# N289UP: 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: [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: 48455 - Year built: 1992 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 21, 2007 - Certificate issued: June 12, 2007 - Expires: August 31, 2027 - Mode S code: A2F13A - 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=289UP - Page: https://openairdocs.org/aircraft/N289UP 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/N289UP/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 N289UP. ## FAA accident and incident reports None matched to N289UP. ## Service difficulty reports (333, 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 IPXA2025091625213](https://openairdocs.org/sdr/IPXA2025091625213), Sep 15, 2025: BATTERY PACK. DISCHARGED. DURING PDC, FOUND ŒEMERGENCY LIGHT BATTERY 1 LOW?, DURING TEST OF EMERGENCY LIGHTING POWER SUPPLY. R & R IAW AMM 33-51-01/401. LIGHTING CHECKS SERVICEABLE IAW A - [SDR IPXA2025071671035](https://openairdocs.org/sdr/IPXA2025071671035), Jun 29, 2025: AUTOPILOT SYS. INOPERATIVE. HAND FLEW THE ENTIRE FLIGHT WITH NO AUTOPILOT AND REQUIRED 3 DEGREES OF AILERON TRIM UPON FURTHER INVESTIGATION, PER MEL 27-13-2-0-1 AILERON DEFLECT INOP IS NOT - [SDR IPXA2025063071035](https://openairdocs.org/sdr/IPXA2025063071035), Jun 29, 2025: AUTOPILOT SYS. MALFUNCTIONED. HAND FLEW THE ENTIRE FLIGHT WITH NO AUTOPILOT AND REQUIRED 3 DEGREES OF AILERON TRIM UPON FURTHER INVESTIGATION, PER MEL 27-13-2-0-1 AILERON DEFLECT INOP IS NOT - [SDR IPXA2025062026148](https://openairdocs.org/sdr/IPXA2025062026148), Jun 20, 2025: ACTUATOR. OUT OF RANGE. AIR TURNBACK-AFTER TAKEOFF WHEN FLAPS AND SLATS RETRACTED LEVEL 2 ALERT AIL DEFLECT DISAGREE ALERT DISPLAYED. RAN QRH PROCEDURE, NO HELP, ALERT REMAINED. AIRCRA - [SDR IPXA2025041394788](https://openairdocs.org/sdr/IPXA2025041394788), Apr 13, 2025: BATTERY. DISCHARGED. EMERGENCY LIGHT BATTERY LOW EXIT SIGN WAS FIXED ON ASSIGNED FAULT, EMERGENCY LIGHTING TEST NOW PASSES PER AMM 33-51-01-700-802. THIS CLOSES 2842014, PLACARD REM - [SDR IPXA2025040777721](https://openairdocs.org/sdr/IPXA2025040777721), Mar 21, 2025: SKIN. CRACKED. **SUPPLEMENTAL SDR** STR- FOUND BENT FUSELAGE SKIN ABOVE RADOME RH HINGE. INSTALLED REPAIR DOUBLER AND REPAIR FILLER AT FUSELAGE SKIN ABOVE RADOME R/H IAW MD11 - [SDR IPXA2025040277721](https://openairdocs.org/sdr/IPXA2025040277721), Mar 21, 2025: SKIN. CRACKED. **SDR FILED OPEN** STR- FOUND BENT FUSELAGE SKIN ABOVE RADOME RH HINGE. ATA 53 OUT OF SEQUENCE VERIFIED STEP 2 AND 6 AND 7 RII - [SDR IPXA2025040874515](https://openairdocs.org/sdr/IPXA2025040874515), Mar 15, 2025: SKIN. CRACKED. LEFT HAND FWD. AC DOOR HAS A (POSSIBLE) CRACK ON THE OB SKIN OF DOOR, TOP SIDE. PM040-100, ATA 