# N287UP: 1994 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: [Pratt & Whitney PW4460](https://openairdocs.org/engine/pratt-whitney-pw4460) (registry code 51673)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE) (The Boeing Company), [TCDS E24NE](https://openairdocs.org/tcds/E24NE) (Pratt & Whitney Division) (OpenAirDocs)
- Serial number: 48539
- Year built: 1994
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 14, 2007
- Certificate issued: January 23, 2007
- Expires: May 31, 2029
- Mode S code: A2E9CC
- 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=287UP
- Page: https://openairdocs.org/aircraft/N287UP

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): 212 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 (Pratt & Whitney PW4460)

- [AD 2026-21-06](https://openairdocs.org/ad/2026-21-06): Engine Fuel and Control · Pratt & Whitney Division PW4052, PW4056, PW4060 and 10 more. Effective Nov 23, 2026
- [AD 2018-13-02](https://openairdocs.org/ad/2018-13-02): Turbine Engine Combustion Section · Pratt & Whitney Division PW4052, PW4056, PW4060 and 7 more. Effective Jul 20, 2018
- [AD 2016-08-09](https://openairdocs.org/ad/2016-08-09): HPC 10th stage disk · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Jun 1, 2016
- [AD 2015-22-03](https://openairdocs.org/ad/2015-22-03): LPT 4th stage IAS · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Dec 1, 2015
- [AD 2012-22-16](https://openairdocs.org/ad/2012-22-16): 3rd stage LPT duct segments · Pratt & Whitney Division PW4050, PW4052, PW4056 and 13 more. Effective Dec 19, 2012
- [AD 2012-14-09](https://openairdocs.org/ad/2012-14-09): 3rd and 4th stage vane fractures · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Nov 7, 2012
- [AD 2012-18-17](https://openairdocs.org/ad/2012-18-17): HPC drum rotor disk assembly · Pratt & Whitney Division PW4052, PW4056, PW4060 and 16 more. Effective Oct 22, 2012
- [AD 2012-18-03](https://openairdocs.org/ad/2012-18-03): 1st stage HPT air seal rings · Pratt & Whitney Division PW4050, PW4052, PW4056 and 18 more. Effective Oct 11, 2012
- [AD 2012-16-01](https://openairdocs.org/ad/2012-16-01): High-pressure turbine (HPT) stage 1 front hubs · Pratt & Whitney Division PW4052, PW4056, PW4060 and 14 more. Effective Sep 28, 2012
- [AD 2012-06-18](https://openairdocs.org/ad/2012-06-18): Engine · Pratt & Whitney Division PW4050, PW4052, PW4056 and 13 more. Effective Apr 27, 2012
- [AD 2012-04-04](https://openairdocs.org/ad/2012-04-04): fuel metering units (FMUs) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 13 more. Effective Apr 5, 2012
- [AD 2011-25-09](https://openairdocs.org/ad/2011-25-09): PW4000 turbofan engines · Pratt & Whitney Division PW4050, PW4052, PW4056 and 18 more. Effective Jan 10, 2012
- [AD 2010-24-14](https://openairdocs.org/ad/2010-24-14): HPC 10th stage disk · Pratt & Whitney Division PW4050, PW4052, PW4056 and 17 more. Effective Jan 21, 2011
- [AD 2010-24-09](https://openairdocs.org/ad/2010-24-09): No. 3 bearing oil pressure tubes · Pratt & Whitney Division PW4050, PW4052, PW4056 and 34 more. Effective Dec 28, 2010
- [AD 2008-24-13](https://openairdocs.org/ad/2008-24-13): Electronic engine controls (EECs) · Pratt & Whitney Division PW4052, PW4056, PW4060 and 6 more. Effective Jan 8, 2009
