# N260UP: 1992 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: 48418
- Year built: 1992
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 24, 2007
- Certificate issued: July 31, 2006
- Expires: November 30, 2027
- Mode S code: A280CD
- 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=260UP
- Page: https://openairdocs.org/aircraft/N260UP

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/N260UP/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 N260UP.

## 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 20100604035079I](https://openairdocs.org/incident/20100604035079I), Jun 4, 2010: Mcdonnell D MD-11F (N260UP), Anchorage, AK, Substantial damage. Aircraft N260UP departed rwy 14. At approximately 600' AGL, the #3 engine fire indication came on for approximately 5 seconds and then extinguished. The…

## Service difficulty reports (329, 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 IPXA2025050129299](https://openairdocs.org/sdr/IPXA2025050129299), Apr 18, 2025: FITTING. CORRODED. UPON REMOVAL OF LONGERON FITTING P/N AAA7088 AT L51R STA 6-70 TO 6-90 FOUND TO BE CRACK AND CORRODED ATA-53-00 REMOVED & REPLACED LONGERON 51R (P/N: AAA7088-1 P
- [SDR IPXA2025050643072](https://openairdocs.org/sdr/IPXA2025050643072), Apr 16, 2025: SKIN. CORRODED. CORROSION FOUND APPROX 18 INCHES FWD OF CENTER WING BOX AND APPROX AT RBL 88. 49-036 ATA 53-00 CENTER WING TANK UPPER FWD SKIN BETWEEN STA XCW=-74 TO XSW=-111 A
- [SDR IPXA2025050245994](https://openairdocs.org/sdr/IPXA2025050245994), Apr 16, 2025: LONGERON. CORRODED. CORROSION FOUND IN CAC STA 6-70 TO 6-90 / LONGERON R51. PM040-80. ATA-51-00 LONGERON SPLICE REPAIR ACCOMPLISHED @ FWD EXTENDED FUSELAGE SECTION LONGERON 51R (P/
- [SDR IPXA2025050928077](https://openairdocs.org/sdr/IPXA2025050928077), Apr 15, 2025: STIFFENER. CRACKED. (STR) AFT CGO COMP FLOOR BEAM AREA STA 1841 RBL 30" STIFFENER HAS CRAKED. 74-033 ATA CODE 53 INSTALLED NEW STIFFENER AT AFT CARGO COMPARTMENT FLOOR BEAM AREA, S
- [SDR IPXA2025050692110](https://openairdocs.org/sdr/IPXA2025050692110), Apr 13, 2025: DOUBLER. CRACKED. CRACKED BEADED DOUBLER AT RH LE APPROX 15 INCHES I/B OF #9 SLAT TRACK. 49-005 ATA 57-00 INSTALLED BEADED DOUBLER AND REMOVED EWIS PROTECTION AT R/H L/E I/B OF S
- [SDR IPXA2025031446915](https://openairdocs.org/sdr/IPXA2025031446915), Mar 14, 2025: STRUCTURE. DAMAGED. LWR FWR CARGO CEILING-STRUCTURE FWD OF AFT FLOOD LAMP -DAMAGED- NUTPLATE RIPPED OUT -HOLE SIZE IS .375 AND JAGGED EDGES.ACCOMPLISHED STEPS 1-7 OF EO-93152-REQ1
- [SDR IPXA2025031447024](https://openairdocs.org/sdr/IPXA2025031447024), Mar 14, 2025: STRUCTURE. DAMAGED. LWR FWD CARGO COMPT-CEILING-STRUCTURE AT INBD SIDE OF AFT FLOOD LAMP DAMAGED -BENT DOWN-MISSING NUTPLATE REF. ACCOMPLISHED STEPS 1-6 OF EO-93150-REQ1
- [SDR IPXA2025030445471](https://openairdocs.org/sdr/IPXA2025030445471), Mar 4, 2025: BOTTLE. LOW PRESSURE. R1 DOOR ASSIST BOTTLE PRESSURE BELOW GREEN BAND. SERVICED R1 DOOR ASSIST BOTTLE WITH REF TO AMM 12-25-04-600-801. NO LEAKS NOTED DURING LEAK CHECK. THIS CLEARS 
- [SDR IPXA2025012825896](https://openairdocs.org/sdr/IPXA2025012825896), Jan 28, 2025: BOTTLE. LOW PRESSURE. ON PRE-FLIGHT R1 DOOR PNEUMATIC PRESSURE BELOW LIMITS (OUT OF GREEN BAND). SERVICED THE R1 DOOR PNEUMATIC STORAGE SYSTEM IAW MD11 AMM 12-25-04. THIS CLEARS MEL.
