# N522AX: 1988 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: 48315
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 20, 2000
- Certificate issued: December 2, 2013
- Expires: December 31, 2029
- Mode S code: A69072
- 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=522AX
- Page: https://openairdocs.org/aircraft/N522AX

From the FAA registry file of October 21, 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/N522AX/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 N522AX.

## 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; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20160709016709I](https://openairdocs.org/incident/20160709016709I), Jul 9, 2016: Mcdonnell-Douglas DC-10-30 (N522AX), Pueblo, CO, Minor damage. On July 9, 2016 at approximately 2045 mountain daylight time, a Mcdonnell Douglas DC-10 aircraft, N522AX received minor damage when the aircraft taxied into a…

## Service difficulty reports (25)

As reported by operators and repair stations.

- [SDR ZTRR20200708001](https://openairdocs.org/sdr/ZTRR20200708001), Jul 3, 2020: BOLT. MISSING. "AT ROTATE SPEED NR 2 ENG INDICATED FIRE. ALL ENG INDICATORS DISPLAYED NORMAL PARAMETERS FOR CONDITIONS. PERFORMED ENG SHUTDOWN IAW QRH. UPON PLACING FUEL LEVER
- [SDR CNMA20110024](https://openairdocs.org/sdr/CNMA20110024), May 2, 2011: LIGHT. NO TEST. L1 DOOR SLIDE EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING OPS TEST. SLIDE DEPLOYED NORMALLY. REPLACED SLIDE ASSY.
- [SDR CNMA20100036](https://openairdocs.org/sdr/CNMA20100036), Dec 29, 2010: SCAVENGE PUMP. LEAKING. NR 3 ENG OIL QTY WENT TO ZERO IN FLIGHT, VERIFIED BY LOSS OF OIL PRESS & LOW OIL PRESS LIGHT. TROUBLESHOT DOWN TO NR 3 ENGINE OIL LUBE AND SCAVENGE PUMP ASSY. R
- [SDR CNMA20100028](https://openairdocs.org/sdr/CNMA20100028), Jul 24, 2010: PANEL. CORRODED. EXFOLIATED CORROSION ON RT WING LOWER PLATE BELOW ACCESS PANEL 616BB AT XQRS 346. REMOVED DAMAGED SECTION OF LOWER WING SKIN, ACCOMPLISHED SURFACE SCAN AND OPEN
- [SDR CNMA20090007](https://openairdocs.org/sdr/CNMA20090007), Mar 13, 2009: SUPPORT FITTING. DAMAGED. BS 1997-2007, LBL 60 CORROSION ON SUPPORT FITTING. DAMAGED AREA REMOVED. REINFORCED AREA WITH REPAIR DOUBLER (PN 5340599-1-3) IAW SWG NO 5340599-1 USING FASTENE
- [SDR CNMA20090145](https://openairdocs.org/sdr/CNMA20090145), Mar 4, 2009: BULKHEAD. DENTED. AFT OF CTR LANDING GEAR THERE IS A DENT AT LONGERON 52 APPROX BS 1545. DENTED SKIN LOCALLY TRIMMED, AT DENT PERIPHERY. AREA REINFORCED WITH REPAIR DOUBLERS AND 
- [SDR AAAAACNMA20090144](https://openairdocs.org/sdr/AAAAACNMA20090144), Mar 4, 2009: WEB. CRACKED. BS 1741-1721, S-31R APPROX, DURING CTR CARGO DOOR REPAIR WAS FOUND CRACK ON THE INNER WEB. CRACK WAS TRIMMED OUT. AREA WAS REINFORED WITH A DOUBLER PN N522AX-NR
- [SDR CNMA20090143](https://openairdocs.org/sdr/CNMA20090143), Mar 4, 2009: TEE FITTING. DAMAGED. BS 2007, RBL 53, DURING TEE FITTING REPAIR WAS FOUND FITTING WITH 5 EA DAMAGED HOLES. DAMAGED FITTING REMOVED. NEW INSTALLED PN: AJC7634-2 IAW SRM VOL 2 51-31-0
- [SDR CNMA20090142](https://openairdocs.org/sdr/CNMA20090142), Mar 4, 2009: TEE FITTING. CORRODED. BS 2007, RBL 53 DURING CHANNEL REMOVING IAW NRC 715 WAS FOUND CORROSION ON TEE CHORD UNDERNEATH MENTIONED CHANNEL. DAMAGED PARTS REMOVED. REINFORCED AREA WITH N
- [SDR CNMA20090141](https://openairdocs.org/sdr/CNMA20090141), Mar 4, 2009: FLOORBEAM. CRACKED. FOUND CRACKS ON FLOOR PANEL SUPPORTS AT STD 1980 RBL- 2 AND LBL- 5. DAMAGED FLOORBEAM PARTS REMOVED. NEW FABRICATED SEGMENT PN OAI-53-00121-0013 IAW SRM VOL 3 5
- [SDR CNMA2009A0140](https://openairdocs.org/sdr/CNMA2009A0140), Mar 4, 2009: FLOORBEAM. CRACKED. FOUND CRACK ON FLOOR PANEL SUPPORT AT STD 1900 LBL - 5. DAMAGED SUPPORT REMOVED NEW FABRICATED PN OAI-53-0011 IAW SRM VOL 3 53-16-01 AND GMM 4.45 USING FASTENER
