# Douglas DC-10-30F

- Type: Aircraft model (FAA registry)
- Registry code: 3023503
- Manufacturer (registry): DOUGLAS
- Model: DC-10-30F
- 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: 1
- Page: https://openairdocs.org/model/douglas-dc-10-30f

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 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 2007-13-10](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 2005-02-04](https://openairdocs.org/ad/2005-02-04): Cargo compartment smoke detectors · Boeing DC-10-10F, DC-10-30F (KC-10A, KDC-10), MD-10-10F and 2 more. Effective Feb 8, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-18-15](https://openairdocs.org/ad/2004-18-15): Flight engineer's station · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Oct 19, 2004
- [AD 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

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 261: https://openairdocs.org/model/douglas-dc-10-30f/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)

- [N8201](https://openairdocs.org/aircraft/N8201): [Omega Air Inc](https://openairdocs.org/faa-owner/OMEGA%20AIR%20INC), [Selma, TX](https://openairdocs.org/faa-place/TX/Selma), S/N 48201

## NTSB investigations (4)

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 DCA07WA010](https://openairdocs.org/ntsb/DCA07WA010), Nov 17, 2006: McDonnell Douglas DC-10-30F (N305FE), Baranquilla, Colombia, incident, minor damage
- [NTSB MIA97LA125](https://openairdocs.org/ntsb/MIA97LA125), Apr 9, 1997: McDonnell Douglas DC10-30F (N310FE), Memphis, TN, substantial damage. Probable cause: A stall buffet or a high speed buffet event which occurred at an undetermined time.
- [NTSB DCA76RA017](https://openairdocs.org/ntsb/DCA76RA017), Jan 2, 1976: Douglas DC-10 (N1031F), Istanbul, TU, substantial damage
- [NTSB DCA76AZ010](https://openairdocs.org/ntsb/DCA76AZ010), Nov 12, 1975: Douglas DC-10 (N1032F), Jamaica, NY, destroyed

## FAA accident and incident reports (6)

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 20071029826869I](https://openairdocs.org/incident/20071029826869I), Oct 29, 2007: Doug DC1030F (N478CT), Valencia, No damage. (-23) During climb out the crew felt a vibration and had smoke in the cockpit. The number one engine oil quantity went to zero and the oil pressure was…
- [Accident 19970409045889A](https://openairdocs.org/incident/19970409045889A), Apr 9, 1997: Doug DC1030F (N310FE), Memphis, TN, Substantial damage. (.4)Upon arrival in Memphis the aircraft was found to have wrinkling damage to the outboard elevators and elevator counter weights. The flightcrew reported…
- [Incident 19910301007399I](https://openairdocs.org/incident/19910301007399I), Mar 1, 1991: Doug DC1030F (N1858U), Honolulu, HI, Minor damage. A section of RH wing fillet fairing departed aircraft on descent. Landed safely. Interim report pending findings.
- [Incident 19900325014619I](https://openairdocs.org/incident/19900325014619I), Mar 25, 1990: Doug DC1030F (N1858U), San Francisco, CA, Minor damage. Pieces of wheel assembly left on runway after departure. Landed safely. Failure due to manufactured defective parts
- [Incident 19880630043359I](https://openairdocs.org/incident/19880630043359I), Jun 30, 1988: Doug DC1030F (N309FE), Memphis, TN. Loud bang and flames from NR3 engine on takeoff with warning lights on. Aborted safely. Turbine bolts not torque.
- [Incident 19850223015479I](https://openairdocs.org/incident/19850223015479I), Feb 23, 1985: Doug DC1030F (N107WA), Bangor, ME. Engine shutdown due to low oil pressure. Diverted, safe landing. Broken oil line caused by chafing nr 1 engine.

