# N264UP: 2000 Boeing MD-11F

- Status: Valid registration
- Airframe: [Boeing MD-11F](https://openairdocs.org/model/boeing-md-11f) (registry code 3023604, 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: 48800
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 20, 2021
- Certificate issued: February 3, 2021
- Expires: February 29, 2028
- Mode S code: A28FA9
- 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=264UP
- Page: https://openairdocs.org/aircraft/N264UP

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 (Boeing 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/N264UP/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 N264UP.

## FAA accident and incident reports

None matched to N264UP.

## Service difficulty reports (101, 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 IPXA2025101577220](https://openairdocs.org/sdr/IPXA2025101577220), Oct 15, 2025: FUEL SYS. WARNING MESSAGE. DIVERTED DURING TAXI OUT WE RECEIVED LEVEL 2 LAT FUEL INBALANCE THAT CORRECTED ITSELF PRIOR TO TAKEOFF. AFTER TAKEOFF RECEIVED A LEVEL 2 FUEL QTY AND MISSING 24
- [SDR IPXA2025101081235](https://openairdocs.org/sdr/IPXA2025101081235), Oct 9, 2025: DOOR. MALFUNCTIONED. L1 DOOR DOES NOT OPEN ELECTRICALLY. REPOSITIONED REAR FACING COURIER SEATS TO RETRACTED POSITION, OPERATED L1 DOOR ELECTRICALLY SEVERAL TIMES. NO FAULTS NOTED.
- [SDR IPXA2025082327433](https://openairdocs.org/sdr/IPXA2025082327433), Aug 23, 2025: MANIFOLD. BROKEN. EMERGENCY DECLARED, DIVERSION, LVL 2 HYD 3 FAIL. STARTED HYD 3 ELEV OFF THEN HYD 3 OFF. REMOVED & REPLACED #3 ENGINE UPPER (LEFT) EDP PER AMM TASK 29-11-20-400-
- [SDR IPXA2025071643387](https://openairdocs.org/sdr/IPXA2025071643387), Jul 15, 2025: CONNECTOR. LOOSE. L1 DOOR UNABLE TO ARM. FOUND CONNECTOR ON SOLENOID NEAR AFT BAR RECEIVER LOOSE. TIGHTENED AS REQUIRED. DOOR OPERATES AND ARMS NORMALLY. REF AMM TASK 52-10-01-70
- [SDR IPXA2025032295372](https://openairdocs.org/sdr/IPXA2025032295372), Mar 6, 2025: FRAME. CRACKED. AFT AVI COMP R/H SIDE FRAME STA 475 AT LIGHTING HOLE HAS A CRACKED. INSTALLED THE REPLACEMENT FRAME SPLICE, -3 REPAIR ANGLE, -5 REPAIR STRAP AND ROUND DOUBLER I
- [SDR IPXA2025032861369](https://openairdocs.org/sdr/IPXA2025032861369), Mar 4, 2025: STIFFENER. CRACKED. AFT CGO COMP STA 1841 FLOOR PANEL FRAME RBL 26" STIFFENER HAS CRACKED. 74-059 ATA CODE 53. INSTALLED STIFFNER AT AFT CARGO COMP STA 1841 RBL26" REF MD11 SRM 51-
- [SDR IPXA2025032961156](https://openairdocs.org/sdr/IPXA2025032961156), Mar 4, 2025: FRAME. CRACKED. AFT CGO COMP WASTE TANK BILGE AREA STA 1986-2007 LONGERON 45L HAS CRACKED. 74-058 ATA CODE 53. INSTALLED 1EA LONGERON REPLACEMENT 45LH, 1 EA LONGERON SPLICE, 4 
- [SDR IPXA2025032261156](https://openairdocs.org/sdr/IPXA2025032261156), Mar 4, 2025: LONGERON. CRACKED. AFT CGO COMP WASTE TANK BILGE AREA STA 1986-2007 LONGERON 45L HAS CRACKED. 74-058 ATA CODE 53 INSTALLED 1EA LONGERON REPL 45LH, 1 EA LONGERON SPLICE, 4 EA BRACK
