# Mcdonnell-Douglas DC-10-30

- Type: Aircraft model (FAA registry)
- Registry code: 3023501
- Manufacturer (registry): MCDONNELL-DOUGLAS
- Model: DC-10-30
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 3 · Turbo-fan
- Seats: 345
- Weight class: 20,000 lb and over
- Cruise speed: 427 mph
- Certification: Type certificated
- Data sheet: [TCDS A22WE](https://openairdocs.org/tcds/A22WE) (OpenAirDocs)
- Holder: The Boeing Company
- Registered aircraft: 5
- Page: https://openairdocs.org/model/mcdonnell-douglas-dc-10-30

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 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 2011-21-08](https://openairdocs.org/ad/2011-21-08): Equipment/Furnishings · ATR - GIE Avions de Transport Régional ATR42-200, ATR42-300, ATR42-320 and 202 more. Effective Nov 23, 2011
- [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 2010-21-13](https://openairdocs.org/ad/2010-21-13): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-30 and 3 more. Effective Nov 18, 2010
- [AD 2010-20-13](https://openairdocs.org/ad/2010-20-13): Fuel · Boeing DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40 and 2 more. Effective Nov 9, 2010
- [AD 2010-20-14](https://openairdocs.org/ad/2010-20-14): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Nov 5, 2010
- [AD 2010-09-12](https://openairdocs.org/ad/2010-09-12): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Jun 8, 2010
- [AD 2009-21-10 R1](https://openairdocs.org/ad/2009-21-10-R1): Oxygen · Airbus A300 B4-605R, A300 B4-620, A300 B4-622 and 138 more. Effective Feb 4, 2010
- [AD 2008-06-21 R1](https://openairdocs.org/ad/2008-06-21-R1): Fuel tank systems · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Dec 10, 2009
- [AD 2009-03-02](https://openairdocs.org/ad/2009-03-02): Auxiliary hydraulic pumps · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 31, 2009
- [AD 2008-17-16](https://openairdocs.org/ad/2008-17-16): Fuel boost pump · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Oct 2, 2008
- [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008
- [AD 2007-25-20](https://openairdocs.org/ad/2007-25-20): Thrust reverser command wiring · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Jan 22, 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 2007-19-02](https://openairdocs.org/ad/2007-19-02): Fuel tank and the fuel transfer pump housing flange · Boeing DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40 and 4 more. Effective Oct 17, 2007
- [AD 2007-13-10](https://openairdocs.org/ad/2007-13-10): Fuel pump wire harness · Boeing DC-10-30 and DC-10-30F (KC-10A, KDC-10). Effective Aug 3, 2007
- [AD 2007-11-15](https://openairdocs.org/ad/2007-11-15): Center main wheel well · Boeing DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40 and 2 more. Effective Jul 5, 2007
- [AD 2007-10-12](https://openairdocs.org/ad/2007-10-12): Reinforced flight deck door · Reinforced cockpit door (Safran Cabin STC ST01335LA or 2 others). Effective Jun 27, 2007
- [AD 2007-04-17](https://openairdocs.org/ad/2007-04-17): Control modules of the fire detection systems · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Mar 23, 2007
- [AD 2006-19-03](https://openairdocs.org/ad/2006-19-03): Fabrication and installation of a wire harness guard in the right wheel well of the main  
 landing gear (MLG) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Oct 17, 2006
- [AD 2006-16-12](https://openairdocs.org/ad/2006-16-12): Fuel tanks 1, 2, and 3 · Boeing DC-10-10, DC-10-10F, DC-10-30 and 3 more. Effective Sep 13, 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 2005-14-10](https://openairdocs.org/ad/2005-14-10): Structural inspections · Boeing DC-10-10, DC-10-10F, DC-10-15 and 4 more. Effective Aug 18, 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 2004-10-12](https://openairdocs.org/ad/2004-10-12): Power Feeder Cable Assembly of the Auxiliary Power Unit (APU) · Boeing DC-10-30. Effective Jun 25, 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 2003-25-13](https://openairdocs.org/ad/2003-25-13): Power feeder cables · Boeing DC-10-10, DC-10-10F, DC-10-15 and 4 more. Effective Jan 27, 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 2003-17-07 R1](https://openairdocs.org/ad/2003-17-07-R1): Auxiliary power unit (APU) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 57 more. Effective Sep 24, 2003

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 2006-16-03](https://openairdocs.org/ad/2006-16-03) (historical): Bonding straps · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 5 more. Effective Sep 7, 2006
- [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 2004-05-20](https://openairdocs.org/ad/2004-05-20) (historical): Electric motor operated auxiliary hydraulic pumps · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 9 more. Effective Apr 15, 2004
- [AD 2003-17-07](https://openairdocs.org/ad/2003-17-07) (historical): Fire Extinguishers for the Engine and Auxiliary Power Unit (APU) · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 60 more. Effective Sep 24, 2003
- [AD 2003-14-04](https://openairdocs.org/ad/2003-14-04) (historical): Flight Deck Door Pressure Relief Latch Assemblies · Boeing 737-200 Series, 737-300 Series, 737-400 Series and 14 more. Effective Jul 25, 2003
- [AD 2003-03-15](https://openairdocs.org/ad/2003-03-15) (historical): Airplane Flight Manual (AFM) - Oxygen Masks · Boeing 707 Series (all), 720 Series (all), 727 Series (all) and 75 more. Effective Mar 7, 2003
- [AD 2000-16-10](https://openairdocs.org/ad/2000-16-10) (historical): Inboard and Outboard Flap Assembly · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 3 more. Effective Sep 25, 2000
- [AD 95-04-07 R2](https://openairdocs.org/ad/95-04-07-R2) (historical): Engine Mount Bolts · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 2 more. Effective Nov 10, 1999
- [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996
- [AD 96-07-01](https://openairdocs.org/ad/96-07-01) (historical): Vertical Stabilizer Attachments · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 4 more. Effective Apr 24, 1996
- [AD 95-04-07 R1](https://openairdocs.org/ad/95-04-07-R1) (historical): Lockwires On Forward Engine Mount Bolts · McDonnell Douglas DC-10-10, DC-10-15, DC-10-30 and 1 more. Effective Mar 17, 1995
- [AD 95-04-07](https://openairdocs.org/ad/95-04-07) (historical): Lockwires on Engine Mount Bolts · McDonnell Douglas DC-10-10, DC-10-15, DC-10-30 and 1 more. Effective Mar 17, 1995
- [AD 91-21-05](https://openairdocs.org/ad/91-21-05) (historical): Wing Rear Spar · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15 and 4 more. Effective Oct 23, 1991
- [AD 88-16-02 R1](https://openairdocs.org/ad/88-16-02-R1) (historical): Landing gear brakes · McDonnell Douglas DC-10-30, DC-10-30F (KC-10A, KDC-10) and DC-10-40. Effective Oct 14, 1988
- [AD 75-04-11](https://openairdocs.org/ad/75-04-11) (historical): Ingestion of Ice and Snow · McDonnell Douglas DC-10-10, DC-10-10F, DC-10-30 and 1 more. Effective Feb 21, 1975

All 262: https://openairdocs.org/model/mcdonnell-douglas-dc-10-30/ads.md

## Information bulletins (advisory) (3)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [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

## Registered aircraft (5)

- [N17085](https://openairdocs.org/aircraft/N17085): [Bc Aircraft Leasing LLC](https://openairdocs.org/faa-owner/BC%20AIRCRAFT%20LEASING%20LLC), [Albuquerque, NM](https://openairdocs.org/faa-place/NM/Albuquerque), built 1975, S/N 47957
- [N522AX](https://openairdocs.org/aircraft/N522AX): [Bc Aircraft Leasing LLC](https://openairdocs.org/faa-owner/BC%20AIRCRAFT%20LEASING%20LLC), [Albuquerque, NM](https://openairdocs.org/faa-place/NM/Albuquerque), built 1988, S/N 48315
- [N603AX](https://openairdocs.org/aircraft/N603AX): [Bc Aircraft Leasing LLC](https://openairdocs.org/faa-owner/BC%20AIRCRAFT%20LEASING%20LLC), [Albuquerque, NM](https://openairdocs.org/faa-place/NM/Albuquerque), S/N 48267
- [N612AX](https://openairdocs.org/aircraft/N612AX): [Bc Aircraft Leasing LLC](https://openairdocs.org/faa-owner/BC%20AIRCRAFT%20LEASING%20LLC), [Albuquerque, NM](https://openairdocs.org/faa-place/NM/Albuquerque), S/N 48290
- [N621AX](https://openairdocs.org/aircraft/N621AX): [Bc Aircraft Leasing LLC](https://openairdocs.org/faa-owner/BC%20AIRCRAFT%20LEASING%20LLC), [Albuquerque, NM](https://openairdocs.org/faa-place/NM/Albuquerque), S/N 48319

