# N262UP: 2001 Mcdonnell Douglas MD-11F

- Status: Valid registration
- Airframe: [Mcdonnell Douglas MD-11F](https://openairdocs.org/model/mcdonnell-douglas-md-11f) (registry code 3023600, 7 seats)
- Engine: [GE CF6-80C2D1F](https://openairdocs.org/engine/ge-cf6-80c2d1f) (registry code 30110)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE) (The Boeing Company), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 48806
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 29, 2020
- Certificate issued: February 19, 2020
- Expires: February 28, 2030
- Mode S code: A2883B
- Registered owner: [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: Corporation
- Owner's area on the map: 38.2585° N, 85.5398° W: Placed by OpenAirDocs at the center of ZIP code 40223, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=262UP
- Page: https://openairdocs.org/aircraft/N262UP

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

## ADs that may apply (OpenAirDocs): 224 in force

### Matched by airframe (Mcdonnell Douglas MD-11F)

- [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 2025-02-07](https://openairdocs.org/ad/2025-02-07): Navigation · Modification of Rockwell Collins, Inc. Multi-Mode Receiver (STC ST01883WI or 4 others). Effective Mar 17, 2025
- [AD 2024-24-03](https://openairdocs.org/ad/2024-24-03): Engine Exhaust · Boeing MD-11, MD-11F and CF6-80C2D1F. Effective Jan 13, 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 2021-24-02](https://openairdocs.org/ad/2021-24-02): Electrical power · Boeing MD-11 and MD-11F. Effective Feb 1, 2022
- [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 2018-07-20](https://openairdocs.org/ad/2018-07-20): Fuel · Boeing MD-11 and MD-11F. Effective May 21, 2018
- [AD 2018-01-01](https://openairdocs.org/ad/2018-01-01): Fuel · Boeing MD-11 and MD-11F. Effective Feb 7, 2018
- [AD 2017-14-10](https://openairdocs.org/ad/2017-14-10): Fuel System · Boeing MD-11 and MD-11F. Effective Aug 21, 2017
- [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014
- [AD 2011-25-06](https://openairdocs.org/ad/2011-25-06): Horizontal stabilizer structure · Boeing MD-11 and MD-11F. Effective Jan 17, 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 2011-02-01](https://openairdocs.org/ad/2011-02-01): Fuel · Boeing MD-11 and MD-11F. Effective Feb 16, 2011
- [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 2010-16-03](https://openairdocs.org/ad/2010-16-03): Ice and rain protection · Boeing MD-11 and MD-11F. Effective Sep 9, 2010
- [AD 2010-11-12](https://openairdocs.org/ad/2010-11-12): Fuel · Boeing MD-11 and MD-11F. Effective Jul 6, 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 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 2007-19-15](https://openairdocs.org/ad/2007-19-15): Flight management system (FMS) · Boeing 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Oct 26, 2007
- [AD 2007-19-02](https://openairdocs.org/ad/2007-19-02): Fuel tank and the fuel transfer pump housing flange · Boeing DC-10-30, DC-10-30F (KC-10A, KDC-10), DC-10-40 and 4 more. Effective Oct 17, 2007
- [AD 2007-11-16](https://openairdocs.org/ad/2007-11-16): Center main wheel well · Boeing MD-11 and MD-11F. 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 2007-07-04](https://openairdocs.org/ad/2007-07-04): Principal structural elements (PSEs) · Boeing MD-11 and MD-11F. Effective May 2, 2007
- [AD 2007-01-02](https://openairdocs.org/ad/2007-01-02): Power feeder cables of the integrated drive generator (IDG) · Boeing MD-11 and MD-11F. Effective Feb 14, 2007
- [AD 2006-25-09](https://openairdocs.org/ad/2006-25-09): Auxiliary power unit (APU) power feeder wires · Boeing MD-11F. Effective Dec 27, 2006
- [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 2006-16-15](https://openairdocs.org/ad/2006-16-15): Airplane flight manual (AFM) · Boeing MD-10-10F, MD-10-30F, MD-11 and 1 more. Effective Sep 22, 2006
- [AD 2006-13-07](https://openairdocs.org/ad/2006-13-07): Upper and lower reading lights · Boeing MD-11 and MD-11F. Effective Jul 27, 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 2005-02-08](https://openairdocs.org/ad/2005-02-08): Power feeder cables of the auxiliary power unit (APU) · Boeing MD-11 and MD-11F. Effective Mar 7, 2005
- [AD 2005-02-06](https://openairdocs.org/ad/2005-02-06): Oil pressure transmitter to the main oil circuit · Boeing MD-11 and MD-11F. Effective Mar 7, 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