- [SDR IPXA2025011519891](https://openairdocs.org/sdr/IPXA2025011519891), Jan 15, 2025: DOOR. INOPERATIVE. L1 DOOR INOP. REMOVED AND REPLACED SOLENOID S2-730 REFERENCE AMM<BR>52-10-06-401. RAN DOOR MULTIPLE TIMES WITH NO FAULTS.<BR>THIS CLEARS 2834297. PLACARD REMOVE
- [SDR IPXA2024102979210](https://openairdocs.org/sdr/IPXA2024102979210), Oct 26, 2024: SKIN. DAMAGED. BIRDSTRIKE ON BASE-TO-FINAL TURN FOR PHL RWY 27R. POST-FLIGHT REVEALED EXTENSIVE DAMAGE TO RH WING LEADING EDGE INBOARD OF #3 ENGINE. INSTALLED R/H WING #2 SLAT
- [SDR IPXA2024102879210](https://openairdocs.org/sdr/IPXA2024102879210), Oct 26, 2024: SKIN. DAMAGED. *SDR FILED OPEN* BIRDSTRIKE ON BASE-TO-FINAL TURN FOR PHL RWY 27R. POST-FLIGHT REVEALED EXTENSIVE DAMAGE TO RH WING LEADING EDGE INBOARD OF #3 ENGINE. REMOVED #
- [SDR IPXA2024072392472](https://openairdocs.org/sdr/IPXA2024072392472), Jul 19, 2024: STRUCTURE. DAMAGED. *SUPPLEMENTAL SDR* #1 ENGINE PYLON DAMAGED. REMOVED AND REPLACED #1 ENG WING PYLON AFT LOWER FAIRING PER AMM 54-81-01 AND SRM 51-31-01.
- [SDR IPXA2024071992472](https://openairdocs.org/sdr/IPXA2024071992472), Jul 19, 2024: FAIRING. DAMAGED. NR 1 ENGINE PYLON DAMAGED. UPDATE : PYLON DAMAGE IS REFERRING TO #1 ENG WING PYLON AFT LOWER FAIRING.
- [SDR IPXA2023121123218](https://openairdocs.org/sdr/IPXA2023121123218), Dec 11, 2023: UNKNOWN. UNKNOWN. LEFT ENTRY DOOR OPEN CLOSE OPERATION INOP. FOUND DEBRIS LODGED BEHIND DRAWER ASSEMBLY UNDER COURIER SEATS. REMOVED MATERIAL LOCKED SEATS IN FORWARD POSITION DOO
- [SDR IPXA2023120502061](https://openairdocs.org/sdr/IPXA2023120502061), Dec 5, 2023: UNKNOWN. UNKNOWN. L1 ENTRY DOOR INOP FOUND COURIER SEAT NOT PROPERLY STOWED PAST GREEN STOW LINE MARKED ON FLOOR PER INSTRUCTIONS POSTED ABOVE L1 DOOR SWITCH. STOWED COURIER SEAT
- [SDR IPXA2023112188188](https://openairdocs.org/sdr/IPXA2023112188188), Nov 21, 2023: UNKNOWN. UNKNOWN. L1 DOOR POWER SWITCH DOES NOT WORK AFTER LANDING. BOTH INSIDE & OUTSIDE SWITCH INOP. **OII 2** FOUND DEBRIS LODGED BEHIND COURIER SEATS PREVENTING FULL TRAVEL I
- [SDR IPXA2023082894036](https://openairdocs.org/sdr/IPXA2023082894036), Aug 27, 2023: ADI. INOPERATIVE. INSPECTION TYPE:NA*ATB* ALT FLAG CAPT'S ADI CLIMBOUT THRU 2500' WSHEAR DET FAIL CLIMB THRU 5000' ALT FLAG FO ADI CLIMBING 10,000' IAS FLAG CAPT ADI BTWN 14-15,0
- [SDR IPXA2023042092928](https://openairdocs.org/sdr/IPXA2023042092928), Apr 20, 2023: BATTERY. DISCHARGED. INSPECTION TYPE:NA*SDR FILED OPEN* ON PREFLIGHT EMERG LIGHT BAT 1 LOW (LEVEL 1) ALERT. DEFERRED EMERGENCY LIGHTING SYS PER MEL 33 50 4. DMP 33 50 4. C/W PLACARD
- [SDR IPXA2023041192795](https://openairdocs.org/sdr/IPXA2023041192795), Apr 10, 2023: STIFFENER. CRACKED. INSPECTION TYPE:C1AFT CARGO COMPARTMENT STEP UP BULKHEAD HAS CRACKED STIFFNER AT STA Y1841 / STR 49RREMOVED, FABBED, AND INSTALLED STIFFNER AT STA. Y1841 AND ST