51-70. INSTALLED CONICAL WASHERS AND OK TO INSTALL REPAIR PARTS P - [SDR IPXA2025032274515](https://openairdocs.org/sdr/IPXA2025032274515), Mar 15, 2025: SKIN. NO DISCREPANCY. LEFT HAND FWD AC DOOR HAS A (POSSIBLE) CRACK ON THE OB SKIN OF DOOR, TOP SIDE. PM040-100, ATA 51-70 ACCOMPLISHED HFEC SURFACE/OPEN HOLRE INSP OF LH FWD AC DOOR - [SDR IPXA2025041052041](https://openairdocs.org/sdr/IPXA2025041052041), Mar 14, 2025: ANGLE. CORRODED. MAIN CABIN WING BOX R/H TUNNEL AREA HAS CORROSION JUST BEFORE THE PRESSURE PANEL. REMOVED AND REPLACED OUTBOARD SLANT PANEL ANGLE P/N ANB7392-2 PER DAC DWG ANB7 - [SDR IPXA2025032252041](https://openairdocs.org/sdr/IPXA2025032252041), Mar 14, 2025: ANGLE. CORRODED. MAIN CABIN WING BOX R/H TUNNEL AREA HAS CORROSION JUST BEFORE THE PRESSURE PANEL. OPEN - [SDR IPXA2025032033562](https://openairdocs.org/sdr/IPXA2025032033562), Mar 13, 2025: LONGERON. CORRODED. CORROSION FOUND IN CENTER CARGO SUMP FLOOR AREA AT STA 1701 R LONGERON 49. INSTALLED FABRICATED LONGERON REPLACMENT SECTION ON REF TRAVELER #70031341220001 IN L - [SDR IPXA2025032233562](https://openairdocs.org/sdr/IPXA2025032233562), Mar 13, 2025: LONGERON. CORRODED. CORROSION FOUND IN CENTER CARGO SUMP FLOOR AREA AT STA 1701 R LONGERON 49. VERIFIED STEP 19 RII. OPEN - [SDR IPXA2025032010109](https://openairdocs.org/sdr/IPXA2025032010109), Mar 12, 2025: LONGERON. CORRODED. LONGERON 47 RBL AT STA 6-95 (CAC BAY) HAS CORROSION. LOCATED AND DRILLED RPR SPLICE IN REF SRM 51-33-01-0G-0 . OK TO INSTALL RPR SPLICE AT LONGERON 47 RBL BTW S - [SDR IPXA2025032010191](https://openairdocs.org/sdr/IPXA2025032010191), Mar 12, 2025: LONGERON. CORRODED. LONGERON 52 AT STA 1120 (CAC BAY) HAS CORROSION, FWD OF ACCESS DOOR. NO STICKER, PM040, ATA 53-10. INSTALLED REPLAMENT LONGERON SPLICE AND REINSTALLED 2EA. INTE - [SDR IPXA2025032210191](https://openairdocs.org/sdr/IPXA2025032210191), Mar 12, 2025: LONGERON. CORRODED. LONGERON 52 AT STA 1120 (CAC BAY) HAS CORROSION, FWD OF ACCESS DOOR. NO STICKER, PM040, ATA 53-10 VERIFIED CORROSION REMOVAL STEP 2. OPEN - [SDR IPXA2025032210109](https://openairdocs.org/sdr/IPXA2025032210109), Mar 12, 2025: LONGERON. CORRODED. LONGERON 47 RBL AT STA 6-95 (CAC BAY) HAS CORROSION. NO STICKER, PM040, ATA 53-10 VERIIFED STEP 15 OK TO INSTALL REPLACEMENT SECTION OF L47R @ FS 6-50. OPEN - [SDR IPXA2025041078814](https://openairdocs.org/sdr/IPXA2025041078814), Mar 11, 2025: PAN. CRACKED. LWR FWD CORNER OF L/H CTR GEAR DOOR PAN IS CRACKED WHERE MKD. INSTALLED 2EA.SEALS AND RETAINERS 1 EA. SPLICE PLATE, 1 EA. RUBSTRIP AND 3EA.INSPECTION CAPS AND I - [SDR IPXA2025040378814](https://openairdocs.org/sdr/IPXA2025040378814), Mar 11, 2025: PAN. CRACKED. **SDR FILED OPEN** LWR FWD CORNER OF L/H CTR GEAR DOORPAN IS