### Matched by engine (GE CF6-80C2D1F)

- [AD 2021-26-22](https://openairdocs.org/ad/2021-26-22): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 14, 2022
- [AD 2021-14-11](https://openairdocs.org/ad/2021-14-11): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 25 more. Effective Aug 27, 2021
- [AD 2021-03-02](https://openairdocs.org/ad/2021-03-02): Fuel Control/Turbine Engines · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Mar 31, 2021
- [AD 2020-22-02](https://openairdocs.org/ad/2020-22-02): Engine Fuel and Control · General Electric CF6-80C2A5F, CF6-80C2B1F, CF6-80C2B2F and 13 more. Effective Dec 3, 2020
- [AD 2016-08-10](https://openairdocs.org/ad/2016-08-10): Accessory heat shield · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Jun 1, 2016
- [AD 2014-21-01](https://openairdocs.org/ad/2014-21-01): Fuel manifold · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Nov 28, 2014
- [AD 2013-08-20](https://openairdocs.org/ad/2013-08-20): Fuel tube · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 14 more. Effective May 31, 2013
- [AD 2012-03-12](https://openairdocs.org/ad/2012-03-12): No. 3 bearing packing · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Apr 5, 2012
- [AD 2009-21-07](https://openairdocs.org/ad/2009-21-07): Thrust and thrust control · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Dec 1, 2009
- [AD 2009-07-03](https://openairdocs.org/ad/2009-07-03): Eddy current inspection (ECI) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Apr 30, 2009
- [AD 2009-04-10](https://openairdocs.org/ad/2009-04-10): Critical life-limited parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 30 more. Effective Mar 30, 2009
- [AD 2008-21-11](https://openairdocs.org/ad/2008-21-11): Low-pressure turbine (LPT) cases · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Nov 28, 2008
- [AD 2007-22-07](https://openairdocs.org/ad/2007-22-07): Electronic control unit (ECU) · General Electric CF6-80C2D1F. Effective Nov 28, 2007
- [AD 2007-11-20](https://openairdocs.org/ad/2007-11-20): Fuel shroud retaining rings · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 22 more. Effective Jul 10, 2007
- [AD 2007-05-14](https://openairdocs.org/ad/2007-05-14): Cast titanium weld- repaired forward engine mount platforms · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 9, 2007
- [AD 2006-16-06](https://openairdocs.org/ad/2006-16-06): Certain stage 1 high- pressure turbine (HPT) rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Sep 5, 2006
- [AD 2006-06-08](https://openairdocs.org/ad/2006-06-08): Latching system of the fan reverser · General Electric CF6-80C2D1F. Effective Apr 25, 2006
- [AD 2005-17-05](https://openairdocs.org/ad/2005-17-05): High pressure compressor rotor (HPCR) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Sep 27, 2005
- [AD 2004-22-07](https://openairdocs.org/ad/2004-22-07): Stage 2 nozzle guide vanes (HPT S2 NGVs) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 1, 2004
- [AD 2004-07-13](https://openairdocs.org/ad/2004-07-13): High pressure turbine (HPT) stage 1 disks · General Electric CF6-80C2A5F, CF6-80C2B5F, CF6-80C2B7F and 1 more. Effective May 6, 2004
- [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 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2000-12-08](https://openairdocs.org/ad/2000-12-08): Mount Link Assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 4 more. Effective Aug 28, 2000
- [AD 2000-03-04](https://openairdocs.org/ad/2000-03-04): General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Apr 10, 2000
- [AD 99-01-01](https://openairdocs.org/ad/99-01-01): Accessory Gearbox (AGB) idler adapters · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jan 21, 1999
- [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 96-16-07](https://openairdocs.org/ad/96-16-07): Rear Right Hand Mount Link · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective Aug 28, 1996
- [AD 95-10-11](https://openairdocs.org/ad/95-10-11): Fan Reversers · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective May 31, 1995
- [AD 94-20-06](https://openairdocs.org/ad/94-20-06): Oil System · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 27, 1994
- [AD 94-06-03](https://openairdocs.org/ad/94-06-03): High Pressure Turbine Disk · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 29, 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 91-15-25](https://openairdocs.org/ad/91-15-25): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Sep 6, 1991
- [AD 91-11-05](https://openairdocs.org/ad/91-11-05): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Jul 5, 1991
- [AD 91-05-21](https://openairdocs.org/ad/91-05-21): High Pressure Turbine · General Electric CF6-80C2A5, CF6-80C2B6, CF6-80C2B6F and 1 more. Effective Mar 27, 1991