- [SDR IPXA2024092134968](https://openairdocs.org/sdr/IPXA2024092134968), Sep 21, 2024: CHAIN. BROKEN. L1 ENTRY DOOR EMERGENCY PNEUMATIC DRIVE MOTOR DRIVE CHAIN MISSING. FOUND BROKEN CHAIN LOCATED ON CEILING PANEL. INSTALLED NEW CHAIN ASSY REF MM 52-11-09. DOOR O
- [SDR IPXA2024061915026](https://openairdocs.org/sdr/IPXA2024061915026), Jun 18, 2024: WIRE. DAMAGED. ATB, ON DEPARTURE, WHILE STILL CONFIGURED, GOT A LEVEL 1 AIL DEFLECT INOP. AFTER FLAP RETRACT, GOT A LEVEL 2 AIL DEFLECT DISAG. WE ENGAGED A/P 2 AND THE AIRCRAF
- [SDR IPXA2024011811319](https://openairdocs.org/sdr/IPXA2024011811319), Jan 18, 2024: UNKNOWN. UNKNOWN. R1 DOOR ASSIST BOTTLE PRESSURE LOW SVC'D R1 DOOR ASSIST BOTTLE AS REQ'D REF AMM 12-24-04
- [SDR IPXA2023090694099](https://openairdocs.org/sdr/IPXA2023090694099), Sep 5, 2023: BATTERY. DISCHARGED. EMERGENCY LIGHT BAT 1 LO STATUS MESSAGE. R & R EMERGENCY BATTERY POWER IAW AMM 33-51-01-400. OPS CHKS GOOD.
- [SDR IPXA2023071393653](https://openairdocs.org/sdr/IPXA2023071393653), Jul 12, 2023: DOOR. INOPERATIVE. INSPECTION TYPE:NACREW DOOR LOUVRE PANEL DETACHED FROM DOORRESECURED AND INSTALLED FLIGHT COMPARTMENT CREW DOOR LOUVRE PANEL IAW AMM 52-54-02-400-801. NO DEFECT
- [SDR IPXA2023062593511](https://openairdocs.org/sdr/IPXA2023062593511), Jun 24, 2023: LIGHT. INOPERATIVE. L1 DOOR EMERGENCY LIGHT EXIT SIGN HALF OUT. RELAMPED NO HELP. R/R L1 DOOR EXIT SIGN REF AMM 33-27-05 PB 401. OPS CHECKS GOOD.
- [SDR IPXA2023052293296](https://openairdocs.org/sdr/IPXA2023052293296), May 22, 2023: DOOR. INOPERATIVE. BEFORE BLOCK OUT I HAD DIFFICULTY ARMING THE FWD CABIN DOOR UPON LANDING I WAS OT ABLE TO DIS ARM THE DOORFOUND DEBRIS IN R1 DOOR ARMING HANDLE AND GIRT BAR DIS
- [SDR IPXA2023051993270](https://openairdocs.org/sdr/IPXA2023051993270), May 9, 2023: SEAT TRACK. CORRODED. INSPECTION TYPE:C3*MAJOR REPAIR* MAIN CABIN L/H SIDE SEAT TRACK HAS CORROSION AT STA Y=5-73 - Y=1568 AND X=8.50 .REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN 
- [SDR IPXA2023051993269](https://openairdocs.org/sdr/IPXA2023051993269), May 9, 2023: SEAT TRACK. CORRODED. INSPECTION TYPE:3C*MAJOR REPAIR* MAIN CABIN L/H SIDE SEAT TRACK HAS CORROSION BETWEEN STA Y=1581-1601 AND X=8.5.REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN L
- [SDR IPXA2023051193193](https://openairdocs.org/sdr/IPXA2023051193193), May 8, 2023: FLOOR PANEL. CORRODED. INSPECTION TYPE:N/ACOURIER AREA R/H FLOOR PANEL JUST I/B OF LAV. HAS CORROSION AT STA Y=392 - Y=421.578 X=0 - X=-17REPLACED FOR PANEL PER DWG SP11530074,ABA8225
- [SDR IPXA2023051993272](https://openairdocs.org/sdr/IPXA2023051993272), May 7, 2023: SKIN. PUNCTURED. INSPECTION TYPE:3C*** MAJOR REPAIR *** R/W FIXED L/E SKIN HAS TWO PUNCTURES THROUGH SKIN O/B OF SLAT TRACK BETWEEN STA XIS=250 - XIS=263.REPAIRED SKIN AT THE R/
