# Douglas DC-10-40F

- Type: Aircraft model (FAA registry)
- Registry code: 3023507
- Manufacturer (registry): DOUGLAS
- Model: DC-10-40F
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 3 · Turbo-jet
- Seats: 380
- 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: 1
- Page: https://openairdocs.org/model/douglas-dc-10-40f

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 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 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 2008-11-14](https://openairdocs.org/ad/2008-11-14): Horizontal pressure panel · Boeing DC-10-10F, DC-10-30F (KC-10A, KDC-10), DC-10-40F and 4 more. Effective Jul 3, 2008
- [AD 2007-25-20](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 2007-11-15](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 2007-04-17](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 2004-05-06](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
- [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 2003-11-04](https://openairdocs.org/ad/2003-11-04): Linear variable differential transducers (LVDTs) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 4 more. Effective Jul 3, 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

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 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 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 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 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

All 175: https://openairdocs.org/model/douglas-dc-10-40f/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 (1)

- [N141WE](https://openairdocs.org/aircraft/N141WE): [Omega Air Inc](https://openairdocs.org/faa-owner/OMEGA%20AIR%20INC), [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio), S/N 46661

## NTSB investigations (1)

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 WAS02RA037](https://openairdocs.org/ntsb/WAS02RA037), Apr 27, 2002: McDonnell Douglas DC-10-40F (N141WE), San Salvador, El Salvador, substantial damage

## FAA accident and incident reports (1)

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 20000217003429I](https://openairdocs.org/incident/20000217003429I), Feb 17, 2000: Doug DC1040F (N141WE), Panama, PN, Minor damage. Crew grounded. All crew members 3 hr safety course. Capt line check. Safety briefing ground crew.