### Historical (superseded or no longer in force)

- [AD 2025-23-51](https://openairdocs.org/ad/2025-23-51) (historical): Nacelles/pylons · Boeing MD-11 and MD-11F. Effective Dec 1, 2025
- [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 2020-03-20](https://openairdocs.org/ad/2020-03-20) (historical): Navigation · Modification of Rockwell Collins, Inc. Multi-Mode Receiver (STC ST01883WI or 4 others). Effective Feb 18, 2020
- [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 2014-03-07](https://openairdocs.org/ad/2014-03-07) (historical): Fuel · Boeing MD-11 and MD-11F. Effective Mar 26, 2014
- [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013
- [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 2009-26-16](https://openairdocs.org/ad/2009-26-16) (historical): Fuel · Boeing MD-11 and MD-11F. 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 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 2004-18-04](https://openairdocs.org/ad/2004-18-04) (historical): Airplane Flight Manual (AFM) · McDonnell Douglas 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Sep 20, 2004
- [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 2004-01-17](https://openairdocs.org/ad/2004-01-17) (historical): Integrated drive generator · McDonnell Douglas MD-11 and MD-11F. Effective Feb 24, 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 2002-14-11](https://openairdocs.org/ad/2002-14-11) (historical): Ground cables of the galley external power and main external power · McDonnell Douglas MD-11 and MD-11F. Effective Aug 23, 2002
- [AD 2002-14-09](https://openairdocs.org/ad/2002-14-09) (historical): Power feeder cable terminal lugs · McDonnell Douglas MD-11 and MD-11F. Effective Aug 23, 2002
- [AD 99-25-14](https://openairdocs.org/ad/99-25-14) (historical): Wire Harnesses Of Tail Tank Fuel Transfer Pumps · McDonnell Douglas MD-11 and MD-11F. Effective Jan 18, 2000
- [AD 99-09-04](https://openairdocs.org/ad/99-09-04) (historical): Circuit Breakers · McDonnell Douglas MD-11 and MD-11F. Effective May 7, 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 94-26-51](https://openairdocs.org/ad/94-26-51) (historical): AFM Changes - Autoland Operation · Boeing MD-11 and MD-11F. Effective Feb 6, 1995
- [AD 94-11-06](https://openairdocs.org/ad/94-11-06) (historical): External Power Feeder Cables · McDonnell Douglas MD-11 and MD-11F. Effective Jun 15, 1994
- [AD 2020-20-13](https://openairdocs.org/ad/2020-20-13) (historical): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Nov 12, 2020
- [AD 2018-15-04](https://openairdocs.org/ad/2018-15-04) (historical): Turbine/Turboprop Engine--Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Oct 2, 2018
- [AD 2009-05-02](https://openairdocs.org/ad/2009-05-02) (historical): Drainless fuel manifold assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Mar 31, 2009
- [AD 2004-04-07](https://openairdocs.org/ad/2004-04-07) (historical): Stage 1 HPT rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 12, 2004
- [AD 2002-07-12](https://openairdocs.org/ad/2002-07-12) (historical): Life Limits Section of Continued Airworthiness (ICA) - Selected Critical Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 27 more. Effective May 15, 2002
- [AD 2001-10-07](https://openairdocs.org/ad/2001-10-07) (historical): High Pressure Turbine Rotor Disks · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jun 18, 2001
- [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 2000-04-14](https://openairdocs.org/ad/2000-04-14) (historical): Fuel tube flange seating · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective May 1, 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 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999
- [AD 91-20-02](https://openairdocs.org/ad/91-20-02) (historical): Fuel Manifolds · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective Nov 25, 1991
- [AD 90-26-01](https://openairdocs.org/ad/90-26-01) (historical): Fuel Manifold Systems · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 11 more. Effective Dec 20, 1990

All 261: https://openairdocs.org/aircraft/N262UP/ads.md

## Information bulletins (advisory) (10 in force)

- [SAIB NM-18-33](https://openairdocs.org/saib/NM-18-33): Engine Fuel and Control. Issued Dec 17, 2018
- [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
- [SAIB NM-07-31](https://openairdocs.org/saib/NM-07-31): Rigid hydraulic case drain lines. Issued Apr 24, 2007
- [SAIB NM-06-57](https://openairdocs.org/saib/NM-06-57): Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.. Issued Jul 27, 2006
- [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023
- [SAIB NE-11-27](https://openairdocs.org/saib/NE-11-27): Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel Nozzles. Issued Apr 5, 2011
- [SAIB NE-10-37](https://openairdocs.org/saib/NE-10-37): Engine Fuel and Control: FADEC Fuel Metering Valve Resolver Feedback Faults. Issued Jul 12, 2010
- [SAIB NE-08-44](https://openairdocs.org/saib/NE-08-44): Engine Thrust Reverser  Transcowl Clevis Pin. Issued Sep 3, 2008
- [SAIB NE-07-01](https://openairdocs.org/saib/NE-07-01): Dual engine flameouts on twin engine airplanes. Issued Oct 12, 2006

## NTSB investigations

None matched to N262UP.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20250722020559I](https://openairdocs.org/incident/20250722020559I), Jul 22, 2025: Mcdonnell Douglas MD-11F (N262UP), Miami, FL, Minor damage. At touchdown, runway 8L, the #10 center landing gear tire failed with debris striking the center gear right-hand flying gear door causing minor deformation to…

