# N17085: 1975 Mcdonnell-Douglas DC-10-30

- Status: Valid registration
- Airframe: [Mcdonnell-Douglas DC-10-30](https://openairdocs.org/model/mcdonnell-douglas-dc-10-30) (registry code 3023501, 345 seats)
- Engine: [GE CF6-50 series](https://openairdocs.org/engine/ge-cf6-50-series) (registry code 30018)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE) (The Boeing Company), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (General Electric Company) (OpenAirDocs)
- Serial number: 47957
- Year built: 1975
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 31, 1997
- Certificate issued: May 12, 2014
- Expires: May 31, 2027
- Mode S code: A11CBB
- Registered owner: [Bc Aircraft Leasing LLC](https://openairdocs.org/faa-owner/BC%20AIRCRAFT%20LEASING%20LLC)
- Location: [Albuquerque, NM](https://openairdocs.org/faa-place/NM/Albuquerque)
- Owner type: LLC
- Owner's area on the map: 35.0071° N, 106.6098° W: Placed by OpenAirDocs at the center of ZIP code 87106, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17085
- Page: https://openairdocs.org/aircraft/N17085

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. The registry lists only the engine series, so ADs for every GE CF6-50 model are included.

## ADs that may apply (OpenAirDocs): 282 in force

### Matched by airframe (Mcdonnell-Douglas DC-10-30)

- [AD 2026-13-15](https://openairdocs.org/ad/2026-13-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jul 1, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-23-53](https://openairdocs.org/ad/2025-23-53): Nacelles/pylons · Boeing MD-11, MD-11F, MD-10-10F and 8 more. Effective Dec 1, 2025
- [AD 2023-12-15](https://openairdocs.org/ad/2023-12-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jun 21, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2021-08-10](https://openairdocs.org/ad/2021-08-10): Nacelles/pylons · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective May 25, 2021
- [AD 2020-22-15](https://openairdocs.org/ad/2020-22-15): Fuselage · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Dec 18, 2020
- [AD 2018-22-10](https://openairdocs.org/ad/2018-22-10): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Dec 12, 2018
- [AD 2015-02-05](https://openairdocs.org/ad/2015-02-05): Navigation · Boeing 717-200, DC-10-10, DC-10-10F and 13 more. Effective Mar 5, 2015
- [AD 2014-21-05](https://openairdocs.org/ad/2014-21-05): Fuselage · Boeing DC-10-10, DC-10-10F, DC-10-30 and 4 more. Effective Dec 2, 2014
- [AD 2012-19-03](https://openairdocs.org/ad/2012-19-03): Fuselage · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Nov 5, 2012
- [AD 2011-21-08](https://openairdocs.org/ad/2011-21-08): Equipment/Furnishings · ATR - GIE Avions de Transport Régional ATR42-200, ATR42-300, ATR42-320 and 202 more. Effective Nov 23, 2011
- [AD 2011-12-01](https://openairdocs.org/ad/2011-12-01): Equipment/Furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 268 more. Effective Aug 1, 2011
- [AD 2011-11-05](https://openairdocs.org/ad/2011-11-05): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 10 more. Effective Jul 6, 2011
- [AD 2010-21-13](https://openairdocs.org/ad/2010-21-13): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-30 and 3 more. Effective Nov 18, 2010
- [AD 2010-20-13](https://openairdocs.org/ad/2010-20-13): Fuel · Boeing DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40 and 2 more. Effective Nov 9, 2010
- [AD 2010-20-14](https://openairdocs.org/ad/2010-20-14): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Nov 5, 2010
- [AD 2010-09-12](https://openairdocs.org/ad/2010-09-12): Fuel · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Jun 8, 2010
- [AD 2009-21-10 R1](https://openairdocs.org/ad/2009-21-10-R1): Oxygen · Airbus A300 B4-605R, A300 B4-620, A300 B4-622 and 138 more. Effective Feb 4, 2010
- [AD 2008-06-21 R1](https://openairdocs.org/ad/2008-06-21-R1): Fuel tank systems · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Dec 10, 2009
- [AD 2009-03-02](https://openairdocs.org/ad/2009-03-02): Auxiliary hydraulic pumps · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 31, 2009
- [AD 2008-17-16](https://openairdocs.org/ad/2008-17-16): Fuel boost pump · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Oct 2, 2008
- [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008
