# N513SN: 1994 Mcdonnell Douglas MD-11

- Status: Valid registration
- Airframe: [Mcdonnell Douglas MD-11](https://openairdocs.org/model/mcdonnell-douglas-md-11) (registry code 3023602, 240 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: 48513
- Year built: 1994
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 13, 2016
- Certificate issued: July 29, 2015
- Expires: July 31, 2028
- Mode S code: A66E31
- Registered owner: [M48513 LLC](https://openairdocs.org/faa-owner/M48513%20LLC)
- Location: [Esters, FL](https://openairdocs.org/faa-place/FL/Esters)
- Owner type: LLC
- Owner's area on the map: 26.4357° N, 81.6973° W: Placed by OpenAirDocs at the center of ZIP code 33928, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=513SN
- Page: https://openairdocs.org/aircraft/N513SN

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): 230 in force

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

- [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 2007-19-13](https://openairdocs.org/ad/2007-19-13): Hydrolok retaining pin · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 66 more. Effective Oct 3, 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 2006-19-03](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 2004-22-20](https://openairdocs.org/ad/2004-22-20): Low base terminal boards · Boeing MD-11 and MD-11F. Effective Dec 14, 2004

### 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 2002-17-06](https://openairdocs.org/ad/2002-17-06) (historical): Galley Load Control Unit Within the No. 3 Bay Electrical Power Center · Boeing MD-11. Effective Sep 16, 2002
- [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 2002-14-05](https://openairdocs.org/ad/2002-14-05) (historical): Wire assembly terminal lugs · McDonnell Douglas MD-11. Effective Aug 23, 2002
- [AD 2001-21-05](https://openairdocs.org/ad/2001-21-05) (historical): Airplane Flight Manual--Flight Management Computers · McDonnell Douglas MD-11 Series (all). Effective Nov 26, 2001
- [AD 2001-17-12](https://openairdocs.org/ad/2001-17-12) (historical): Air Driven Generator Wire Assembly · McDonnell Douglas MD-11 Series (all). Effective Sep 26, 2001
- [AD 2001-17-09](https://openairdocs.org/ad/2001-17-09) (historical): Main Observer's Station · McDonnell Douglas MD-11 Series (all). Effective Sep 26, 2001
- [AD 2001-17-08](https://openairdocs.org/ad/2001-17-08) (historical): Number 2 Integrated Drive Generator · McDonnell Douglas MD-11 Series (all). Effective Sep 26, 2001
- [AD 2001-14-08](https://openairdocs.org/ad/2001-14-08) (historical): Electric Motors of the Auxiliary Hydraulic Pump · McDonnell Douglas DC-10 Series (all), MD-10-10F, MD-10-30F and 1 more. Effective Aug 16, 2001
- [AD 2001-07-08](https://openairdocs.org/ad/2001-07-08) (historical): Airplane Flight Manual - Limitations Section · McDonnell Douglas MD-11 Series (all). Effective Apr 25, 2001
- [AD 2000-24-15](https://openairdocs.org/ad/2000-24-15) (historical): Electrical Wiring · McDonnell Douglas MD-11 Series (all). Effective Jan 8, 2001
- [AD 2000-24-13](https://openairdocs.org/ad/2000-24-13) (historical): Main External Power Ground Cables · McDonnell Douglas MD-11 Series (all). Effective Jan 8, 2001