- [AD 2005-25-09](https://openairdocs.org/ad/2005-25-09): Engine manufacturer's time limits section (TLS) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 26 more. Effective Jun 12, 2006
- [AD 2003-19-15](https://openairdocs.org/ad/2003-19-15): High-Pressure-Compressor (HPC) Surges · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Oct 30, 2003
- [AD 2002-12-15](https://openairdocs.org/ad/2002-12-15): Front Drum Rotors · Pratt & Whitney Division PW4052, PW4056, PW4060 and 6 more. Effective Jul 31, 2002
- [AD 2001-05-07](https://openairdocs.org/ad/2001-05-07): Low Pressure Turbine (LPT) 4th Stage Air Seal · Pratt & Whitney Division PW4052, PW4056, PW4060 and 11 more. Effective Mar 30, 2001
- [AD 99-15-01](https://openairdocs.org/ad/99-15-01): Low Pressure Turbine Disks · Pratt & Whitney Division PW4056, PW4152, PW4156A and 3 more. Effective Sep 14, 1999
- [AD 98-23-08](https://openairdocs.org/ad/98-23-08): High Pressure Compressor  Blade Tips · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Jan 12, 1999
- [AD 98-19-03](https://openairdocs.org/ad/98-19-03): High Pressure Turbine Rotating Airseals · Pratt & Whitney Division PW4052, PW4056, PW4060 and 9 more. Effective Nov 9, 1998
- [AD 96-13-08](https://openairdocs.org/ad/96-13-08): AFT Cascade Support Frame Assembly · Pratt & Whitney assembly Part Number 221D5015, Revision A (STC SE744NE). Effective Aug 1, 1996
- [AD 90-22-02](https://openairdocs.org/ad/90-22-02): Low Pressure Turbine Shaft · Pratt & Whitney Division PW4050, PW4052, PW4056 and 6 more. Effective Oct 18, 1990

### 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 2010-18-13](https://openairdocs.org/ad/2010-18-13) (historical): Blade · Pratt & Whitney Division PW4052, PW4056, PW4060 and 16 more. Effective Oct 18, 2010
- [AD 2003-11-18](https://openairdocs.org/ad/2003-11-18) (historical): High-Pressure-Compressor (HPC) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Jul 7, 2003
- [AD 2002-21-10](https://openairdocs.org/ad/2002-21-10) (historical): High pressure compressor (HPC) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Nov 12, 2002
- [AD 2002-03-08](https://openairdocs.org/ad/2002-03-08) (historical): Time Limits Section of Engine Manuals (EM's) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 25 more. Effective Apr 16, 2002
- [AD 2001-25-11](https://openairdocs.org/ad/2001-25-11) (historical): Compressor Surges · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Jan 17, 2002
- [AD 2001-20-13](https://openairdocs.org/ad/2001-20-13) (historical): High Pressure Compressor Front Drum Rotors · Pratt & Whitney Division PW4052, PW4056, PW4060 and 6 more. Effective Nov 16, 2001
- [AD 2001-15-12](https://openairdocs.org/ad/2001-15-12) (historical): High Pressure Compressors (HPC) · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective Aug 10, 2001
- [AD 2001-09-07](https://openairdocs.org/ad/2001-09-07) (historical): High Pressure Compressor (HPC) Surge · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more. Effective May 14, 2001
- [AD 2001-08-52](https://openairdocs.org/ad/2001-08-52) (historical): Multiple-engine power loss due to HPC surges · Pratt & Whitney Division PW4050, PW4052, PW4056 and 12 more