- [SDR IPXA2022102187316](https://openairdocs.org/sdr/IPXA2022102187316), Oct 19, 2022: DOOR. INTERMITTENT. L1 DOOR WORKING INTERMITTENTLY WITH INTERNAL & EXTERNAL CONTROL PANELS. DEFERRED L1 DOOR PER MEL 52-10-3-1-2-1-2 PLACARD INSTALLED. LINKED TO EO MD11-2520-85062
- [SDR IPXA2022102087316](https://openairdocs.org/sdr/IPXA2022102087316), Oct 19, 2022: CONTROL PANEL. INTERMITTENT. L1 DOOR WORKING INTERMITTENTLY WITH INTERNAL & EXTERNAL CONTROL PANELS. LINKED TO EO MD11-2520-85062. INSTALLED 4 SCREWS AT MAIN CARGO DOOR CONTROL ACCESS PANEL
- [SDR IPXA2022062483427](https://openairdocs.org/sdr/IPXA2022062483427), Jun 23, 2022: DOOR. INOPERATIVE. INSPECTION TYPE:NAR1 (ONE) DOOR INOPREPLACED R1 DOOR LOCK PIN (ILLEG) PER MM 52-10-06-401 AND R1 DOOR CONTROL RELAY PER RPM 20-10-00 DOOR OPS CHECK GOOD PER 52-
- [SDR IPXA2022021679058](https://openairdocs.org/sdr/IPXA2022021679058), Feb 15, 2022: LIGHT. INOPERATIVE. INSPECTION TYPE:N/A**SUPPLEMENTAL SDR** EMERGENCY LIGHTS INOP. DEFER EMERGENCY LIGHTS IAW MEL 33-50-4. DMP C/W INSTALLED PLACARD ASSIGNED M772946 TRIED REPLACIN
- [SDR IPXA2021090773666](https://openairdocs.org/sdr/IPXA2021090773666), Sep 3, 2021: INDICATOR. INOPERATIVE. INSPECTION TYPE:N/AL-1 DOOR EVAC SLIDE REMOTE PRESSURE PRESS TO TEST IND INOP. DEFERRED PER MEL 25-61-2 M 755635 ASSIGNED C/W DMP VERIFIED SLIDE PRESSURE GOOD L
- [SDR IPXA2021033067543](https://openairdocs.org/sdr/IPXA2021033067543), Mar 23, 2021: FLOOR SUPPORT. CORRODED. INSPECTION TYPE: 3C FLOOR SUPPORT ANGLE IS CORRODED AT STA. 1387. REMOVED, FABRICATED AND REPLACED SUPPORT ANGLE IAW DWG. AEA0397 AND SRM 51-35-01. (MINOR)
- [SDR IPXA2021032967438](https://openairdocs.org/sdr/IPXA2021032967438), Mar 22, 2021: SEAT TRACK. CORRODED. INSPECTION TYPE:3CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 1501 TO 1521 AT X= -107.25.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 1501 TO 1521 AT X= -107.
- [SDR IPXA2021033067531](https://openairdocs.org/sdr/IPXA2021033067531), Mar 7, 2021: SKIN. CRACKED. INSPECTION TYPE:3CL/H WING LOWER SKIN FUEL ACCESS PANEL BETWEEN STA. XORS. 683.4 TO XORS. 713.6 HAS 2 EA. SCREW HOLES WITH CRACKS.REPAIRED L/H LOWER SKIN IAW SR
- [SDR IPXA2021032867387](https://openairdocs.org/sdr/IPXA2021032867387), Mar 4, 2021: SEAT TRACK. CORRODED. INSPECTION TYPE:3CMAIN CABIN SEAT TRACK IS CORRODED BETWEEN STA. 745 TO 800 AT X= 8.50.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 745 TO 800 AT X= 8.50 IAW SRM 5
- [SDR IPXA2021032867384](https://openairdocs.org/sdr/IPXA2021032867384), Mar 4, 2021: INTERCOSTAL. CRACKED. INSPECTION TYPE:3CFWD. CARGO INTERCOSTAL IS CRACKED AT STA. 6-40 AND LOING. 42L.REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG. ACA7049 AND SRM 51-33-01. 