- [AD 2000-24-12](https://openairdocs.org/ad/2000-24-12) (historical): Center Accessory Compartment Terminal Strips Electrical Wires · McDonnell Douglas MD-11 Series (all). Effective Jan 8, 2001
- [AD 2000-24-11](https://openairdocs.org/ad/2000-24-11) (historical): Sliding Ceiling Panel Entry Light Connector · McDonnell Douglas MD-11 Series (all). Effective Jan 8, 2001
- [AD 2000-15-14](https://openairdocs.org/ad/2000-15-14) (historical): Remote Control Circuit Breakers · McDonnell Douglas MD-11 Series (all). Effective Aug 23, 2000
- [AD 2000-14-12](https://openairdocs.org/ad/2000-14-12) (historical): Upper and Lower Reading Lights in the Forward Crew Rest Area · McDonnell Douglas MD-11 Series (all). Effective Aug 23, 2000
- [AD 2000-14-18](https://openairdocs.org/ad/2000-14-18) (historical): Powered Drive Unit Power Wires · McDonnell Douglas MD-11 Series (all). Effective Aug 11, 2000
- [AD 2000-08-03](https://openairdocs.org/ad/2000-08-03) (historical): Cargo Control Units (CCU) · McDonnell Douglas MD-11 Series. Effective May 5, 2000
- [AD 2000-07-02](https://openairdocs.org/ad/2000-07-02) (historical): Map Light Assemblies · McDonnell Douglas MD-11 Series. Effective Apr 20, 2000
- [AD 2000-03-15](https://openairdocs.org/ad/2000-03-15) (historical): Terminal Strips · McDonnell Douglas MD-11 Series (all). Effective Mar 23, 2000
- [AD 2000-03-13](https://openairdocs.org/ad/2000-03-13) (historical): Wire Bundle Installation behind the First Observer's Station · McDonnell Douglas MD-11 Series (all). Effective Mar 23, 2000
- [AD 2000-03-12](https://openairdocs.org/ad/2000-03-12) (historical): Air Driven Generator (ADG) Wire Assembly · McDonnell Douglas MD-11 Series. Effective Mar 23, 2000
- [AD 2000-03-10](https://openairdocs.org/ad/2000-03-10) (historical): Sliding Ceiling Panel · McDonnell Douglas MD-11 Series. Effective Mar 23, 2000
- [AD 2000-05-01](https://openairdocs.org/ad/2000-05-01) (historical): Cargo Control Units (CCU) · McDonnell Douglas MD-11 Series. Effective Mar 20, 2000
- [AD 99-26-03 C1](https://openairdocs.org/ad/99-26-03-C1) (historical): Galley Load Control Unit (GLCU) · McDonnell Douglas MD-11 Series (all)
- [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 99-26-03](https://openairdocs.org/ad/99-26-03) (historical): Galley Load Control Unit (GLCU) · McDonnell Douglas MD-11 Series (all). Effective Jan 4, 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 98-25-11 R1](https://openairdocs.org/ad/98-25-11-R1) (historical): Sliding Ceiling Panel · McDonnell Douglas MD-11 Series (all). Effective Dec 28, 1998
- [AD 98-25-11](https://openairdocs.org/ad/98-25-11) (historical): Sliding Ceiling Panel · McDonnell Douglas MD-11 Series (all). Effective Dec 28, 1998
- [AD 98-24-51](https://openairdocs.org/ad/98-24-51) (historical): AFM - Autoland System · McDonnell Douglas MD-11 Series (all). Effective Dec 7, 1998
- [AD 98-24-02](https://openairdocs.org/ad/98-24-02) (historical): Electrical Failure In Dimmer Controls · McDonnell Douglas MD-11 Series (all). Effective Nov 30, 1998