## Service difficulty reports (1,152, newest 50)

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

- [SDR 2019F00027](https://openairdocs.org/sdr/2019F00027), May 21, 2018: SLIDE RAFT. DEFECTIVE. AIRCRAFT DECLARED AN IFE FOR SMOKE IN THE COCKPIT. UPON LANDING CREW DEPLOYED THE LEFT FORWARD DOOR (DOOR 1L) SLIDE/RAFT BUT IT FAILED TO FULLY INFLATE. FLIGHT 
- [SDR FDEA201708222473](https://openairdocs.org/sdr/FDEA201708222473), Aug 22, 2017: CHANNEL. CHAFED. LWR RT NR 2 ENG FAN COWL & IDG SHOW DEEP CHAFED IN STRUCTURE. TAPE/RED MARK REPAIRED AJC7415-6 CHAFED SECTION REF 55-00-01 FIG 7 SH 1-4 PG 25-28 VOL I.
- [SDR CA151123011](https://openairdocs.org/sdr/CA151123011), Nov 22, 2015: CIRCUIT BREAKER. FAULTY. (CAN) IN FLIGHT, THE AIRCRAFT EXPERIENCED A LT EMERGENCY AC BUSS ELECTRICAL FAILURE. THE FLIGHT CREW ACCOMPLISHED THE APPROPRIATE CHECKLIST PROCEDURES AND DECLA
- [SDR CA150303009](https://openairdocs.org/sdr/CA150303009), Feb 17, 2015: THRUST REVERSER. DAMAGED. (CAN) AFTER LANDING, THE FLIGHT CREW NOTICED THE NR 2 ENGINE THRUST REVERSER PRESSURE AND UNLOCK LIGHT REMAINED ILLUMINATED AFTER BEING SELECTED TO CLOSE. UPON 
- [SDR CA150212009](https://openairdocs.org/sdr/CA150212009), Feb 11, 2015: DIMMER. FAILED. (CAN) IN FLIGHT, THE FLIGHT CREW NOTICED SMOKE EMITTING FROM THE COCKPIT OVERHEAD PANEL. THE ELECTRICAL SMOKE PROCEDURE CHECKLIST WAS CARRIED OUT AND THE SMOKE 
- [SDR CA141208005](https://openairdocs.org/sdr/CA141208005), Dec 5, 2014: SWITCH. INTERMITTENT. (CAN) AT TOP OF CLIMB, THE NR 2 ENGINE OIL STRAINER CLOGGED LIGHT ILLUMINATED. CREW COMPLETED THE INFLIGHT SHUT DOWN PROCEDURE. AFTER LANDING SAFELY, THE OIL ST
- [SDR CA140321017](https://openairdocs.org/sdr/CA140321017), Mar 17, 2014: LINE. SPLIT. (CAN) THE NR 3 ENGINE WAS SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE CAUSED BY OIL DEPLETION. THE FLIGHT CONTINUED TO THE NEAREST SUITABLE AIRPORT WHERE MAINTEN
- [SDR CA131218026](https://openairdocs.org/sdr/CA131218026), Dec 13, 2013: CONTROL HANDLE. STICKING. (CAN) ON APPROACH, AFTER EXTENDING THE GEAR THE FLT DECK INDICATION FOR THE GEAR, GREEN, FAILED TO ILLUMINATE ON BOTH THE FRONT AND REAR PANELS, ONLY THE RED UN
- [SDR CA130405007](https://openairdocs.org/sdr/CA130405007), Apr 3, 2013: WHEEL HALF. CRACKED. (CAN) 0.700" LONG CRACK FOUND ON OTBD WHEEL HALF DURING ROUTINE O/H PROCEDURES. METHOD USED TO DETECT CRACK WAS HFEC. CRACK ORIGINATES ON MATING SURFACE, BETWEE
- [SDR FDEA201211063883](https://openairdocs.org/sdr/FDEA201211063883), Nov 6, 2012: SKIN. DENTED. LT OTBD FLAP BOTTOM SKIN HAS A CLUSTER OF SHARP DENTS JUST INBD OF VANE ROLLER ACCESS PANEL 557DB. INSPECTED DAMAGE AREA FOUND TO BE SERIES OF GOUGE SHARP CREAS
- [SDR CA130702005](https://openairdocs.org/sdr/CA130702005), Mar 19, 2012: ACM. FAILED. (CAN) NR 1 ACM COOLING TURBINE WHEEL SHAFT FAILED DURING GROUND RUNS, TURBINE EXITED ACFT THROUGH EXHAUST DOOR. THE ACM WAS REPLACED AND THE ACFT RETURNED TO SE
- [SDR FDEA201103261187](https://openairdocs.org/sdr/FDEA201103261187), Mar 26, 2011: SWITCH. FAILED. ON INITIAL CLIMBOUT, RECEIVED ENG 2 OIL FILTER ALERT. USED MIN IDLE POWER AS ALERT WENT ON AND OFF SEVERAL TIMES FOR SEVEAL MINUTES EVENTUALLY REMAINED ON STEAD