- [SDR CNMA20090139](https://openairdocs.org/sdr/CNMA20090139), Mar 4, 2009: LONGERON. CRACKED. FOUND CRACK ON U CHANNEL BETWEEN STA 1119-1139 STA 51 AREA . DAMAGED CHANNEL REMOVED. NEW FABRICATED PN OAI-53-0008 IAW SRM VOL 3 53-13-01 FIG 11A AND GMM 4.45 
- [SDR CNMA20090138](https://openairdocs.org/sdr/CNMA20090138), Mar 4, 2009: FITTING. CRACKED. LWR AUX FUEL TANK FITTING AT STA 1257, LBL 11, IS CRACKED. CRACKED ANGLE REMOVED NEW ANGLE PN OAI - 53-0005 INSTALLED USING HL18P138-6 HI LOWA B/N 6010-01 WITH 
- [SDR CNMA20090137](https://openairdocs.org/sdr/CNMA20090137), Mar 4, 2009: FITTING. CRACKED. LWR AUX FUEL TANK FITTING AT STA 1278 RBL 11 IS CRACKED. CRACKED ANGLE REMOVED. NEW ANGLE PN OAI 53-0004 INSTALLED USING HL18PB8-6 HI LOWS (BN 6010U-01) WITH HL
- [SDR CNMA20090136](https://openairdocs.org/sdr/CNMA20090136), Mar 4, 2009: SEAT TRACK. CORRODED. CORROSION ON LWR SIDE OF RAIL TRACK NEAR STA 2007. DAMAGED AREA TRIMMED OUT REINFORCED AREA WITH DOUBLER AND FILLER PN N522AX, NRC717-1/2 IAW SRM VOL 1, 53-00-0
- [SDR CNMA20090135](https://openairdocs.org/sdr/CNMA20090135), Mar 4, 2009: FLOORBEAM. CORRODED. CORROSION ON CHANNEL STA 2007, RBL 53. DAMAGED FLOOR SUPPORT REMOVED. NEW FABRICATED PN OAI 53-0003 IAW SRM VOL 3 53-16-01 AND OMNI 4.45 USING FASTENERS IAW SRM
- [SDR CNMA20090134](https://openairdocs.org/sdr/CNMA20090134), Mar 4, 2009: SUPPORT FITTING. CORRODED. BS 1997-2007, LBL 60, CORROSION ON SUPPORT FITTING. DAMAGED AREA REMOVED. REINFORCED AREA WITH REPAIR DOUBLER PN 5340599-1-3 IAW SWG NR 5340599-1 USING FASTENER
- [SDR CNMA20090133](https://openairdocs.org/sdr/CNMA20090133), Mar 4, 2009: SUPPORT. CORRODED. BS 427, RBL 30 CORROSION ON GALLEY SUPPORT. DAMAGED FLOOR SUPPORT REMOVED. NEW FABRICATED PN OAI 53-0002 IAW SRM VOL 3 53-11-01, FIG 1 AND GMM 4.45 USING FASTER
- [SDR CNMA20090132](https://openairdocs.org/sdr/CNMA20090132), Mar 4, 2009: SUPPORT. CORRODED. BS 457-495, RBL 53 CORROSION ON LAVATORY SUPPORT AT 2 EA PLCS. CORRRODED SUPPORT REMOVED. NEW FABRICATED PN OAI-53-001 IAW SRM VOL 3 53-11-01, FIG 1 AND GMM 4.4
- [SDR CNMA20090131](https://openairdocs.org/sdr/CNMA20090131), Mar 4, 2009: CARGO TRACK. CORRODED. B5 457-475, RBL 56 CORROSION ON TIE DOWN TRACK. DAMAGED AREA TRIMMED OUT. REINFORCED AREA WITH 2 PLATES AND FILLER PN N522AX -NRC595-1/2/3 IAW SRM VOL 1 53-00-0
- [SDR CNMA20090130](https://openairdocs.org/sdr/CNMA20090130), Mar 4, 2009: WEB. CRACKED. CRACK ON WEB OF PASS DOOR 3L LWR FWD CORNER B/T STA 1256, STA 1273, STR 27L. DAMAGED AREA TRIMMED OUT REINFORCED AREA WITH PN N522AX-NRC301-1 IAW SRM VOL 1 53-0
- [SDR CNMA20090129](https://openairdocs.org/sdr/CNMA20090129), Mar 4, 2009: WEB. CRACKED. CRACK ON WEB OF PASS DOOR 3R LWR FWD CORNER B/T STA 1256-1273 STR 27R. CRACKED AREA TRIMMED OUT. REINFORCED AREA WITH DOUBLER AND FILLER PN N522AX-NRC495-2/2 IA
- [SDR CNMA20090128](https://openairdocs.org/sdr/CNMA20090128), Mar 4, 2009: ANGLE. BROKEN. ANGLE IS BROKEN C/TO EXTERNAL FUSELAGE SKIN B/T STA 1239 AND STA 1256 STR 27L AND STR 28L. BROKEN ANGLE WAS REMOVED AND REPLACED WITH NEW PN OAI 53-0007 FABRICA
- [SDR CNMA20090127](https://openairdocs.org/sdr/CNMA20090127), Mar 4, 2009: BRACKET. BROKEN. BRACKETS ARE BROKEN C/TO FRAME OF FAIRING STA 1099, STR 30L AND STR 30R. 2 BRACKETS REMOVED NEW FABRICATED PN: OAI-53-0009/-0010 IAW SRM VOL 3 53-53-01 FIG. 3A 
- [SDR CNMA20090126](https://openairdocs.org/sdr/CNMA20090126), Mar 4, 2009: SUPPORT CHANNEL. TORN. TEAR ON SUPPORT CHANNEL, STA 1739 ABOVE STR 52. DAMAGED (TEAR) AREA TRIMMED OUT. REINFORCED AREA WITH ANGLE REPAIR PN N522AX NRC301-1 IAW SRM VOL 1 DC 10 53-00-

## Related

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

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