- [AD 2007-25-20](https://openairdocs.org/ad/2007-25-20): Thrust reverser command wiring · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Jan 22, 2008
- [AD 2007-19-17](https://openairdocs.org/ad/2007-19-17): System 3 hydraulic piping · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Oct 26, 2007
- [AD 2007-19-02](https://openairdocs.org/ad/2007-19-02): Fuel tank and the fuel transfer pump housing flange · Boeing DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40 and 4 more. Effective Oct 17, 2007
- [AD 2007-13-10](https://openairdocs.org/ad/2007-13-10): Fuel pump wire harness · Boeing DC-10-30 and DC-10-30F (KC-10A, KDC-10). Effective Aug 3, 2007
- [AD 2007-11-15](https://openairdocs.org/ad/2007-11-15): Center main wheel well · Boeing DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40 and 2 more. Effective Jul 5, 2007
- [AD 2007-10-12](https://openairdocs.org/ad/2007-10-12): Reinforced flight deck door · Reinforced cockpit door (Safran Cabin STC ST01335LA or 2 others). Effective Jun 27, 2007
- [AD 2007-04-17](https://openairdocs.org/ad/2007-04-17): Control modules of the fire detection systems · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Mar 23, 2007
- [AD 2006-19-03](https://openairdocs.org/ad/2006-19-03): Fabrication and installation of a wire harness guard in the right wheel well of the main  
 landing gear (MLG) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Oct 17, 2006
- [AD 2006-16-12](https://openairdocs.org/ad/2006-16-12): Fuel tanks 1, 2, and 3 · Boeing DC-10-10, DC-10-10F, DC-10-30 and 3 more. Effective Sep 13, 2006
- [AD 2006-04-04](https://openairdocs.org/ad/2006-04-04): Smoke detectors · ATR - GIE Avions de Transport Régional ATR42-200, ATR42-300, ATR42-320 and 37 more. Effective Mar 24, 2006
- [AD 2006-03-13](https://openairdocs.org/ad/2006-03-13): Inboard and outboard hinge fittings · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 16, 2006
- [AD 2006-02-11](https://openairdocs.org/ad/2006-02-11): Drain holes of the pitot tubes · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 3, 2006
- [AD 2005-20-15](https://openairdocs.org/ad/2005-20-15): Rudder pedal torque tube assembly · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Nov 10, 2005
- [AD 2005-17-04](https://openairdocs.org/ad/2005-17-04): Fire extinguishing system · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Sep 26, 2005
- [AD 2005-15-12](https://openairdocs.org/ad/2005-15-12): Exterior emergency control handle assemblies of the forward passenger doors · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Aug 30, 2005
- [AD 2005-15-03](https://openairdocs.org/ad/2005-15-03): Exterior emergency control handle assemblies · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Aug 25, 2005
- [AD 2005-14-10](https://openairdocs.org/ad/2005-14-10): Structural inspections · Boeing DC-10-10, DC-10-10F, DC-10-15 and 4 more. Effective Aug 18, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-18-15](https://openairdocs.org/ad/2004-18-15): Flight engineer's station · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Oct 19, 2004
- [AD 2004-10-12](https://openairdocs.org/ad/2004-10-12): Power Feeder Cable Assembly of the Auxiliary Power Unit (APU) · Boeing DC-10-30. Effective Jun 25, 2004
- [AD 2004-05-06](https://openairdocs.org/ad/2004-05-06): Number one passenger door slide · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Apr 7, 2004
- [AD 2004-02-06](https://openairdocs.org/ad/2004-02-06): Forward aft bracket · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Mar 5, 2004
- [AD 2003-25-13](https://openairdocs.org/ad/2003-25-13): Power feeder cables · Boeing DC-10-10, DC-10-10F, DC-10-15 and 4 more. Effective Jan 27, 2004
- [AD 2003-24-10](https://openairdocs.org/ad/2003-24-10): Rudder pedal arm assembly · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 more. Effective Jan 8, 2004
- [AD 2003-03-15 R1](https://openairdocs.org/ad/2003-03-15-R1): Airplane Flight Manual (AFM) - oxygen masks · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 90 more. Effective Dec 22, 2003
- [AD 2003-19-05](https://openairdocs.org/ad/2003-19-05): Inboard and outboard flaps · Boeing DC-10-10, DC-10-10F, DC-10-15 and 6 more. Effective Oct 27, 2003
- [AD 2003-17-07 R1](https://openairdocs.org/ad/2003-17-07-R1): Auxiliary power unit (APU) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 57 more. Effective Sep 24, 2003