- [SDR FDEA201007212632](https://openairdocs.org/sdr/FDEA201007212632), Jul 21, 2010: DOOR FRAME. CRACKED. MAIN CABIN CRACK ON WEB L3 DOOR LOWER JAMB AT STA 1251 REPAIRED IAW SRM 53-50-00 FIG 19, SH 1, VOL 1.
- [SDR FDEA201006252146](https://openairdocs.org/sdr/FDEA201006252146), Jun 25, 2010: SKIN. GOUGED. EXISTING GOUGE IN FUSELAGE SKIN ADJACENT TO NOSE JACK POINT ALIGNMENT HOLE REPAIRED IAW EA 8-5330-123164.
- [SDR CA100528012](https://openairdocs.org/sdr/CA100528012), May 28, 2010: BOLT. CORRODED. DURING A RECENT SCHEDULED MX CHECK AND NR 2 ENGINE CHANGE PERSONNEL NOTICED EXCESSIVE PLAY AT THE TAIL PYLON THRUST LINK ASSY, PN AVB7320-501, LOWER ATTACHMENT.
- [SDR FDEA201005071481](https://openairdocs.org/sdr/FDEA201005071481), May 7, 2010: SILL. CORRODED. MODERATE CORROSION ON INTERIOR STRUCTURE OF LOWER AFT CARGO COMPT DOOR SILL. REPAIRED IAW EA 8-5310-123168 AND SRM 53-50-00 FIG.22, FIG.1, FIG.9, FIG.15A VOL.1.
- [SDR 22AA201000070](https://openairdocs.org/sdr/22AA201000070), May 3, 2010: PROXIMITY SWITCH. INOPERATIVE. AFTER TAKEOFF WITH GEAR HANDLE UP ALL (4) RED UNSAFE LIGHTS REMAINED ILLUMINATED. COMPLETED APPROPIATED CHECK LIST, NO CHANGE IN THE LIGHTS INDICATION. NOTIFIED
- [SDR FDEA201004291395](https://openairdocs.org/sdr/FDEA201004291395), Apr 29, 2010: SKIN. WORN. RT WING L/E DROOPED EXT FOUND DEEP WEAR ON SKIN. REPAIRED AREA IAW SRM 57-10-00, VOL I, FIG 39.
- [SDR FDEA201004261362](https://openairdocs.org/sdr/FDEA201004261362), Apr 26, 2010: RELAY. MALFUNCTIONED. AFTER TAKEOFF, ENG ANTI-ICE ON, RECEIVED AIR SYS 2 LEVEL 1 ALERT. 45 SECS LATER RECEIVED MANF 2 FAIL LEVEL 3 ALERT. COMPLIED WITH QRH & DIVERTED. AFTER 4 MINS W
- [SDR FDEA201004211265](https://openairdocs.org/sdr/FDEA201004211265), Apr 21, 2010: LONGERON. CORRODED. LT WING UPPER SIDE WING TO FUSELAGE FILLETS. AFTER REMOVING THE FILLETS 151 FT AND 151 ET WITH NRC NR N00866 THE FOLLOWING DEFECT HAVE BEEN FOUND EXFOLIATION CO
- [SDR FDEA201004131170](https://openairdocs.org/sdr/FDEA201004131170), Apr 13, 2010: PANEL. DELAMINATED. RT WING UPPER SURFACE T/E. REMOVING WING PANEL ARC0340-504 WITH N00458. FOUND DELAMINATION ON AFT EDGE. (REMOVED PART). REPAIRED DELAMINATION IAW SRM 51-71-00 P
- [SDR FDEA201003190931](https://openairdocs.org/sdr/FDEA201003190931), Mar 19, 2010: SKIN. CORRODED. CTR CARGO COMPT BILGE, 2 EA U/S ANCHOR PLATE ON SKIN. DURING ANCHOR PLATE REPLACEMENT FOUND CORROSION ON SKIN. REPAIRED SKIN IAW SRM 53-20-00 FIG.13 SH.6 VOL.1.
- [SDR FDEA201003090704](https://openairdocs.org/sdr/FDEA201003090704), Mar 9, 2010: WEB. CRACKED. COCKPIT AREA FOUND CRACKS ON WEB. REPAIRED CRACK IAW SRM 53-00-01, FIG 4, SHT 2, VOL I.
- [SDR FDEA201003040649](https://openairdocs.org/sdr/FDEA201003040649), Mar 4, 2010: WARNING LIGHT. ILLUMINATED. AT CRUISE ALTITUDE 350, RECEIVED LEVEL 3 ALERT "AIR MANF 2 FAIL" COMPLIED WITH QRH AND PROCEEDED TO NEAREST SUITABLE KOKC FOUND SYSTEM TEST GOOD PER AMM 36-23-0
- [SDR 22AA201000066](https://openairdocs.org/sdr/22AA201000066), Feb 24, 2010: SKIN. CRACKED. DURING "C" CHECK, LOWER FUSELAGE, ALONG LONGERON 44L, ALONG STA 1701 FUSELAGE SKIN FOUND CRACKED THROUGH. NON-ROUTINE NR 0425, CRACK AREA AT LONGERON 44L ALONG 