CRACKED WHERE MKD. TAG DBG-3. STRUCTURES SKILL. ATA 32-14. QC AUDIT C/W - [SDR IPXA2025022061243](https://openairdocs.org/sdr/IPXA2025022061243), Feb 20, 2025: CABLE. BROKEN. L1 DOOR AFT RAISE AND LOWERING CABLE BROKEN. INSTALLED SERVICABLE L1 DOOR AFT UPPER AND LOWER CABLES PER AMM 52-11-03. - [SDR IPXA2025022062146](https://openairdocs.org/sdr/IPXA2025022062146), Feb 20, 2025: PIN. BROKEN. L1 DOOR EMERGENCY EXIT DOOR LENS HAS A BROKEN GUIDE PIN. REMOVED AND INSTALLED NEW EXIT LIGHT ASSEMBLY IAW/ AMM 33-27-05 - [SDR IPXA2024110342655](https://openairdocs.org/sdr/IPXA2024110342655), Nov 2, 2024: CHAIN. BROKEN. L 1 DOOR EMERGENCY PNEUMATIC AIR MOTOR CHAIN FOUND BROKEN AND LAYING ABOVE OVERHEAD PANELS. REPLACED L1 DOOR EMERGENCY AIR MOTOR CHAIN IAW AMM 52-11-02. OPS NOR - [SDR IPXA2024110335327](https://openairdocs.org/sdr/IPXA2024110335327), Oct 29, 2024: SOLENOID. INTERMITTENT. L1 DOOR WONT OPERATE ELECTRICALLY. DRC SUBTASK C/W. T/S PER WDM 52-11-01-4. FOUND DOOR LOCK PIN SOLENOID MICRO SWITCH A2 AND A1 INTERMITTENTLY FAILING. REMOVED - [SDR IPXA2024102935327](https://openairdocs.org/sdr/IPXA2024102935327), Oct 29, 2024: ACTUATOR. INTERMITTENT. SDR FILED OPEN, L1 DOOR WONT OPERATE ELECTRICALLY TS PER FIM 52-11-03. DOOR OPERATES OPEN AND CLOSED INTERMITTENTLY. SUSPECT FAULTY ELECTRIC MOTOR ACTUATOR. ACT - [SDR IPXA2024101532795](https://openairdocs.org/sdr/IPXA2024101532795), Oct 15, 2024: DOOR. INTERMITTENT. DURING PREFLIGHT L1 DOOR ELECTRIC OPEN/CLOSE ELECTRIC FUNCTION FAILED. -END- PERFORMED OPS CHECK OF L1 DOOR USING BOTH INSIDE AND OUTSIDE SWITCHES. OPS CHECK GO - [SDR IPXA2024091999139](https://openairdocs.org/sdr/IPXA2024091999139), Sep 19, 2024: BATTERY. NO TEST. EMERGENCY LIGHT TEST SHOWS BATTERY 1 LOW AFTER TEST REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY IAW MD11 AMM 33-51-00/501 OPS CHECK GOOD THIS CLEARS. ME - [SDR IPXA2024082773585](https://openairdocs.org/sdr/IPXA2024082773585), Aug 27, 2024: DOOR. INOPERATIVE. L1 DOOR WILL NOT OPEN/CLOSE INTERNALLY OR EXTERNALLY USING SWITCH. OPERATED L1 DOOR NUMEROUS TIMES USING BOTH THE INTERIOR AND THE EXTERIOR SWITCH IAW MD-11 AMM - [SDR IPXA2024061291564](https://openairdocs.org/sdr/IPXA2024061291564), Jun 11, 2024: LAMP. INOPERATIVE. *** SUPPLEMENTAL SDR *** L1 DOOR DISARM LIGHT INOP RELAMPED L1 "DOOR DISARM" INDICATOR AND PERFORMED OPS CK IAW AMM 52-10-01-700-801 TABLE 201. OPS CK GOOD. - [SDR IPXA2024061191564](https://openairdocs.org/sdr/IPXA2024061191564), Jun 11, 2024: LAMP. INOPERATIVE. L1 DOOR DISARM LIGHT INOP RELAMPED L1 "DOOR DISARM" INDICATOR AND PERFORMED OPS CK IAW AMM 52-10-01-700-801 TABLE 201. OPS CK GOOD. - [SDR IPXA2024041862457](https://openairdocs.org/sdr/IPXA2024041862457), Apr 18, 2024: CONTROL UNIT. FAILED. BLOCK