900418010239A](https://openairdocs.org/incident/19900418010239A), Apr 18, 1990: Doug DC1010F (N68056), Los Angeles, CA, Substantial damage. Excessive pitch up on landing flare causing tail strike.
- [Incident 19860323014249I](https://openairdocs.org/incident/19860323014249I), Mar 23, 1986: Doug DC1010F (N68051), Houston, TX, Minor damage. While taxiing into a gate not normally used by DC10 engine inlet struck at tug.
- [Incident 19850203007079I](https://openairdocs.org/incident/19850203007079I), Feb 3, 1985: Doug DC1010F (N68050), Memphis, TN. Electronics compartment door warning light came on. Door was reclosed, departed. Follow up check at destination.
- [Incident 19820205002059I](https://openairdocs.org/incident/19820205002059I), Feb 5, 1982: Doug DC1010F (N68051), Chicago, IL. Aborted takeoff due to a differential in takeoff power. Replaced a malfunctioning EGT indicator.
- [Incident 19801006082419I](https://openairdocs.org/incident/19801006082419I), Oct 6, 1980: Doug DC1010F (N68056), Houston, TX. Hydraulic quantity dropped to one gallon en route. Replaced isolation valve and one hydraulic pump.
- [Incident 19800924070799I](https://openairdocs.org/incident/19800924070799I), Sep 24, 1980: Doug DC1010F (N68052), Denver, CO, Substantial damage. Takeoff aborted after loud bang. Found engine turbine section failed.
- [Incident 19800512090801I](https://openairdocs.org/incident/19800512090801I), May 12, 1980: Doug DC1010F (N68050), Chicago, IL, Minor damage. Struck aircraft while both were taxiing. N776NC.
- [Incident 19800308024329I](https://openairdocs.org/incident/19800308024329I), Mar 8, 1980: Doug DC1010F (N68051), Chicago, IL. Engine shutdown in flight due to vibration.
- [Incident 19790915049249I](https://openairdocs.org/incident/19790915049249I), Sep 15, 1979: Doug DC1010F (N68051), Chicago, IL. Turn back due to loud noise, rise in EGT and engine shut down. Hole burned through 7th stage case.
- [Incident 19790222200169I](https://openairdocs.org/incident/19790222200169I), Feb 22, 1979: Doug DC10/ (N68052), Houston, TX. Main landing gear wheel & tire departed aircraft on takeoff. Uneventful landing at destination.
- [Incident 19790216006029I](https://openairdocs.org/incident/19790216006029I), Feb 16, 1979: Doug DC1010F (N68050), Houston, TX. Ground observer thought tire blew on takeoff.
- [Incident 19790215007139I](https://openairdocs.org/incident/19790215007139I), Feb 15, 1979: Doug DC1010F (N68049), Junction, TX, Minor damage. Note found in blue room stating explosive chemical onboard. Proceeded to cuba. Normal landing.
- [Incident 19781106023209I](https://openairdocs.org/incident/19781106023209I), Nov 6, 1978: Doug DC10/ (N68050), Houston, TX. Crew heard noises in tail. After landing found cargo door seal hanging out. It was slapping the airplane.
- [Incident 19781105023449I](https://openairdocs.org/incident/19781105023449I), Nov 5, 1978: Doug DC10/ (N68052), Austin, TX. Engine shutdown due to RPM sticking. Replaced jammed throttle cable.
- [Incident 19780826039089I](https://openairdocs.org/incident/19780826039089I), Aug 26, 1978: Doug DC1010F (N68052), San Antonio, TX. Phone call to reservations stated bomb onboard flight. Returned for search.
- [Incident 19780601041459I](https://openairdocs.org/incident/19780601041459I), Jun 1, 1978: Doug DC10/ (N68053), Denver, CO. Complete instrument failure after failure of a generator drive end bearing failure. Landed safely.
- [Incident 19780510032939I](https://openairdocs.org/incident/19780510032939I), May 10, 1978: Doug DC10/ (N68052), Dallas, TX. Engine shutdown, flight diverted. Found compressor dragging, changed the engine.