## Service difficulty reports (52, newest 50)

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

- [SDR 22AA20090203](https://openairdocs.org/sdr/22AA20090203), Feb 22, 2009: INDICATOR. INOPERATIVE. TAKEOFF ABORTED FROM MHLM AT 110 KTS. ON TAKEOFF ROLL ENGINE NR 2 EPR GAUGE FAILED AT 1.20 EPR. POINTER AND ANALOG DIGITS FAILED IN PLACED WITH NO FLAG IN VIEW.
- [SDR 22AA20081003](https://openairdocs.org/sdr/22AA20081003), Oct 19, 2008: MECHANISM. LACK OF LUBE. UPON RETRACTING FLAPS 2 1/2 UNITS OF AILERON TRIM TO THE RT MUST BE USED TO KEEP WINGS LEVEL. PERFORMED AILERONS SYSTEM TEST IN ACCORDANCE WITH M/M 27-10-00. FO
- [SDR ARWA20080801](https://openairdocs.org/sdr/ARWA20080801), Aug 5, 2008: WARNING SYSTEM. MALFUNCTIONED. ATC REPORT FOR DOOR OPEN ON ACFT. RETURN TO RAMP. INSPECTED ACFT. FOUND NO DOOR OPEN, NORMAL CONDITION IAW WITH MM 52-00-00. ALL CLOSED AND LIGHT OFF. (S)
- [SDR ARWA20080702](https://openairdocs.org/sdr/ARWA20080702), Jul 18, 2008: O-RING. LEAKING. HYDRAULIC SYSTEM QTY STARTED TO DROP AT OP OF DESCENT. PERFORMED THE HYD QTY LOSS ALTERATIVE. OPS CHECKLIST. FLUID LOSS CONTINUED. PERFORMED SINGLE HYD SYS FAIL
- [SDR ARQA20080703](https://openairdocs.org/sdr/ARQA20080703), Jul 18, 2008: LINE. LEAKING. EVIDENCE OF HYDRAULIC LEAK LT HAND WHEEL WB 11. REPAIRED SECTION OF HYDRAULIC LINE DAMAGED, USING TYPE 3 REPAIRED IN ACCORDANCE WITH DC10-MM 20-10-01. LEAK CHEC
- [SDR ARWA20080603](https://openairdocs.org/sdr/ARWA20080603), Jun 22, 2008: THROTTLE. OBSTRUCTED. UPON INITIATION OF TAKEOFF ROLL NR 3 POWER LEVER WOULD NOT ADVANCE BEYOND 128 EPR. RETURNED TO RAMP. OPENED ENGINE FOUND HYD TEMP C/P WIRE AROUND THROTTLE BELL 
- [SDR ARWA20080503](https://openairdocs.org/sdr/ARWA20080503), May 17, 2008: THERMOCOUPLE. SHORTED. IN FLIGHT NR 2 ENGINE EGT INDICATOR FLUCTUATING 20 TO 30 DEGREES BOTH POINTER AND COUNTER, ALL OTHER PARAMETERS NORMAL. TROUBLE SHOT IN ACCORDANCE WITH TAFY MAN
- [SDR ARWA20080502](https://openairdocs.org/sdr/ARWA20080502), May 17, 2008: INDICATOR. FAULTY. IN FLIGHT NR 2 ENGINE EGT INDICATOR FLUCTUATING 20 TO 30 DEGREES BOTH POINTER AND COUNTER ALL OTHER PARAMETERS NORMAL. REMOVED AND REPLACED NR 2 EGT INDICATOR C
- [SDR ARWA20070801](https://openairdocs.org/sdr/ARWA20070801), Aug 3, 2007: DOOR. DAMAGED. AFTER GEAR RETRACTION RED LEFT LGD GEAR LIGHT ON FWD AND F/E PANELS REMAINED ON. PERFORMED THE APPROPRIATE CHECK-LIST AND RETURN TO LANDING AFTER DUMPING FUEL T
- [SDR ARWA20070603](https://openairdocs.org/sdr/ARWA20070603), Jun 6, 2007: VALVE. UNKNOWN. 3 IDLE OIL PRESSURE 23 PSI. REMOVED AND REPLACED NR 3 ENGINE OIL PRESSURE FILTER ADJUSTED OIL PRESSURE RELIEF VALVE IN ACCORDANCE WITH DC-10 M/M 71-00-01. PERFO
- [SDR ARWA20070307](https://openairdocs.org/sdr/ARWA20070307), Mar 23, 2007: CONNECTOR. LOOSE. ON ROTATION, NR 1 ENGINE REVERSER UNLOCK LIGHT CAME ON AND REMAINED ON; SHUT ENGINE DOWN AND RETURNED TO MIAMI. PERFORMED ELECTRICAL SYSTEM CHECK AND FOUND LOOS
- [SDR ARWA20070305](https://openairdocs.org/sdr/ARWA20070305), Mar 22, 2007: CABLE. BROKEN. ON TAKEOFF ROLL, NR 2 ENGINE REVERSER UNLOCK LIGHT CAME ON. ABORTED TAKEOFF AS SOON AS THROTTLES WERE ADVANCED. DEACTIVATED NR 2 ENGINE THRUST REVERSER AS PER M