- [AD 2000-25-06](https://openairdocs.org/ad/2000-25-06) (historical): Low Pressure Turbine (LPT) 4th Stage Air Seal · Pratt & Whitney Division PW4052, PW4056, PW4060 and 11 more. Effective Dec 29, 2000
- [AD 2000-22-01](https://openairdocs.org/ad/2000-22-01) (historical): High Pressure Compressor Cutback Stator · Pratt & Whitney Division PW4050, PW4052, PW4056 and 6 more. Effective Nov 9, 2000
- [AD 2000-12-02](https://openairdocs.org/ad/2000-12-02) (historical): Critical Life-Limited Part · Pratt & Whitney Division PW4050, PW4052, PW4056 and 24 more. Effective Sep 13, 2000
- [AD 99-17-16](https://openairdocs.org/ad/99-17-16) (historical): Pratt & Whitney Division PW4050, PW4052, PW4056 and 11 more. Effective Sep 24, 1999
- [AD 99-08-15](https://openairdocs.org/ad/99-08-15) (historical): Pratt & Whitney Division PW4050, PW4052, PW4056 and 20 more. Effective May 13, 1999

All 251: https://openairdocs.org/aircraft/N287UP/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 2025-06](https://openairdocs.org/saib/2025-06): High Pressure Turbines. Issued Jul 22, 2025
- [SAIB NE-19-02](https://openairdocs.org/saib/NE-19-02): Turbine Engine Compressor Section -- Low-pressure turbine uncontainment. Issued Feb 19, 2019
- [SAIB NE-16-01R1](https://openairdocs.org/saib/NE-16-01R1): Turbine Section. Issued Jan 14, 2016
- [SAIB NE-15-19](https://openairdocs.org/saib/NE-15-19): Turbine Section. Issued Jul 14, 2015
- [SAIB NE-13-31](https://openairdocs.org/saib/NE-13-31): Turbine Engine Oil System  Scavenge Oil Tube Coking and Proper Cleaning at Overhaul. Issued May 9, 2013
- [SAIB NE-16-01](https://openairdocs.org/saib/NE-16-01) (historical): Turbine Section. Issued Oct 5, 2015

## NTSB investigations

None matched to N287UP.

## FAA accident and incident reports

None matched to N287UP.

## Service difficulty reports (343, 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 IPXA2025121765208](https://openairdocs.org/sdr/IPXA2025121765208), Dec 16, 2025: SLIDE. NO DISCREPANCY. R1 SLIDE LOCK PIN INSTALLED INSTALLED LOCK PIN INTO REGULATOR/VALVE ASSY @ R1 SLIDE IRW MD11 AMM 25-61-15-000-801 STEP C (1) FOM SLIDE DEACTIVATION REF SUBTASK 
- [SDR IPXA2025121600179](https://openairdocs.org/sdr/IPXA2025121600179), Dec 16, 2025: SLIDE. NO DISCREPANCY. L1 SLIDE LOCK PIN INSTALLED INSTALLED LOCK PIN INTO REGULATOR/VALVE ASSY @ L1 SLIDE IRW MD11 AMM 25-61-15-000-801 STEP C (1) FOM SLIDE DEACTIVATION REF SUBTASK 
- [SDR IPXA2025090267453](https://openairdocs.org/sdr/IPXA2025090267453), Sep 2, 2025: BATTERY PACK. INOPERATIVE. EMER LT BAT 1 LO ON STATUS PAGE. R & R EMER SUPPLY BATTERY IAW AMM 33-51-01-401.
- [SDR IPXA2025061301745](https://openairdocs.org/sdr/IPXA2025061301745), Jun 13, 2025: SLIDE. MISOVERHAULED. FOUND R1 DOOR SLIDE HANGING DOWN AND INCORRECTLY PACKED IN DOOR HOUSING. DOOR SLIDE IS REMOVED. INSTALLED THE R1 EVACUATION SLIDE/RAFT AND CONTAINER IAW AMM 25-
- [SDR IPXA2024112225630](https://openairdocs.org/sdr/IPXA2024112225630), Nov 1, 2024: PANEL. CRACKED. L1 DOOR LWR PANEL P/N AWE7758-11 IS CRACK, 52-10. INSTALLED L1 DOOR LOWER ACCESS PANEL P/N AWE7758-11 IN REF TO MD-11 SRM 51-31-01. REVIEWED.