- [SDR IPXA2023051193192](https://openairdocs.org/sdr/IPXA2023051193192), May 5, 2023: FLOOR PANEL. CORRODED. INSPECTION TYPE:N/ACORROSION FOUND ON MAIN CABIN FLOOR PANEL AT STA Y=386 - Y=421.578 AND BETWEEN X= 27.5 TO X=42REPLACED MAIN CABIN FLOOR PANEL AT STA Y=386 TO
- [SDR IPXA2023050293095](https://openairdocs.org/sdr/IPXA2023050293095), May 2, 2023: STRINGER. CRACKED. INSPECTION TYPE:C3*MAJOR REPAIR* R/H FIXED LE LOWER STRINGER IS CRACKED AT PANEL LANDING 11 IN O/B OFSLAT TRACK 12 , STA XOS=787REPAIRED R/H WING FIXED LE LOWER
- [SDR IPXA2023051693250](https://openairdocs.org/sdr/IPXA2023051693250), Apr 25, 2023: SEAT TRACK. CORRODED. INSPECTION TYPE:3CCOURIER AREA R/H SEAT TRACK HAS CORROSION AT STA STA 421.578 X=-27.500 FROM CL.REPAIRED CORRODED SEAT TRACK AT THE COURIER AREA R/H SIDE STA 4
- [SDR IPXA2023051293203](https://openairdocs.org/sdr/IPXA2023051293203), Apr 25, 2023: SEAT TRACK. CORRODED. INSPECTION TYPE:3CCOURIER AREA HAS A SEAT TRACK AT STA X=0.00 WITH CORROSION BETWEEN Y=420.77 AND Y=515.93.REMOVED, FABRICATED AND REPLACED CORRODED SEAT TRACK 
- [SDR IPXA2023050693139](https://openairdocs.org/sdr/IPXA2023050693139), Apr 25, 2023: FLOOR PANEL. CORRODED. INSPECTION TYPE:3CCOURIER AREA R/H SIDE HAS A FLOOR PANEL WITH CORROSION 68 INCH FROM CL AT STA 421.578.REPLACED CORRODED FLOOR PANEL AT THE COURIER AREA R/H SI
- [SDR IPXA2023051993271](https://openairdocs.org/sdr/IPXA2023051993271), Apr 23, 2023: SKIN. CORRODED. INSPECTION TYPE:3C*** MAJOR REPAIR *** AFT FUSELAGE R/H SIDE BODY FAIRING AREA STA Y=2140-Y=2160 AND LONGERON 33R-35R LWR EXTERNAL SURFACE HAS CORROSION.REPAIRE
- [SDR IPXA2023051893262](https://openairdocs.org/sdr/IPXA2023051893262), Apr 22, 2023: SPLICE. CRACKED. INSPECTION TYPE:3CMAIN CABIN L/H WALL AT STA Y=5-123, LONGERON 14L HAS A PRODUCTION SPLICE WITH A CRACKED.REMOVED, FABRICATED AND REPLACED CRACKED SPLICE AT THE
- [SDR IPXA2023051893261](https://openairdocs.org/sdr/IPXA2023051893261), Apr 22, 2023: SPLICE. CRACKED. INSPECTION TYPE:3CMAIN CABIN R/H WALL AT STA Y=5-123, LONGERON 8R HAS A PRODUCTION SPLICE WITH A CRACKED.REMOVED, FABRICATED AND REPLACED CRACKED SPLICE AT THE 
- [SDR IPXA2023051893260](https://openairdocs.org/sdr/IPXA2023051893260), Apr 22, 2023: SPLICE. CRACKED. INSPECTION TYPE:3CMAIN CABIN R/H WALL AT STA Y=5-123, LONGERON 6R HAS PRODUCTION SPLICE WITH A CRACKED.REMOVED, FABRICTED AND REPLACED CRACKED SPLICE AT THE MAI
- [SDR IPXA2023051993268](https://openairdocs.org/sdr/IPXA2023051993268), Apr 21, 2023: STRINGER. CRACKED. INSPECTION TYPE:3C*MAJOR REPAIR* UPPER CENTER AUXILIARY TANK HAS CRACKED EXISTING REPAIR BETWEEN STA XCW =-46 AND XCW =-17 ON STRINGER 47.REPAIRED CRACKED STRIN