## Service difficulty reports (82, newest 50)

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 IPXA2025082916221](https://openairdocs.org/sdr/IPXA2025082916221), Aug 29, 2025: CIRCUIT BREAKER. TRIPPED. COULDN`T GET MAIN ENTRY DOOR TO CLOSE. FOUND LEFT CABIN DOOR FWD POWER CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER IAW AMM 20-30-13-865-801. PERFORMED OPS CHE
- [SDR IPXA2025051315997](https://openairdocs.org/sdr/IPXA2025051315997), May 10, 2025: EVAS UNIT. FAILED. CAPTAINS EVAS OPS CHECK FAILED. BLOWER DOES NOT RUN. REMOVED AND REPLACED CAPTAINS EVAS PER AMM 25-69-00. OPS CHECK GOOD.
- [SDR IPXA2025051215997](https://openairdocs.org/sdr/IPXA2025051215997), May 10, 2025: EVAS UNIT. NO TEST. CAPTAINS EVAS OPS CHECK FAILED. BLOWER DOES NOT RUN. REMOVED AND REPLACED CAPTAINS EVAS PER AMM 25-69-00. OPS CHECK GOOD.
- [SDR IPXA2025010867217](https://openairdocs.org/sdr/IPXA2025010867217), Jan 8, 2025: DOOR. UNKNOWN. R1 CREW ENTRY DOOR INTERMITTENT INOP. COMPLIED WITH AMM 52-11-02-830-027 AND 20-30-05. PLACARD REMOVED.
- [SDR IPXA2024112566316](https://openairdocs.org/sdr/IPXA2024112566316), Nov 23, 2024: DOOR. OBSTRUCTED. CREW ENTRY DOOR WON`T CLOSE. FOUND SUPERNUMERARY SEAT LEG REST NOT STOWED. STOWED LEG REST. OPS CHECK GOOD AT THIS TIME. MM 52-11-02.
- [SDR IPXA2024101888190](https://openairdocs.org/sdr/IPXA2024101888190), Oct 17, 2024: SWITCH. INOPERATIVE. RIGHT CREW DOOR SWITCH IS GETTING WONKY. IT WOULD NOT OPEN DOOR, EVENTUALLY WORKED FOUND R/T CREW ENTRY DOOR LOCK PIN RELEASE SOLENOID TO BE INTERMITTENT AND SL
- [SDR IPXA2024101770959](https://openairdocs.org/sdr/IPXA2024101770959), Oct 17, 2024: SWITCH. INOPERATIVE. LEFT CREW ENTRY DOOR WOULD NOT CLOSE WITH ELECTRICAL SWITCH. FOUND THE COURIER STATION NOT COMPLETELY STOWED, STOWED STATION AND OPS CK OF DOOR WAS SATISFACTORY
- [SDR IPXA2024090670330](https://openairdocs.org/sdr/IPXA2024090670330), Aug 14, 2024: TEE ANGLE. CRACKED. MAIN CABIN L3 DOOR AFT CUTOUT T-SUPPORT FRAME IS CRACKED AT STRINGER 15. LOCATED DRILLED HOLES AND INSTALLED REPLACEMENT T-SUPPORT FRAME ON MAIN CABIN L3 DOOR C
- [SDR IPXA2023120743426](https://openairdocs.org/sdr/IPXA2023120743426), Dec 6, 2023: UNKNOWN. UNKNOWN. L1 DOOR WILL NOT OPEN ELECTRICALLY REMOVED AND REPLACED DOOR LOCK PIN RELEASE SOLENOID IAW AMM 52-10-06, OPS CHECK GOOD. THIS CLEAR DMI, PLACARD REMOVED.
- [SDR IPXA32863](https://openairdocs.org/sdr/IPXA32863), Dec 6, 2023: UNKNOWN. UNKNOWN. DURING GROUND OPS THE LEFT CREW DOOR WOULD NOT OPEN FROM EITHER INSIDE OR OUTSIDE ELECTRICALLY OR MECHANICAL NEEDED TO USE THE 1/4€? TOOL TO OPEN THE DOOR. CYC
- [SDR IPXA2023112435751](https://openairdocs.org/sdr/IPXA2023112435751), Nov 24, 2023: UNKNOWN. UNKNOWN. L1 DOOR WOULD NOT OPEN ELECTRICALLY USED EMERGENCY PNEUMATIC HANDLE TO EXIT. PERFORMED OPERATIONAL CHECK OK L1 DOOR NORMAL MODE IAW AMM TASK 52-10-01-700-801. U
- [SDR IPXA2023111599751](https://openairdocs.org/sdr/IPXA2023111599751), Nov 15, 2023: UNKNOWN. UNKNOWN. CREW ENTRY DOOR (L-1) WILL NOT OPEN W/ INTERIOR OR EXTERIOR SWITCH PERFORMED OPS CK OF DOOR REF AMM 52-10-01, CKS NORMAL FROM INTERIOR AND EXTERIOR SWITCHES , T
- [SDR IPXA2023082293977](https://openairdocs.org/sdr/IPXA2023082293977), Aug 21, 2023: SEAT TRACK. DAMAGED. INSPECTION TYPE:N/A*MAJOR REPAIR* MAIN DEACK SEAT TRACK POS 10RH/11RH Y-27.50 DAMAGED.REPAIRED PER MD11-5310-87863-A.