All 306: https://openairdocs.org/aircraft/N513SN/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 N513SN.

## FAA accident and incident reports

None matched to N513SN.

## Service difficulty reports (49)

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 9WGA2023072051301](https://openairdocs.org/sdr/9WGA2023072051301), Jul 20, 2023: UNKNOWN. UNKNOWN. ON CLIMB OUT AUTO PILOT 2 INOP. THREE HOURS INTO FLIGHT AUTO PILOT 1 INOP. REMOVED AND REPLACED LEFT OUTBOARD AILERON LVDT PER AMM 27-13-34. PERFORMED FCC 2 RTS
- [SDR 9WGA2022111651301](https://openairdocs.org/sdr/9WGA2022111651301), Nov 16, 2022: CONTROLLER. INOPERATIVE. DISCREPANCY: LEVEL 2 "FUEL QTY/USED CHK" MESSAGE, FUEL BURN VS. QTY REMAIN DISCREPANCY, 1100KG AFTER 1.5 HOURS OF FLIGHT. CORRECTIVE ACTION: T/S IAW FIM 28-14-0
- [SDR 9WGA2022060651301](https://openairdocs.org/sdr/9WGA2022060651301), Jun 6, 2022: TIRE. FAILED. DISCREPANCY: ON TAKE-OFF ROLL, LEVEL 2 ALERT TIRE FAILURE, TAKE-OFF CONTINUED. DUMPED FUEL TO LANDING WEIGHT. AIR RETURNED TO ANC. CORRECTIVE ACTION: FAULT REVI
- [SDR 9WGA202109151301](https://openairdocs.org/sdr/9WGA202109151301), Sep 14, 2021: CABIN PRESSURE. MALFUNCTIONED. PACK 3 OFF DURING FLIGHT "CABIN AIRFLOW LOW" DURING CRUISE AND DESCENT UNTIL CABIN REGULATED ITSELF. CABIN NOT HOLDING CABIN PRESSURE AT ALTITUDE.
- [SDR 9WGA2021080655131](https://openairdocs.org/sdr/9WGA2021080655131), Aug 5, 2021: COMPRESSOR. VIBRATION. DIVERSION DUE TO ENG 3 VIB HIGH COMP OVER 4.0 ON CLIMB ON MULTIPLE OCCASION AND HAD TO RETARD #3 MORE THAN 1 CROWN TO REDUCE THE VIBRATION.
- [SDR 9WGA2021041951301](https://openairdocs.org/sdr/9WGA2021041951301), Apr 19, 2021: WARNING MESSAGE. ILLUMINATED. CABIN ALTITUDE ALERT ON DESCENT AT FL190.
- [SDR 9WGA201904230002](https://openairdocs.org/sdr/9WGA201904230002), Apr 23, 2019: SPAR CAP. CORRODED. DURING INSPECTION FOUND CORROSION ON LEFT WING UPPER REAR SPAR CAP BETWEEN XORS 1041.8 AND XORS 1046.8
- [SDR 9WGA2019041601](https://openairdocs.org/sdr/9WGA2019041601), Apr 16, 2019: LONGERON. CORRODED. LONGERON 52 E STA 6 - 33 HAS CORRODED SECTION
- [SDR KO0R201603110048](https://openairdocs.org/sdr/KO0R201603110048), Mar 11, 2016: LONGERON. CRACKED. FORWARD END OF LONGERON LOCATED AT BS 1540, LONGERON 48R IS CRACKED.
- [SDR KO0R201601260041](https://openairdocs.org/sdr/KO0R201601260041), Jan 26, 2016: SKIN. CORRODED. EVIDENCE OF CORROSION ON THE CTR WING TANK UPPER SURFACE AT STATION 1229, RBL 84.
- [SDR KO0R201601260040](https://openairdocs.org/sdr/KO0R201601260040), Jan 26, 2016: SKIN. CORRODED. EVIDENCE OF CORROSION ON THE CTR WING TANK UPPER SURFACE AT STATION 1229, RBL 78.
- [SDR KO0R201601260039](https://openairdocs.org/sdr/KO0R201601260039), Jan 26, 2016: SKIN. CORRODED. MAIN DECK CENTER SKIN HAS CORROSION AT WING TANK STR 8, BS 1281.0, LBL 103.5 AND 110.5.
- [SDR KO0R201601260038](https://openairdocs.org/sdr/KO0R201601260038), Jan 26, 2016: SKIN. CORRODED. MAIN DECK CTR WING, UPPER SKIN HAS CORROSION AT WING TANK STRINGER 19, STATION 1197.0, LBL 110.0.
- [SDR KO0R201601260037](https://openairdocs.org/sdr/KO0R201601260037), Jan 26, 2016: SKIN. CORRODED. MAIN DECK CTR WING, UPPER SKIN HAS CORROSION AT WING TANK, STRINGER 20, STATION 1189.0, LBL 112.0.