## NTSB investigations (19)

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 DCA09FA048](https://openairdocs.org/ntsb/DCA09FA048), May 6, 2009: Boeing DC-10 (N139WA), Baltimore, MD, substantial damage. Probable cause: the captain’s inappropriate control inputs following a firm landing, resulting in two hard nose-gear impacts before executing a go-around. Contributing to the inappropriate control inputs was the…
- [NTSB ENG09IA004](https://openairdocs.org/ntsb/ENG09IA004), Mar 26, 2009: Mcdonnell-Douglas DC-10-30 (N526MD), Bogota, Colombia, incident, minor damage. Probable cause: Failure of the low pressure turbine stage 3 disk due to a design that is vulnerable to high pressure turbine unbalance-induced synchronous vibration that cannot be detected in flight, and the…
- [NTSB DCA08FA062](https://openairdocs.org/ntsb/DCA08FA062), May 19, 2008: Mcdonnell Douglas DC10 (N720AX), Pacific Ocean, no damage. Probable cause: An inadvertent in-flight encounter with unforecasted clear air turbulence
- [NTSB MIA07IA088](https://openairdocs.org/ntsb/MIA07IA088), May 2, 2007: Mcdonnell Douglas DC-10-30 (N270AX), Atlanta, GA, incident, no damage. Probable cause: The improper overhaul of the horizontal stabilizer chain drive unit drive assembly.
- [NTSB DCA04WA043](https://openairdocs.org/ntsb/DCA04WA043), Apr 28, 2004: Boeing DC-10-30 (N189AX), Bogota, Colombia, substantial damage
- [NTSB NYC04TA103](https://openairdocs.org/ntsb/NYC04TA103), Apr 11, 2004: McDonnell Douglas DC-10-30 (N14075), Atlantic Ocean (Atlantic Ocean), substantial damage. Probable cause: The failure of the number two upper forward right engine cowling attachment, which resulted in substantial damage to the right inboard elevator. A factor was the inadequate procedures in the airliner…
- [NTSB NYC00WA260](https://openairdocs.org/ntsb/NYC00WA260), Sep 7, 2000: McDonnell Douglas DC-10-30 (N15069), Amsterdam, Netherlands, incident, minor damage
- [NTSB NYC00IA250](https://openairdocs.org/ntsb/NYC00IA250), Sep 5, 2000: McDonnell Douglas DC-10-30 (N14090), Newark, NJ, incident, minor damage. Probable cause: The sequential failure of the 2nd-stage low pressure turbine nozzle locks, which allowed the 2nds stage turbine nozzle segments to rotate within the low pressure turbine case, machining a hole…
- [NTSB DCA00WA046](https://openairdocs.org/ntsb/DCA00WA046), Apr 30, 2000: Douglas DC-10-30 (N800WR), Entebbe, Uganda, substantial damage, 12 fatal
- [NTSB NYC00FA122](https://openairdocs.org/ntsb/NYC00FA122), Apr 25, 2000: McDonnell Douglas DC-10-30 (N39081), Newark, NJ, substantial damage. Probable cause: Stress rupture of the 2nd-stage low pressure turbine anti-rotation nozzle locks, resulting from inadequate nozzle lock design.
- [NTSB DCA00WA014](https://openairdocs.org/ntsb/DCA00WA014), Dec 18, 1999: McDonnell Douglas DC-10-30F (N800WR), Amsterdam, Netherlands, substantial damage
- [NTSB DCA99WA004](https://openairdocs.org/ntsb/DCA99WA004), Oct 13, 1998: McDonnell Douglas DC-10-30 (N230NW), Amsterdam, Netherlands, incident, minor damage
- [NTSB DCA98WA088](https://openairdocs.org/ntsb/DCA98WA088), Sep 20, 1998: McDonnell Douglas DC-10-30 (N14063), Shannon, Ireland, incident, minor damage
- [NTSB DCA93MA040](https://openairdocs.org/ntsb/DCA93MA040), Apr 14, 1993: Douglas DC-10-30 (N139AA), Dallas/Ft Worth, TX, substantial damage. Probable cause: THE NATIONAL TRANSPORTATION SAFETY BOARD DETERMINES THAT THE PROBABLE CAUSE OF THE ACCIDENT WAS THE FAILURE OF THE CAPTAIN TO USE PROPER DIRECTIONAL CONTROL TECHNIQUES TO MAINTAIN THE AIRPLANE ON THE…
- [NTSB CHI92IA061](https://openairdocs.org/ntsb/CHI92IA061), Dec 23, 1991: Mcdonnell Douglas DC-10-30 (N142AA), Chicago, IL, incident, no damage. Probable cause: THE LOCAL CONTROLLER'S NOT UNDERSTANDING READ BACK OF RADIO COMMUNICATIONS. FACTORS INCLUDE THE PILOT-IN-COMMAND OF FLIGHT 73 NOT UNDERSTANDING VERBAL INSTRUCTIONS; LOCAL CONTROLLER NOT VISUALLY…
- [NTSB FTW88NA106](https://openairdocs.org/ntsb/FTW88NA106), May 21, 1988: Mcdonnell Douglas DC-10-30 (N136AA), Dfw Airport, TX, substantial damage
- [NTSB FTW88LA050](https://openairdocs.org/ntsb/FTW88LA050), Jan 10, 1988: Mcdonnell Douglas DC-10 (N142AA), Dfw Airport, TX, no damage. Probable cause: UNEXPECTED OPENING OF THE IL DOOR, WHICH CAUGHT THE PASSENGER BETWEEN IT AND THE BULKHEAD AS THE DOOR MOVED INWARD AND UPWARD. A SECONDARY CAUSE WAS THE FAILURE OF THE FLIGHT ATTENDANTS TO FOLLOW…
- [NTSB FTW83IA072](https://openairdocs.org/ntsb/FTW83IA072), Dec 30, 1982: Mcdonnell-Douglas DC-10-30 (N137AA), Thermal, CA, incident, no damage
- [NTSB UNK78X0123](https://openairdocs.org/ntsb/UNK78X0123), May 27, 1978: Douglas DC-10 (N54629), Pacific Ocean (Pacific Ocean), no 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.