- [SDR 22AA201000065](https://openairdocs.org/sdr/22AA201000065), Feb 24, 2010: ROLLER TRAY. CORRODED. DURING "C" CHECK, CTR CARGO COMPARTMENT LT OTBD CARGO ROLLER TRAY FOUND CORRODED AFTER CARGO SIDE GUIDE RAIL REMOVED TO FACILITATE FOR STRUCTURE REPAIR AT STA 1
- [SDR 22AA201000064](https://openairdocs.org/sdr/22AA201000064), Feb 24, 2010: SEAT TRACK. CORRODED. DURING "C" CHECK, CABIN CORROSION FOUND ON INNER SURFACE OF SEAT TRACK AT STATION 1139 TO STATION 1156, X= 47.5. NON-ROUTINE NR 0314, SEAT TRACK FROM STATION 11
- [SDR 22AA201000063](https://openairdocs.org/sdr/22AA201000063), Feb 24, 2010: INTERCOSTAL. CORRODED. DURING "C" CHECK, CTR CARGO COMPARTMENT BILGE, INTERCOASTAL FOUND CORRODED AFTER SIDE GUIDE RAIL, REMOVED TO FACILITATE FOR STRUCTURE REPAIR AT STA 1764, L42 TO
- [SDR 22AA201000062](https://openairdocs.org/sdr/22AA201000062), Feb 24, 2010: SKIN. CORRODED. DURING "C" CHECK, CABIN CORROSION FOUND ON CTR WING SECTION SURFACE AT STA 1156 TO STA 1221 X = 107.5 (RT). NON-ROUTINE 0220, CTR WING SECTION SURFACE AT STA 11
- [SDR 22AA201000061](https://openairdocs.org/sdr/22AA201000061), Feb 24, 2010: RIB. CRACKED. DURING "C" CHECK, NR 2 ENGINE RT CORE COWL AFT RIB LOWER SIDE FOUND WITH CRACK. NON-ROUTINE NR 0297, CRACK AREA AT NR 2 ENGINE RT CORE COWL AFT RIB LOWER SIDE A
- [SDR 22AA201000060](https://openairdocs.org/sdr/22AA201000060), Feb 24, 2010: RIB. CRACKED. DURING "C" CHECK, NR 2 ENGINE LT CORE COWL AFT RIB LOWER SIDE FOUND WITH CRACK. NON-ROUTINE NR 0296, CRACK AREA AT NR 2 ENGINE LT CORE COWL AFT RIB LOWER SIDE A
- [SDR 22AA201000059](https://openairdocs.org/sdr/22AA201000059), Feb 24, 2010: LONGERON. CRACKED. DURING "C" CHECK, NR 2 ENG RT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0202, CRACKED UPPER LONGERON AT NR 2 ENGINE RT CORE COWL AREA REPAIRED I
- [SDR 22AA201000057](https://openairdocs.org/sdr/22AA201000057), Feb 24, 2010: SKIN. WORN. DURING "C" CHECK, NR 2 ENG LT CORE COWL UPPER AFT RUB STRIP FOUND WORN TO COWLING SKIN. NON-ROUTINE NR 0198, WORN COWLING SKIN AREA AT NR 2 ENG LT CORE COWL UPP
- [SDR 22AA201000056](https://openairdocs.org/sdr/22AA201000056), Feb 24, 2010: LONGERON. CRACKED. DURING "C" CHECK, NR 2 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0197, CRACK AREA AT NR 2 ENGINE LT CORE COWL UPPER LONGERON AREA REPA
- [SDR 22AA201000055](https://openairdocs.org/sdr/22AA201000055), Feb 24, 2010: LONGERON. CRACKED. DURING "C" CHECK, NR 2 ENGINE LT CORE COWL LOWER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0196, CRACK AREA AT NR 2 ENGINE LT CORE COWL LOWER LONGERON AREA REPA
- [SDR 22AA201000054](https://openairdocs.org/sdr/22AA201000054), Feb 24, 2010: RIB. WORN. DURING "C" CHECK, NR 2 ENGINE LT CORE COWL AFT MOST RIB FOUND WITH WEAR MARK. NON-ROUTINE NR 0195, WORN AREA AT NR 2 ENGINE LT CORE COWL AFT MOST RIB AREA REPAI
- [SDR 22AA201000053](https://openairdocs.org/sdr/22AA201000053), Feb 24, 2010: LONGERON. CRACKED. DURING "C" CHECK, NR 3 ENGINE RT CORE COWL LOWER LONGERON CRACKED AT APPROX AT MID AND AFT FRAME SECTION. NON-ROUTINE NR 0163, CRACK AREA AT MID AND AFT SECTION