TURN-BACK AT 0829 DUE MECHANICAL. ON APU POWER JUST PRIOR TO ENGINE START ALL ELEC,EXCEPT STANDBY POWER, LOST WITH EXTERNAL POWER RECONNECTED POWER RESTOR - [SDR IPXA2024031204625](https://openairdocs.org/sdr/IPXA2024031204625), Mar 12, 2024: BATTERY. NO TEST. EMERGENCY LIGHT TEST BATTERY LOW EMERGENCY LIGHTING SYSTEM R/R EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01. OPS CKS GOOD. - [SDR IPXA2023122758810](https://openairdocs.org/sdr/IPXA2023122758810), Dec 27, 2023: BOTTLE. UNKNOWN. R1 DOOR ASSIST BOTTLE EMPTY. SERVICED R1 DOOR ASSIST BOTTLE PER AMM 12-25-04 AND PERFORMED LEAK CHECK. NO LEAKS NOTED. NO PRESSURE DROP NOTED FOR 2.5 HOURS. THI - [SDR IPXA2023101942411](https://openairdocs.org/sdr/IPXA2023101942411), Oct 18, 2023: UNKNOWN. UNKNOWN. L1 DOOR SLIDE DISARMED INDICATOR LIGHT BROKEN. C/W R&R'D L1 DOOR SLIDE DISARMED INDICATOR LIGHT IAW IPC 52-11-70-01-170 & SWPM 20-20-03. PERFORMED OPERATIONAL C - [SDR IPXA2023083094052](https://openairdocs.org/sdr/IPXA2023083094052), Aug 29, 2023: DOOR. INOPERATIVE. MAIN ENTRY DOOR WILL NOT SHUT. ONCE IT REACHES THE CLOSED POSITION IT REOPENS. THEN WITH DOOR SWITCH IN THE DOWN CLOSED POSITION THE DOOR OPENS. REMOVED AND REP - [SDR IPXA2023080993852](https://openairdocs.org/sdr/IPXA2023080993852), Aug 8, 2023: COVER. DETACHED. INSPECTION TYPE:NAEXIT LIGHT COVER ON 1L POPPED OFF WHILE OPENING 1L DOOR.REINSTALLED L1 DOOR EXIT LIGHT COVER PER M/M 33 27 05 - [SDR IPXA2023072693742](https://openairdocs.org/sdr/IPXA2023072693742), Jul 26, 2023: LIGHT. UNKNOWN. DURING PREFLIGHT. EMER LT BAT LO. ITEM DEFERRED PER MEL 33-50-4. DMP ACCOMPLISHED, CONTROL# M810768, PLACARDS INSTALLED.REPLACED EMERGENCY LIGHT BATTERY PACK PE - [SDR IPXA2023071993695](https://openairdocs.org/sdr/IPXA2023071993695), Jul 19, 2023: FRAME. GOUGED. INSPECTION TYPE:N/A*MAJOR REPAIR* DAMAGE ON FRAME STA 535 BETWEEN S32R - S33RREAPIRED IAW EO# MD11-5330-87120-B. - [SDR IPXA2023071993694](https://openairdocs.org/sdr/IPXA2023071993694), Jul 19, 2023: SKIN. CRACKED. INSPECTION TYPE:N/A*MAJOR REPAIR* RT SIDE AIR CONDITIONING DOOR JAMB CORNEWR SKIN CRACKEDREPAIRED IAW EO# MD11-5330-87120-B - [SDR IPXA2023071393655](https://openairdocs.org/sdr/IPXA2023071393655), Jul 13, 2023: DOOR. INOPERATIVE. L1- MAIN ENTRY DOOR/SLIDES - ALL CARGO CONFIG DOORS L1/R1 [EXTENDED OVERWATER] USE R1 DOOR. L1 DOOR DEFERRED PER MEL 52-10-3-1-2-1-2 / M810363 PLACARD INSTALLED - [SDR IPXA2023071293648](https://openairdocs.org/sdr/IPXA2023071293648), Jul 11, 2023: DOOR. INOPERATIVE. L CREW DOOR WILL NOT CLOSE LOCK FROM SWITCH ON INSIDE PANEL. DEFERRED PER MEL 52-10-3-1-2-1 M 810294 ASSIGNEDCLOSED DEFERRAL DUE TO MEL REF. CHANGE REVISION. RE - [SDR IPXA2023070893617](https://openairdocs.org/sdr/IPXA2023070893617), Jul 