- [SDR IPXA2021032867382](https://openairdocs.org/sdr/IPXA2021032867382), Mar 4, 2021: SUPPORT FITTING. CRACKED. INSPECTION TYPE:3CCENTER TANK SUPPORT FITTING IS CRACKED AT STA. 1156 AND X= 01.REMOVED, FABRICATED AND REPLACED FITTING IAW DWG. APB7350 AND SRM 51-33-01. (MIN
- [SDR IPXA2021032867389](https://openairdocs.org/sdr/IPXA2021032867389), Mar 3, 2021: SEAT TRACK. CORRODED. INSPECTION TYPE:3CMAIN CABIN SEAT TRACK IS CORRODED AT STA. 1110 AND X= 8.50.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 1099 TO 1119 AT X= 8.50 IAW SRM 53-00-52 
- [SDR IPXA2021032867388](https://openairdocs.org/sdr/IPXA2021032867388), Mar 3, 2021: SEAT TRACK. CORRODED. INSPECTION TYPE:3CMAIN CABIN SEAT TRACK IS CORRODED AT STA. 1119 AND X= -8.50.REPAIRED CORRODED SEAT TRACK AT STA. 1119 AND X= -8.50 IAW SRM 53-00-52 REPAIR 5 F
- [SDR IPXA2021032867386](https://openairdocs.org/sdr/IPXA2021032867386), Mar 3, 2021: CARGO TRACK. CORRODED. INSPECTION TYPE:3CAFT CARGO SEAT TRACK IS CORRODED BETWEEN STA. 1841-1967 AT X= -20.REMOVED, FABRICATED AND REPLACED SEAT TRACK BETWEEN STA. 1841-1967 AT X= -20
- [SDR IPXA2021032867385](https://openairdocs.org/sdr/IPXA2021032867385), Mar 3, 2021: RETAINER. CRACKED. INSPECTION TYPE:3CCENTER CARGOFLOOR PANEL RETAINER IS CRACKED AT STA. 1521 AND RBL 26.REMOVED, FABRICATED AND REPLACED RETAINER IAW DWG. AEA0341 AND SRM 51-31-0
- [SDR IPXA2021032867383](https://openairdocs.org/sdr/IPXA2021032867383), Mar 3, 2021: ATTACH ANGLE. CRACKED. INSPECTION TYPE:3CCENTER CARO SLOPE PANEL ATTACH ANGLE IS CRACKED AT STA. 1661 L/H SIDE.REMOVED, FABRICATED AND REPLACED SLOPE PANEL ATTACH ANGLE IAW VT-SAA EA 
- [SDR IPXA2021032867381](https://openairdocs.org/sdr/IPXA2021032867381), Mar 3, 2021: STIFFENER. CRACKED. INSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LBL 25.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-31-01. (M
- [SDR IPXA2021032867380](https://openairdocs.org/sdr/IPXA2021032867380), Mar 3, 2021: FLOOR SUPPORT. CORRODED. INSPECTION TYPE:3CAFT CARGO FLOOR SUPPORT IS CORRODED AT STA. 1964 L/H SIDEUNDER PANEL 187DF.REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG. AGA7195 AND SRM 5
- [SDR IPXA2021032867377](https://openairdocs.org/sdr/IPXA2021032867377), Mar 3, 2021: STIFFENER. CRACKED. INSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LBL 19.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-33-01. (M
- [SDR IPXA2021032867376](https://openairdocs.org/sdr/IPXA2021032867376), Mar 3, 2021: SUPPORT. CRACKED. INSPECTION TYPE:3CCENTER CARGO FLOOR BEAM SUPPORT IS CRACKED AT STA. 5-53, RBL=18.REMOVED, FABRICATED AND REPLACED FLOOR BEAM SUPPORT IAW DWG ADA0033 AND SRM 51
- [SDR IPXA2021032867375](https://openairdocs.org/sdr/IPXA2021032867375), Mar 3, 2021: SUPPORT. CRACKED. INSPECTION TYPE:3CCENTER CARGO FLOOR BEAM SUPPORT IS CRACKED AT STA. 5-32, RBL=18.REMOVED, FABRICATED AND REPLACED FLOOR BEAM SUPPORT IAW DWG. AFA3168 AND SRM 5