### Matched by engine (GE CF6-50 series)

- [AD 2023-04-11](https://openairdocs.org/ad/2023-04-11): Turbine Section · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 28, 2023
- [AD 2011-23-04](https://openairdocs.org/ad/2011-23-04): Forward engine mount assembly side links · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Dec 12, 2011
- [AD 2011-07-01](https://openairdocs.org/ad/2011-07-01): Forward and aft centerbodies · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 22, 2011
- [AD 2007-11-18 R1](https://openairdocs.org/ad/2007-11-18-R1): Forward fan stator cases · General Electric CF6-50C, CF6-50C1 and CF6-50C2. Effective Jan 4, 2010
- [AD 2008-02-17](https://openairdocs.org/ad/2008-02-17): Thrust reverser actuation systems · General Electric CF6-50A, CF6-50C, CF6-50C1 and 16 more. Effective Feb 28, 2008
- [AD 2007-19-06](https://openairdocs.org/ad/2007-19-06): Compressor discharge pressure (CDP) · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Oct 23, 2007
- [AD 2005-26-06](https://openairdocs.org/ad/2005-26-06): Low pressure turbine (LPT) stage 2 interstage seal assemblies · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jan 26, 2006
- [AD 2005-07-05](https://openairdocs.org/ad/2005-07-05): Low pressure turbine (LPT) · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective May 4, 2005
- [AD 2005-08-04](https://openairdocs.org/ad/2005-08-04): Low-cycle-fatigue (LCF) · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 28, 2005
- [AD 2003-09-06](https://openairdocs.org/ad/2003-09-06): Low pressure turbine (LPT) · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more. Effective Jun 3, 2003
- [AD 2003-02-07](https://openairdocs.org/ad/2003-02-07): Low pressure turbine (LPT) shrouds · General Electric CF6-50A, CF6-50C, CF6-50C1 and 30 more. Effective Mar 3, 2003
- [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08): High pressure compressor rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Jan 23, 2003
- [AD 2002-05-03](https://openairdocs.org/ad/2002-05-03): Life-Limited Rotating Parts · General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective Apr 12, 2002
- [AD 2002-02-09](https://openairdocs.org/ad/2002-02-09): Low Pressure Turbine Rotor (LPTR) Stage 2 Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Mar 15, 2002
- [AD 2001-12-20](https://openairdocs.org/ad/2001-12-20): Air Ducts and Reworked Mating Hardware · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more. Effective Jul 26, 2001
- [AD 2001-04-16](https://openairdocs.org/ad/2001-04-16): Low Pressure Turbine (LPT) Nozzle Lock Assembly Studs · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more. Effective Mar 21, 2001
- [AD 2000-11-12](https://openairdocs.org/ad/2000-11-12): High Pressure Compressor Disk Lock Slots · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Aug 14, 2000
- [AD 98-22-06](https://openairdocs.org/ad/98-22-06): Fan Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 41 more. Effective Nov 23, 1998
- [AD 97-22-14](https://openairdocs.org/ad/97-22-14): (HPCR) 3-9 Spool · General Electric CF6-50A, CF6-50C, CF6-50C1 and 29 more. Effective Nov 17, 1997
- [AD 95-08-03](https://openairdocs.org/ad/95-08-03): High Pressure Turbine Rotor Stage 2 Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jun 12, 1995
- [AD 91-10-03 R1](https://openairdocs.org/ad/91-10-03-R1): High Pressure Compressor · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 28, 1995
- [AD 94-08-05](https://openairdocs.org/ad/94-08-05): Fan Stator Case · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jul 5, 1994
- [AD 94-09-18](https://openairdocs.org/ad/94-09-18): High Pressure Turbine Disk · General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective Jun 6, 1994
- [AD 93-14-18](https://openairdocs.org/ad/93-14-18): High pressure turbine (HPT) thermal shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Oct 4, 1993
- [AD 93-13-10](https://openairdocs.org/ad/93-13-10): Compressor Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Sep 21, 1993
- [AD 91-23-13](https://openairdocs.org/ad/91-23-13): Fan Disks · General Electric CF6-50A, CF6-50C, CF6-50C1 and 12 more. Effective Nov 22, 1991
- [AD 91-15-16](https://openairdocs.org/ad/91-15-16): High Pressure Turbine Thermal Shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Sep 4, 1991
- [AD 91-01-04](https://openairdocs.org/ad/91-01-04): Fan Disk · General Electric CF6-45A, CF6-45A2, CF6-50A and 19 more. Effective Jan 22, 1991
- [AD 90-23-15](https://openairdocs.org/ad/90-23-15): Turbine Mid-frame · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Dec 6, 1990
- [AD 90-19-09](https://openairdocs.org/ad/90-19-09): High Pressure Turbine Stage One Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Oct 1, 1990
- [AD 90-12-06](https://openairdocs.org/ad/90-12-06): Low Pressure Turbine · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jun 25, 1990
- [AD 89-01-02](https://openairdocs.org/ad/89-01-02): High Pressure Turbine Stage 2 Disks · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more. Effective Dec 29, 1988
- [AD 87-23-06](https://openairdocs.org/ad/87-23-06): High Pressure Turbine Impeller Spacer · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Nov 5, 1987
- [AD 86-12-03](https://openairdocs.org/ad/86-12-03): High Pressure Turbine Rotor (HPTR) Stage 1 Disk · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Jun 29, 1986
- [AD 84-01-01](https://openairdocs.org/ad/84-01-01): Compressor Assemblies · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Feb 10, 1984
- [AD 82-25-08](https://openairdocs.org/ad/82-25-08): HPT Spacer/Impeller · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Dec 30, 1982
- [AD 82-20-03](https://openairdocs.org/ad/82-20-03): Inspect First Stage HPT Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Oct 31, 1982
- [AD 77-08-08](https://openairdocs.org/ad/77-08-08): Compressor · General Electric CF6-50A, CF6-50C, CF6-50C1 and 2 more. Effective Feb 14, 1980
- [AD 76-17-01](https://openairdocs.org/ad/76-17-01): High Pressure Compressor · General Electric CF6-50A, CF6-50C, CF6-50E and 1 more. Effective Aug 20, 1976
- [AD 76-05-10](https://openairdocs.org/ad/76-05-10): Turbofan Engines · General Electric CF6-50A, CF6-50C, CF6-50E and 3 more. Effective Mar 24, 1976
- [AD 85-25-56 R1](https://openairdocs.org/ad/85-25-56-R1): Seventh Stage Low Pressure Turbine (LPT) Cooling Air Manifold Tube · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more
- [AD 79-13-09](https://openairdocs.org/ad/79-13-09): Compressor Rotor Spools · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more