- [SDR KO0R201601260036](https://openairdocs.org/sdr/KO0R201601260036), Jan 26, 2016: STIFFENER. CRACKED. STATION 1912, LONGERON 28R, DAMAGED FRAME STIFFENER.
- [SDR KO0R201601260035](https://openairdocs.org/sdr/KO0R201601260035), Jan 26, 2016: SKIN PANEL. CRACKED. OUTER WING LOWER SKIN PANEL ACCESS DOOR CUT OUT, RT WING HAS 4 CRACK INDICATIONS IN FASTENER HOLES. WING STATION XORS 700.
- [SDR KO0R201601260034](https://openairdocs.org/sdr/KO0R201601260034), Jan 26, 2016: SKIN PANEL. CRACKED. OUTER WING LOWER SKIN PANEL ACCESS DOOR CUT OUT, LT WING HAS 3 EACH CRACK INDICATIONS IN FASTENER HOLES. WING STATION XORS 700.
- [SDR KO0R201601260033](https://openairdocs.org/sdr/KO0R201601260033), Jan 26, 2016: WINDOW FRAME. CORRODED. LEFT WINDSHIELD FRAME HAS NUMEROUS WINDOW MOUNTING HOLES & AREAS AROUND HOLES WITH CORROSION.
- [SDR KO0R201601260032](https://openairdocs.org/sdr/KO0R201601260032), Jan 26, 2016: WINDOW FRAME. CORRODED. RIGHT WINDSHIELD FRAME HAS SEVERAL HOLES & AREAS AROUND HOLES WITH CORROSION.
- [SDR KO0R201601060031](https://openairdocs.org/sdr/KO0R201601060031), Jan 6, 2016: SIGN. INOPERATIVE. L1 DOOR EMERGENCY EXIT SIGN FAILED. OPS CHECK OK.
- [SDR KO0R201601060030](https://openairdocs.org/sdr/KO0R201601060030), Jan 6, 2016: FAILSAFE. CORRODED. NR 1 PYLON HAS EVIDENCE OF CORROSION ON UPPER SPAR LOWER SURFACE AFT OF NACELLE BS 302, BULKHEAD AROUND MULTIPLE FASTENERS.
- [SDR KO0R201601060029](https://openairdocs.org/sdr/KO0R201601060029), Jan 6, 2016: SPAR. CORRODED. NR 1 PYLON HAS EVIDENCE OF CORROSION ON UPPER SPAR UPPER SURFACE AFT OF NACELLE BS 302 BULKHEAD AROUND SEVERAL FASTENERS.
- [SDR KO0R201601060028](https://openairdocs.org/sdr/KO0R201601060028), Jan 6, 2016: SPAR. CORRODED. NR 3 PYLON OTBD AFT UPPER SPAR WEB IS CORRODED AT NACELLE BS 350.
- [SDR KO0R201601060027](https://openairdocs.org/sdr/KO0R201601060027), Jan 6, 2016: SPAR. CORRODED. NR 3 PYLON AFT UPPER SPAR WEB IS CORRODED AT NACELLE BS 350.
- [SDR KO0R201601050026](https://openairdocs.org/sdr/KO0R201601050026), Jan 5, 2016: SUPPORT. CRACKED. LEFT WING INBD AILERON, SUPPORTING STRUCTURE AT STATION XORS 430, IS CRACKED IN 2 PLACES.
- [SDR KO0R201601050025](https://openairdocs.org/sdr/KO0R201601050025), Jan 5, 2016: STRINGER SPLICE. CRACKED. CRACKED STRINGER 31R SPLICE AT STATION 1921.
- [SDR KO0R201601050024](https://openairdocs.org/sdr/KO0R201601050024), Jan 5, 2016: SKIN. CORRODED. LEFT WING UPPER SKIN AT STRINGER 7, WING STATION 526 IS CORRODED.
- [SDR KO0R201601050023](https://openairdocs.org/sdr/KO0R201601050023), Jan 5, 2016: LONGERON. CORRODED. CORROSION ON LONGERON 12R, FROM STATION 1139 TO STATION 1159, MAIN DECK CROWN AREA.
- [SDR KO0R201601050022](https://openairdocs.org/sdr/KO0R201601050022), Jan 5, 2016: LONGERON. CORRODED. EXTRUDED LONGERON 19L AT STATION 1336 IS CORROSION.
- [SDR KO0R201601050021](https://openairdocs.org/sdr/KO0R201601050021), Jan 5, 2016: LONGERON FITTING. CORRODED. CENTER ACCESSORY COMPARTMENT STATION 6.70 - 6.90, LONGERON 52, END FITTING HAS CORROSION RUNNING FWD TO AFT.
- [SDR KO0R201601050020](https://openairdocs.org/sdr/KO0R201601050020), Jan 5, 2016: SKIN. CORRODED. LEFT WING TIP LOWER SURFACE HAS CORROSION TOWARDS THE TRAILING EDGE.
- [SDR KO0R201601050019](https://openairdocs.org/sdr/KO0R201601050019), Jan 5, 2016: LONGERON. CORRODED. CORROSION ON LONGERON 48R, BETWEEN STATION 5-73 TO 5-93.