- [SDR IPXA2024110425630](https://openairdocs.org/sdr/IPXA2024110425630), Nov 1, 2024: PANEL. CRACKED. L1 DOOR LWR PANEL P/N AWE7758-11 IS CRACK, 52-10 VERIFIED STEP 3 IS C/W
- [SDR IPXA2024111667686](https://openairdocs.org/sdr/IPXA2024111667686), Oct 25, 2024: ROLLER TRAY. CORRODED. FWD CARGO LOADING SYSTEM TRAY ASSY HAS CORROSION AT STA 1099 (114-12) ATA 53-10. ACCOMPLISHED EO-92095-REQ1 & VT-SAA EA 011-2555-01-B0305 I/R. VERIFIED REPAIR I
- [SDR IPXA2024111467702](https://openairdocs.org/sdr/IPXA2024111467702), Oct 25, 2024: FLOOR PANEL. DAMAGED. FWD CARGO FLOOR PANEL 127CH AND 127AH (PANELS P/N WSP1126-507 2EA) CORNER DAMAGED. (114-13) FABRICATED FWD CARGO FLR PANEL 127CH IAW SREO-27386-REQ001/ DWG/SAMP
- [SDR IPXA2024110620506](https://openairdocs.org/sdr/IPXA2024110620506), Oct 24, 2024: SKIN. DENTED. NOSE LOWER FUSEIAGE SKIN HAS A DENT NOT IN THE ADM MAPPING AT STA 380 BETWEEN LONGERON 51R AND 52 . MARK MM001. ACCOMPLISHED REPAIR PER MD11 53-00-01-2R-1 REPAI
- [SDR IPXA2024112258138](https://openairdocs.org/sdr/IPXA2024112258138), Oct 21, 2024: PANEL. BROKEN. L-1 ENTRY DOOR SLIDING CEILING PANEL EXIT' SIGN ESCUTCHEON IS BROKEN, HELD ON WITH CARGO PIT TAPE. MKD AS DBT-100. APG SKILL. ATA 52-10. REMOVED AND REPLACED GR
- [SDR IPXA2024102258138](https://openairdocs.org/sdr/IPXA2024102258138), Oct 21, 2024: STRUCTURE. BROKEN. **SDR FILED OPEN**L-1 ENTRY DOOR SLIDING CEILING PANEL EXIT' SIGN ESCUTCHEON IS BROKEN, HELD ON WITH CARGO PIT TAPE. MKD AS DBT-100. APG SKILL. ATA 52-10.
- [SDR IPXA2024080579730](https://openairdocs.org/sdr/IPXA2024080579730), Aug 3, 2024: WINDOW. DELAMINATED. L1 WINDOW DELAMINATED AND CRACKED R/R L1 WINDOW PER AMM 56-11-01-401 CONFIG 1. OPS CK NORMAL. ACCOMPLISHED RII STEPS AS REQUIRED PER GMM 04.02.01.15 CHAPTER 56 
- [SDR IPXA2024070284184](https://openairdocs.org/sdr/IPXA2024070284184), Jun 16, 2024: SKIN. DENTED. DENT ON AFT UPPER FUSELAGE VERIFIED ALL REPAIR STEPS COMPLETED REF EO-90533-REQ3 [T3F18E004RSS0].
- [SDR IPXA2024061684184](https://openairdocs.org/sdr/IPXA2024061684184), Jun 16, 2024: SKIN. DENTED. DENT ON AFT UPPER FUSELAGE.