- [SDR ARWA20061002](https://openairdocs.org/sdr/ARWA20061002), Oct 12, 2006: LINE. DAMAGED. IN CRUISE FLIGHT TO MAINTAIN NR 1 ENGINE N1 ALIGNMENT WITH ALL OTHER ENGINES N1 NR 1 EPR INDICATING 1.15 NR 2 EPR 1.32 AND NR 3 EPR 1.32 ALL N2 ALIGNED. PERFORM
- [SDR CLC2005F00003](https://openairdocs.org/sdr/CLC2005F00003), Jul 21, 2005: CONTROL CABLE. CORRODED. DURING PREFLIGHT, FOUND RUDDER NOSE RIGHT CABLE 2D BROKEN. FOUND RT RUDDER CONTROL CABLE 2D CORRODED AND BROKEN. REMOVED AND REPLACED RUDDER CONTROL CABLE NOSE 
- [SDR CLC2005F00007](https://openairdocs.org/sdr/CLC2005F00007), Jul 11, 2005: RING. DAMAGED. DURING PREFLIGHT CHECK, DAMAGE WAS FOUND TO NR 2 ENGINE INTAKE AND FAN BLADES. ENGINE INTAKE HAS DAMAGE TO UPPER AND LOWER BELL MOUTH ADAPTOR RINGS, INTAKE INLE
- [SDR CLC2005F00006](https://openairdocs.org/sdr/CLC2005F00006), Jul 11, 2005: INLET. DAMAGED. DURING PREFLIGHT CHECK, DAMAGE WAS FOUND NR 2 ENGINE INTAKE AND FAN BLADES. ENG INTAKE HAS DAMAGE TO UPPER AND LWR BELL MOUTH ADAPTOR RINGS, INTAKE INLET LIP HA
- [SDR CLC2005F00005](https://openairdocs.org/sdr/CLC2005F00005), Jul 11, 2005: SEAL. DAMAGED. DURING PREFLIGHT CHECK, DAMAGE WAS FOUND TO NR 2 ENGINE INTAKE AND FAN BLADES. ENGINE INTAKE HAS DAMAGE TO UPPER AND LWR BELLMOUTH ADAPTOR RINGS, INTAKE INLET L
- [SDR CLC2005F00004](https://openairdocs.org/sdr/CLC2005F00004), Jul 11, 2005: ADAPTER RING. DAMAGED. DURING PREFLIGHT CHECK, DAMAGE WAS FOUND TO NR 2 ENGINE INTAKE AND FAN BLADES. ENGINE INTAKE HAS DAMAGE TO UPPER AND LOWER BELL MOUTH ADAPTOR RINGS, INTAKE INLE
- [SDR CLC2006F00006](https://openairdocs.org/sdr/CLC2006F00006), Jul 28, 2004: WINDOW FRAME. OUT OF ADJUST. R1 DOOR WILL NOT DISARM, WHILE TROUBLESHOOTING THE DOOR THE SLIDE DEPLOYED. FOUND VIEW WINDOW FRAME FOR THE ARMED LEVER BINDING. REPOSITIONED VIEW WINDOW FRAME,
- [SDR 2004F00201](https://openairdocs.org/sdr/2004F00201), Apr 29, 2004: PIN. SHEARED. HORIZONTAL STABILIZER JAMMED AT APPROXIMATELY 1.5 ANU DURING CRUISE. ABNORMAL PROCEDURES COMPLIED WITH FOR LANDING. LANDING AT DESTINATION UNEVENTFL. FOUND SHEA
- [SDR 2003F00115](https://openairdocs.org/sdr/2003F00115), Dec 4, 2002: COWLING. DELAMINATED. DURING SCHEDULED MAINTENANCE, NR 1 FAN COWL PREVIOUS REPAIR WAS FOUND DELAMINATED ON THE INBOARD LOWER CORNER. REPAIRED IAW AS11 DRAWING AS11476, DOUBLER REPAIR
- [SDR 2003F00088](https://openairdocs.org/sdr/2003F00088), Nov 8, 2002: WEDGE. DAMAGED. DURING ROUTINE MAINTENANCE, THE LEFT WING OUTBOARD FLAP INBOARD TRAILING EDGE WEDGE WAS FOUND DAMAGED. ACCOMPLISHED REPAIR IAW AS11 DRAWING AS11467, AND 8110-3 
- [SDR 2003F00089](https://openairdocs.org/sdr/2003F00089), Nov 3, 2002: THRUST REVERSER. DEBONDED. DURING ROUTINE MAINTENANCE, THE NR 2 ENGINE THRUST REVERSER INNER SURFACE WAS FOUND DEBONDED. REMOVED DEBONDED AREA, FABRICATED DOUBLER REPAIR AND REPAIRED AREA
- [SDR 2002F00629](https://openairdocs.org/sdr/2002F00629), Apr 27, 2002: HYDRAULIC SYSTEM. MALFUNCTIONED. FLT 558 - MSLP-KMIA - DURING CLIMB-OUT, LOST HYDRAULIC SYSTEMS ONE AND TWO. RETURNED TO MSLP AND A NORMAL LANDING WITHOUT INCIDENT WAS MADE. NR 1 TIRE MISSING A