8, 2023: DOOR. INTERMITTENT. INSPECTION TYPE:NADURING PREFLIGHT THE L1 DOOR WAS INTERMITTENT.PERFORMED OPERATIONAL CHECK OF THE FORWARD PASSENGER DOOR LEFT IN NORMAL MODE IAW/ AMM 52-10-01 - [SDR IPXA2023032492215](https://openairdocs.org/sdr/IPXA2023032492215), Mar 14, 2023: WEB. WORN. INSPECTION TYPE:3CTAILCONE SNUBBER LOWER WEB IS WORN AT STA 2244.000REPLACED WORN WEB AT THE TAILCONE SNUBBER LOWER SIDE AT STA 2244.000 IAW 51-33-01 AND 51-35- - [SDR IPXA2023032792311](https://openairdocs.org/sdr/IPXA2023032792311), Mar 2, 2023: PANEL. CORRODED. INSPECTION TYPE:3CFOUND SKIN CORROSION AT L/H TUNNEL APPOX FS 808 - 824 LONGERON 37 TO L38.REPAIRED CORRODED SKIN AT L/H TUNNEL AT FS 808-824 AND LONGERON 37 - - [SDR IPXA2023032892351](https://openairdocs.org/sdr/IPXA2023032892351), Mar 2, 2023: SKIN. CORRODED. INSPECTION TYPE:3CR/H UPPER HORIZONTAL STAB AT FUSELAGE FAIRING ATTACH SKIN AREA HAS CORROSION AT BETWEEN STA Y=2122.881 - Y=2163.685.REPAIRED CORRODED SKIN AT - [SDR IPXA2023032392177](https://openairdocs.org/sdr/IPXA2023032392177), Mar 2, 2023: FITTING. GOUGED. INSPECTION TYPE:C3RCB WALL FITTING #12 IS GOUGED AT STATIC STRAP ATTACHMENTREPAIRED #12 RCB WALL FITTING IAW VTSAA EA 011-5340-01-A9876 I/R DATED 03/20/2023 (MI - [SDR IPXA2023032392169](https://openairdocs.org/sdr/IPXA2023032392169), Mar 2, 2023: FITTING. GOUGED. INSPECTION TYPE:C3RCB WALL FITTING # 6 IS GOUGEDREPAIRED # 6 FITTING IAW VTSAA EA011-5340-01 A9872 REV I/R AND UPS EOMD11-5340-862276-A.(MINOR) - [SDR IPXA2023032392168](https://openairdocs.org/sdr/IPXA2023032392168), Mar 2, 2023: FITTING. GOUGED. INSPECTION TYPE:C3RCB WALL FITTING # 13 IS GOUGED AT STATIC STRAP ATTACHMENT.REPAIRED # 13 RCB FITIING IAW VTSAA EA 011-5340-01-A9875 I/R DATED 03/20/2023. (MIN - [SDR IPXA2023032392167](https://openairdocs.org/sdr/IPXA2023032392167), Mar 2, 2023: FITTING. GOUGED. INSPECTION TYPE:C3RCB WALL FITTING #11 IS GOUGED AT STATIC STRAP ATTACHMENT .REPAIRED #11 POSITION RCB WALL FITTING IAW VTSAA EA 011-5340-01-A9877 IR DATED 03/2 - [SDR IPXA2023032592241](https://openairdocs.org/sdr/IPXA2023032592241), Mar 1, 2023: RUDDER. CORRODED. INSPECTION TYPE:3CAFT UPPER RUDDER L/H SIDE SURFACE HAS CORROSION.REPLACED AFT UPPER RUDDER IAW AMM 27-20-30 (MINOR) - [SDR IPXA2023032492214](https://openairdocs.org/sdr/IPXA2023032492214), Mar 1, 2023: LONGERON. CORRODED. INSPECTION TYPE:C3CAC INSIDE COMP BILGE AREA LONGERON 51R HAS CORROSION BELOW A/C BATTERY AT STA Y=1139REPLACED LONGERON 51R SECTION IN CAC COMP. BELOW A/C BATT All 333: https://openairdocs.org/aircraft/N289UP/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/N289UP/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 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.