- [Incident 20160709016709I](https://openairdocs.org/incident/20160709016709I), Jul 9, 2016: Mcdonnell-Douglas DC-10-30 (N522AX), Pueblo, CO, Minor damage. On July 9, 2016 at approximately 2045 mountain daylight time, a Mcdonnell Douglas DC-10 aircraft, N522AX received minor damage when the aircraft taxied into a…
- [Incident 20110808017959I](https://openairdocs.org/incident/20110808017959I), Aug 8, 2011: Mcdonnell-Douglas DC-10-30 (N603AX), Bangor, ME, Substantial damage. Failed turbine blade on nr 1 engine during level off.
- [Accident 20090506006299A](https://openairdocs.org/incident/20090506006299A), May 6, 2009: Doug DC1030 (N139WA), Baltimore, MD, Substantial damage. (-23) On may 6, 2009, at approximately 1255 eastern daylight time, world 8535, N139WA, a mcdonnell-douglas 10-10-30 operated by world airways impacted runway…
- [Incident 20070502831409I](https://openairdocs.org/incident/20070502831409I), May 2, 2007: Doug DC1030 (N270AX), Atlanta, GA, No damage. (-23) Atl FSDO on scene initial start of the incident, on 5-16-07 FAA icc turned over to the dfw FSDO. Preliminary classification as an incident based on NTSB…
- [Incident 20051020030999I](https://openairdocs.org/incident/20051020030999I), Oct 20, 2005: Doug DC1030 (N326FE), Minneapolis, MN, Minor damage. (-23) During approach, a 5-foot section of the left inboard flap vane separated from the aircraft, it was discovered missing during the post flight inspection.
- [Incident 20040608011459I](https://openairdocs.org/incident/20040608011459I), Jun 8, 2004: Doug DC1030 (N221NW), Billings, MT. (-23) The captain stated that the smoke indicator on the flight engineer's panel went off, indicating smoke in the forward cargo bay. The crew donned their…
- [Accident 20040410006949A](https://openairdocs.org/incident/20040410006949A), Apr 10, 2004: Doug DC1030 (N14075), Substantial damage. (-23) On April 10, 2004 at 2258 EDT, world airways aircraft N14075, DC-10-30, s/n 46922, was on flight 725 from naples, italy to naval air station norfolk.…
- [Incident 20030105000449I](https://openairdocs.org/incident/20030105000449I), Jan 5, 2003: Doug DC1030 (N526MD), Dothan, AL, Minor damage. (-23) While taxiing for take-off aircraft ran over a runway light. Number 1 and 5 main tires blew out on take-off. The Dothan control tower informed the crew…
- [Incident 20020829030779I](https://openairdocs.org/incident/20020829030779I), Aug 29, 2002: Doug DC1030 (N14075), Charleston, SC, Minor damage. (-23) On August 29, 2002, at approximately 10:23 am, N14075 was on the ground while maintenance personnel were performing routine servicing of the aircraft.…
- [Incident 20020330008139I](https://openairdocs.org/incident/20020330008139I), Mar 30, 2002: Doug DC1030 (N630AX), Oranjestad, AA, Minor damage. (-23) The omni air international (cnma) captain reported upon landing at Oranjestad, aruba (aua) on 03/30/02 that the control tower advised the crew that a…
- [Incident 20010322009639I](https://openairdocs.org/incident/20010322009639I), Mar 22, 2001: Doug DC1030 (N14063), Houston, TX, Minor damage. (-23)Taxiing to runway 15L on WA while making the left turn from WA to wc, the left main gear departed the hard surface onto the grassy area adjacent to the…
- [Incident 20000905023919I](https://openairdocs.org/incident/20000905023919I), Sep 5, 2000: Doug DC1030 (N14090), Newark, NJ, Minor damage. (-23)Aircraft aborted take-off on rwy 4L due to loss of power on no. 2 engine. The engine sustained an uncontained failure of the 2nd stage lpt nozzle assembly…
- [Incident 20000625032189I](https://openairdocs.org/incident/20000625032189I), Jun 25, 2000: Doug DC1030 (N211NW), Newark, NJ, Minor damage. (-23)Northwest airlines DC-10 Boeing pushed back for repositioning off of gate B-52 struck a Continental airlines DC-10 parked at gate B-51. Investigation…
- [Accident 20000425038759A](https://openairdocs.org/incident/20000425038759A), Apr 25, 2000: Doug DC1030 (N39081), Newark, NJ, No damage. (19) On April 25, 2000, at 1942 eastern daylight time, a mcdonnell-douglas DC10-30, N39081, operating as Continental airlines flight 60, was substantially…
- [Incident 20000124000959I](https://openairdocs.org/incident/20000124000959I), Jan 24, 2000: Doug DC1030 (N211NW), Newark, NJ, 1 fatal. (-23) Upon landing mechanic [privacy data omitted] was performing a security check of the aircraft when he noticed a small bag in the forward part of the right…
- [Incident 19981013033149I](https://openairdocs.org/incident/19981013033149I), Oct 13, 1998: Doug DC1030 (N230NW), Detroit, MI, Minor damage. After klm cfrs performed maintenance on the engine #2 anti-ice valve. The maintenance personnel did not latch the l/t fan cowl fairing. The cowl fairing…
- [Incident 19971201040539I](https://openairdocs.org/incident/19971201040539I), Dec 1, 1997: Doug DC1030 (N14062), Newark, NJ, Minor damage. Left main gear retract cylinder boss fa iled allowing cylinder to sever hydraulic lines. Landed without incident
- [Incident 19971008036659I](https://openairdocs.org/incident/19971008036659I), Oct 8, 1997: Doug DC1030 (N232NW), Newark, NJ. After holding. Low fuel NR2 engine flamed out. Fe mismanaged fuel.
- [Incident 19970625023839I](https://openairdocs.org/incident/19970625023839I), Jun 25, 1997: Doug DC1030 (N13067), Houston, TX, Minor damage. Landing turned off high speed taxiway. ATC advised make next turn. Ran off taxiway. Gear inspected for side load.
- [Incident 19961003037909I](https://openairdocs.org/incident/19961003037909I), Oct 3, 1996: Doug DC1030 (N223NW), UK. Narrative: #3 engine failed after take-off. Dumped fuel and aircraft returned without incident. Root cause of engine failure still under investigation by klm.
- [Incident 19960222024389I](https://openairdocs.org/incident/19960222024389I), Feb 22, 1996: Doug DC1030 (N87070), Houston, TX, Minor damage. Narrative: on 02/22/96 @ iah a/p aircraft N-87070, DC-10-30, rejected take-off at approximately 100 KTS due to #3 engine failure. The aircraft stopped on…