- [SDR 2002F00334](https://openairdocs.org/sdr/2002F00334), Dec 1, 2001: THRUST REVERSER. DAMAGED. DURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN WAS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALLED IAW REO-G08284. THE AIRCRAFT WAS RETUR
- [SDR 2002F00333](https://openairdocs.org/sdr/2002F00333), Dec 1, 2001: STRUCTURE. CORRODED. DURING C-CHECK, THE FORWARD LT AIR CONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 48L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS INS
- [SDR 2002F00332](https://openairdocs.org/sdr/2002F00332), Dec 1, 2001: LONGERON. CRACKED. DURING C-CHECK, LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED. THE AIRCRAFT WAS RETURNED TO REVENUE S
- [SDR 2002F00331](https://openairdocs.org/sdr/2002F00331), Dec 1, 2001: STRUCTURE. CORRODED. DURING C-CHECK, THE LEFT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMITS. A REPAIR ANGLE WAS INSTALLED IAW TIM
- [SDR 2002F00330](https://openairdocs.org/sdr/2002F00330), Dec 1, 2001: THRUST REVERSER. DAMAGED. DURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN WAS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALLED IAW REO-G08284 AND A 8110-3 WAS ISSUED
- [SDR 2002F00318](https://openairdocs.org/sdr/2002F00318), Dec 1, 2001: ANGLE. CORRODED. DURING C-CHECK, THE FORWARD LEFT AIRCONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 48L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS IN
- [SDR 2002F00317](https://openairdocs.org/sdr/2002F00317), Dec 1, 2001: LONGERON. CRACKED. DURING C-CHECK, LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED IAW TIMCO REO-GO8321 REV IR AND FAA FOR
- [SDR 2002F00316](https://openairdocs.org/sdr/2002F00316), Dec 1, 2001: FRAME. CORRODED. DURING C-CHECK, THE LT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMITS. A REPAIR ANGLE WAS INSTALLED IAW TIMCO
- [SDR 2002F00025](https://openairdocs.org/sdr/2002F00025), Dec 1, 2001: FRAME. CORRODED. DURING C-CHECK, THE LEFT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMITS. A REPAIR ANGLE WAS INSTALLED IAW TIM
- [SDR 2002F00024](https://openairdocs.org/sdr/2002F00024), Dec 1, 2001: LONGERON. CRACKED. DURING C-CHECK, LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED IAW TIMCO REO-GO8321 REV IR AND FAA FOR
- [SDR 2002F00023](https://openairdocs.org/sdr/2002F00023), Dec 1, 2001: ANGLE. CORRODED. DURING C-CHECK, THE FORWARD LEFT AIR CONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 48L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS I
- [SDR 2002F00022](https://openairdocs.org/sdr/2002F00022), Dec 1, 2001: THRUST REVERSER. DAMAGED. DURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN WAS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALLED IAW REO-G08284 AND A 8110-3. THE AIRCR
- [SDR 2002F00021](https://openairdocs.org/sdr/2002F00021), Dec 1, 2001: FRAME. CORRODED. DURING C-CHECK, THE LEFT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMITS. A REPAIR ANGLE WAS INSTALLED IAW TIM
- [SDR 2002F00020](https://openairdocs.org/sdr/2002F00020), Dec 1, 2001: LONGERON. CRACKED. DURING C-CHECK, FOUND LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED IAW TIMCO REO-G08321 REV IR AND F