- [SDR IPXA2023030191439](https://openairdocs.org/sdr/IPXA2023030191439), Feb 28, 2023: RESTRAINT. DISLODGED. INSPECTION TYPE:N/APBE RESTRAINT SYSTEM ON LEFT BULKHEAD NEEDS REPAIR. PBE DISLODGED DURING TAKEOFF ROLLRESECURED PBE RESTRAINT SYSTEM ON L BULKHEAD AS REQ'D IA
- [SDR IPXA2022111988232](https://openairdocs.org/sdr/IPXA2022111988232), Nov 18, 2022: LIMIT SWITCH. INOPERATIVE. R1 ENTRY DOOR INOP. R/R UP LIMIT SWITCH ON R1 DOOR & OPS CHECK GOOD IAW AMM 52-16-01.
- [SDR IPXA2022102487437](https://openairdocs.org/sdr/IPXA2022102487437), Oct 18, 2022: FLOOR SUPPORT. BROKEN. INSPECTION TYPE:3C, SLOPE PANEL ATTACH FLOOR SUPPORT AT BS 1721 FOUND BROKEN AT LT FLOOR LEVEL.REMOVED, REPLACED FLOOR SUPPORT IAW SRM 51-31-01, 51-35-01 (MINOR
- [SDR IPXA2022102787567](https://openairdocs.org/sdr/IPXA2022102787567), Oct 4, 2022: HINGE. CORRODED. INSPECTION TYPE:3CL/H I/B FLAP O/B FWD HINGE LWR LUG I/B FACE HAS CORROSION.REPAIRED L/H I/B FLAP O/B FWD HINGE LWR LUG I/B FACE IAW VT-SAA EA 011-5740-01-A9735
- [SDR IPXA2022102787563](https://openairdocs.org/sdr/IPXA2022102787563), Oct 4, 2022: HINGE. CORRODED. INSPECTION TYPE:3CL/H I/B FLAP O/B FWD HINGE LWR LUG O/B FACE HAS CORROSION.REPAIRED L/H I/B FLAP O/B FWD HINGE LWR LUG IAW VT-SAA EA 011-5740-01-A9735 I/R AND 
- [SDR IPXA2022102687533](https://openairdocs.org/sdr/IPXA2022102687533), Oct 4, 2022: HINGE FITTING. CORRODED. INSPECTION TYPE:3C, R/H I/B FLAP O/B FWD HINGE LWR LUG O/B FACE HAS CORROSION.REPAIRED R/H I/B FLAP O/B FWD HINGE LWR LUG O/B FACE IAW VT-SAA EA 011-5740-01-A97
- [SDR IPXA2022102687532](https://openairdocs.org/sdr/IPXA2022102687532), Oct 4, 2022: HINGE FITTING. CORRODED. INSPECTION TYPE:3CR/H I/B FLAP O/B FWD HINGE LWR I/B FACE HAS CORROSION.REPAIRED R/H I/B FLAP O/B FWD HINGE I/B FACE IAW EA 011-5740-01-A9736 REV I/R AND EO MD1
- [SDR IPXA2022102687531](https://openairdocs.org/sdr/IPXA2022102687531), Oct 4, 2022: HINGE FITTING. CORRODED. INSPECTION TYPE:3C, R/H AFT I/B FLAP O/B LWR BORE HOLE HAS CORROSION.REPAIRED R/H AFT I/B FLAP HINGE O/B LWR BORE IAW EA 011-5750-01-A9734 REV I/R AND EO MD11-5
- [SDR IPXA2022102687535](https://openairdocs.org/sdr/IPXA2022102687535), Oct 4, 2022: HINGE FITTING. WORN. INSPECTION TYPE:3C, L/H I/B AFT FLAP O/B HINGE I/B LWR BORE HOLE IS WORN.REPAIRED L/H I/B AFT FLAP O/B HINGE I/B LWR BORE IAW EA 011-5750-01-A9733 REV I/R AND U
- [SDR IPXA2022102687530](https://openairdocs.org/sdr/IPXA2022102687530), Oct 4, 2022: HINGE FITTING. CORRODED. INSPECTION TYPE:3CL/H O/B FLAP I/B AFT HINGE LWR I/B LUG BORE HOLE HAS CORROSION.REPAIRED L/H O/B FLAP I/B AFT HINGE LWR I/B LUG BORE IAW VT-SAA EA 011-5740-01-
- [SDR IPXA2022102587509](https://openairdocs.org/sdr/IPXA2022102587509), Oct 4, 2022: STRINGER. CRACKED. INSPECTION TYPE:3CCENTER UPPER AUXILIARY TANK STR 47 EXISTING REPAIR BETWEEN STA X-17 AND X=17 IS CRACKED.REPAIRED CRACKED STRINGER 47 AT STA XCW=-32.00,XCW=32.