- [Incident 19940326025629I](https://openairdocs.org/incident/19940326025629I), Mar 26, 1994: Doug DC1030 (N19072), Denver, CO. ILS system failure on approach to Denver, diverted to Colorado springs. Replaced ILS control panel.
- [Incident 19930916043439I](https://openairdocs.org/incident/19930916043439I), Sep 16, 1993: Doug DC1030 (N144AA), Dallas-Ft Worth, TX, Minor damage. Engine reverser light on.NR1 engine shut down. Dumped fuel, returned. Engine fan blades replaced.
- [Incident 19930715030359I](https://openairdocs.org/incident/19930715030359I), Jul 15, 1993: Doug DC1030 (N142AA), Dallas-Ft Worth, TX, Minor damage. Pilot struck two obstruction lights above a blast fence as he taxied to depart. Departed. Not aware of the damage.
- [Accident 19930414009339A](https://openairdocs.org/incident/19930414009339A), Apr 14, 1993: Doug DC1030 (N139AA), Dallas-Ft Worth, TX, Substantial damage. Veered off runway into mud on landing. Pilot failed use proper crosswind control. Allowed aircraft to weathervane.
- [Incident 19920804041819I](https://openairdocs.org/incident/19920804041819I), Aug 4, 1992: Doug DC1030 (N14063), Honolulu, HI. NR1 engine experienced compressor stall after departure. Dumped fuel. Returned. Found progressive compressor damage
- [Incident 19920730030639I](https://openairdocs.org/incident/19920730030639I), Jul 30, 1992: Doug DC1030 (N12061), San Francisco, CA. Aircraft developed leak in NR3 hydraulic system. All pressure lost. Diverted. Found o ring oil leak.
- [Incident 19920415012729I](https://openairdocs.org/incident/19920415012729I), Apr 15, 1992: Doug DC1030 (N221NW), San Francisco, CA. Fuel stopped transferring from lower tank. Dumped fuel and made unscheduled landing.
- [Incident 19920306008939I](https://openairdocs.org/incident/19920306008939I), Mar 6, 1992: Doug DC1030 (N13066), Newark, NJ, Minor damage. Had a left outboard flap vane failure on final. Landed safely. 5 ft section of left flap vane had departed airplane
- [Incident 19910728035209I](https://openairdocs.org/incident/19910728035209I), Jul 28, 1991: Doug DC1030 (N140AA), San Francisco, CA. NR2 engine fire warning en route. Diverted and landed safely. No fire. Loops separated by failed duct.
- [Incident 19901118060699I](https://openairdocs.org/incident/19901118060699I), Nov 18, 1990: Doug DC1030 (N140AA), Los Angeles, CA. Smoke in cabin. Turned off lights in area. Diverted for landing. Ballast had overheated.
- [Incident 19901109058449I](https://openairdocs.org/incident/19901109058449I), Nov 9, 1990: Doug DC1030 (N144AA), Honolulu, HI. Pilot shut down NR2 engine on descent due to a stuck throttle. Alcohol was applied to throttle cable.
- [Incident 19901102054299I](https://openairdocs.org/incident/19901102054299I), Nov 2, 1990: Doug DC1030 (N143AA), New York, NY, Minor damage. NR1 main tire recap separated on departure. Diverted to jfk international airport. Landed safely.
- [Incident 19901009059009I](https://openairdocs.org/incident/19901009059009I), Oct 9, 1990: Doug DC1030 (N142AA), Detroit, MI, Minor damage. Aircraft became mired in soft earth at a sharp intersection turn while taxiing for departure.
- [Incident 19900717035659I](https://openairdocs.org/incident/19900717035659I), Jul 17, 1990: Doug DC1030 (N13066), Honolulu, HI, 1 fatal. Passenger under control of a doctor lapsed into a terminal condition and expired while en route to Honolulu.
- [Incident 19890729054729I](https://openairdocs.org/incident/19890729054729I), Jul 29, 1989: Doug DC1030 (N1853U), Honolulu, HI. Low fuel. Aircraft was diverted to Honolulu. Pilot requested expedited handling to gate.
- [Incident 19881231067289I](https://openairdocs.org/incident/19881231067289I), Dec 31, 1988: Doug DC1030 (N14062), Honolulu, HI. Crew window became unseated on takeoff roll. Aborted and stopped on runway. Found window seal loose. Replaced seal.
- [Incident 19881230069129I](https://openairdocs.org/incident/19881230069129I), Dec 30, 1988: Doug DC1030 (N164AA), Buffalo, NY. Coffee spilled on passengers shoulder and back. Paramedics met flight and treated passenger for burns.
- [Accident 19880521029359A](https://openairdocs.org/incident/19880521029359A), May 21, 1988: Doug DC1030 (N136AA), Dallas-Ft Worth, TX, Substantial damage. Slat flaps disagree light and warning horn on takeoff at V1. Aborted. Unable to stop due brake fade. Overran runway
- [Incident 19880224014879I](https://openairdocs.org/incident/19880224014879I), Feb 24, 1988: Doug DC1030 (N144AA), Dallas-Ft Worth, TX, Minor damage. Engine shutdown. Fuel dumped. Returned to airport. Found damage to compression blades.
- [Incident 19880110013839I](https://openairdocs.org/incident/19880110013839I), Jan 10, 1988: Doug DC1030 (N142AA), Dallas-Ft Worth, TX. Passenger was getting luggage, adjacent door was opened inward trapping him against bulkhead hurting arm and head.
- [Incident 19871112077979I](https://openairdocs.org/incident/19871112077979I), Nov 12, 1987: Doug DC1030 (N14063), Honolulu, HI, Minor damage. Number 2 engine left core cowl separated on takeoff due to improper installation. Created runway hazard.
- [Incident 19870825058329I](https://openairdocs.org/incident/19870825058329I), Aug 25, 1987: Doug DC1030 (N136AA), Frankfurt, GE. Fire warning on no 2 engine. Used fire bottles dumped fuel and returned. Found loose bleed air line.
- [Incident 19870131006549I](https://openairdocs.org/incident/19870131006549I), Jan 31, 1987: Doug DC1030 (N19072), Honolulu, HI. First officer became ill en route. Flight engineer changed positions with ill crewmember. Suspect flu.
- [Incident 19860507038749I](https://openairdocs.org/incident/19860507038749I), May 7, 1986: Doug DC1030 (N1855U), Chicago, IL. Returned due to slat disagreement light and stick shaker activating. Replaced air data computer.