- [Incident 19780509032769I](https://openairdocs.org/incident/19780509032769I), May 9, 1978: Doug DC10/ (N68054), Anchorage, AK, Minor damage. Aircraft taxiing to gate truck improperly adjusted jetway.
- [Incident 19780128004359I](https://openairdocs.org/incident/19780128004359I), Jan 28, 1978: Doug DC1010 (N68051), Seattle, WA, Minor damage. Loud bang after slat extension. Disagreement lights. Inspection revealed damage from over extension.

## Service difficulty reports (4,917, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR FDEA202105271414](https://openairdocs.org/sdr/FDEA202105271414), May 27, 2021: ENGINE. MALFUNCTIONED. AT FL380 ALL ENGINES WERE OPERATING NORMALLY. AS WE BEGAN OUR DESCENT AND THROTTLES CAME BACK TOWARDS IDLE ECS SURGED FOLLOWED BY A LEVEL 2 AIRSYS 2 PRES LO AND
- [SDR 2021F00070](https://openairdocs.org/sdr/2021F00070), Apr 8, 2021: COLLAR. BROKEN. UNUSUAL VIBRATION ON NLG DURING LANDING & TAXI (OB). DURING INSPECTION THE COMPONENT COLLAR ASSY FIN ACG7008-7 FOUND BROKEN. REPLACED COLLAR ASSY FIN ACG7008-7 
- [SDR FDEA202101030003](https://openairdocs.org/sdr/FDEA202101030003), Jan 3, 2021: INDICATOR. INOPERATIVE. EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATOR LIGHT INOP L1 DOOR. RELEASED FOR SERVICE PER MEL : 25-61-02. L1 EVAC SLIDE REMOTE PRESS INDICATOR - INO
- [SDR FDEA202012173172](https://openairdocs.org/sdr/FDEA202012173172), Dec 17, 2020: SWITCH. FAILED. DURNING CRUISE AFTER TURNING OFF WING ICE THE RED MANF LIGHT ILLUMINATED ON #3 WITH ASSOCIATED "MAN 3 FAIL" LEVEL 1 ALERT. FOUND PRESSURE SWITCH FAULT BALL DROP
- [SDR FDEA202012103114](https://openairdocs.org/sdr/FDEA202012103114), Dec 10, 2020: SUPPORT. CORRODED. AFT CARGO COMPARTMENT BILGE, CORROSION ON VERTICAL FRAME SUPPORT BELOW FLOOR AT FWD BULKHEAD STA 1781 L-52, MARKED NR 2, 2020-12-10. REMOVED AND REPLACED THE ST
- [SDR FDEA202012060010](https://openairdocs.org/sdr/FDEA202012060010), Dec 6, 2020: ATTACH ANGLE. CRACKED. AT CAC BAY LT SIDE, A CRACK FOUND ON 'ATTACHMENT ANGLE' FOR SUGAR SCOOP FITTING (P/N-NYB6042-7) AT FUS STA-1156. REMOVED AND REPLACED SUGAR SCOOP ATTACHMENT ANG
- [SDR FDEA202012030015](https://openairdocs.org/sdr/FDEA202012030015), Dec 3, 2020: STOP FITTING. CRACKED. L-1 DOOR UPPER FWD CORNER STOP APPEARS TO BE CRACKED. REMOVED DAMAGED ABA7191-506 STOP ASSEMBLY AND INSTALLED NEW PART REFERENCE DRAWING ABA7191 AND EA NR 8-521
- [SDR FDEA202011183198](https://openairdocs.org/sdr/FDEA202011183198), Nov 18, 2020: SKIN. CRACKED. LT HORIZ LEADING EDGE CENTER SECTION (INTERAL) MULTIPLE CRACKS AT BEADED DOUBLE, APPROXIMATELY 27" OUTBOARD OF INBOARD EDGE (BETWEEN FRAMES 5-6). CRACKS WERE CO
- [SDR FDEA202011112832](https://openairdocs.org/sdr/FDEA202011112832), Nov 11, 2020: SKIN. CRACKED. FWD CARGO DOOR CUT OUT, AFT LOWER CORNER, SKIN HAS MINOR GOUGES ON EDGE OF REPAIR. REPAIRED LOWER AFT CORNER OF FWD CARGO DOOR FRAME, REF SRM 53-50-00 FIGURE 26
- [SDR FDEA202011032903](https://openairdocs.org/sdr/FDEA202011032903), Nov 3, 2020: SKIN. CORRODED. AFT FUSELAGE, RT SIDE STA 2163 LONG 33 NUTPLATE HOLE CORRODED OUT OF LIMITS. CONFIRMED WITH NDT. COMPLIED WITH FUSELAGE SKIN REPAIR, PER MD-10 SRM 53-20-00 PG 1
- [SDR FDEA202011022761](https://openairdocs.org/sdr/FDEA202011022761), Nov 2, 2020: SKIN. CORRODED. CORROSION DISCOVERED ON LEFT SIDE FUSELAGE SKIN UNDER LONGERON 46L AT STA BS 1957 TO BS 1961.