- [SDR 22AA201000052](https://openairdocs.org/sdr/22AA201000052), Feb 24, 2010: LONGERON. CRACKED. DURING "C" CHECK, NR 3 ENGINE LT CORE COWL LOWER LONGERON AFT SECTION FOUND CRACKED. NON-ROUTINE NR 0159, CRACK AREA AT NR 3 ENGINE LT CORE COWL LOWER LONGERON 
- [SDR 22AA201000051](https://openairdocs.org/sdr/22AA201000051), Feb 24, 2010: LONGERON. CRACKED. DURING "C" CHECK, NR 1 ENG, RT CORE COWL LOWER LONGERON AND STRAP FOUND CRACKED. NON-ROUTINE NR 0125, CRACKED STRAP AND LOWER LONGERON AT NR 1 ENGINE RT CORE CO
- [SDR 22AA201000050](https://openairdocs.org/sdr/22AA201000050), Feb 24, 2010: LONGERON. CRACKED. DURING "C" CHECK, NR 1 ENG LT CORE COWL LOWER LONGERON FOUND CRACKED. NON-ROUTINE NR 0124, CRACK AREA AT NR 1 ENGINE LT CORE COWL LOWER LONGERON AREA REPAIRED I
- [SDR 22AA201000049](https://openairdocs.org/sdr/22AA201000049), Feb 24, 2010: LONGERON. CRACKED. DURING "C" CHECK, NR 1 ENGINE LT CORE COWL UPPER LONGERON FOUND CRACK. NON-ROUTINE NR 0123, CRACK AREA AT NR 1 ENG LT CORE COWL UPPER LONGERON AREA REPAIR IAW E
- [SDR FDEA201002230494](https://openairdocs.org/sdr/FDEA201002230494), Feb 23, 2010: CLAMP. LOOSE. BASED ON MX REPORT, DECIDED TO GIVE A LITTLE EXTRA TIME FOR ACCELERATION . IT WAS NECESSARY TO GO FULL QUADRANT TO GET CLOSE TO TAKEOFF POWER. WHEN THE AUTOFLIG
- [SDR FDEA201002180447](https://openairdocs.org/sdr/FDEA201002180447), Feb 18, 2010: SKIN. DENTED. RT HORIZONTAL STAB EXTERIOR SURFACE FOUND DEEP NICK ON SKIN. (REMOVED PART). REPAIRED EDGE FWD SKIN IAW SRM 55-10-00 FIG.13 VOL.1, REPAIRED LEADING REAR SKIN IA
- [SDR FDEA201002180448](https://openairdocs.org/sdr/FDEA201002180448), Feb 18, 2010: SKIN. WORN. LT WING L/E DEEP WEARS & 4 EA FASTENERS U/S ON LOWER SKIN. REPAIRED AREA IAW EA 8-5710-137482 & SRM 57-10-00 FIG 83, VOL I.
- [SDR FDEA201002150426](https://openairdocs.org/sdr/FDEA201002150426), Feb 15, 2010: SKIN. CRACKED. LT WING INBD FLAP UPPER SURFACE FOUND CRACK ON SKIN. REPAIRED SKIN IAW SRM 57-10-00, FIG 85, SHT 2 & 4 VOL I.
- [SDR 22AA201000048](https://openairdocs.org/sdr/22AA201000048), Feb 13, 2010: FRAME. CORRODED. DURING "C" CHECK , AFT CARGO COMPARTMENT BILGE AREA FRAME (STA 1996) LOWER CHORD CORRODED AT LBL 15 TO RBL 15 AS MARKED. NON-ROUTINE NR 0610, AFT CARGO COMPARTM
- [SDR 22AA201000047](https://openairdocs.org/sdr/22AA201000047), Feb 13, 2010: LONGERON. CRACKED. DURING "C" CHECK, NR 2 ENG RT CORE COWL LOWER LONGERON AND STRAP FOUND CRACKED. NON-ROUTINE NR 394, CRACKED LONGERON AND STRAP AT NR 2 ENG RT CORE COWL LOWER LO
- [SDR 22AA201000046](https://openairdocs.org/sdr/22AA201000046), Feb 13, 2010: LONGERON. CRACKED. DURING "C" CHECK, NR 2 ENG RT CORE COWL UPPER LONGERON FOUND WITH CRACK AT 02 LOCATIONS. NON-ROUTINE NR 392, CRACKED LONGERON 02 EACH LOCATIONS AT NR 2 ENGINE R
- [SDR 22AA201000045](https://openairdocs.org/sdr/22AA201000045), Feb 13, 2010: LONGERON. CRACKED. DURING "C" CHECK, NR 1 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 324, CRACKED NR 1 ENG LT CORE COWL UPPER LONGERON AREA REPAIRED IAW E
- [SDR 22AA201000044](https://openairdocs.org/sdr/22AA201000044), Feb 13, 2010: LONGERON. CRACKED. DURING "C" CHECK, NR 3 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 323, CRACKED LONGERON AT NR 3 ENG LT CORE COWL UPPER AREA REPAIRED IA