## Service difficulty reports (2,776, newest 50)

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

- [SDR ZTRR20200910002](https://openairdocs.org/sdr/ZTRR20200910002), Aug 30, 2020: HINGE. DEPARTED. 2020-08-30 UPON LANDING DURING MX WALK-AROUND NR 2 ENGINE RIGHT CORE COWL WAS NOTICED TO HAVE FAILED DURING FLIGHT, PI-REP ENG 2 CORE COWL DAMAGED AND PIECES MI
- [SDR ZTRR20200708001](https://openairdocs.org/sdr/ZTRR20200708001), Jul 3, 2020: BOLT. MISSING. "AT ROTATE SPEED NR 2 ENG INDICATED FIRE. ALL ENG INDICATORS DISPLAYED NORMAL PARAMETERS FOR CONDITIONS. PERFORMED ENG SHUTDOWN IAW QRH. UPON PLACING FUEL LEVER
- [SDR FDEA201311072713](https://openairdocs.org/sdr/FDEA201311072713), Nov 7, 2013: INDICATOR. FAILED. DOOR EVACUATION SLIDE REMOTE PRESS-TO-TEST SWITCH DOESN'T LIGHT WHEN PRESSED. REPLACED LAMP AND CHANGED BATTERIES IAW AMM 25-61-03-2, SWITCH STILL DOES NOT LIGH
- [SDR CA130704005](https://openairdocs.org/sdr/CA130704005), Jul 3, 2013: WINDSHIELD. CRACKED. (CAN) IN FLIGHT, THE L1 WINDOW BEGAN ARCING AND THE OUTER PANE, CRAZED, CRACKED INTO MULTIPLE PIECES. THE CREW TURNED OFF THE ANTI-ICE AND THE ACFT CONTINUED TO
- [SDR CA120523001](https://openairdocs.org/sdr/CA120523001), May 19, 2012: CABLE. BROKEN. (CAN) IN CRUISE CREW NOTICED THAT THE LT SIDE OF THE HORIZONTAL STABILIZER MECHANICAL CONTROL LEVERS, LT SIDE OF THE SUITCASE HANDLES. RAPIDLY MOVED TO THE NOSE
- [SDR CA120504010](https://openairdocs.org/sdr/CA120504010), Apr 30, 2012: VALVE. MALFUNCTIONED. (CAN) IN CRUISE, ENGINE NR 2 REVERSER PRESSURE LIGHT ILLUMINATED IAW AOM PROCEDURE, CREW PERFORMED A PRECAUTIONARY SHUTDOWN AND RETURNED TO DEPARTING STATION. M
- [SDR CA120504008](https://openairdocs.org/sdr/CA120504008), Apr 27, 2012: CONNECTOR. SHEARED. (CAN) IN CRUISE, CREW EXPERIENCED MULTIPLE POWER INTERRUPTIONS CAUSING, BUSS OFF. LIGHTS TO ILLUMINATE. CREW LANDED AT NEAREST SUITABLE AIRPORT WHERE MAINTENANC
- [SDR CA120211001](https://openairdocs.org/sdr/CA120211001), Feb 7, 2012: BLOCKER DOOR. DAMAGED. (CAN) AFTER LANDING, CREW OBSERVED THE NR 3 REVERSER, UNLOCK AND PRESSURE, LIGHTS REMAINED ILLUMINATED. MAINTENANCE DISCOVERED THAT THE BLOCKER DOORS AND THE BR
- [SDR CNMA20110034](https://openairdocs.org/sdr/CNMA20110034), Aug 8, 2011: ENGINE. FAILED. 2000 FT FROM LEVEL OFF NR1 ENGINE SHUTDOWN, EGT RED FLAG WITH NO N1 OR N2. PREFORMED QRH PROCEEDURE. METAL IN TAILPIPE & EXCESSIVE DAMAGE TO LPT. R & R NR1 ENG 
- [SDR CNMA20110032](https://openairdocs.org/sdr/CNMA20110032), Jun 11, 2011: DRIVE ASSY. SHEARED. A/P OUT OF TRIM LT CAME ON INTERMITTENTLY DURING FLT. STAYED ON FOR 30 SEC TO 3 MTS. NO PITCH TRIM CHANGE DURING ILLUMINATION. TURNED OFF AP & ACFT IN TRIM DURI
- [SDR CNMA20110029](https://openairdocs.org/sdr/CNMA20110029), May 26, 2011: OVEN. BURNED. AFT GALLEY OVEN FIRE. INSIDE OF 2-21. FOLLOWED QRH PROCEDURES. CONTINUED (ALL OVENS NEED TO BE CLEANED) R & R OVEN IAW 25-30 CLEANED ALL OTHER OVENS. NO EXCESS 
- [SDR CNMA20110026](https://openairdocs.org/sdr/CNMA20110026), May 6, 2011: CONNECTOR. DAMAGED. NR 2 ENGINE FIRE INDICATION ILLUMINATED (LOOP A ONLY W/ ALL ASSOC WARNINGS - LOOP B WAS DEFERRED) PERFORMED ENGINE FIRE CL (QRH 4-1-1-1) NR 1 FIRE BOTTLE FIRED 
- [SDR CNMA20110024](https://openairdocs.org/sdr/CNMA20110024), May 2, 2011: LIGHT. NO TEST. L1 DOOR SLIDE EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING OPS TEST. SLIDE DEPLOYED NORMALLY. REPLACED SLIDE ASSY.
- [SDR CNMA20110010](https://openairdocs.org/sdr/CNMA20110010), Apr 11, 2011: COALESCER BAG. ODOR. OILY BURNING ODOR THROUGHOUT CABIN AND FLIGHT DECK. AFTER REPLACEMENT OF NR 1 PACK & COALESER BAGS, RAN ENGINES AT MPA ONE AT A TIME & ISOLATED PNEUMATICS, NO O
- [SDR CNMA20110007](https://openairdocs.org/sdr/CNMA20110007), Mar 24, 2011: PAN. CORRODED. FWD P17, STA 870, LWR BILGE LAV DUMP PAN HAS SEVERAL AREAS OF CORROSION ON TOP AND RT SIDE OF PAN. REMOVED CORROSION FROM RT SIDE OF PAN FOUND TO BE WITHIN LIMI
- [SDR CNMA20110011](https://openairdocs.org/sdr/CNMA20110011), Mar 19, 2011: INTERCOSTAL. CORRODED. SUPPORT ANGLE AND INTERCOSTAL AT APPROX LONGERON 44L HAS AREAS OF CORROSION AND FASTENER HEADS POPPED FROM STA 535 TO 595. REPAIRED INTERCOSTAL IAW SRM VOL I 53
- [SDR CNMA20110006](https://openairdocs.org/sdr/CNMA20110006), Mar 19, 2011: ATTACH ANGLE. CORRODED. CORROSSION ON FUSELAGE FRAME ATTACH ANGLE AT LONGERON 51L STA. 1119. REMOVED CORROSSION FOUND OUT OF LIMITS FABRICATED REPAIR DOUBLER FROM .080 7075-0 HEAT TREA
- [SDR CNMA20110005](https://openairdocs.org/sdr/CNMA20110005), Mar 19, 2011: DOOR FRAME. CORRODED. SURFACE CORROSSION ON AFT PIT DOOR FWD SIDE OF FRAME ON LOWER AFT SIDE AT LONGERON 42L TO 46L AT STA 1957. R & R FRAME AT STA 1957 IAW SRM VOL II 51-35-01, PG 1
- [SDR CNMA20110004](https://openairdocs.org/sdr/CNMA20110004), Mar 19, 2011: BULKHEAD. CRACKED. NR 3 PYLON HAS CRACK ON AFT BULKHEAD UPPER INBD FLANGE COMING OUT OF RADIUS AT PYLON STA 418. REMOVED NR 3 PYLON REPLACED AFT PYLON BULKHEAD IAW DWG NR AWB70125
- [SDR CA110209015](https://openairdocs.org/sdr/CA110209015), Feb 7, 2011: SENSOR. MISRIGGED. AFTER DEPARTURE THE LANDING GEAR WOULD NOT RETRACT NORMALLY, HAD TO USE THE OVERRIDE. LANDING GEAR ANTI-RETRACTION PUSH/PULL CABLES ADJUSTED IAW AMM 32-31-01 AN
- [SDR CNMA20110002](https://openairdocs.org/sdr/CNMA20110002), Feb 7, 2011: ENGINE. FAILED. NR 2 ENG SHUTDOWN DURING CLIMB ACCOMPLISHED QRH PROCEDURE. REPLACED NR 2 ENGINE PER CARD 10UN-201 OPS CHECK NORMAL LEAK CHECKED OK POWER ASSURANCE OK.
- [SDR CNMA20110001](https://openairdocs.org/sdr/CNMA20110001), Feb 6, 2011: MEC. DEFECTIVE. AFTER 1+ 25 INTO FLT. NOTICED NR 3 ENG N 2 FLUX BETWEEN 95-87 PERCENT N 2 ALSO NOTICE CONSIDERABLE VIBRATION NR 3 FUEL LEVER. AFTER NR 3 THROTTLE TO IDLE NOTICE
- [SDR CNMA20100036](https://openairdocs.org/sdr/CNMA20100036), Dec 29, 2010: SCAVENGE PUMP. LEAKING. NR 3 ENG OIL QTY WENT TO ZERO IN FLIGHT, VERIFIED BY LOSS OF OIL PRESS & LOW OIL PRESS LIGHT. TROUBLESHOT DOWN TO NR 3 ENGINE OIL LUBE AND SCAVENGE PUMP ASSY. R
- [SDR CNMA20100035](https://openairdocs.org/sdr/CNMA20100035), Dec 29, 2010: STRAINER. CLOGGED. ENG 3 OIL STRAINER CLOG LIGHT ILLUMINATED STEADY IN FLIGHT, ACCOMPLISHED QRH PROCEDURE NR3 ENGINE SHUTDOWN. C/A: REPLACED ENGINE.
- [SDR CNMA20100034](https://openairdocs.org/sdr/CNMA20100034), Nov 28, 2010: SMOKE DETECTOR. FALSE ACTIVATION. ONE SMOKE DETECTOR LIGHT ON AND APPLICABLE CARGO FIRE LIGHT ON (FWD CARGO FIRE LIGHT ON DISCHARGED FIRE BOTTLES). REPLACED FWD CARGO NR3 SMOKE DETECTOR IAW AMN 