- [SDR FDEA202011022747](https://openairdocs.org/sdr/FDEA202011022747), Nov 2, 2020: LONGERON. CORRODED. AFT CARGO, APPROXIMATELY STA 1967, SECTION OF LONGERON L46 IS EXFOLIATED OUT OF LIMITS.
- [SDR FDEA202011012876](https://openairdocs.org/sdr/FDEA202011012876), Nov 1, 2020: STIFFENER. CRACKED. REWORK NR 343 FABRICATED PART NOT ACCEPTED: NR 3 ENGINE PYLON INTERNAL STRUCTURE/BOX AFT ANGLE SUPPORT FOR ACCESS DOOR 488BL COMPLETELY BROKEN OFF AND CRACKED V
- [SDR FDEA202011012744](https://openairdocs.org/sdr/FDEA202011012744), Nov 1, 2020: LONGERON. CORRODED. LOWER FUSELAGE EXT SKIN HAS RIVET SHEARED STA 1967 L46L, FOUND LONG L46 EXFOLIATED.
- [SDR FDEA202010292835](https://openairdocs.org/sdr/FDEA202010292835), Oct 29, 2020: ACCESS PANEL. CORRODED. RIGHT HAND LEADING EDGE INBOARD SIDE P/N ACL7051-2-401 HAS CORROSION UNDER STRINGERS AROUND ACCESS PANEL 341, AT MARKED NR 14 (REQ RDR SDR). REPLACED DOUBLER P/
- [SDR FDEA202010283006](https://openairdocs.org/sdr/FDEA202010283006), Oct 28, 2020: SKIN. CRACKED. RT HORIZONTAL STABILIZER, AFT BODY FAIRING, HAS THREE DAMAGED NUTPLATES, AREA MARKED. COMPLIED WITH DOUBLER REPAIR INSTALLATION AT FUSELAGE SKIN STA 2163 BETWEE
- [SDR FDEA202010262657](https://openairdocs.org/sdr/FDEA202010262657), Oct 26, 2020: SUPPORT. CRACKED. RT WING NR 3 FUEL TANK REFUELING/DEFUELING T-LINE SUPPORT BRACKET CRACKED P/N ARL0501-44. FABRICATED NEW SUPPORT BRACKET, REF DAC DWG ARL0501.
- [SDR FDEA202010242768](https://openairdocs.org/sdr/FDEA202010242768), Oct 24, 2020: DOUBLER. CORRODED. LEFT HORIZONTAL LEADING EDGE INBOARD SECTION ALC7051-1-401 HAS EXTENSIVE CORROSION. INSIDE AND OUTSIDE SKIN IS SWOLLEN AROUND FASTENERS, MARKED NR 15 AND NR 16.