- [SDR IPXA2022101987278](https://openairdocs.org/sdr/IPXA2022101987278), Oct 4, 2022: WINDOW FRAME. CORRODED. INSPECTION TYPE:3CWINDOW REPLACEMENT FOUND CORROSION ON LOWER VERTICAL WINDOW FRAME BETWEEN STA Y=275 - Y=295.REPAIRED VERTICAL WINDOW FRAME IAW VT-SAA EA 011-5
- [SDR IPXA2022101287082](https://openairdocs.org/sdr/IPXA2022101287082), Oct 4, 2022: SPAR. CRACKED. INSPECTION TYPE:3CCENTER UPPER AUXILIARY TANK FRONT SPAR CLIP BETWEEN STA X17 AND X46 IS CRACKED.REPLACED CRACKED CLIP IN CTR UPPER AUXILIARY TANK IAW SRM 51-33
- [SDR IPXA2022102787560](https://openairdocs.org/sdr/IPXA2022102787560), Oct 3, 2022: SKIN. DAMAGED. INSPECTION TYPE:3CNO REPAIR DOUBER HISTORY ON RUDDER ASS AFT UPPER SKIN STA ZV = 487.312 R/H AFT SIDE.REMOVED, REPAIRED EXISTING REPAIR DOUBLER ON AFT UPPER RUD
- [SDR IPXA2022102687534](https://openairdocs.org/sdr/IPXA2022102687534), Oct 1, 2022: ANGLE. CRACKED. INSPECTION TYPE:3C, LT I/B ELEVATOR ANGLE BRAKET AT STA STA XE=125.8 O/B SIDE IS CRACKED.REPAIRED CRACKED ANGLE AT STA XE=125.8 ON THE L/H I/B ELEVATOR IAW EA 0
- [SDR IPXA2022102587499](https://openairdocs.org/sdr/IPXA2022102587499), Sep 29, 2022: LONGERON SPLICE. CORRODED. INSPECTION TYPE:3CAFT CARGO BILGE AREA LONGERON 51L HAS A CLIP SPLICE WITH CORROSION AT STA 1941-1954.REMOVED, FABRICATIED, REPLACED THE CLIP SPLICE AT STA 1941
- [SDR IPXA2022102087315](https://openairdocs.org/sdr/IPXA2022102087315), Sep 29, 2022: WEB. CORRODED. INSPECTION TYPE:3CCENTER CARGO BLIGE AREA HAS A CLIP, VERTICAL INTERCOSTAL-WEB AT STA 1730 RBL5 WITH CORROSION.REPLACED THE CLIP, INTERCOSTAL-WEB IAW SRM 51-31-
- [SDR IPXA2022102087314](https://openairdocs.org/sdr/IPXA2022102087314), Sep 29, 2022: TEE FITTING. CORRODED. INSPECTION TYPE:3CCENTER CARGO BLIGE AT STA 1745 RBL5 HAS A TEE-CLIP WITH CORROSION.REPLACED TEE-CLIP AT STA 1745 RBL5 IAW SRM-51-31-01. (MINOR)
- [SDR IPXA2022101587151](https://openairdocs.org/sdr/IPXA2022101587151), Sep 29, 2022: SUPPORT BRACKET. CRACKED. INSPECTION TYPE:3CCAC COMPARTMENT R/H LRU RACK R/H LWR SUPPORT BRACKET IS CRACKED.REPLACED SUPPORT BRACKET IN THE CAC COMPARTMENT ON THE R/H LRU RACK IAW SRM 51
- [SDR IPXA2022101287076](https://openairdocs.org/sdr/IPXA2022101287076), Sep 28, 2022: SUPPORT. DAMAGED. INSPECTION TYPE:3CDAMAGED PANEL SUPPORT SIDE BRACE AT L/H O/B AILERON AT APPOX XORS 948.REPLACED DAMAGED SUPPORT IAW SRM 51-33-01 (MINOR)