- [SDR IPXA2023082193971](https://openairdocs.org/sdr/IPXA2023082193971), Aug 21, 2023: PANEL. DENTED. INSPECTION TYPE:N/A*MAJOR REPAIR* LT LOWER VERTICAL STAB LOWER ACCESS PANEL DENTPANEL REPAIRED PER EO MD11-55-30-86966B
- [SDR IPXA2023060193354](https://openairdocs.org/sdr/IPXA2023060193354), Jun 1, 2023: DOOR. INOPERATIVE. L1 ENTRY DOOR NOT CLOSING. DEFERRED AS PER MEL 52-10-1-2-0-1. PLACARD INSTALLED. C/W DMP 52-10-1-2-0-1. PERFORMED OP CK OF L1 DOOR INSIDE AND OUTSIDE SWITCHES P
- [SDR IPXA2023040592619](https://openairdocs.org/sdr/IPXA2023040592619), Apr 4, 2023: REMOTE SWITCH. FAILED. L1 REMOTE PRESS TO TEST FAIL TO ILLUMINATE. DEFERRED PRESS TO TEST INDICATING SYSTEM PER 25-61-2. L1 SLIDE BOTTLE PRESS CK GOOD AT THIS TIME PER MD-11 MEL 25-61
- [SDR IPXA2023032892361](https://openairdocs.org/sdr/IPXA2023032892361), Mar 27, 2023: LIGHT. INOPERATIVE. SLIDE RAFT PRESSURE LIGHT ON L1 DOOR INOP. DEFERRED L1 SLIDE REMOTE PRESSURE PRESS TO TEST INDICATING SYSTEM IAW MEL 25-61-2. C/W DMPRELAMPED AND RELACED BATTER
- [SDR IPXA2022092686607](https://openairdocs.org/sdr/IPXA2022092686607), Sep 22, 2022: CONTROLLER. FAULTED. EMERGENCY DECLARED, A/C LANDED UNEVENTFULLY, A/C OOS, LEVEL 3, CABIN ALT. CW FIM 21-33-00 AND AMM 21-31-00. NO DEFECTS NOTED. Q-ALERT ISSUED; TO REPLACE PN 2119
- [SDR IPXA2022082085439](https://openairdocs.org/sdr/IPXA2022082085439), Aug 5, 2022: RIB. CRACKED. INSPECTION TYPE:1CR/H O/B WING L/E RIB IS CRACKED JUST I/B OF #9 SLAT TRACK AT STA XOS=584.891 .REPAIRED R/H O/B WING L/E RIB AT STA XOS= 584.891 IAW SRM 57-00-
- [SDR IPXA2022081685328](https://openairdocs.org/sdr/IPXA2022081685328), Aug 5, 2022: DOUBLER. CRACKED. INSPECTION TYPE:1CRH WING L/E FORMER STRAP DOUBLER CRACK JUST O/B OF #10 SLAT TRACK.REMOVED,FABRICATED AND INSTALLED CRACKED STRAP DOUBLER IAW DWG ARB3954 AND S
- [SDR IPXA2022081685327](https://openairdocs.org/sdr/IPXA2022081685327), Aug 5, 2022: DOUBLER. CRACKED. INSPECTION TYPE:1CRH WING L/E BEADED DOUBLER CRACK BETWEEN STA. XOS=692.0 TO XOS=703-5.REPAIRED RH WING L/E CRACKED BEADED DOUBLER BETWEEN STA. XOS=692.0 TO XOS
- [SDR IPXA2022081585243](https://openairdocs.org/sdr/IPXA2022081585243), Aug 5, 2022: BRACKET. CRACKED. INSPECTION TYPE:1CCAC HAS A CRACKED BRACKET AT THE RADIO RACK LWR O/B SIDE.REPLACED BRACKET IAW SRM 51-31-01 (MINOR)
- [SDR IPXA2022081585242](https://openairdocs.org/sdr/IPXA2022081585242), Aug 5, 2022: DOUBLER. CRACKED. INSPECTION TYPE:C1CTR WHEEL WELL L/H BULKHEAD FWD PRODUCTION DOUBLER CRACKED.REPLACED PRODUCTION DOUBLER IAW SRM 51-33-01. (MINOR)
- [SDR IPXA2022081385189](https://openairdocs.org/sdr/IPXA2022081385189), Aug 5, 2022: STIFFENER. CRACKED. INSPECTION TYPE:1CRH MLG W/W O/B WEB VERTICAL STIFFENER CRACK AT LOWER END.REMOVED AND REPLACED CRACKED STIFFENER IAW SRM51-35-01 AND 51-33-01 (MINOR).
- [SDR IPXA2022061783205](https://openairdocs.org/sdr/IPXA2022061783205), Jun 16, 2022: NONE. NONE. INSPECTION TYPE:NA***SUPPLEMENTAL SDR*** @ OAK L1 DOOR STOPS 2/3 OF THE WAY OPEN IT DOES NOT SEEM TO BE THE SWITCH.R&R ED S1-248, S2-730, R2-5324 REF SWPM 20-20