- [SDR CNMA20100032](https://openairdocs.org/sdr/CNMA20100032), Nov 4, 2010: SUPPORT FITTING. CORRODED. CTR LANDING GEAR LT AND RT TRUNNION SUPPORT FITTING CORRODED ON TOP AROUND BOLT HOLES. CLEANED CORROSION IAW EO 5310E0973 ROTARY PEEN REWORK AREA IAW DPS 4.999-
- [SDR WRLA20100810431](https://openairdocs.org/sdr/WRLA20100810431), Aug 10, 2010: SLIDE RAFT. DEPLOYED. L 1 DOOR SLIDE WAS FOUND TO BE PARTIALLY DEPLOYED WHILE STILL ATTACHED TO THE DOOR. THE GIRT BAR WAS NOT ENGAGED. THE DOOR ASSIST BOTTLE WAS FULL. THE SLIDE/RAF
- [SDR CNMA20100028](https://openairdocs.org/sdr/CNMA20100028), Jul 24, 2010: PANEL. CORRODED. EXFOLIATED CORROSION ON RT WING LOWER PLATE BELOW ACCESS PANEL 616BB AT XQRS 346. REMOVED DAMAGED SECTION OF LOWER WING SKIN, ACCOMPLISHED SURFACE SCAN AND OPEN
- [SDR CNMA20100027](https://openairdocs.org/sdr/CNMA20100027), Jul 2, 2010: CONTROL HANDLE. MALFUNCTIONED. LANDING GEAR HANDLE WOULD NOT COME UP. FOLLOWED QRH PROCEDURE, RETURNED TO DEPARTURE. JACK ACFT IAW MM-07-11, PERFORM EXTENSION & RETRACTION OF ALL MLG'S. OPS C
- [SDR WRLA20100621395](https://openairdocs.org/sdr/WRLA20100621395), Jun 21, 2010: WEB. CRACKED. WHILE IN ATL DURING A-5 CHECK A SPECIAL INSPECTION (SI) WAS PERFORMED ON THE NR 3 PYLON AND THE UPPER WEB WAS FOUND CRACKED AT THE CORNER OF THE GENERATOR FEEDE
- [SDR CNMA20100026](https://openairdocs.org/sdr/CNMA20100026), Jun 2, 2010: SLIDE. DEFECTIVE. DOOR 3L EVACUATION SLIDE REMOTE PRESURE PRESS TO TEST INDICATOR LIGHT STAYS ON CONTINUOUSLY. REPLACED L-3 DOOR SLIDE ASSY - OPS CHECK NORMAL. OK FOR SERVICE. M/
- [SDR CNMA20100024](https://openairdocs.org/sdr/CNMA20100024), May 14, 2010: DUCT. BLOWN. NR 1 ENGINE FIRE WARNING DURING CLIMB OUT AT 13000 FT. N1'S 103.5. FIRE WARNING EXTINGUISHED WHEN THROTTLE WAS RETARDED. COMPLIED WITH QRH 4-1-1-1. INSP NR 1 EN
- [SDR CNMA20100019](https://openairdocs.org/sdr/CNMA20100019), May 8, 2010: DECODER. FAILED. F/A'S BROUGHT TO ATTENTION OF COCKPIT THAT IF READING LIGHTS, CALL LIGHTS AND AUDIO INOP IN B ZONE MAY EFFECT O2 GENERATORS, MAINT CONTROL CONFIRMED RETURNED TO
- [SDR CNMA20100020](https://openairdocs.org/sdr/CNMA20100020), May 6, 2010: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR PANEL SUPPORT BS 485-515 RBL 55-60. DAMAGED FLOOR SUPPORT WAS REMOVED. NEW FLOOR SUPPORT PN OAI-53-0002 WAS FABRICATED AND INSTALLED USING FA
- [SDR 22AA201000068](https://openairdocs.org/sdr/22AA201000068), Apr 25, 2010: STUD. DAMAGED. OIL PRESSURE NR 2 GAUGE DROPPED TO ZERO AND NR 2 OIL PRESS LOW LIGHT CAME ON, ENGINE SHUTDOWN IAW CHECK LIST. FOUND OIL LEAK COMING FROM CRANK PAD COVER, INSTAL
- [SDR WRLA20100422353](https://openairdocs.org/sdr/WRLA20100422353), Apr 22, 2010: FITTING. CORRODED. REF DELTA N/R 93 CENTER LINE LANDING GEAR LT ATTACH FITTING CENTER BORE PITTED IN FITTING. REWORK CTR LANDING GEAR LT TRUNNION FITTING IAW DELTA ERA 481717-14.
- [SDR CNMA20100023](https://openairdocs.org/sdr/CNMA20100023), Apr 11, 2010: INTERCOSTAL. DAMAGED. CORROSION ON INTERCOSTAL BS 1900-1921 STR 43R. DAMAGED INTERCOSTAL AND ADJACENT ANGLE WERE REMOVED. NEW INTERCOSTAL AND ANGLE PN OAI53-004/005 WERE FABRICATED A
- [SDR CNMA20100022](https://openairdocs.org/sdr/CNMA20100022), Apr 11, 2010: ANGLE. CORRODED. CORROSION ON NUT PLATE ANGLE BS 1099 LBL 41. REMOVED ANGLE AND NEW PN AOA7GG7-23 INSTALLED WITH NEW ANCHOR NUTS AND RIVETS IAW SRM VOL 2 51-31-01. PN BACB30NWGK
- [SDR CNMA20100021](https://openairdocs.org/sdr/CNMA20100021), Apr 7, 2010: ANGLE. CORRODED. CORROSION ON ANGLE C/T AFT CARGO TANK WALL BS 1781 4 PLACES RBL 30, RBL 36, LBL 30, LBL 36. DAMAGED ANGLE REMOVED, NEW FABRICATED PN OAI-53-00-11 IAW DWG AFA754
- [SDR 22AA201000067](https://openairdocs.org/sdr/22AA201000067), Apr 5, 2010: RECEPTACLE. LOOSE. PASSING FL 8000 AFT CARGO DOOR A & B LIGHT ILLUMINATED INTERMITTENT UNABLE TO PRESSURIZE, RETURN TO DEPARTURE. TROUBLE SHOOTING FOUND LOOSE CONNECTOR ON LATCH D
- [SDR CNMA20100018](https://openairdocs.org/sdr/CNMA20100018), Apr 1, 2010: FLOORBEAM. CORRODED. BS 2007, LBL 20-28 CORROSION ON M/D FLOOR SUPPORT TEE CHORD. ALL OPEN HOLES WERE NDT INSPECTED - NO CRACKS OR CORROSION WERE FOUND. THIS SECTION OF CHORD WAS IN
- [SDR CNMA20100017](https://openairdocs.org/sdr/CNMA20100017), Apr 1, 2010: FLOORBEAM. CORRODED. BS 2007, LBL 53-68 CORROSION ON FLOOR SUPPORT TEE CHORD. ALL OPEN HOLES NDT INSPECTED - NO CRACKS OR CORROSION FOUND. THIS SECTION WAS INCLUDED IN THE REPAIR OF
- [SDR CNMA20100016](https://openairdocs.org/sdr/CNMA20100016), Apr 1, 2010: FLOORBEAM. CORRODED. BS 2007 LBL 77 CORROSION ON TEE CHORD FLOOR SUPPORT. ALL OPEN HOLES WERE NDT INSPECTED - NO CRACKS OR CORROSION FOUND. THIS SECTION OF CHORD WAS INCLUDED IN THE
- [SDR CNMA20100015](https://openairdocs.org/sdr/CNMA20100015), Apr 1, 2010: FLOORBEAM. CORRODED. BS 2007, LBL16 CORROSION ON THE TEE CHORD FLOOR STRUCTURE. CORRODED SECTION OF CHORD WAS TRIMMED OUT. NEW SECTION FABRICATED FROM THE TEE PN NJC6040-175 WAS INS
- [SDR CNMA20100014](https://openairdocs.org/sdr/CNMA20100014), Mar 28, 2010: FLOOR SUPPORT. CORRODED. CORROSION ON CTR CARGO LWR PANEL SUPPORT BS 1700-1781 BL-0.3, DAMAGED AREAS TRIMMED OUT. AREAS REINFORCED WITH DOUBLERS PN N621AX-NRC361-1 (QTY X3) FABRICATED A
- [SDR CNMA20100013](https://openairdocs.org/sdr/CNMA20100013), Mar 28, 2010: FLOORBEAM. CORRODED. CORROSION ON CTR CARGO LWR PANEL SUPPORT BS 1741 LBL 16. DAMAGED SUPPORT REMOVED NEW FABRICATED PN OAI-53-0008 IAW SRM DWG AD0145-30 & OMNI GMM 4.45 AND INSTALL
- [SDR CNMA20100012](https://openairdocs.org/sdr/CNMA20100012), Mar 28, 2010: FLOORBEAM. CORRODED. CORROSION ON CTR CARGO LWR PANEL SUPPORT BS 1741 RBL 16. DAMAGED SUPPORT REMOVED NEW FABRICATED PN OAI-53-0007 IAW SRM DWG AD00145 OMNI GMM 4.45 AND INSTALLED W
- [SDR CNMA20100011](https://openairdocs.org/sdr/CNMA20100011), Mar 28, 2010: FLOORBEAM. CORRODED. CORROSION ON CTR CARGO LWR PANEL SUPPORT BS 1741 RBL 12-14. DAMAGED SUPPORT REMOVED NEW FABRICATED PN OAI-53-0009 IAW DWG AD00145 & OMNI GMM 4-45 AND INSTALLED 
- [SDR 22AA201000067A](https://openairdocs.org/sdr/22AA201000067A), Mar 28, 2010: CONTROL CABLE. BROKEN. ACFT ROLLS WHEN SPEED BRAKE IS EXTENDED. DIFFERENCE SHOWS ON SPI. DURING INSP FOUND RT/LT INBD AILERONS OUT OF RIGGING. ALSO ON PRE/FLT FOUND LT WING GROUND SPO
- [SDR CNMA20100005](https://openairdocs.org/sdr/CNMA20100005), Mar 12, 2010: FAN. SHORTED. AFTER T/O, BURNED SMELL FROM "A" ZONE WAS NOTICED. CABIN AIR RECIRC FAN NR1 SW WAS TRIPPED, BUT FAN NR15 WAS STILL THERE IN AFT "A" ZONE, SO ALL RECIRC FANS TUR