- [SDR IPXA2022102087317](https://openairdocs.org/sdr/IPXA2022102087317), Sep 27, 2022: SKIN. DAMAGED. INSPECTION TYPE:3CL/H WING FIX L/E SKIN O/B OF #8 SLAT IS DAMAGED.REPAIRED FIX L/E SKIN IAW SRM 57-40-01 REPAIR 16. (MINOR)
- [SDR IPXA2022102787568](https://openairdocs.org/sdr/IPXA2022102787568), Sep 26, 2022: DOOR FRAME. GOUGED. INSPECTION TYPE:3C, CLG WHEEL WELL R/H FWD DOOR FRAME HAS A DEEP GOUGE. REPLACED FWD SIDE DOOR FRAME IAW SRM 51-35-01, 51-33-01. (MINOR)
- [SDR IPXA2022090285842](https://openairdocs.org/sdr/IPXA2022090285842), Sep 1, 2022: FLOOR SKIN. INOPERATIVE. INSPECTION TYPE:N/A**SDR FILED OPEN**L1 DOOR ELECTRICAL ACTUATION INOP. ITEM TRANSFERRED TO DEFERRAL IAW MEL 52-10-3-1-2-12. PLACARD INSTALLED MUST USE R-1 DOOR
- [SDR IPXA2021111175873](https://openairdocs.org/sdr/IPXA2021111175873), Nov 11, 2021: NONE. NONE. INSPECTION TYPE:N/A**SUPPLEMENTAL SDR ** L1 DOOR SLIDE PRESSURE GUAGE CANNOT BE READ THROUGH INSPECTION WINDOW. DEFERRED L1 SLIDE IAW MEL 52-10-3-1-2-1 REF M762
- [SDR IPXA2021100674649](https://openairdocs.org/sdr/IPXA2021100674649), Oct 5, 2021: NONE. NONE. INSPECTION TYPE:N/A**SUPPLEMENTAL SDR** EMERG LIGHT BAT 3 LO LEVEL ONE ALERT CAME ON DURING EMERGENCY LIGHT TEST DURING PRE FLIGHT. DEFERRED PER MEL 33-50-2 AND
- [SDR IPXA2021092974403](https://openairdocs.org/sdr/IPXA2021092974403), Sep 29, 2021: DOOR. BROKEN. INSPECTION TYPE:N/ALEFT FORWARD CREW ENTRY DOOR SNAPPED ITS CABLES DUING ELECTRICAL SWITCH OPENNINGR&R'D FWD AND AFT LEFT CABLES ON L1 DOOR PER AMM 52-11-03-000
- [SDR IPXA2021092074046](https://openairdocs.org/sdr/IPXA2021092074046), Sep 19, 2021: LIGHT. NO TEST. EMER LT BAT 3 LOW. DEFERRED EMERG LT SYS TEST FUNCTION UNDER MEL 33-50-2. ACCOMPLISHED DMP 33-50-2-. VERIFIED EMERG LTS ILLUMINATE. PLACARDED AFFECTED SWITCH. C
- [SDR IPXA2021050469001](https://openairdocs.org/sdr/IPXA2021050469001), May 3, 2021: BATTERY PACK. FAULTED. INSPECTION TYPE:NAEMERG LT BATT 1 FAULT.DEFERRED PER MEL33-50-4 M-743320 ASSIGNED DMP C/W PLACARD INSTALLED.R& R'D EMERGENCY POWER SUPPLY BATTRERY OPS CHECK GOO
- [SDR IPXA2020111562399](https://openairdocs.org/sdr/IPXA2020111562399), Nov 12, 2020: STIFFENER. CRACKED. INSPECTION TYPE: 2C INTERCOSTAL CRACKED NEAR RT MLG WHEEL WELL HYD RESV ASSEMBLY. REMOVED, FABRICATED, AND REPLACED STIFFENER, IAW DWG AEA7035 AND SRM 51-33-01.