### 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
- [AD 2012-02-07](https://openairdocs.org/ad/2012-02-07) (historical): LPT rotor stage 3 disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Mar 6, 2012
- [AD 2011-18-01](https://openairdocs.org/ad/2011-18-01) (historical): LPT rotor stage 3 disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Sep 26, 2011
- [AD 2011-02-07](https://openairdocs.org/ad/2011-02-07) (historical): Rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Feb 22, 2011
- [AD 2010-12-10](https://openairdocs.org/ad/2010-12-10) (historical): High-pressure turbine (HPT) · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Jun 24, 2010
- [AD 2010-06-15](https://openairdocs.org/ad/2010-06-15) (historical): Low-pressure turbine (LPT) stage 3 disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 9 more. Effective Apr 1, 2010
- [AD 2009-04-17](https://openairdocs.org/ad/2009-04-17) (historical): Long fixed core exhaust nozzle (LFCEN) assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 10 more. Effective Apr 2, 2009
- [AD 2007-11-18](https://openairdocs.org/ad/2007-11-18) (historical): Forward fan stator cases · General Electric CF6-50C, CF6-50C1, CF6-50C2 and 1 more. Effective Jul 5, 2007
- [AD 2006-12-24](https://openairdocs.org/ad/2006-12-24) (historical): Five-link forward mount assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Jul 21, 2006
- [AD 2000-08-11](https://openairdocs.org/ad/2000-08-11) (historical): Life-limited Parts · General Electric Aircraft Engines CF6-45 Series (all), CF6-50 Series (all) and CF6-6 Series (all). Effective Oct 23, 2000
- [AD 2000-20-02](https://openairdocs.org/ad/2000-20-02) (historical): Turbine Nozzle Lock Assemblies · General Electric CF6-50A, CF6-50C, CF6-50C1 and 8 more. Effective Oct 17, 2000
- [AD 2000-16-12](https://openairdocs.org/ad/2000-16-12) (historical): High Pressure Compressor Rotor Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Sep 5, 2000
- [AD 99-24-15](https://openairdocs.org/ad/99-24-15) (historical): High Pressure Compressor Rotor (HPCR) Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Jan 28, 2000
- [AD 99-18-20](https://openairdocs.org/ad/99-18-20) (historical): Inadvertent In-flight Thrust Reverser · General Electric Aircraft Engines CF6-50 Series (all), CF6-80A1, CF6-80A3 and 6 more. Effective Nov 2, 1999
- [AD 99-08-18](https://openairdocs.org/ad/99-08-18) (historical): General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective May 13, 1999
- [AD 95-17-15](https://openairdocs.org/ad/95-17-15) (historical): Engine Mount Pylon · General Electric Aircraft Engines CF6-45 Series (all) and CF6-50 Series (all). Effective Oct 10, 1995

All 319: https://openairdocs.org/aircraft/N17085/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

None matched to N17085.

## FAA accident and incident reports

None matched to N17085.