- [SDR FDEA202010242631](https://openairdocs.org/sdr/FDEA202010242631), Oct 24, 2020: DRIVE CHAIN. BROKEN. L1 DOOR EMERGENCY OPERATION CHECK FAILED FOUND DRIVE CHAIN BROKEN. REPLACED CHAIN, PER CMM 52-11-09 AND GMM 52-10-01-2. OPERATIONS CHECKED EMERGENCY DOOR, PER W
- [SDR FDEA202010223228](https://openairdocs.org/sdr/FDEA202010223228), Oct 22, 2020: FITTING. CRACKED. LT FUSELAGE STRUCTURE, STA 1156 L39, SUGER SCOOP FITTING (AYB 7000) CRACKED APPROX 1 INCH BEYOND PREVIOUS STOP DRILL, MARKED. REMOVED AND REPLACED SUGAR SCOOP F
- [SDR FDEA202010183191](https://openairdocs.org/sdr/FDEA202010183191), Oct 18, 2020: FRAME. CORRODED. CENTER CARGO BILGE-STR 52 STA 1641-CORROSION AT FRAME, LOWER ANGLE AFT. REPAIRED CENTER CARGO BILGE STR 52 STA 1641 FRAME, REF SRM 53-30-00 FIG 5 (SHEET 1) VOL 
- [SDR FDEA202010182552](https://openairdocs.org/sdr/FDEA202010182552), Oct 18, 2020: VANE. DELAMINATED. LT OUTBOARD FLAP VANE HAS DELAMINATION UNDER NR 5 RUBSTRIP. REPAIRED LT OUTBOARD FLAP VANE DELAMINATION UNDER NR 5 RUBSTRIP AS REQUIRED, REF SRM 57-00-01 AND 51
- [SDR FDEA202010172610](https://openairdocs.org/sdr/FDEA202010172610), Oct 17, 2020: FRAME. CORRODED. AFT CARGO COMPT BILGE, CORROSION ON FRAME, LOWER HAT SECTION, AT STA 1921 L-52 (MARKED #10) STA 1921, FRAME AGA7130-11, LOWER HAT, BETWEEN LONG L51 TO R51 REMOV
- [SDR FDEA202010172608](https://openairdocs.org/sdr/FDEA202010172608), Oct 17, 2020: FRAME. CORRODED. AFT CARGO COMPT BILGE, CORROSION ON FRAME, LOWER HAT SECTION, AT STA 1853 L-52 (MARKED #7) REMOVED CORROSION ON FRAME AGA0016-3, LOWER HAT SECTION, AT STA 1853 
- [SDR FDEA202010172607](https://openairdocs.org/sdr/FDEA202010172607), Oct 17, 2020: FRAME. CORRODED. AFT CARGO COMPT BILGE, CORROSION ON FRAME, LOWER HAT SECTION, AT STA 1841 L-52 (MARKED #11) CORROSION ON FORMER/FRAME (2 PIECE) LWR CHANNEL AT STA 1841, LONG 50
- [SDR FDEA202010160017](https://openairdocs.org/sdr/FDEA202010160017), Oct 16, 2020: CAP. CRACKED. LT WING, FUSELAGE STRUCTURE SEEN THROUGH WING BODY FAIRING 154AB, STA 1156 STRINGER 39, FITTING CRACKED, MARKED. REPAIRED AREA REFERENCE EA 8-5310-T0357883.
- [SDR FDEA202010162691](https://openairdocs.org/sdr/FDEA202010162691), Oct 16, 2020: FITTING. CRACKED. RT FUSELAGE AT STA 1156, FRAME FITTING (SUGAR SCOOP) CRACKED (CRACK CONTINUE PROPOGATE FROM PREVIOUS STOP DRILL INBOARD, VIEW FROM OUTSIDE. INSTALLED NEW EXTERN
- [SDR FDEA202010162689](https://openairdocs.org/sdr/FDEA202010162689), Oct 16, 2020: SKIN. CRACKED. RT FUSELAGE APPROXIMATELY AT STA 1156 SKIN HAS A 3" CRACK, PROPAGATING FROM EXTERNAL DOUBLER FORWARD BETWEEN STRINGER 38 AND 37, INSTALLED NEW EXTERNAL REPAIR D
- [SDR FDEA202010152582](https://openairdocs.org/sdr/FDEA202010152582), Oct 15, 2020: STIFFENER. CRACKED. NR 3 ENGINE PYLON INTERNAL STRUCTURE/BOX AFT ANGLE SUPPORT FOR ACCESS DOOR 488BL COMPLETLY BROKEN OFF AND CRACKED WING THRU ACCESS DOOR 488BR. (DOT 9) REMOVED A
- [SDR FDEA202010142885](https://openairdocs.org/sdr/FDEA202010142885), Oct 14, 2020: SKIN. DENTED. RT FUSELAGE EXTERIOR APPROXIMATELY STA 1853 BETWEEN LONGERON 37R-38R DENT. ENTERED IN ERROR.