All 2,776: https://openairdocs.org/model/mcdonnell-douglas-dc-10-30/reports.md

## STCs that may be installed (OpenAirDocs) (382, 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 ST00272AT](https://openairdocs.org/stc/ST00272AT): Installation of an Airshow 210 enter- tainment system. AIRCRAFT RECONFIG TECHNOLOGIES, LLC. Lists DC-10 Series
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [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 SA5040NM](https://openairdocs.org/stc/SA5040NM): Installation of cargo pallet and net. Satco Inc
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC SA1368NM](https://openairdocs.org/stc/SA1368NM): Installation of C&D Interiors P/N 1441002. Safran Cabin Inc
- [STC SA1369NM](https://openairdocs.org/stc/SA1369NM): Installation of closets. Safran Cabin Inc
- [STC SA2049NM](https://openairdocs.org/stc/SA2049NM): Installation of C&D Interiors P/N 1751001-101, -102. Safran Cabin Inc
- [STC SA2175NM](https://openairdocs.org/stc/SA2175NM): Installation of the Centerline Overhead Stowage Retrofit Kit. Safran Cabin Inc
- [STC SA2471NM](https://openairdocs.org/stc/SA2471NM): Installation of centerline bin, overhead side bin. Safran Cabin Inc
- [STC SA2499NM](https://openairdocs.org/stc/SA2499NM): Installation of closet/windscreen. Safran Cabin Inc
- [STC SA3127NM](https://openairdocs.org/stc/SA3127NM): Installation of Closet. Safran Cabin Inc
- [STC SA3422NM](https://openairdocs.org/stc/SA3422NM): Installation of a galley. Safran Cabin Inc
- [STC SA3460NM](https://openairdocs.org/stc/SA3460NM): Installation of centerline stowage bins. Safran Cabin Inc. Lists DC-10 Series
- [STC SA3804NM](https://openairdocs.org/stc/SA3804NM): Installation of the Centerline SkyBin Stowage Interior kit. Safran Cabin Inc
- [STC SA3967NM](https://openairdocs.org/stc/SA3967NM): Installation of bi-fold lavatory door. Safran Cabin Inc
- [STC SA4832NM](https://openairdocs.org/stc/SA4832NM): Installation of C&D Interiors Part Numbers 3001001-105 Credenza, 4761001-101 C/L Closet, and 4771001-101 and -102 L.H. and R.H. Closet. Safran Cabin Inc
- [STC SA5492NM](https://openairdocs.org/stc/SA5492NM): Installation of galleys, dividers, closet, and fold-down table. Safran Cabin Inc
- [STC SA8001NM](https://openairdocs.org/stc/SA8001NM): Installation of C&D Interiors class divider and ceiling panel. Safran Cabin Inc
- [STC ST00495LA](https://openairdocs.org/stc/ST00495LA): Installation of lavatories. Safran Cabin Inc
- [STC ST00584LA](https://openairdocs.org/stc/ST00584LA): Installation of centerline bin kits. Safran Cabin Inc
- [STC ST00650LA](https://openairdocs.org/stc/ST00650LA): Installation of lavatories. Safran Cabin Inc
- [STC ST01077LA](https://openairdocs.org/stc/ST01077LA): Installation of passenger service unit (PSU). Safran Cabin Inc
- [STC ST01391LA](https://openairdocs.org/stc/ST01391LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC SA3411NM](https://openairdocs.org/stc/SA3411NM): Installation of floor proximity emergency escape path marking system. Bruce Aerospace Inc
- [STC ST01694AT](https://openairdocs.org/stc/ST01694AT): Installation of additional sensors for recording additional parameters on Digital Flight Data Recorder (DFDR). Acron Aviation 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 ST02117CH](https://openairdocs.org/stc/ST02117CH): Installation of Honeywell Enhanced Ground Proximity Warning System and GPS antenna. Amphenol Cable and Interconnect Technologies Inc
- [STC ST02184CH](https://openairdocs.org/stc/ST02184CH): Installation of elementary or enhanced surveillance Mode S transponders. Amphenol Cable and Interconnect Technologies Inc
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST02131AT](https://openairdocs.org/stc/ST02131AT): Installation of SAF-T-GLO photoluminescent floor proximity emergency escape with marking system (FPEEPMS). STG Aerospace Inc
- [STC SA3474NM](https://openairdocs.org/stc/SA3474NM): Installation of Galley 1, Galley 2, Galley 1A, Coartoom and Lavatories. Safran Cabin Inc
- [STC ST01986CH](https://openairdocs.org/stc/ST01986CH): Installation of a Honeywell RESCU 406AF Emergency Locator Transmitter (ELT) system. Honeywell International Inc
- [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [STC SA1220NW](https://openairdocs.org/stc/SA1220NW): Installation of Universal flight data recorder. Honeywell International Inc
- [STC SA3046SO](https://openairdocs.org/stc/SA3046SO): Installation of a single/dual TRA-67 Mode S ATC transponder system. Honeywell International Inc
- [STC SA3061SO](https://openairdocs.org/stc/SA3061SO): Installation of a CAS-81 TCAS II system. Honeywell International Inc
- [STC SA5794NM](https://openairdocs.org/stc/SA5794NM): Installation of Mark VII ground proximity and windshear warning system. Honeywell International Inc
- [STC ST00536SE](https://openairdocs.org/stc/ST00536SE): Installation of the Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS). Honeywell International Inc
- [STC SA5672SW-D](https://openairdocs.org/stc/SA5672SW-D): Modification of air to air heat exchanger (P/N 187900-9). Honeywell International Inc
- [STC SA8928SW](https://openairdocs.org/stc/SA8928SW): Replace core assembly of AiResearch Bleed Air Precooler, part numbers 187890-3 and 189740-3. Honeywell International Inc
- [STC SA8757SW](https://openairdocs.org/stc/SA8757SW): Replace core assembly of Janitrol Constant Speed Drive (CSD) Oil Cooler, part number B63D89. Honeywell International Inc
- [STC SA7419SW](https://openairdocs.org/stc/SA7419SW): Rebuild DC-10 Auxiliary Power Unit Oil Cooler Assembly by manufacturing a new core assembly. Honeywell International Inc. Lists DC-10 Series
- [STC SA4010WE](https://openairdocs.org/stc/SA4010WE): Installation of video projection system. Burrana Inc
- [STC SA4070WE](https://openairdocs.org/stc/SA4070WE): A video projection system is installed. Burrana Inc
- [STC SA451NE](https://openairdocs.org/stc/SA451NE): Installation of Inflight Services video projection system DC-10 Bangladesh P/N 105-D-1228. Burrana Inc
- [STC SA930EA](https://openairdocs.org/stc/SA930EA): Installation of Inflight Motion Pictures, Inc., Projection Unit Assembly DC-10 16mm Tri-Jet System, P/N 10300 or Light Weight Tri-Jet Projection System, DC-10, P/N 10307. Burrana Inc
- [STC SA947EA](https://openairdocs.org/stc/SA947EA): Installation of Inflight Motion Pictures, Inc. screen assemblies. Burrana Inc
- [STC SA990EA](https://openairdocs.org/stc/SA990EA): Installation of Inflight Motion Pictures 16mm projection unit assembly and center stowage bins, P/N 10310 and/or P/N 10311. Burrana Inc