- [SDR 2002F00019](https://openairdocs.org/sdr/2002F00019), Dec 1, 2001: SKIN. CORRODED. DURING C-CHECK, THE FORWARD LEFT AIR CONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 47L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS I
- [SDR 2002F00018](https://openairdocs.org/sdr/2002F00018), Dec 1, 2001: THRUST REVERSER. DAMAGED. DURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN AS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALLED IAW REO-GO8284 AND A 8110-3 WAS ISSUED.
- [SDR 2001F00421](https://openairdocs.org/sdr/2001F00421), Jun 11, 2001: SKIN. CHAFED. DURING C-CHECK, FOUND RIGHT OUTBOARD FLAP UPPER SKIN WAS FOUND CHAFED NEAR STATION XOF 759. REPAIRED CHAFED SKIN ON RIGHT OUTBOARD FLAP UPPER SKIN NEAR STATION 
- [SDR 2001F00420](https://openairdocs.org/sdr/2001F00420), Jun 11, 2001: PANEL. CORRODED. DURING C-CHECK, FOUND CORROSION ON THE NR 3 ENGINE OUTBOARD THRUST REVERSER INTERNAL SKIN ACOUSTICAL PANEL. CORROSION WAS REMOVED AND THE PANEL WAS REPAIRED IAW
- [SDR 2001F00419](https://openairdocs.org/sdr/2001F00419), Jun 11, 2001: DOOR FRAME. CORRODED. DURING C-CHECK, FOUND CORROSION ON THE LOWER FORWARD END OF THE FORWARD CARGO DOOR JAMB FRAME AT STATION 886. CORROSION WAS REMOVED AND REPAIRED IAW EA NR 10-53
- [SDR 2001F00418](https://openairdocs.org/sdr/2001F00418), Jun 11, 2001: FLAP. CORRODED. DURING C-CHECK, THE RIGHT OUTBOARD FLAP OUTBOARD HINGE ATTACH POINTS HAVE HEAVY EXFOLIATION AT LOWER MOUNT BULKHEAD FITTING (VIEWED INTERNALLY). RIGHT OUTBOARD 
- [SDR 2001F00417](https://openairdocs.org/sdr/2001F00417), Jun 11, 2001: SPAR CAP. CORRODED. DURING C-CHECK, FOUND CORROSION IN THE NR 3 ENGINE WING SPAR FITTING BULKHEAD UPPER CAP NR 3 ATTACH HOLE. THE CORROSION WAS REMOVED AND THE UPPER CAP WAS REPAIR
- [SDR 2001F00416](https://openairdocs.org/sdr/2001F00416), Jun 11, 2001: RIB. CORRODED. DURING C-CHECK, THE LEFT OUTBOARD FLAP HAS CORROSION BETWEEN FRONT SPAR CAP STATION 538 THROUGH 554. SURFACE CORROSION ON RIBS AT STATION 538. LEFT OUTBOARD FLA
- [SDR 2001F00415](https://openairdocs.org/sdr/2001F00415), Jun 11, 2001: RIB. CRACKED. DURING C-CHECK, THE RIGHT WING NR 8 SLAT RIB AT STATION XOS1158 WAS FOUND CRACKED, 12 INCHES LONG. THE CRACK WAS REPAIRED IAW EA NR 10-5755-24-A0886. AIRCRAFT W
- [SDR 20010126SG001](https://openairdocs.org/sdr/20010126SG001), Dec 28, 2000: PIN. SHEARED. FLT 95 - MIA-SVMI - STABILIZER JAM FULL NOSE UP POSITION. FOUND SHEAR PIN SHEARED ON HORIZONTAL STABILIZER DRIVE UNIT. REPLACED HORIZONTAL STAB CHAIN DRIVE UNIT
- [SDR 20000630AP001](https://openairdocs.org/sdr/20000630AP001), Mar 25, 2000: FLANGE. CORRODED. DURING C-CHECK, FOUND CORROSION ON RIGHT WING REAR SPAR UPPER CAP AT STATION XORS 562.390, UNDER THE INBOARD FLAP HINGE OF THE OUTBOARD FLAP. CORROSION WAS REMO
- [SDR 2000ZZZX214](https://openairdocs.org/sdr/2000ZZZX214), Sep 30, 1999: OIL CAP. MISSING. KMIA/SEQU - FLT 85 AT 17:45 Z - DISCREPANCY AFTER TAKEOFF FROM MIA, EXPERIENCED LOSS OF OIL QUANTITY, ENGINE NR 1 FROM 11 GALLONS TO SIX GALLONS WHERE IT THEN S

