# N141WE: Douglas DC-10-40F

- Status: Valid registration
- Airframe: [Douglas DC-10-40F](https://openairdocs.org/model/douglas-dc-10-40f) (registry code 3023507, 380 seats)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 46661
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Certificate issued: December 5, 2023
- Expires: December 31, 2030
- Mode S code: A0A860
- Registered owner: [Omega Air Inc](https://openairdocs.org/faa-owner/OMEGA%20AIR%20INC)
- Location: [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio)
- Owner type: Corporation
- Owner's area on the map: 29.5553° N, 98.3640° W: Placed by OpenAirDocs at the center of ZIP code 78233, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=141WE
- Page: https://openairdocs.org/aircraft/N141WE

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 162 in force

### Matched by airframe (Douglas DC-10-40F)

- [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/aircraft/N141WE/ads.md

## Information bulletins (advisory) (3 in force)

- [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

## 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 (26)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR 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 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 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 20001128AP001](https://openairdocs.org/sdr/20001128AP001), Jun 21, 2000: SPAR CAP. CORRODED. DURING C-CHECK, FOUND CORROSION ON LT WING UPPER REAR SPAR CAP AFT FLANGE AT THREE LOCATIONS, STATIONS ORS 433, 451 AND 455. FOUND CORROSION WAS REMOVED AND FAS
- [SDR 20001127AP015](https://openairdocs.org/sdr/20001127AP015), Jun 21, 2000: SKIN. CORRODED. DURING C-CHECK, FOUND CORROSION ON THE LT WING TRAILING EDGE UPPER SKIN AT STATION XRS 230. CORROSION WAS REMOVED AND FASTENERS WERE REPLACED IAW EO CH-00-009 A
- [SDR 20001127AP014](https://openairdocs.org/sdr/20001127AP014), Jun 21, 2000: SKIN. CORRODED. DURING C-CHECK, FOUND CORROSION ON THE RIGHT WING FIXED LEADING EDGE AT STATION XOS 420-25. CORROSION WAS BLENDED OUT AND FASTENERS WERE REPLACED IAW EO CH-00-0
- [SDR 20001127AP013](https://openairdocs.org/sdr/20001127AP013), Jun 21, 2000: SPACER. CORRODED. DURING C-CHECK, THE RIGHT MLG UPPER SPACER IS CRACKED BY CORROSION AT STATION XW=212 TO XW=214. INTERIM REPAIR WAS MADE IAW EO CH-00-0010 AND BOEING TLX CAC-FCO
- [SDR 20001127AP012](https://openairdocs.org/sdr/20001127AP012), Jun 21, 2000: SKIN. CORRODED. DURING C-CHECK, FOUND CORROSIONI ON LT WING LOWER AFT SKIN AT STATION XORS 340.00. FOUND CORROSION BLENDED OUT AND SHOTPEENED IAW EO CH-00-0011 AND BOEING TLX T
- [SDR 20001127AP011](https://openairdocs.org/sdr/20001127AP011), Jun 21, 2000: SPAR CAP. CORRODED. DURING C-CHECK, FOUND CORROSION ON RIGHT WING REAR SPAR CAP AFT TANG UPPER SURFACE BETWEEN STATION XORS 917 TO 885. FOUND CORROSION BLENDED OUT IAW EO CH-00-012

## STCs that may be installed (OpenAirDocs) (112, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Douglas DC-10-40F)

- [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/aircraft/N141WE/stcs.md

## Related

- Other Douglas DC-10-40F aircraft: https://openairdocs.org/model/douglas-dc-10-40f/aircraft.md

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