## Service difficulty reports (33)

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 CNMA20060032](https://openairdocs.org/sdr/CNMA20060032), Dec 18, 2006: BATTERY PACK. DISCHARGED. WHILE TESTING EMERGENCY LIGHTS MID-CABIN BATTERY FAILED. REMOVED AND REPLACED MID-CABIN EMERGENCY LIGHT BATTERY PACK OPS CHECK GOOD IAW MM 33-51.
- [SDR CNMA20060010](https://openairdocs.org/sdr/CNMA20060010), May 15, 2006: ROTOR. DAMAGED. NR 3 ENGINE 3RD STAGE LPT ROTOR IS RUBBING ON 4TH STAGE ROTOR. REMOVED AND REPLACED ENGINE S/N 517720.
- [SDR 2005000011](https://openairdocs.org/sdr/2005000011), Jul 19, 2005: PUMP. FAILED. REJECTED TAKE OFF AT 80 KNOTS NR 2 ENGINE WILL NOT MAKE POWER ONLY WENT TO 110 PERCENT N1 LOWER THAN 1&3. CORRECTIVE ACTION REMOVED AND REPLACED THE FUEL PUMP A
- [SDR 2005000004](https://openairdocs.org/sdr/2005000004), May 18, 2005: POWER SUPPLY. FAILED. ON PRE-FLIGHT, FOUND EMERGENCY LIGHT TEST LAMP INOP (GREEN LIGHT ON OVERHEAD PANEL). REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY PER MM 33-51.
- [SDR 2004000012](https://openairdocs.org/sdr/2004000012), Oct 4, 2004: FLOOR PANEL. OVERHEATED. EXCESSIVE HEAT COMING FROM FLOOR AND WALL FORWARD AND AFT OF L-2 DOOR. TROUBLESHOOTING AS OF 10/5/04.
- [SDR 2004000013](https://openairdocs.org/sdr/2004000013), Oct 3, 2004: DUCT. BLOWN. AIRCRAFT DIVERTED TO BWI ,DUE TO BLEED AIR LEAK IN L2 DOOR AREA. NR 3 PNEUMATIC SYSTEM ALREADY DEFERRED. REPLACED BLOWN DUCT IN FWD CARGO AREA.
- [SDR CNMA200300007](https://openairdocs.org/sdr/CNMA200300007), Dec 2, 2003: BATTERY PACK. FAILED. EMERGENCY EGRESS LIGHTS FAIL TO TEST. BATTERY PACK FAILED.
- [SDR CALA0100815](https://openairdocs.org/sdr/CALA0100815), Aug 28, 2001: SKIN. CRACKED. INSPECTION FOUND A 1" CRACK IN FORWARD CARGO DOOR SKIN(DOUBLER) ON LATCH ACCESSORY DOOR CUTOUT AREA. THE CRACKED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTA
- [SDR CALA0100814](https://openairdocs.org/sdr/CALA0100814), Aug 28, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND MAIN DECK SEAT TRACK CORRODED AT Y = 1860, X = -60.00, JUST AFT OF R-4 ATTENDANT SEAT. THE CORRODED SECTION OF SEAT TRACK WAS CUT OUT AND A NEW
- [SDR CALA0100808](https://openairdocs.org/sdr/CALA0100808), Aug 26, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND MAIN DECK SEAT TRACK CORRODED AT X = 107.25 AND Y = 800-824. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK SECTION WAS SP
- [SDR CALA0001209](https://openairdocs.org/sdr/CALA0001209), Aug 5, 2000: PANEL. DELAMINATED. INSPECTION FOUND NR 2 ENGINE NOSE COWL PANEL 363AL DELAMINATED. THE PANEL WAS REPLACED IAW MM 20-50-02.
- [SDR CALA9900784](https://openairdocs.org/sdr/CALA9900784), Jul 2, 1999: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN NR 2 ENGINE PYLON SKIN WITH LOOSE FASTENERS ON PYLON FIN. THE SKIN WAS REPAIRED IAW SRM 54-20-00, FIGURE 6 AND FASTENERS WERE
- [SDR CALA9900783](https://openairdocs.org/sdr/CALA9900783), Jul 2, 1999: SKIN. CORRODED. INSPECTION FOUND LT WING O/B AILERON UPPER SKIN CORRODED AT STA 917. THE AILERON WAS REPLACED IAW MM 27-10-02.
- [SDR CALA9900782](https://openairdocs.org/sdr/CALA9900782), Jul 2, 1999: SKIN. DELAMINATED. INSPECTION FOUND THE UPPER AND LOWER SURFACE OF RT WING NR 4 SPOILER SKIN DELAMINATED. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-60-01.
- [SDR CALA9900800](https://openairdocs.org/sdr/CALA9900800), Jun 29, 1999: LONGERON. CRACKED. INSPECTION FOUND A 1 CRACK IN LEFT LONGERON AND A 1 CRACK IN RT LONGERON OF NR 2 ENGINE CORE COWL. THE CRACKS WERE LOCATED NEAR HINGES. THE LONGERONS WERE REPAI
- [SDR CALA9900799](https://openairdocs.org/sdr/CALA9900799), Jun 26, 1999: FLOORBEAM. CRACKED. INSPECTION FOUND A 3 CRACK IN CENTER CARGO STRUCTURAL FLOORBEAM NR 12 BETWEEN STA 1721 AND 1741. A NEW BEAM WAS INSTALLED IAW MM 53-00-00 AND DRAWING AFT7009.