- [SDR FDEA202010142789](https://openairdocs.org/sdr/FDEA202010142789), Oct 14, 2020: DOUBLER. CRACKED. CENTER WHEEL WELL FWD BULKHEAD RT OUTBOARD SPOILER PUSH/PULL M.J RODS FEED THROUGH DOUBLER LOWER AFT CORNER CRACKED. P/N AEA0526. R & R THE DOUBLER (P/N-AEA0526
- [SDR FDEA202010142662](https://openairdocs.org/sdr/FDEA202010142662), Oct 14, 2020: STIFFENER. CRACKED. RT WING FIXED LEADING, INNER SURFACE, SKIN STIFFENER IS CRACKED AT STA XOS 697. REPAIRED STIFFENER, PER EA 8-5710-T0357549 "WINGS-BASIC WING STRUCTURE-RT WING L
- [SDR FDEA202010142661](https://openairdocs.org/sdr/FDEA202010142661), Oct 14, 2020: DOUBLER. CRACKED. RT WING FIXED LEADING EDGE, INNER UPPER SURFACE, PILLOW DOUBLER IS CRACKED AT STA XOS 697. REPAIRED CRACKED DOUBLER, PER SRM 57-10-00 FIG 71 VOL 1.
- [SDR FDEA202010142601](https://openairdocs.org/sdr/FDEA202010142601), Oct 14, 2020: SKIN. CRACKED. RT WING FIXED LEADING EDGE, INNER SURFACE, PILLOW DOUBLER IS CRACKED AT STA XOS 669. INSTALLED REPAIR DOUBLER AS REQUIRED, REF SRM 57-10-00 VOL 1 FIG 71 AND SRM
- [SDR FDEA202010132690](https://openairdocs.org/sdr/FDEA202010132690), Oct 13, 2020: SKIN. CRACKED. CENTER CARGO DOOR AFT SKIN CUT-OUT AT APPROXIMATELY STA 1787 BETWEEN LONGERON 39L-41L. REPAIR DOUBLERS DAMAGED AT CENTER CARGO DOOR LOWER AFT CORNER STA 1787 BE
- [SDR FDEA202010132731](https://openairdocs.org/sdr/FDEA202010132731), Oct 13, 2020: SKIN. DAMAGED. FWD CARGO DOOR CUT-OUT SKIN AT APPROXIMATELY STA 959 BETWEEN LONGERONS 40-41-REPAIR DOUBLERS ARE DAMAGED. R & R REPAIR DOUBLERS AND FILLER, REF SRM 53-50-00 VOL
- [SDR FDEA202010132496](https://openairdocs.org/sdr/FDEA202010132496), Oct 13, 2020: SKIN. WORN. REWORK SNRM 820 LT WING: DROOP LEADING EDGE OUTBOARD EDGE HAS WEAR MARKS AND DOUBLER IS WORN THROUGH, MARKED AND DOT 44. DISCREPANCY IS A MAJOR REPAIR, PER GMM-
- [SDR FDEA202010122533](https://openairdocs.org/sdr/FDEA202010122533), Oct 12, 2020: DOUBLER. CRACKED. RT WING, FWD LOWER LEADING EDGE: CRACK ON INTERCOSTAL. OUTBOARD OF NR 12 SLAT TRACK, STA XOS 790. REMOVED AND REPLACED CRACKED ARB1249-28, REF SRM 51-33-01 VOL 
- [SDR FDEA202010112766](https://openairdocs.org/sdr/FDEA202010112766), Oct 11, 2020: HINGE. CORRODED. LT WING, OUTBOARD FLAP, INBOARD HINGE HAS CORROSION ON UPPER INBOARD VALLEY. REMOVED CORROSION FROM WEB AREA SURFACE, PER WINGS-ATTACH FITTINGS-LT WING OUTBOARD
- [SDR FDEA202010112568](https://openairdocs.org/sdr/FDEA202010112568), Oct 11, 2020: BRACKET. CRACKED. LT WING LEADING EDGE NR 2 SLAT COVER BRACKET OUTBOARD FWD SECTION CRACKED, MARKED. FABRICATED A NEW SLAT COVER BRACKET P/N ARB1379-11, PER DOUGLAS DWG ARB1379 R