All 1,152: https://openairdocs.org/model/douglas-dc-10-30f/reports.md

## STCs that may be installed (OpenAirDocs) (167, 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 ST09142SC](https://openairdocs.org/stc/ST09142SC): Installation of a cargo/executive "combi" interior. Omega Air 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 SA2175NM](https://openairdocs.org/stc/SA2175NM): Installation of the Centerline Overhead Stowage Retrofit Kit. 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 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 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 ST01986CH](https://openairdocs.org/stc/ST01986CH): Installation of a Honeywell RESCU 406AF Emergency Locator Transmitter (ELT) system. Honeywell International Inc
- [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 SA5672SW-D](https://openairdocs.org/stc/SA5672SW-D): Modification of air to air heat exchanger (P/N 187900-9). Honeywell International Inc
- [STC ST00178MC](https://openairdocs.org/stc/ST00178MC): Modification of an existing APX-119 ADS-B Out (DO-260A) transponder installation, CDUA-7000F software upgrade, and GPS-4000S upgrade. Rockwell Collins 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 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 ST01120LA](https://openairdocs.org/stc/ST01120LA): Installation of insulation blankets. Triumph Insulation Systems LLC
- [STC ST10619SC](https://openairdocs.org/stc/ST10619SC): Installation of a Model 71180 Pedestal Table. Enflite Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST00399DE](https://openairdocs.org/stc/ST00399DE): Installation of nose radome shell assembly. The NORDAM Group 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 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 SA5466NM](https://openairdocs.org/stc/SA5466NM): Installation of Telair International cargo loading systems. Telair International LLC
- [STC ST01347LA](https://openairdocs.org/stc/ST01347LA): Installation of a lower lobe anti-rollout latch Telair part number 92036-1, -2. 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

All 167: https://openairdocs.org/model/douglas-dc-10-30f/stcs.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Mcdonnell Douglas DC-10-30F](https://openairdocs.org/model/mcdonnell-douglas-dc-10-30f): 12 registered aircraft, registry code 3023504
- [Mcdonnell Douglas DC-10-30F (KDC-10)](https://openairdocs.org/model/mcdonnell-douglas-dc-10-30f-kdc-10): 1 registered aircraft, registry code 3023505

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