- [SDR IPXA2022051182000](https://openairdocs.org/sdr/IPXA2022051182000), May 11, 2022: BATTERY PACK. DISCHARGED. EMER LT BAT LO1. REPLACED EMER PWR SUPPLY BATTERY. SYS OPS NORMAL REF AMM 33-51-01.
- [SDR IPXA2022041781218](https://openairdocs.org/sdr/IPXA2022041781218), Apr 16, 2022: LEVER. NONE. INSPECTION TYPE:NA**ATB** **EMERGENCY DECLARED** LEVEL 2 FLAP DISAG ALERT ON FLAP RETRACTION FROM 10*-0* POSITION FLAP HANDLE AT 10* FLAPS THEN RETRACTED SLOWLY
- [SDR IPXA2022031179990](https://openairdocs.org/sdr/IPXA2022031179990), Mar 10, 2022: NONE. NONE. INSPECTION TYPE:NAAVNCS FAN OVRD CAME ON DURING DESCENT.FOUND 2 18" SECTIONS OF MAIN CARGO DOOR SEAL OUT OF RETAIN ER- INSTALLED IN RETAINERS REF AMM 52-00-00.
- [SDR IPXA2022030279633](https://openairdocs.org/sdr/IPXA2022030279633), Mar 2, 2022: NONE. NONE. INSPECTION TYPE:NA** EMERGENCY DECLARED** **LANDING MADE WITHOUT INCIDENT** ON APPROACH TO ONT WHEN FLAPS WERE SELECTED TO 35 FLAPS EXTENDED TO 32/29 WENT AROUN
- [SDR IPXA2021102275216](https://openairdocs.org/sdr/IPXA2021102275216), Oct 20, 2021: NONE. NONE. INSPECTION TYPE:NARI DOOR PRESS TO TEST FOR DOOR EVACUATION PRESS IJOPR&R REMOTE PRESSURE INDICATOR ASSY. IAW MD11 AMM 25-61-04-401. THIS CLEARS M760178.
- [SDR IPXA2021101274872](https://openairdocs.org/sdr/IPXA2021101274872), Oct 11, 2021: SLIDE. INOPERATIVE. INSPECTION TYPE:N/A**SUPPLEMENTAL SDR** R1 SLIDE PRESS TO TEST SWITCH INOP. DEFERRED IAW MEL 25-61-2. DMP 25-61-2 ACCOMPLISHED. M759324 ASSIGNED.PERF OPS CK OF 
- [SDR IPXA2021091173795](https://openairdocs.org/sdr/IPXA2021091173795), Sep 10, 2021: INDICATOR. FAILED. INSPECTION TYPE:N/A1R1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INOPT/S TO BAD INDICATOR (C6-207) SWITCH REMOVED IAW WDM 25-61-02. R/R R1-SW REMOTE P
- [SDR IPXA2021060870276](https://openairdocs.org/sdr/IPXA2021060870276), Jun 7, 2021: POWER SUPPLY. INOPERATIVE. EMERG LIGHT SYST INOP. DFRD PER MEL 33-50-4 M FUNCTION C/W DMP C/W.R/R'D POWER SUPPLY EMERGENCY LIGHT BATTERY IAW MM 33-51-01. OPS CHECK GOOD.
- [SDR IPXA2020122163673](https://openairdocs.org/sdr/IPXA2020122163673), Dec 21, 2020: LIMIT SWITCH. INOPERATIVE. CABIN DOOR FWD L ALERT REMAINED ON AFTER ARMING L1 DOOR. DEFERRED EAD DOOR OPEN ALERT, IAW MEL 52 40 1 1 0 1. DOOR CLOSED & ARMED. REPLACED DOOR DOWN LIMIT SWIT
- [SDR IPXA2020112762823](https://openairdocs.org/sdr/IPXA2020112762823), Nov 27, 2020: BUSHING. UNSECURE. INSPECTION TYPE: N/A L1 DOOR WILL NOT DRIVE ELECTRICALLY. RESECCURED PLUNGER BUSHING AT S1 592 L1 DOOR. OPERATIONS AS NORMAL, REF AMM 52-00-02. THIS CLEARS M727
- [SDR IPXA2020112562780](https://openairdocs.org/sdr/IPXA2020112562780), Nov 24, 2020: FAN. INOPERATIVE. INSPECTION TYPE: N/A AT LEVEL OFF RECEIVED A LEVEL ONE AIR "AVIONICS FAN OVERHEAD" ALERT REMAINED ON UNTIL APPROXIMATELY 2,000 FT ABOVE FIELD ELEVATION AT KSDF 
- [SDR IPXA2020072057976](https://openairdocs.org/sdr/IPXA2020072057976), Jun 9, 2020: CARGO TRACK. CORRODED. INSPECTION TYPE:3C, RIGHT SIDE O/B SEAT TRACK HAS CORROSION UNDERNEATH FASTENER HOLES BETWEEN STA 1530 AND 1545 X = -107.REPAIRED CORRODED SEAT TRACK IN MAIN CA
- [SDR IPXA2020070357253](https://openairdocs.org/sdr/IPXA2020070357253), Jun 3, 2020: ANGLE. CRACKED. INSPECTION TYPE:3C LT WING T ANGLE SUPPORT BETWEEN UPPER AND LOWER T/E SKIN IS CRACKED APPROX 12" FWD OF O/B L/E I/B AILERON. REMOVED CRACKED T ANGLE, FABRICATE