- [SDR CALA9900798](https://openairdocs.org/sdr/CALA9900798), Jun 26, 1999: JAMB. CRACKED. INSPECTION FOUND A 1 CRACK IN CENTER CARGO DOOR JAMB AT STA 1721. THE JAMB WAS REPLACED IAW SRM 53-10-00.
- [SDR CALA9900797](https://openairdocs.org/sdr/CALA9900797), Jun 26, 1999: FLOORBEAM. CRACKED. INSPECTION FOUND ONE EACH 1 CRACK IN CENTER CARGO STRUCTURAL FLOORBEAMS NR 9 AND NR 10 BETWEEN STA 1761 AND 1741. THE BEAMS WERE REPLACED IAW SRM 53-00-00 AND M
- [SDR CALA9900796](https://openairdocs.org/sdr/CALA9900796), Jun 26, 1999: ANGLE. CRACKED. INSPECTION FOUND A 1 CRACK IN ANGLE AT UPPER AFT SECTION OF CENTER CARGO DOOR. THE ANGLE WAS REPLACED IAW SRM 51-30-00.
- [SDR CALA9900795](https://openairdocs.org/sdr/CALA9900795), Jun 26, 1999: BEAM. CRACKED. INSPECTION FOUND A 3 CRACK IN CENTER CARGO NR 12 FLOOR STRUCTURAL BEAM AT STA 1821. A NEW BEAM WAS INSTALLED IAW SRM 51-30-00 AND MM 25-50-00.
- [SDR CALA9900794](https://openairdocs.org/sdr/CALA9900794), Jun 26, 1999: SKIN. DELAMINATED. INSPECTION FOUND LEFT WING INBOARD FLAP UPPER SKIN UNBONDED ON INBOARD SIDE. THE SKIN WAS REPLACED IAW SRM 51-30-00.
- [SDR CALA9900793](https://openairdocs.org/sdr/CALA9900793), Jun 24, 1999: SKIN. DENTED. INSPECTION FOUND LEFT WING LOWER SKIN DENTED AT STA 1090. THE SKIN WAS REPLACED IAW SRM 51-30-00.
- [SDR CALA9900792](https://openairdocs.org/sdr/CALA9900792), Jun 24, 1999: SKIN. CRACKED. INSPECTION FOUND A 2 CRACK IN LEFT WING NR 2 SLAT SKIN. REPAIRED IAW SRM 57-10-00, FIGURE 31.
- [SDR CALA9900791](https://openairdocs.org/sdr/CALA9900791), Jun 23, 1999: SKIN. CRACKED. INSPECTION FOUND A 1.25 CRACK ON RT WING UPPER SKIN DROOPED LEADING EDGE. A REPAIR WAS INSTALLED IAW SRM 57-10-00.
- [SDR CALA9900790](https://openairdocs.org/sdr/CALA9900790), Jun 23, 1999: BOLT. BROKEN. INSPECTION FOUND TRAPEZOIDAL PANEL BOLT IN RT MLG WHEEL WELL BROKEN AT STA 1370. THE BOLT WAS REPLACED IAW MM 20-50-02.
- [SDR CALA9900789](https://openairdocs.org/sdr/CALA9900789), Jun 19, 1999: STRAP. CRACKED. INSPECTION FOUND A 1.5 CRACK IN RT WING LOWER SKIN LEADING EDGE STRAP BETWEEN STA XORS 433 AND XORS 455. A NEW STRAP WAS INSTALLED IAW DRAWING ARB2935 AND SRM 5
- [SDR CALA9900788](https://openairdocs.org/sdr/CALA9900788), Jun 19, 1999: SKIN. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN INTERNAL SKIN OF RT WING LEADING EDGE SLAT NR 4. A REPAIR WAS PERFORMED IAW SRM 57-00-01, PAGE 12, FIGURE 4, SHEET 2.
- [SDR CALA9900787](https://openairdocs.org/sdr/CALA9900787), Jun 19, 1999: STRAP. CRACKED. INSPECTION FOUND A 2 INCH EFTACK IN LEFT WING LEADING EDGE STRIP AT STA XORS 455 AND XORS 506. REPAIRED IAW DRAWING 2933 AND SRM 51-30-00.
- [SDR CALA9900498](https://openairdocs.org/sdr/CALA9900498), May 7, 1999: BOTTLE. BLOWN. DOOR 4L DOOR ASSIST BOTTLE BLOWN. RESET HANDLE AND SERVICED DOOR ASSIST BOTTLE, OPERATES NORMAL.
- [SDR CALA9800777](https://openairdocs.org/sdr/CALA9800777), May 5, 1998: RECIRC FAN. FAILED. A/C DIVERTED TO MAD FROM FCO DUE TO ELECTRIC SMELL IN CABIN. FOUND NR 4 CABIN AIR RECIRCULATION FAN FAILED. FAN TO BE REPLACED.
- [SDR CALA9800515](https://openairdocs.org/sdr/CALA9800515), Mar 20, 1998: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1 INCH CRACK ON LOWER CAP OF INTERCOSTAL AT CEILING CENTER CARGO, RBL 82, STA 1721 WITH DISTORTION ON CEILING SUPPORT AT RBL 78. A REPAIR WAS
- [SDR CALA9701787](https://openairdocs.org/sdr/CALA9701787), Dec 21, 1997: TRANSFER VALVE. LEAKING. THE AIRCRAFT LOST NR 1 HYDRAULIC SYSTEM QUANTITY AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR
- [SDR CALA9701360](https://openairdocs.org/sdr/CALA9701360), Sep 14, 1997: BLADE. MISINSTALLED. T/O WAS REJECTED AT 5 KNOTS WHEN NR 3 ENG COMPRESSOR STALLED. THE NR 3 ENG WAS SHUT DOWN AND THE ACFT RETURNED TO THE GATE. MX INSPECTED THE NR 3 ENG AND FOUND 