- [SDR KO0R2016010500018](https://openairdocs.org/sdr/KO0R2016010500018), Jan 5, 2016: SKIN. CORRODED. LEFT WING UPPER SKIN AT STRINGER 6, WS 675 IS CORRODED.
- [SDR KO0R201601040017](https://openairdocs.org/sdr/KO0R201601040017), Jan 4, 2016: SKIN. CORRODED. LEFT WING UPPER SKIN AT STRINGER 6, WS 160 IS CORRODED.
- [SDR KO0R201601040016](https://openairdocs.org/sdr/KO0R201601040016), Jan 4, 2016: SKIN. CORRODED. LEFT WING UPPER SKIN AT STRINGER 13, WS 165 IS CORRODED.
- [SDR KO0R201601040015](https://openairdocs.org/sdr/KO0R201601040015), Jan 4, 2016: SKIN. CORRODED. LEFT WING UPPER SKIN AT STRINGER 22, WS 125 IS CORRODED.
- [SDR KO0R201601040014](https://openairdocs.org/sdr/KO0R201601040014), Jan 4, 2016: SKIN. CORRODED. LEFT WING UPPER SKIN AT STRINGER 22, WS 105 IS CORRODED.
- [SDR KO0R201601040013](https://openairdocs.org/sdr/KO0R201601040013), Jan 4, 2016: SKIN. CORRODED. MAIN DECK CTR WING UPPER SKIN HAS CORROSION AT WING TANK STRINGER 15, STATION 1229.0 AT RBL 75.
- [SDR KO0R201601040012](https://openairdocs.org/sdr/KO0R201601040012), Jan 4, 2016: SKIN. CORRODED. MAIN DECK CTR WING UPPER SKIN HAS CORROSION AT WING TANK STRINGER 15, STATION 1229.0 AT RBL 60.
- [SDR KO0R201601040011](https://openairdocs.org/sdr/KO0R201601040011), Jan 4, 2016: SKIN. CORRODED. MAIN DECK CTR WING UPPER SKIN HAS CORROSION AT WING TANK STRINGER 15, STATION 1229.0 AT LBL 43.
- [SDR KO0R201601040010](https://openairdocs.org/sdr/KO0R201601040010), Jan 4, 2016: SKIN. CORRODED. MAIN DECK CTR WING UPPER SKIN HAS CORROSION AT WING TANK STRINGER 15, STATION 1227.0 AT LBL 8.5.
- [SDR KO0R201601040009](https://openairdocs.org/sdr/KO0R201601040009), Jan 4, 2016: SKIN. CORRODED. MAIN DECK CTR WING UPPER SKIN HAS CORROSION AT WING TANK STRINGER 15, STATION 1227.0 AT LBL 1.5.
- [SDR KO0R201601040008](https://openairdocs.org/sdr/KO0R201601040008), Jan 4, 2016: SKIN. CORRODED. MAIN DECK CTR WING UPPER SKIN HAS CORROSION AT WING TANK STRINGER 15, STATION 1227.0 AT RBL 1.
- [SDR KO0R201601040007](https://openairdocs.org/sdr/KO0R201601040007), Jan 4, 2016: SKIN. CORRODED. MAIN DECK CTR WING UPPER SKIN HAS CORROSION AT WING TANK STRINGER 15, STATION 1227.0 AT RBL 24.5.
- [SDR KO0R201601040006](https://openairdocs.org/sdr/KO0R201601040006), Jan 4, 2016: SKIN. CORRODED. MAIN DECK CTR WING UPPER SKIN HAS CORROSION AT WING TANK STRINGER 15, STATION 1227.0 AT RBL 22.
- [SDR KO0R201601040005](https://openairdocs.org/sdr/KO0R201601040005), Jan 4, 2016: SKIN. CORRODED. MAIN DECK CTR WING UPPER SKIN HAS CORROSION AT WING TANK STRINGER 15, STATION 1227.0 AT RBL 13.
- [SDR KO0R201601040004](https://openairdocs.org/sdr/KO0R201601040004), Jan 4, 2016: SKIN. CORRODED. MAIN DECK CTR WING UPPER SKIN HAS CORROSION AT WING TANK STRINGER 15, STATION 1227.0 AT RBL 8.
- [SDR KO0R201601040003](https://openairdocs.org/sdr/KO0R201601040003), Jan 4, 2016: SUPPORT ANGLE. CORRODED. MAIN DECK CTR WING UPPER AUXILIARY TANK VERTICAL SUPPORT ANGLE HAS CORROSION AT STATION 1331.5 AT RBL 100.
- [SDR KO0R201601040001](https://openairdocs.org/sdr/KO0R201601040001), Jan 4, 2016: SKIN. CORRODED. MAIN DECK CTR WING UPPER SKIN HAS CORROSION AT WING TANK STRINGER 15, STATION 127.0 AT LBL 14.5.