- [SDR IPXA2021032767357](https://openairdocs.org/sdr/IPXA2021032767357), Mar 3, 2021: TRUSS FITTING. CRACKED. INSPECTION TYPE:3CCAC COMPARTMENT LONGERON 27R TRUSS FITTING AT STA 1159 IS CRACKED.REMOVED AND REPLACED CRACKED CAC COMPARTMENT LONGERON 27R TRUSS FITTING AT S
- [SDR IPXA2021032767356](https://openairdocs.org/sdr/IPXA2021032767356), Mar 3, 2021: STIFFENER. CHAFED. INSPECTION TYPE:3CFWD TAIL CONE R/H PATIO DOOR UPPER FWD STIFFENER IS CHAFED.REMOVED AND REPLACED CHAFED FWD TAIL CONE R/H PATIO DOOR UPPER FWD STIFFENER IAW SR
- [SDR IPXA2021032767354](https://openairdocs.org/sdr/IPXA2021032767354), Mar 3, 2021: BEAM. BENT. INSPECTION TYPE:3CFWD TAIL CONE FWD UPPER INTERCOSTAL (BEAM) AND WEB ARE BENT AT TAIL CONE SAFETY LATCH.REMOVED AND REPLACED BENT FWD TAIL CONE FWD UPPER INTERC
- [SDR IPXA2021032767353](https://openairdocs.org/sdr/IPXA2021032767353), Mar 3, 2021: FRAME. CRACKED. INSPECTION TYPE:3CFWD TAIL CONE R/H AFT FRAME IS CRACKED AT UPPER LATCH KEEPER.REPAIRED CRACKED FWD TAIL CONE R/H AFT FRAME AT UPPER LATCH KEEPER IAW SRM 53-80-
- [SDR IPXA2021032767352](https://openairdocs.org/sdr/IPXA2021032767352), Mar 3, 2021: STRINGER CLIP. CRACKED. INSPECTION TYPE:3C#1 MAIN FUEL TANK STRINGER 38 CLIP IS CRACKED AT STA XORS 506.REMOVED AND REPLACED CRACKED #1 MAIN FUEL TANK STRINGER CLIP AT STA XORS 506 IAW
- [SDR IPXA2021040967981](https://openairdocs.org/sdr/IPXA2021040967981), Mar 2, 2021: TEE FITTING. CRACKED. INSPECTION TYPE:3CMAIN CABIN LONGERON 15R TEE ANGLE BRACKET IS CRACKED AT STA 1341.REMOVED AND REPLACED CRACKED MAIN CABIN LONGERON 15R TEE ANGLE BRACKET AT STA
- [SDR IPXA2021040967980](https://openairdocs.org/sdr/IPXA2021040967980), Mar 2, 2021: TEE FITTING. CRACKED. INSPECTION TYPE:3CMAIN CABIN LONGERON 15L TEE ANGLE IS CRACKED BETWEEN STA 1219 AND STA 1239.REMOVED AND REPLACED CRACKED MAIN CABIN LONGERON 15L TEE ANGLE BETW
- [SDR IPXA2021040567778](https://openairdocs.org/sdr/IPXA2021040567778), Mar 2, 2021: FRAME. DENTED. INSPECTION TYPE:3CMAIN CABIN FRAME IS DENTED AT STA. 695 BETWEEN LONG. 12R TO 13R.REPAIRED DENTED FRAME AT STA. 695 BETWEEN LONG. 12R TO 13R IAW VT-SAA EA 011-5
- [SDR IPXA2021032867392](https://openairdocs.org/sdr/IPXA2021032867392), Mar 2, 2021: FLOORBEAM. CRACKED. INSPECTION TYPE:3CLOWER FWD. CARGO FLOOR BEAM IS CRACKED AT STA. 6-70, X= 57.5 AND Z= -98.REPAIRED CRACKED FLOOR BEAM AT STA. 6-70, X= 57.5 AND Z= -98 IAW SRM 5
- [SDR IPXA2021032867391](https://openairdocs.org/sdr/IPXA2021032867391), Mar 2, 2021: FLOORBEAM. CRACKED. INSPECTION TYPE:3CFWD. LOWER CARGO FLOOR BEAM IS CRACKED AT STA. 6-70, X= -57.5 AND Z= -98.REPAIRED CRACKED FLOOR BEAM AT STA. 6-70, X= -57.5 AND Z= -98 IAW SRM

All 101: https://openairdocs.org/aircraft/N264UP/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 (Boeing 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/N264UP/stcs.md

## Related

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

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