# N950FD: 1994 Boeing 757-236

- Status: Valid registration
- Airframe: [Boeing 757-236](https://openairdocs.org/model/boeing-757-236) (registry code 1384971, 178 seats)
- Engine: [Rolls-Royce RB211-535E4 series](https://openairdocs.org/engine/rolls-royce-rb211-535e4-series) (registry code 54223)
- Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM) (The Boeing Company), [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 25806
- Year built: 1994
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 26, 2011
- Certificate issued: January 12, 2011
- Expires: January 31, 2030
- Mode S code: AD3528
- Registered owner: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP)
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Corporation
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=950FD
- Page: https://openairdocs.org/aircraft/N950FD

From the FAA registry file of October 21, 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. The registry lists only the engine series, so ADs for every Rolls-Royce RB211-535E4 model are included.

## ADs that may apply (OpenAirDocs): 336 in force

### Matched by airframe (Boeing 757-236)

- [AD 2026-13-16](https://openairdocs.org/ad/2026-13-16): Navigation · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 6 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 2026-08-09](https://openairdocs.org/ad/2026-08-09): Wings · Boeing 757-200 Series and 757-300 Series with STC ST01518SE. Effective Jun 3, 2026
- [AD 2026-04-06](https://openairdocs.org/ad/2026-04-06): Wings · Boeing 757-200 Series and 757-300 Series. Effective Feb 26, 2026
- [AD 2026-01-05](https://openairdocs.org/ad/2026-01-05): Wings · Boeing 757-200 Series and 757-300 Series. Effective Feb 20, 2026
- [AD 2025-23-03](https://openairdocs.org/ad/2025-23-03): Fire protection · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 1 more. Effective Jan 13, 2026
- [AD 2025-20-14](https://openairdocs.org/ad/2025-20-14): Equipment/furnishings · Boeing 757-200 Series. Effective Jan 2, 2026
- [AD 2025-20-04](https://openairdocs.org/ad/2025-20-04): Flight controls · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Nov 6, 2025
- [AD 2025-19-11](https://openairdocs.org/ad/2025-19-11): Landing Gear · Boeing 757-200 Series, 757-200PF Series and 757-200CB Series. Effective Nov 6, 2025
- [AD 2025-11-01](https://openairdocs.org/ad/2025-11-01): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective Jul 8, 2025
- [AD 2025-02-13](https://openairdocs.org/ad/2025-02-13): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-200PF Series. Effective Mar 17, 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 2024-25-09](https://openairdocs.org/ad/2024-25-09): Hydraulic power · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 1 more. Effective Feb 14, 2025
- [AD 2024-24-01](https://openairdocs.org/ad/2024-24-01): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-200PF Series. Effective Jan 13, 2025
- [AD 2024-12-09](https://openairdocs.org/ad/2024-12-09): Wings · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Aug 22, 2024
- [AD 2024-10-07](https://openairdocs.org/ad/2024-10-07): Fuselage · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 1 more. Effective Jul 19, 2024
- [AD 2024-10-05](https://openairdocs.org/ad/2024-10-05): Equipment/Furnishings · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Jul 19, 2024
- [AD 2024-12-07](https://openairdocs.org/ad/2024-12-07): Fuselage · Boeing 757-200 Series with STC ST01529SE or ST02278SE. Effective Jul 11, 2024
- [AD 2024-07-05](https://openairdocs.org/ad/2024-07-05): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective Jun 5, 2024
- [AD 2024-05-09](https://openairdocs.org/ad/2024-05-09): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective May 8, 2024
- [AD 2023-13-12](https://openairdocs.org/ad/2023-13-12): Oxygen · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 17 more. Effective Sep 5, 2023
- [AD 2023-12-12](https://openairdocs.org/ad/2023-12-12): Navigation · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 6 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 2022-20-15](https://openairdocs.org/ad/2022-20-15): Wings · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 1 more. Effective Dec 7, 2022
- [AD 2022-15-09](https://openairdocs.org/ad/2022-15-09): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective Aug 17, 2022
- [AD 2022-15-08](https://openairdocs.org/ad/2022-15-08): Information systems · Airbus A318-111, A318-112, A319-111 and 49 more. Effective Aug 12, 2022
- [AD 2022-13-04](https://openairdocs.org/ad/2022-13-04): Fuselage · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 1 more. Effective Aug 12, 2022
- [AD 2022-07-07](https://openairdocs.org/ad/2022-07-07): Equipment/furnishings · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective May 26, 2022
- [AD 2021-26-28](https://openairdocs.org/ad/2021-26-28): Fuel · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 1 more. Effective Mar 3, 2022
- [AD 2021-22-23](https://openairdocs.org/ad/2021-22-23): Wings · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 1 more. Effective Dec 29, 2021
- [AD 2021-08-04](https://openairdocs.org/ad/2021-08-04): Oxygen · Boeing 737-200 Series, 737-300 Series, 737-400 Series and 23 more. Effective May 26, 2021
- [AD 2021-05-11](https://openairdocs.org/ad/2021-05-11): Flight controls · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Apr 19, 2021
- [AD 2020-20-10](https://openairdocs.org/ad/2020-20-10): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective Nov 10, 2020
- [AD 2020-04-15](https://openairdocs.org/ad/2020-04-15): Air conditioning · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 4 more. Effective May 8, 2020
- [AD 2020-05-25](https://openairdocs.org/ad/2020-05-25): Fuselage · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective May 4, 2020
- [AD 2020-01-18](https://openairdocs.org/ad/2020-01-18): Fuel, Fuselage, Wings · Winglets, wing structural reinforcement (Aviation Partners Boeing STC ST01518SE). Effective Mar 5, 2020
- [AD 2019-24-18](https://openairdocs.org/ad/2019-24-18): Navigation · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 11 more. Effective Feb 3, 2020
- [AD 2019-19-10](https://openairdocs.org/ad/2019-19-10): Fuel · Boeing 737-300 Series, 737-400 Series, 737-500 Series and 21 more. Effective Jan 16, 2020
- [AD 2019-07-04](https://openairdocs.org/ad/2019-07-04): Editorial Note: Rule document 2019-07587 was originally published on pages 15949 through 15952 in the issue of Wednesday, April 17, 2019. In that publication, on page 15951, in the title of  
 the Airworthiness Directive, ''-04'' was inadvertently left out. The corrected document is republished in its entirety. · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective May 22, 2019
- [AD 2018-23-12](https://openairdocs.org/ad/2018-23-12): Equipment/furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 180 more. Effective Dec 28, 2018
- [AD 2018-20-13](https://openairdocs.org/ad/2018-20-13): Fuel · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 13 more. Effective Nov 15, 2018
- [AD 2018-19-23](https://openairdocs.org/ad/2018-19-23): Doors · Boeing 747-100 Series, 747-100B Series, 747-100B SUD Series and 15 more. Effective Nov 7, 2018
- [AD 2018-18-07](https://openairdocs.org/ad/2018-18-07): Fuselage · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Oct 10, 2018
- [AD 2018-06-08](https://openairdocs.org/ad/2018-06-08): Fuselage · Boeing 757-200 Series. Effective Apr 19, 2018
- [AD 2017-26-07](https://openairdocs.org/ad/2017-26-07): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective Feb 7, 2018
- [AD 2017-26-02](https://openairdocs.org/ad/2017-26-02): Doors · Boeing 757-200 Series. Effective Jan 24, 2018
- [AD 2017-22-12](https://openairdocs.org/ad/2017-22-12): Wings · Boeing 757-200 Series, 757-200CB Series and 757-200PF Series. Effective Dec 26, 2017
- [AD 2017-20-05](https://openairdocs.org/ad/2017-20-05): Fuselage · Boeing 757-200 Series and 757-300 Series. Effective Nov 6, 2017
- [AD 2017-19-10](https://openairdocs.org/ad/2017-19-10): Doors · Boeing 757-200 Series, 757-200CB Series and 757-200PF Series. Effective Oct 27, 2017
- [AD 2017-12-14](https://openairdocs.org/ad/2017-12-14): Fuselage · Boeing 757-200 Series and 757-200PF Series. Effective Jul 25, 2017