- [SDR IPXA2023052293273](https://openairdocs.org/sdr/IPXA2023052293273), Apr 20, 2023: SPAR CAP. CORRODED. INSPECTION TYPE:3C*** MAJOR REPAIR *** L/H WING REAR SPAR LOWER CAP LOCATED ABOVE OF O/B FLAP HINGE FITTING STA XORS=737.550 HAS CORROSION.REPAIRED CORRODED REA
- [SDR IPXA2023050993163](https://openairdocs.org/sdr/IPXA2023050993163), Apr 20, 2023: SKIN. CORRODED. INSPECTION TYPE:3CMAIN CABIN R/H CTR WING BOX UPPER SURFACE FWD EDGE HAS CORROSION BETWEEN STA XCW=-96.5 AND XCW=-81.REPAIRED CORRODED SURFACE SKIN AT THE MAIN 
- [SDR IPXA2023050993160](https://openairdocs.org/sdr/IPXA2023050993160), Apr 20, 2023: SEAT TRACK. CORRODED. INSPECTION TYPE:3C*MAJOR REPAIR* MAIN CABIN R/H SEAT TRACK HAS CORROSION AT STA Y=5-11 AND 28 INCH FROM CL.REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN R/H SI
- [SDR IPXA2023050993159](https://openairdocs.org/sdr/IPXA2023050993159), Apr 20, 2023: SEAT TRACK. CORRODED. INSPECTION TYPE:3C*MAJOR REPAIR* MAIN CABIN R/H SEAT TRACK HAS CORROSION AT STA Y=5-11 AND 8.5 INCH FROM CL.REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN AT ST
- [SDR IPXA2023050993158](https://openairdocs.org/sdr/IPXA2023050993158), Apr 20, 2023: SEAT TRACK. CORRODED. INSPECTION TYPE:3C*MAJOR REPAIR* MAIN CABIN R/H SEAT TRACK HAS CORROSION BETWEEN STA Y=1521/5-11 AND X=75.5.REPAIRED CORRODED SEAT TRACK AT THE MAIN CABIN R/H S
- [SDR IPXA2023050993167](https://openairdocs.org/sdr/IPXA2023050993167), Apr 20, 2023: SKIN. CORRODED. INSPECTION TYPE:3CMAIN CABIN R/H CTR WING BOX TUNNEL HAS 3EA AREA OF CORROSION BETWEEN STA Y=1256-1305 AND 105 - 108 INCH FROM CL.REPARIED CORRODED SKIN AT THE 
- [SDR IPXA2023050993166](https://openairdocs.org/sdr/IPXA2023050993166), Apr 20, 2023: SKIN. CORRODED. INSPECTION TYPE:3CMAIN CABIN L/H CTR WING BOX SKIN AT STRINGER 15 HAS CORROSION 98 INCH FROM CL.REPAIRED CORRODED SKIN AT THE MAIN CABIN L/H CTR WING BOX AREA A
- [SDR IPXA2023050593129](https://openairdocs.org/sdr/IPXA2023050593129), Apr 20, 2023: BRACKET. CRACKED. INSPECTION TYPE:3CL/H WING O/B FLAP I/B HINGE FWD TIP STRUCTURE HAS A CRAKCED CLIP.REMOVED, FABRICATED AND REPLACED CLIP AT THE L/H WING O/B FLAP I/B HINGE FWD 
- [SDR IPXA2023050593127](https://openairdocs.org/sdr/IPXA2023050593127), Apr 20, 2023: BRACKET. CRACKED. INSPECTION TYPE:3CR/H O/B FLAP I/B FAIRING FWD O/B BRACKET CLIP IS CRACKED.REMOVED, FABRICATED AND REPLACED CLIP AT THE R/H O/B FLAP FWD SIDE IAW SRM 51-31-01 (
- [SDR IPXA2023051293204](https://openairdocs.org/sdr/IPXA2023051293204), Apr 19, 2023: SLAT. DAMAGED. INSPECTION TYPE:3CL/H WING #5 SLAT I/B UPPER CORNER HAS KNIFE EDGE DAMAGED.REMOVED, FABRICATED AND REPLACED TRAILING EDGE AT THE L/H WING #5 SLAT IAW VTSAA EA 0