All 382: https://openairdocs.org/model/mcdonnell-douglas-dc-10-30/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/DRSDOCID111791513520261009134007.0001): Packing, Preform - Fluorocarbon. Wencor, LLC · PMA PQ1370NM · Replaces S9413-008 · Oct 1, 2026
- [9143FR-0325](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172200643320260909221022.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR-0315](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148776985720260909221013.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR-0200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133606371820260909221004.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116339893920260909220945.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [AF300P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191275281320260717175324.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026
- [AF302](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178154048320260717175326.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026
- [AF300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172513122320260717175322.0001): Repair Kit. AkroFire, Inc. · PMA PQ3730CE · Modification part · May 11, 2026
- [10-M7140-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179611553220260407171344.0001): Pin-Trunion, Steering Nose Landing Gear. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces ACG7140-1 · Mar 25, 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
- [10-M7140-1-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103543850320260407171345.0001): Pin-Trunion, Steering Nose Landing Gear. ALLIANCE AEROSPACE ENGINEERING INC · PMA PQ2532NM · Replaces ACG7140-501 · Mar 25, 2026
- [M840105](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154219509420260325172403.0001): Cylinder Assembly. Ametek Ameron LLC d/b/a Mass Systems · PMA PQ1432NM · Replaces 840105 · Feb 17, 2026
- [M840105](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140279722720260325180521.0001): Cylinder Assembly. Ametek Ameron LLC d/b/a Mass Systems · PMA PQ1432NM · Replaces 840105 · Feb 17, 2026
- [AAP-3502129-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156061776920251125143634.0001): Bearing. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3502129-1 · Nov 6, 2025
- [SP2514-06-1175](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106892706220251119194842.0001): CAP ASSEMBLY. Soundair Aviation Services · PMA PQ2540NM · Replaces 383-0271-1 · Oct 1, 2025
- [1921001-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199487959520260113211602.0001): Centerline Overhead Stowage Bins. Safran Cabin Inc. · PMA PQ1176NM · Replaces 1921001-1 · Aug 7, 2025
- [3011001-107](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196152714420260113211632.0001): Galley Assy. Safran Cabin Inc. · PMA PQ1176NM · Replaces 3011001-107 · Aug 7, 2025
- [Parts as listed per Dwg List No 12078](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195291609920260113211727.0001): Bi-Fold Lavatory Door. Safran Cabin Inc. · PMA PQ1176NM · Replaces Parts as listed per Dwg List No 12078 · Aug 7, 2025
- [2031001-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195228388720260113211641.0001): Windscreen. Safran Cabin Inc. · PMA PQ1176NM · Replaces 2031001-101 · Aug 7, 2025
- [Parts as listed per Dwg List No: 4026000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194869055420260113211732.0001): Centerline Bin Kits. Safran Cabin Inc. · PMA PQ1176NM · Replaces Parts as listed per Dwg List No: 4026000 · Aug 7, 2025
- [17670-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194010622020260113214130.0001): Bustle Assy 
& Structure Continental. Safran Cabin Inc. · PMA PQ1176NM · Modification part · Aug 7, 2025
- [17650-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193305219520260113214130.0001): Galley Assy 1A Continental. Safran Cabin Inc. · PMA PQ1176NM · Modification part · Aug 7, 2025
- [2851001-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192535643220260113211611.0001): Centerline Stowage Bin. Safran Cabin Inc. · PMA PQ1176NM · Replaces 2851001-101 · Aug 7, 2025
- [1751001-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189397424220260113211601.0001): Interior Installation. Safran Cabin Inc. · PMA PQ1176NM · Replaces 1751001-101 · Aug 7, 2025
- [1581001-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189110479220260113211747.0001): Coatroom/Cart Stowage Unit. Safran Cabin Inc. · PMA PQ1176NM · Replaces 1581001-101 · Aug 7, 2025
- [17600-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189087595020260113214129.0001): Galley 1A Upper Section Continental. Safran Cabin Inc. · PMA PQ1176NM · Modification part · Aug 7, 2025
- [17650-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187426215820260113214130.0001): Galley Assy 1A Continental. Safran Cabin Inc. · PMA PQ1176NM · Modification part · Aug 7, 2025
- [2031001-103](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187188833520260113211647.0001): Class Divider. Safran Cabin Inc. · PMA PQ1176NM · Replaces 2031001-103 · Aug 7, 2025
- [17670-201](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184338166820260113214131.0001): Bustle Assy    & Structure Continental. Safran Cabin Inc. · PMA PQ1176NM · Modification part · Aug 7, 2025
- [2021001-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183048593520260113211601.0001): Closet. Safran Cabin Inc. · PMA PQ1176NM · Replaces 2021001-101 · Aug 7, 2025
- [2121001-102](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182897221020260113211605.0001): Closet. Safran Cabin Inc. · PMA PQ1176NM · Replaces 2121001-102 · Aug 7, 2025
- [12295](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181529486920260113211745.0001): Galley Assy. Safran Cabin Inc. · PMA PQ1176NM · Replaces 12295 · Aug 7, 2025
- [17670-21](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181168116620260113214131.0001): Bustle Assy    & Structure Continental. Safran Cabin Inc. · PMA PQ1176NM · Modification part · Aug 7, 2025
- [2021001-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181136054520260113211640.0001): Closet. Safran Cabin Inc. · PMA PQ1176NM · Replaces 2021001-101 · Aug 7, 2025
- [1921001-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180966978020260113211602.0001): Centerline Overhead Stowage Bins. Safran Cabin Inc. · PMA PQ1176NM · Replaces 1921001-3 · Aug 7, 2025
- [Parts as Listed per Index List No 918](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180691040920260113211722.0001): Lavatories. Safran Cabin Inc. · PMA PQ1176NM · Replaces Parts as Listed per Index List No 918 · Aug 7, 2025
- [5381001-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180667557320260113211646.0001): Galley L H. Safran Cabin Inc. · PMA PQ1176NM · Replaces 5381001-501 · Aug 7, 2025
- [17670-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178861149220260113214130.0001): Bustle Assy 
& Structure Continental. Safran Cabin Inc. · PMA PQ1176NM · Modification part · Aug 7, 2025
- [1441001-102](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178358289120260113211746.0001): Cart Stowage Unit. Safran Cabin Inc. · PMA PQ1176NM · Replaces 1441001-102 · Aug 7, 2025
- [3001001-105](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176222598220260113211629.0001): Credenza. Safran Cabin Inc. · PMA PQ1176NM · Replaces 3001001-105 · Aug 7, 2025
- [17600-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175692581320260113214129.0001): Galley 1A Upper Section Continental. Safran Cabin Inc. · PMA PQ1176NM · Modification part · Aug 7, 2025
- [17410-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174757502320260113214127.0001): Galley Assy 1Continental. Safran Cabin Inc. · PMA PQ1176NM · Modification part · Aug 7, 2025
- [4771001-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173631127520260113211629.0001): Closet. Safran Cabin Inc. · PMA PQ1176NM · Replaces 4771001-101 · Aug 7, 2025
- [2031001-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171868802220260113211602.0001): Windscreen. Safran Cabin Inc. · PMA PQ1176NM · Replaces 2031001-101 · Aug 7, 2025
- [A516001-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171651687520260113211733.0001): PSU Installation Zone A. Safran Cabin Inc. · PMA PQ1176NM · Replaces A516001-501 · Aug 7, 2025
- [2851001-103](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170716250620260113211611.0001): Centerline Stowage Bin. Safran Cabin Inc. · PMA PQ1176NM · Replaces 2851001-103 · Aug 7, 2025
- [Parts as Listed per Index List No 1196](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169455552120260113211725.0001): Centerline Bin/ Overhead Side Bin. Safran Cabin Inc. · PMA PQ1176NM · Replaces Parts as Listed per Index List No 1196 · Aug 7, 2025
- [2971001-515](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168648405220260113211640.0001): Centerline Stowage Bins. Safran Cabin Inc. · PMA PQ1176NM · Replaces 2971001-515 · Aug 7, 2025
- [17680-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165073181420260113214131.0001): Lavatory Structure Modification Continental Airlines. Safran Cabin Inc. · PMA PQ1176NM · Modification part · Aug 7, 2025

All of them: https://openairdocs.org/model/mcdonnell-douglas-dc-10-30/pma.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