All 52: https://openairdocs.org/model/douglas-dc-10-40f/reports.md

## STCs that may be installed (OpenAirDocs) (112, 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 ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC SA3460NM](https://openairdocs.org/stc/SA3460NM): Installation of centerline stowage bins. Safran Cabin Inc. Lists DC-10 Series
- [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 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 ST02126AT](https://openairdocs.org/stc/ST02126AT): Courier seat installation. GDC Technics LLC
- [STC ST03879AT](https://openairdocs.org/stc/ST03879AT): Installation of Talon Aerospace Cargo Lights. Aaxico Technical Services Inc
- [STC ST03574AT](https://openairdocs.org/stc/ST03574AT): Installation of a Talon Aerospace Anti-Collision Light. Aaxico Technical Services Inc
- [STC ST04002AT](https://openairdocs.org/stc/ST04002AT): Installation of a Talon LED Replacement Wing and Tail Mounted Anti-Collision Lights. Aaxico Technical Services Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC SA2459NM](https://openairdocs.org/stc/SA2459NM): Installation of HUGHES-AVICOM video entertainment system. Burrana Inc. Lists DC-10 Series
- [STC ST01254CH](https://openairdocs.org/stc/ST01254CH): Installation of a Digital Flight Data Recorder (DFDR) System Upgrade. Amphenol Cable and Interconnect Technologies, Inc
- [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 ST01557LA](https://openairdocs.org/stc/ST01557LA): Installation of Honeywell SCS-1000 Mini-M Aero Satellite Communications System. 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 ST00689AT-D](https://openairdocs.org/stc/ST00689AT-D): Interior reconfiguration. HAECO Cabin Solutions LLC. Lists DC-10 Series
- [STC ST00690AT-D](https://openairdocs.org/stc/ST00690AT-D): Inflight entertainment system provisions. HAECO Cabin Solutions LLC. Lists DC-10 Series
- [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 SA3183SO](https://openairdocs.org/stc/SA3183SO): Installation of a replacement coalescer filter, GAI P/N 20D10-2 or 20D10-3. Purolator Facet, Inc
- [STC ST03967AT](https://openairdocs.org/stc/ST03967AT): Installation of an Avionica, Inc. avWiFi wireless router system. Archeion Holdings LLC
- [STC ST02406LA](https://openairdocs.org/stc/ST02406LA): Installation of TCAS version 7.1. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST00502LA](https://openairdocs.org/stc/ST00502LA): Installation of 9G link cargo barrier net. Thornton Technology
- [STC SA1313NM](https://openairdocs.org/stc/SA1313NM): Installation of Trans Com Video Entertainment System. Rockwell Collins Inc. Lists DC-10 Series
- [STC ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc
- [STC SA7076NM](https://openairdocs.org/stc/SA7076NM): Installation of Stretcher Carrier. Air Medic 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 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 ST02524LA](https://openairdocs.org/stc/ST02524LA): Installation of TCAS version 7.0. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA3892WE](https://openairdocs.org/stc/SA3892WE): Installation of Stowe Corp. service carts. Driessen Aircraft Interior Systems, Inc DBA Zodiac Galleys USA 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 ST00526WI-D](https://openairdocs.org/stc/ST00526WI-D): Modification of Collins VHF COMM Receiver Installation. Rockwell Collins Inc
- [STC ST00337LA](https://openairdocs.org/stc/ST00337LA): Installation of Teledyne Controls' Optical Quick Access Recorder (OQAR). Teledyne Controls
- [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 SA4843NM](https://openairdocs.org/stc/SA4843NM): Installation of Kaiser ElectroPrecision Lavatory Auto-Dump Kit System, installation on DC-10, Main Deck Lavatory positions 1, 2, 3, 4, 5, 6, 7, C and D, in accordance with FAA Approved Kaiser ElectroPrecision Drawing RYY509-027, Revision "A", dated February 7, 1990, or later FAA approved revision. Rockwell Collins Inc
- [STC ST03046AT](https://openairdocs.org/stc/ST03046AT): Installation of an ADAM Communication and Information Management System with IRIDIUM SATCOM System and three Class 2 Electronic Flight Bags in accordance with Avionics Support Group, Inc. Master Drawing List 24652-MDL, Revision H, dated July 12, 2011, or later FAA approved revision. Avionics Support Group Inc
- [STC ST00991AT-D](https://openairdocs.org/stc/ST00991AT-D): Installation and operation of The Shaw Aero Devices, Inc. 331 & 332 Series Waste Drain and 580 Series Lavatory Rinse/Fill Values. Parker Hannifin - Fluid Systems Division
- [STC ST01202WI-D](https://openairdocs.org/stc/ST01202WI-D): Modification of an existing FAA approved Collins TPR-720, TPR-900 or TPR-901 Mode S transponder installation in Part 25 Aircraft using Collins Drawing Index as listed on AML No. ST01202WI-D, latest FAA approved revision. Rockwell Collins Inc
- [STC ST02857CH](https://openairdocs.org/stc/ST02857CH): Installation of Electronic Flight Bag provisions and Aircraft Wireless LAN Unit. Canard Aerospace Corporation

All 112: https://openairdocs.org/model/douglas-dc-10-40f/stcs.md

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