- [SDR IPXA2023050993157](https://openairdocs.org/sdr/IPXA2023050993157), Apr 19, 2023: FLOOR PANEL. CORRODED. INSPECTION TYPE:3CUNDER RCB WALL FLOOR PANEL WSP0791-501 HAS CORROSION AFT OF 1ST FLOOR FITTING.REPLACED CORRODED FLOOR PANEL UNDER RCB WALL AFT OF 1ST FLOOR FI
- [SDR IPXA2023051293202](https://openairdocs.org/sdr/IPXA2023051293202), Apr 18, 2023: FLOOR PANEL. CORRODED. INSPECTION TYPE:3C COURIER FLOOR AREA UNDER MOON MAT HAS BULGING SURFACE BETWEEN STA Y=392 - Y=440.REPLACED CORRODED FLOOR PANEL AT THE COURIER FLOOR AREA AT ST
- [SDR IPXA2023050993161](https://openairdocs.org/sdr/IPXA2023050993161), Apr 18, 2023: ANGLE. BENT. INSPECTION TYPE:3CL/H MLG W/W AREA O/B LWR AFT SIDE WALL ANGLE FRAME HAS A BENT.REPLACED BENT ANGEL AT THE L/H MLG W/W AREA O/B LWR AFT SIDE WALL IAW SRM 51-31-
- [SDR IPXA2023020390568](https://openairdocs.org/sdr/IPXA2023020390568), Feb 3, 2023: DOOR. NOT REPORTED. INSPECTION TYPE:NA*** SUPPLEMENTAL SDR *** DOOR L1 INTERMITTENT CLOSING. DEFERRED L1 CREW ENTRY DOOR IAW MEL 52-10-3-1-2 1 M801890 OPEN.ADJUSTED TIE ROD END ON 
- [SDR IPXA2023012490219](https://openairdocs.org/sdr/IPXA2023012490219), Jan 23, 2023: CONTROL UNIT. FAULTED. L1 DOOR ELECTRIC CONTROL INOP. CW OPS CHECK PER AMM 52-11-02 AFTER CYCLING CB.
- [SDR IPXA2023010389495](https://openairdocs.org/sdr/IPXA2023010389495), Jan 2, 2023: CHAIN. BROKEN. L1 DOOR EMERGENCY OPERATION INOP. L1 EMER DOOR CHAIN BROKEN. R & R THE SPROCKET FOR THE FWD L1 DOOR POWER DRIVE SUPPORT ASSY IAW CMM 52-11-09, REPLACED ROLLER C
- [SDR IPXA2023010289481](https://openairdocs.org/sdr/IPXA2023010289481), Jan 2, 2023: LINE. STRIPPED. DURING INSPECTION OF R1 DOOR BOTTLE LINES, FOUND UNION ON MOTOR DAMAGED. R & R UNION FITTING ON THE MOTOR IAW AMM 52-11-05.
- [SDR IPXA2022122189205](https://openairdocs.org/sdr/IPXA2022122189205), Dec 20, 2022: ANTI-SKID SYS. INOPERATIVE. INSPECTION TYPE:NA ON LANDING A/C DECELERATED NORMALLY W/ AUTO BRAKES WHEN BRAKES WERE DISARMED A/C CONT BRAKING 50% N1 REQUIRD TO EXIT RUNWAY ATTEMPTED SHORT T
- [SDR IPXA2021081172616](https://openairdocs.org/sdr/IPXA2021081172616), Aug 6, 2021: DOOR. INOPERATIVE. INSPECTION TYPE:N/ATRIED CLOSING THE CABIN DOOR FORWARD LEFT AND WOULD NOT OPERATECYCLED CB DOOR POWER , DOOR OPS CHK NML REF AMM 52-10-01
- [SDR IPXA2021062570951](https://openairdocs.org/sdr/IPXA2021062570951), Jun 24, 2021: START VALVE. FAULTED. ATB ** LANDED WITHOUT INCIDENT ** PASSING FL220 START VALVE LIGHT ILLUMINATED. CREW WAS DIVERTED DUE TO ICING CONDITIONS. CREW WILL WORK WITH DISPATCH ON THAT. 

All 329: https://openairdocs.org/aircraft/N260UP/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/N260UP/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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