## STCs that may be installed (OpenAirDocs) (387, 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 (Mcdonnell-Douglas DC-10-30)

- [STC ST00272AT](https://openairdocs.org/stc/ST00272AT): Installation of an Airshow 210 enter- tainment system. AIRCRAFT RECONFIG TECHNOLOGIES, LLC. Lists DC-10 Series
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC SA5040NM](https://openairdocs.org/stc/SA5040NM): Installation of cargo pallet and net. Satco Inc
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC SA1368NM](https://openairdocs.org/stc/SA1368NM): Installation of C&D Interiors P/N 1441002. Safran Cabin Inc
- [STC SA1369NM](https://openairdocs.org/stc/SA1369NM): Installation of closets. Safran Cabin Inc
- [STC SA2049NM](https://openairdocs.org/stc/SA2049NM): Installation of C&D Interiors P/N 1751001-101, -102. Safran Cabin Inc
- [STC SA2175NM](https://openairdocs.org/stc/SA2175NM): Installation of the Centerline Overhead Stowage Retrofit Kit. Safran Cabin Inc
- [STC SA2471NM](https://openairdocs.org/stc/SA2471NM): Installation of centerline bin, overhead side bin. Safran Cabin Inc
- [STC SA2499NM](https://openairdocs.org/stc/SA2499NM): Installation of closet/windscreen. Safran Cabin Inc
- [STC SA3127NM](https://openairdocs.org/stc/SA3127NM): Installation of Closet. Safran Cabin Inc
- [STC SA3422NM](https://openairdocs.org/stc/SA3422NM): Installation of a galley. Safran Cabin Inc
- [STC SA3460NM](https://openairdocs.org/stc/SA3460NM): Installation of centerline stowage bins. Safran Cabin Inc. Lists DC-10 Series
- [STC SA3804NM](https://openairdocs.org/stc/SA3804NM): Installation of the Centerline SkyBin Stowage Interior kit. Safran Cabin Inc
- [STC SA3967NM](https://openairdocs.org/stc/SA3967NM): Installation of bi-fold lavatory door. Safran Cabin Inc
- [STC SA4832NM](https://openairdocs.org/stc/SA4832NM): Installation of C&D Interiors Part Numbers 3001001-105 Credenza, 4761001-101 C/L Closet, and 4771001-101 and -102 L.H. and R.H. Closet. Safran Cabin Inc
- [STC SA5492NM](https://openairdocs.org/stc/SA5492NM): Installation of galleys, dividers, closet, and fold-down table. Safran Cabin Inc
- [STC SA8001NM](https://openairdocs.org/stc/SA8001NM): Installation of C&D Interiors class divider and ceiling panel. Safran Cabin Inc
- [STC ST00495LA](https://openairdocs.org/stc/ST00495LA): Installation of lavatories. Safran Cabin Inc
- [STC ST00584LA](https://openairdocs.org/stc/ST00584LA): Installation of centerline bin kits. Safran Cabin Inc
- [STC ST00650LA](https://openairdocs.org/stc/ST00650LA): Installation of lavatories. Safran Cabin Inc
- [STC ST01077LA](https://openairdocs.org/stc/ST01077LA): Installation of passenger service unit (PSU). Safran Cabin Inc
- [STC ST01391LA](https://openairdocs.org/stc/ST01391LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC SA3411NM](https://openairdocs.org/stc/SA3411NM): Installation of floor proximity emergency escape path marking system. Bruce Aerospace Inc
- [STC ST01694AT](https://openairdocs.org/stc/ST01694AT): Installation of additional sensors for recording additional parameters on Digital Flight Data Recorder (DFDR). Acron Aviation Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST02117CH](https://openairdocs.org/stc/ST02117CH): Installation of Honeywell Enhanced Ground Proximity Warning System and GPS antenna. Amphenol Cable and Interconnect Technologies Inc
- [STC ST02184CH](https://openairdocs.org/stc/ST02184CH): Installation of elementary or enhanced surveillance Mode S transponders. Amphenol Cable and Interconnect Technologies Inc