- [SDR IPXA2020070157194](https://openairdocs.org/sdr/IPXA2020070157194), Jun 3, 2020: DOUBLER. CRACKED. INSPECTION TYPE:3C BEADED DOUBLER ON LT WING FIXED L/E IS CRACKED AROUND FASTENER HOLES AT STA XORS 616. REPAIRED CRACKED BEADED DOUBLER AT LT WING FIXED L/E AT
- [SDR IPXA2020062977054](https://openairdocs.org/sdr/IPXA2020062977054), Jun 3, 2020: DOUBLER. CRACKED. INSPECTION TYPE:3C, BEADED DOUBLER ON FIXED LE IS CRACKED ON LH WING XOS=637 TO XOS=643 INSIDE FUEL ACCESS PANEL 519CB.REPAIRED CRACKED BEADED DOUBLER ON LH WIN
- [SDR IPXA2020062977051](https://openairdocs.org/sdr/IPXA2020062977051), Jun 3, 2020: DOUBLER. CRACKED. INSPECTION TYPE:3C, RH WING O/B FLAP UPPER SURFACE I/B FWD CORNER PRODUCTION DOUBLER IS CRACKED.REMOVED CRACKED DOUBLER, FABRICATED AND INSTALLED IN RH WING O/B
- [SDR IPXA2020062256823](https://openairdocs.org/sdr/IPXA2020062256823), Jun 3, 2020: SKIN. CRACKED. INSPECTION TYPE:3C LT WING FIXED L/E LOWER SKIN HAS A CRACK AROUND NR 11 SLAT TRACK AT STA XOS 717. REPAIRED CRACKED LT WING L/E LOWER SKIN AROUND NR 11 SLAT TR
- [SDR IPXA2020070357261](https://openairdocs.org/sdr/IPXA2020070357261), Jun 2, 2020: SKIN. CORRODED. INSPECTION TYPE:3C RT AFT FUSELAGE SKIN BETWEEN STA 1986 - 2164 LONGERON 33R TO LONGERON 35R BETWEEN HORIZONTAL STAB FAIRING HAS CORROSION. REPAIRED CORRODED SK
- [SDR IPXA2020062977050](https://openairdocs.org/sdr/IPXA2020062977050), May 31, 2020: STIFFENER. CRACKED. INSPECTION TYPE:3C, UPPER FUSELAGE 1EA STIFFENER CRACKED INSIDE ACCESS PANEL 364FR AT STA 2103.REMOVED CRACKED STIFFENER, FABRICATED AND INSTALLED AT UPPER FUSE
- [SDR IPXA2020070857530](https://openairdocs.org/sdr/IPXA2020070857530), May 30, 2020: SKIN. DAMAGED. INSPECTION TYPE:3C AFT EXTENDED TAIL CONE LOWER T/E CAP SKIN AT STA 2318-2325 AND Z=25.925 TO Z=64.075. REPAIRED DAMAGED AFT EXTENDED TAIL CONE IAW EA 011-5380-
- [SDR IPXA2020072097940](https://openairdocs.org/sdr/IPXA2020072097940), May 29, 2020: CARGO TRACK. CORRODED. INSPECTION TYPE:3C, MAIN CARGO TRACK WAS CORRODED FROM BS 1501 TO 5-89, LBL-10. REPAIRED THE CARGO TRACK IAW SRM 53-00-51 REPAIR 1 FIG 201 REV. 66. (MAJOR).
- [SDR IPXA2020072057980](https://openairdocs.org/sdr/IPXA2020072057980), May 29, 2020: CARGO TRACK. CORRODED. INSPECTION TYPE:3CUPPER CARGO COMP SEAT TRACK HAS CORROSION FROM STA 1511 TO STA 5-93 LBL-20.REPAIRED CORRODED SEAT TRACK IN MAIN CARGO STA 1511 TO 5-93 LBL-20 
- [SDR IPXA2020100961122](https://openairdocs.org/sdr/IPXA2020100961122), May 28, 2020: FLOOR SUPPORT. BROKEN. INSPECTION TYPE: 3C MAIN CABIN FLOOR SUPPORT AT STA 1521 LEFT OF CENTERLINE IS BROKEN. REMOVED, FABRICATED, AND REPLACED FLOOR SUPPORT, IAW DWG ACA3763 AND SRM 
- [SDR IPXA2020100961121](https://openairdocs.org/sdr/IPXA2020100961121), May 28, 2020: FLOOR SUPPORT. CORRODED. INSPECTION TYPE: 3C MAIN CABIN FLOOR SUPPORT IS CORRODED AT STA 1481 AND LBL 48. REMOVED, FABRICATED, AND REPLACED FLOOR SUPPORT, IAW DWG ACA3763 AND SRM 51-35-
- [SDR IPXA2020100961120](https://openairdocs.org/sdr/IPXA2020100961120), May 28, 2020: FLOOR SUPPORT. CORRODED. INSPECTION TYPE: 3C MAIN CABIN FLOOR SUPPORT RT OF CENTERLINE AT STA 1501 IS CORRODED. REMOVED, FABRICATED, AND REPLACED SUPPORT, IAW DWG ACA3763 AND SRM 51-35-