## STCs that may be installed (OpenAirDocs) (252, 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-11)

- [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 ST01735AT-D](https://openairdocs.org/stc/ST01735AT-D): Installation of Collins VHG-700B transceivers and gables radio tuning panels with 8.33 KHz spacing. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST01983AT-D](https://openairdocs.org/stc/ST01983AT-D): Interior modification. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [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 SA5040NM](https://openairdocs.org/stc/SA5040NM): Installation of cargo pallet and net. Satco 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 SA5045NM](https://openairdocs.org/stc/SA5045NM): Installation of LH module P/N 15900-1 and RH module P/N 15940-1. Safran Cabin Inc
- [STC SA5046NM](https://openairdocs.org/stc/SA5046NM): Installation of LH closet P/N 15880-1, cart stowage module P/N 15920-1. Safran Cabin Inc
- [STC SA5047NM](https://openairdocs.org/stc/SA5047NM): Installation of partition P/N 16080-1, 16240-1, -2, header assembly P/N 16060-1. Safran Cabin Inc
- [STC SA5048NM](https://openairdocs.org/stc/SA5048NM): Installation of partition P/N 16260-1, header assembly P/N 16070-1. Safran Cabin Inc
- [STC SA5547NM](https://openairdocs.org/stc/SA5547NM): Installation of P/N 1451001-211 meal cart, P/N 1451001-215 beverage cart, P/N 1451001-217 waste cart, and P/N 1451001-219 dish cart. Safran Cabin Inc
- [STC SA5802NM](https://openairdocs.org/stc/SA5802NM): Installation of articulating overhead cabin module bin kit, P/N CDK327-2. Safran Cabin Inc
- [STC SA5806NM](https://openairdocs.org/stc/SA5806NM): Installation of P/N 1451001-111 meal cart, P/N 1451001-115 beverage cart, P/N 1451001-117 waste cart, and P/N 1451001-119 dish cart. Safran Cabin Inc
- [STC SA5850NM](https://openairdocs.org/stc/SA5850NM): Installation of crew rest P/N 15700-1. Safran Cabin Inc
- [STC SA6055NM](https://openairdocs.org/stc/SA6055NM): Installation of forward and aft closets, outboard class dividers, centerline class divider, center partition, curtain assemblies, overhead stowage bin rework kit. Safran Cabin Inc
- [STC SA7065NM](https://openairdocs.org/stc/SA7065NM): Installation of Closet Assembly. Safran Cabin Inc
- [STC ST00547LA](https://openairdocs.org/stc/ST00547LA): Installation of coat closets, L/H and R/H. Safran Cabin Inc
- [STC ST00796LA](https://openairdocs.org/stc/ST00796LA): Installation of interior modification kit. 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 ST03489AT](https://openairdocs.org/stc/ST03489AT): Installation of L-3 Communications Solid State Flight data Recorder (SSFDR) Model FA2100 (any of the following part numbers: 2100-4042-00, 2100-4043-00, 2100-4043-02, or 2100-4044-00) as a replacement for the existing Tape based FDR P/N 980-4100DXUS (or equivalent FDR installed per ARINC 573 / 717). Acron Aviation 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 ST01206LA](https://openairdocs.org/stc/ST01206LA): Installation of In-Seat Power Outlets. Aero Technik Inc
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST02131AT](https://openairdocs.org/stc/ST02131AT): Installation of SAF-T-GLO photoluminescent floor proximity emergency escape with marking system (FPEEPMS). STG Aerospace Inc
- [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 ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [STC ST00447SE](https://openairdocs.org/stc/ST00447SE): Installation of the Honeywell Solid State Flight Data Recorder, per Honeywell Master Drawing 755-3025-001, Revision C, dated May 20, 1997, or later FAA approved revisions. Honeywell International Inc
- [STC ST00536SE](https://openairdocs.org/stc/ST00536SE): Installation of the Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS). Honeywell International Inc
- [STC ST01098AT](https://openairdocs.org/stc/ST01098AT): Installation of RTA-4A Weather Radar Receiver/Transmitter. Honeywell International Inc
- [STC ST01368AT](https://openairdocs.org/stc/ST01368AT): Installation of AlliedSignal Mark II ACARS Communications Management Unit (CMU) system. 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 ST00972SE-D](https://openairdocs.org/stc/ST00972SE-D): Installation of avionics equipment, stowage bins and galley modifications. GDC Technics LLC
- [STC ST01373AT](https://openairdocs.org/stc/ST01373AT): Interior reconfiguration. GDC Technics LLC
- [STC SA5079NM](https://openairdocs.org/stc/SA5079NM): Installation of Sony Trans com Inc., Video Entertainment System. Burrana Inc
- [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

All 252: https://openairdocs.org/aircraft/N513SN/stcs.md

## Related

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

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