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST02131AT](https://openairdocs.org/stc/ST02131AT): Installation of SAF-T-GLO photoluminescent floor proximity emergency escape with marking system (FPEEPMS). STG Aerospace Inc
- [STC SA3474NM](https://openairdocs.org/stc/SA3474NM): Installation of Galley 1, Galley 2, Galley 1A, Coartoom and Lavatories. Safran Cabin Inc
- [STC ST01986CH](https://openairdocs.org/stc/ST01986CH): Installation of a Honeywell RESCU 406AF Emergency Locator Transmitter (ELT) system. Honeywell International Inc
- [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [STC SA1220NW](https://openairdocs.org/stc/SA1220NW): Installation of Universal flight data recorder. Honeywell International Inc
- [STC SA3046SO](https://openairdocs.org/stc/SA3046SO): Installation of a single/dual TRA-67 Mode S ATC transponder system. Honeywell International Inc
- [STC SA3061SO](https://openairdocs.org/stc/SA3061SO): Installation of a CAS-81 TCAS II system. Honeywell International Inc
- [STC SA5794NM](https://openairdocs.org/stc/SA5794NM): Installation of Mark VII ground proximity and windshear warning system. Honeywell International Inc
- [STC ST00536SE](https://openairdocs.org/stc/ST00536SE): Installation of the Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS). Honeywell International Inc
- [STC SA5672SW-D](https://openairdocs.org/stc/SA5672SW-D): Modification of air to air heat exchanger (P/N 187900-9). Honeywell International Inc
- [STC SA8928SW](https://openairdocs.org/stc/SA8928SW): Replace core assembly of AiResearch Bleed Air Precooler, part numbers 187890-3 and 189740-3. Honeywell International Inc
- [STC SA8757SW](https://openairdocs.org/stc/SA8757SW): Replace core assembly of Janitrol Constant Speed Drive (CSD) Oil Cooler, part number B63D89. Honeywell International Inc
- [STC SA7419SW](https://openairdocs.org/stc/SA7419SW): Rebuild DC-10 Auxiliary Power Unit Oil Cooler Assembly by manufacturing a new core assembly. Honeywell International Inc. Lists DC-10 Series
- [STC SA4010WE](https://openairdocs.org/stc/SA4010WE): Installation of video projection system. Burrana Inc
- [STC SA4070WE](https://openairdocs.org/stc/SA4070WE): A video projection system is installed. Burrana Inc
- [STC SA451NE](https://openairdocs.org/stc/SA451NE): Installation of Inflight Services video projection system DC-10 Bangladesh P/N 105-D-1228. Burrana Inc
- [STC SA930EA](https://openairdocs.org/stc/SA930EA): Installation of Inflight Motion Pictures, Inc., Projection Unit Assembly DC-10 16mm Tri-Jet System, P/N 10300 or Light Weight Tri-Jet Projection System, DC-10, P/N 10307. Burrana Inc
- [STC SA947EA](https://openairdocs.org/stc/SA947EA): Installation of Inflight Motion Pictures, Inc. screen assemblies. Burrana Inc
- [STC SA990EA](https://openairdocs.org/stc/SA990EA): Installation of Inflight Motion Pictures 16mm projection unit assembly and center stowage bins, P/N 10310 and/or P/N 10311. Burrana Inc

All 387: https://openairdocs.org/aircraft/N17085/stcs.md

## Earlier aircraft with N17085

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N17085 before.

- [Cancelled 1965-05-18](https://openairdocs.org/deregistered/N17085-1965-05-18): Douglas DC3C-S1C3G, S/N 5094. Owner: [Sinclair Somal Corp](https://openairdocs.org/faa-owner/SINCLAIR%20SOMAL%20CORP), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)

## Related

- Other Mcdonnell-Douglas DC-10-30 aircraft: https://openairdocs.org/model/mcdonnell-douglas-dc-10-30/aircraft.md
- The GE CF6-50 series engine: https://openairdocs.org/engine/ge-cf6-50-series.md

---
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