- [SDR IPXA2020111562397](https://openairdocs.org/sdr/IPXA2020111562397), Nov 9, 2020: ANGLE. CORRODED. INSPECTION TYPE: 2C LT WING OUTBOARD LOWER TRAILING EDGE ANGLE CORRODED. REMOVED AND REPLACED CORRODED ANGLE AT LT WING OUTBOARD LOWER TRAILING EDGE, IAW SRM 51
- [SDR IPXA2020111562390](https://openairdocs.org/sdr/IPXA2020111562390), Nov 6, 2020: ANGLE. CRACKED. INSPECTION TYPE: 2C LT WING TRAILING EDGE SUPPORT PANEL CRACK AT AFT EDGE. REPAIRED CRACKED SUPPORT ANGLE AT LT WING TRAILING EDGE, IAW DWG ARC0679 AND SRM 51-3
- [SDR IPXA2020111562389](https://openairdocs.org/sdr/IPXA2020111562389), Nov 4, 2020: WEB. CRACKED. INSPECTION TYPE: 2C NR 3 PYLON STRUCTURE WEB CRACK AT UPPER END YUS STA 240.5. REPAIRED NR 3 PYLON UPPER CRACKED WEB AT YUS STA 240.5, IAW SRM 54-00-00 REPAIR G
- [SDR IPXA2020111262309](https://openairdocs.org/sdr/IPXA2020111262309), Nov 1, 2020: RIB. CRACKED. INSPECTION TYPE: 2C RT INBOARD AILERON LEADING EDGE RIB CRACK. REMOVED AND REPLACED RT INBOARD AILERON LEADING EDGE CRACKED RIB, IAW SRM 51-31-01 AND SRM 51-35-
- [SDR IPXA2020111162267](https://openairdocs.org/sdr/IPXA2020111162267), Nov 1, 2020: INTERCOSTAL. CRACKED. INSPECTION TYPE: 2C TAILCONE PATIO DECK RT LOWER INTERCOSTAL CRACK AT FWD END. REMOVED AND REPLACED TAILCONE PATIO DECK INTERCOSTAL AT FWD END, IAW SRM 51-35-01
- [SDR IPXA2020110662091](https://openairdocs.org/sdr/IPXA2020110662091), Oct 29, 2020: DOUBLER. CRACKED. INSPECTION TYPE: 2C RT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 653 TO 657.7. REPAIRED CRACKED RT WING FIXED LEADING EDGE BEADED DOUBLE
- [SDR IPXA2020110662090](https://openairdocs.org/sdr/IPXA2020110662090), Oct 29, 2020: DOUBLER. CRACKED. INSPECTION TYPE: 2C RT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 551 TO 555. REPAIRED CRACKED RT WING FIXED LEADING EDGE BEADED DOUBLER 

All 343: https://openairdocs.org/aircraft/N287UP/reports.md

## STCs that may be installed (OpenAirDocs) (122, 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 122: https://openairdocs.org/aircraft/N287UP/stcs.md

## Related

- Other Mcdonnell Douglas MD-11F aircraft: https://openairdocs.org/model/mcdonnell-douglas-md-11f/aircraft.md
- The Pratt & Whitney PW4460 engine: https://openairdocs.org/engine/pratt-whitney-pw4460.md

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