- [SDR FDEA202010112678](https://openairdocs.org/sdr/FDEA202010112678), Oct 11, 2020: PANEL. DAMAGED. RT WING: DROOP LEADING EDGE OUTBOARD SIDE/EDGE, DOUBLER AND FASTENER ARE WORN/CUT INTO. REPAIRED THE RT DROOP LEADING EDGE, IN REF TO SRM 57-10-00 FIG 97, PAGE 
- [SDR FDEA202010112495](https://openairdocs.org/sdr/FDEA202010112495), Oct 11, 2020: BRACKET. CRACKED. LT NR 4 SLAT TRACK LEADING EDGE COVER PLATE HAS A CRACKED LT BRACKET. REMOVED AND REPLACED CRACKED LT BRACKET ON LT NR 4 SLAT TRACK LEADING EDGE COVER PLATE, RE
- [SDR FDEA202010102569](https://openairdocs.org/sdr/FDEA202010102569), Oct 10, 2020: SKIN. WORN. NR 2 ENGINE RT SIDE, APPROXIAMTELY STA YTN 133, 6 O`CLOCK POSITION, GOUGED METAL ON FWD RT FAN COWL LAND. MARKED DOT NR 46 REPAIRED, PER SRM 54-10-00 FIG 20 VOL
- [SDR FDEA202010102523](https://openairdocs.org/sdr/FDEA202010102523), Oct 10, 2020: DOOR FRAME. GOUGED. NR 2 ENGINE LT SIDE, APPROXIMATELY STA YTN 133, 6 O`CLOCK POSITION, GOUGED METAL ON FWD LT FAN COWL LAND. MARKED DOT NR 45. REMOVED GOUGED DOOR JAM & REPLACED W
- [SDR FDEA202010072560](https://openairdocs.org/sdr/FDEA202010072560), Oct 7, 2020: PANEL. CORRODED. AFT FUS ENGINE 2 AREA RT SIDE PANEL (364CR) HAS LIGHT SURFACE CORROSION AROUND HOLES ON A/C SIDE AND INSIDE PANEL, MARKED. 0005202341: ROLON, JUAN M - 19-OCT-20
- [SDR FDEA202010032429](https://openairdocs.org/sdr/FDEA202010032429), Oct 3, 2020: CARGO TRACK. CORRODED. AFT CARGO, CORROSION ON SEAT TRACK AT FLOORBOARD ATTACH POINTS STA 1801-STA 1841 LBL 24, MARKED NR 8. REMOVED AND REPLACED SECTION OF SEAT TRACK, IN REF TO SRM 
- [SDR FDEA202010032480](https://openairdocs.org/sdr/FDEA202010032480), Oct 3, 2020: FLOOR SUPPORT. CRACKED. AFT CARGO, CORROSION AND CRACKS ON FLOOR SUPPORT BRACKET AT INBOARD AND OUTBOARD ENDS AT FWD BULKHEAD STA 1781 RBL 16, MARKED NR 4. REPAIRED THE AFT CARGO FLOOR
- [SDR FDEA202010032476](https://openairdocs.org/sdr/FDEA202010032476), Oct 3, 2020: FLOOR SUPPORT. CORRODED. AFT CARGO, CORROSION AND CRACKS ON FLOOR SUPPORT BRACKET AT INBOARD AND OUTBOARD ENDS AT FWD BULKHEAD STA 1781 LBL 25, MARKED NR 2. REPAIRED THE FLOOR SUPPORT, 
- [SDR FDEA202010012767](https://openairdocs.org/sdr/FDEA202010012767), Oct 1, 2020: HINGE. CORRODED. LT OUTBOARD FLAP INBOARD HINGE AIRCRAFT SIDE, ACTUATOR ATTACH LUG RUSTED AT BASE ON BOTH SIDE. LT OUTBOARD FLAP INBOARD HINGE A/C SIDE CORROSION ON ACTUATOR ATT
- [SDR FDEA202010012667](https://openairdocs.org/sdr/FDEA202010012667), Oct 1, 2020: PANEL. DELAMINATED. LT TRAILING EDGE TOP PANEL JUST ABOVE INBOARD FLAP OUTBOARD HINGE DELAMINATED REPAIRED PANEL ARC 0263-503, PER SRM 51-71-00 VOL 2 AND DWG ARC 0263.