All 82: https://openairdocs.org/aircraft/N262UP/reports.md

## STCs that may be installed (OpenAirDocs) (124, 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 MD-11F)

- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [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 ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [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 SA7065NM](https://openairdocs.org/stc/SA7065NM): Installation of Closet Assembly. Safran Cabin Inc
- [STC ST01391LA](https://openairdocs.org/stc/ST01391LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC ST02111LA](https://openairdocs.org/stc/ST02111LA): Installation of Coatroom. Safran Cabin 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 ST02708CH](https://openairdocs.org/stc/ST02708CH): Installation of EZMountTM Arm mechanical mounting assemblies on lower frame of cockpit sliding windows. Amphenol Cable and Interconnect Technologies Inc
- [STC ST02865CH](https://openairdocs.org/stc/ST02865CH): Upgrade of the internal core software of the ACARS Communications Management Unit (CMU-900). 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 ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST02002WI](https://openairdocs.org/stc/ST02002WI): Replacement of Rockwell Collins LRA-900 Low Range Radio Altimeters with upgraded LRA-900 units for improved RF immunity to 5G cellular data interference. Rockwell Collins, Inc
- [STC ST01986CH](https://openairdocs.org/stc/ST01986CH): Installation of a Honeywell RESCU 406AF Emergency Locator Transmitter (ELT) system. Honeywell International Inc
- [STC ST03516AT](https://openairdocs.org/stc/ST03516AT): Installation of dual Artex Model C406-N Emergency Locator Transmitters (ELT). Woven Electronics, LLC
- [STC ST04538AT](https://openairdocs.org/stc/ST04538AT): Installation of the Cobham Aviator 200S INMARSAT SATCOM Communication System and external HELGA Low Gain Antenna. Avionics Support Group Inc
- [STC ST01719SE](https://openairdocs.org/stc/ST01719SE): Lavatory installation on MD-11F Series airplanes. Commercial Aircraft Interiors Inc
- [STC ST01813SE](https://openairdocs.org/stc/ST01813SE): Lavatory installation on Model MD-11F Series airplanes. Commercial Aircraft Interiors
- [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 SA8757SW](https://openairdocs.org/stc/SA8757SW): Replace core assembly of Janitrol Constant Speed Drive (CSD) Oil Cooler, part number B63D89. Honeywell International Inc
- [STC ST04517AT](https://openairdocs.org/stc/ST04517AT): Installation of hardware to existing side conveyor assemblies. United Parcel Service Company
- [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 ST04092NY](https://openairdocs.org/stc/ST04092NY): Installation of Wireless PCMCIA for DFDAU. Delta Engineering Corporation
- [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 ST04546NY](https://openairdocs.org/stc/ST04546NY): Installation of Sleeper Seat at Courier Module. Lufthansa Technik AG
- [STC ST04547NY](https://openairdocs.org/stc/ST04547NY): Installation of a Secondary Flight Display System (SFDS). Lufthansa Technik AG
- [STC ST04542NY](https://openairdocs.org/stc/ST04542NY): Installation of TCAS Change 7.1. Lufthansa Technik AG
- [STC ST04543NY](https://openairdocs.org/stc/ST04543NY): Installation of a Global Navigation Satellite Sensor Unit (GNSSU) Replacement. Lufthansa Technik AG
- [STC ST04544NY](https://openairdocs.org/stc/ST04544NY): Activation of ADS-B and ELS/EHS Upgrade. Lufthansa Technik AG
- [STC ST01943WI](https://openairdocs.org/stc/ST01943WI): Modification of Rockwell Collins, Inc. Multi-Mode Receiver (MMR) Global Landing System (GLU-2100). Rockwell Collins Inc
- [STC ST02669LA](https://openairdocs.org/stc/ST02669LA): Installation of Honeywell MKV EGPWS with Landing Performance Enhancement (LPE) functionality. Honeywell International Inc
- [STC ST01276WI-D](https://openairdocs.org/stc/ST01276WI-D): Collins CMU-900 ACARS CORE Software Upgrade. Rockwell Collins Inc
- [STC ST02572SE](https://openairdocs.org/stc/ST02572SE): Operated in accordance with the Supplement to United Parcel Service (UPS) Airlines Weight and Balance Manual TTF-16T004-20-1 Revision A, dated October 31, 2017 as listed on the AML. United Parcel Service Company
- [STC SA5546NM](https://openairdocs.org/stc/SA5546NM): Installation of a cabin cargo handling system. Ancra International LLC
- [STC ST00152LA](https://openairdocs.org/stc/ST00152LA): Installation of Ancra International Cargo Handling System. Ancra International LLC
- [STC ST01120LA](https://openairdocs.org/stc/ST01120LA): Installation of insulation blankets. Triumph Insulation Systems LLC
- [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 ST00353LA-1](https://openairdocs.org/stc/ST00353LA-1): Installation of Aircraft Communications, Addressing and Reporting System (ACARS). Teledyne Controls
- [STC ST00399DE](https://openairdocs.org/stc/ST00399DE): Installation of nose radome shell assembly. The NORDAM Group LLC
- [STC ST02639LA](https://openairdocs.org/stc/ST02639LA): Replace the existing Mode S Transponder system. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST01895WI](https://openairdocs.org/stc/ST01895WI): Modification of an existing Rockwell Collins Global Landing Unit (GLU) Multi-Mode Receiver (MMR), Sensor Systems Inc. GPS Antenna and ACSS Transponder Installation. Rockwell International Collins Commercial Avionics
- [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

All 124: https://openairdocs.org/aircraft/N262UP/stcs.md

## Related

- Other Mcdonnell Douglas MD-11F aircraft: https://openairdocs.org/model/mcdonnell-douglas-md-11f/aircraft.md
- The GE CF6-80C2D1F engine: https://openairdocs.org/engine/ge-cf6-80c2d1f.md

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