All 4,917: https://openairdocs.org/model/mcdonnell-douglas-md-10-10f/reports.md

## STCs that may be installed (OpenAirDocs) (59, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [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 59: https://openairdocs.org/model/mcdonnell-douglas-md-10-10f/stcs.md

## PMA parts (OpenAirDocs) (over 1,000, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [S9413-008WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183109801220261009134009.0001): Packing, Preform - Fluorocarbon. Wencor, LLC · PMA PQ1370NM · Replaces S9413-008 · Oct 1, 2026
- [80352-10MIT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174163382120260705233712.0001): Spring-Compression. Mitchell PMA, LLC · PMA PQ00057EB · Replaces 80352-10 · Jun 10, 2026
- [10-D7635-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144137065620260407171342.0001): Sleeve, Assembly. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces ARG7635-1 · Mar 25, 2026
- [10-D7348-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135009003920260407171342.0001): Sleeve-Wheel Bearing, Main Landing Gear. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces ARG7348-501 · Mar 25, 2026
- [BACC45FN10-5S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161097970020260309212952.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN10-5S · Mar 7, 2026
- [4305910270WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162192926720260304181514.0001): Seal Cap. Wencor, LLC · PMA PQ1370NM · Replaces 4305910270 · Oct 30, 2025
- [4305910260WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120636653120260304181513.0001): Washer, Lock. Wencor, LLC · PMA PQ1370NM · Replaces 4305910260 · Oct 30, 2025
- [4133811060WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119960212120260304181515.0001): Holder. Wencor, LLC · PMA PQ1370NM · Replaces 4133811060 · Oct 30, 2025
- [4133801200WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103096752220260304181514.0001): Filter Assy. Wencor, LLC · PMA PQ1370NM · Replaces 4133801200 · Oct 30, 2025
- [4305901030WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102090381020260304181512.0001): Holder Assy - Press. Transducer. Wencor, LLC · PMA PQ1370NM · Replaces 4305901030 · Oct 30, 2025
- [WF329115](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197889510820250602133020.0001): Filter Element, Hydraulic. Donaldson Company Inc · PMA PQ2432CE · Replaces 7554849, AC9279F1, 21-11447, 21-11463 · May 23, 2025
- [21149GK-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183205524620250612143625.0001): Installation Kit, miniQAR / avRDC QAR. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [804-1201, 804-1205, 804-1205-03, 804-1212, 804-1216](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169005250220250612143620.0001): miniQAR MKIII. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [650-0100-05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168808950120250603134030.0001): Cellular Module, avCM LTE. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [400-21149G-3-101, 400-21149G-3-103, 400-21149G-3-105, 400-21149G-3-111, 400-21149G-3-113, 400-21149G-3-115, 400-21149G-3-205, 400-21149G-3-215, 400-21149G-3-715, 400-21149G-3-815](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162632958820250603134037.0001): Assy, LRU Adapter (miniQAR MKIII). Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [400-21149G-3-305, 400-21149G-3-315, 400-21149G-3-405, 400-21149G-3-415, 400-21149G-3-505, 400-21149G-3-515, 400-21149G-3-605, 400-21149G-3-615, 400-21149G-3-915](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126473228120250603134041.0001): Assy, LRU Adapter (avRDC or MAX). Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [804-1250-32](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123521131920250612143633.0001): avRDC MAX QAR. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [804-1250-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109149629420250612143629.0001): avRDC QAR. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [802-0100-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103451199920250603134033.0001): Kit, avCM 4G Adapter. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [650-0100-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101258454220250603134026.0001): Cellular Module (avCM 4G), GSM / GRPS 4G, Quad Band, SMA. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [AAP- 857760-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100610046720250228182135.0001): Seal, Plain, Encased. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell P/N: 857760-1 · Feb 26, 2025
- [10-D7348-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197415106320241219224030.0001): Sleeve-Wheel Bearing, Main Landing Gear. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces ARG7348-501 · Nov 19, 2024
- [10-D7348-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168442919620250219211003.0001): Sleeve-Wheel Bearing, Main Landing Gear. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces ARG7348-501 · Nov 19, 2024
- [10-D7635-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158819243320241219224030.0001): Sleeve, Assembly. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces ARG7635-1 · Nov 19, 2024
- [10-D7635-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137052074720250219211004.0001): Sleeve, Assembly. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces ARG7635-1 · Nov 19, 2024
- [447883LA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196322428720241107175400.0001): Valve, Safety Assy. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 447883 · Nov 5, 2024
- [AAP-3177068-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169303674020241011133359.0001): Bearing. Approved Air Parts Co Inc · PMA PQ4173NE · Replaces Honeywell P/N 3177068-1 · Sep 23, 2024
- [LA495357](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190096363120240904014216.0001): Sleeve. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 495357 · Aug 28, 2024
- [LA490X190A5005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187522492620240904014209.0001): O-Ring. LanAir Research and Development Inc · PMA PQ1031NE · Replaces R00490X190A50D5 · Aug 28, 2024
- [LA555015](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179502746820240904014244.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555015 · Aug 28, 2024
- [LA555153](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176077207620240904014311.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555153 · Aug 28, 2024
- [LA220X160A20B6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167625849320240904014150.0001): O-Ring. LanAir Research and Development Inc · PMA PQ1031NE · Replaces R00220X160A20B6 · Aug 28, 2024
- [LA555033](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163092895920240904014258.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555033 · Aug 28, 2024
- [LA559018](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162659772020240904014319.0001): Dilution Screen. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 559018 · Aug 28, 2024
- [LA3460X240A20B6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141930856220240904014157.0001): O-Ring. LanAir Research and Development Inc · PMA PQ1031NE · Replaces R03460X240A20B6 · Aug 28, 2024
- [LA553008](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136968315520240904014224.0001): Gasket. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 553008 · Aug 28, 2024
- [LA555070](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135895926120240904014304.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555070 · Aug 28, 2024
- [LA555012](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120366974320240904014237.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555012 · Aug 28, 2024
- [LA01000X200A20B6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109294864620241016174854.0001): O-Ring. LanAir Research and Development Inc · PMA PQ1031NE · Replaces R01000X200A20B6 · Aug 28, 2024
- [LA555016](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106568677420240904014250.0001): Diaphragm. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 555016 · Aug 28, 2024
- [LA553044](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102933763320240904014230.0001): Valve. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 553044 · Aug 28, 2024
- [LA412505](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102494946220240904014203.0001): Sleeve. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 412505 · Aug 28, 2024
- [LA449039](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101418419520241016174947.0001): Mask Lock. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 449039 · Aug 28, 2024
- [422B340LA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118809580020240724143345.0001): Overhaul Kit. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 422B340 · Jul 3, 2024
- [387LNCISMI](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135663772120240627191306.0001): LED Lamp. Source Manufacturing Inc · PMA PQ1549CE · Replaces 387, MS25237-387, MS25237-387AS15… · Jun 6, 2024
- [AAP-358474-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127843643720240311212403.0001): Bearing. Approved Air Parts Co Inc · PMA PQ4173NE · Replaces Honeywell P/N 358474-1 · Mar 6, 2024
- [804-1216](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180235390120240924135359.0001): miniQAR MKIII. Avionica LLC. · PMA pq1734ce · Modification part · Dec 8, 2023
- [M422B359](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173360317320231019112534.0001): Main Casing Assembly. Ametek Ameron LLC d/b/a Mass Systems · PMA PQ1432NM · Replaces 422B359 · Oct 4, 2023
- [AAP- 358991-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132389091720231010203037.0001): Bearing. Approved Air Parts Co Inc · PMA PQ4173NE · Replaces Honeywell P/N 358991-1 · Sep 29, 2023
- [297037WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171079028820240919140057.0001): Shaft-Coupling. Wencor, LLC · PMA PQ1370NM · Replaces 297037 · Sep 19, 2023

All of them: https://openairdocs.org/model/mcdonnell-douglas-md-10-10f/pma.md

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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.