### Matched by engine (Rolls-Royce RB211-535E4 series)

- [AD 2024-10-06](https://openairdocs.org/ad/2024-10-06): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jun 27, 2024
- [AD 2020-08-03](https://openairdocs.org/ad/2020-08-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective May 18, 2020
- [AD 2017-24-08](https://openairdocs.org/ad/2017-24-08): Fuel control/Turbine engines · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 16, 2018
- [AD 2016-03-04](https://openairdocs.org/ad/2016-03-04): Life-limited rotating parts · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Mar 15, 2016
- [AD 2013-23-17](https://openairdocs.org/ad/2013-23-17): High-pressure (HP) and intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-C-37 and 3 more. Effective Dec 11, 2013
- [AD 2013-16-23](https://openairdocs.org/ad/2013-16-23): Cracked and distorted FCL metering panel · Rolls-Royce RB211-524B-02, RB211-524B2-19, RB211-524B3-02 and 13 more. Effective Oct 8, 2013
- [AD 2012-25-09](https://openairdocs.org/ad/2012-25-09): Intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19 and 10 more. Effective Feb 6, 2013
- [AD 2012-02-11](https://openairdocs.org/ad/2012-02-11): LP turbine stage 1, 2, and 3 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Mar 6, 2012
- [AD 2009-20-14](https://openairdocs.org/ad/2009-20-14): Eddy current inspection (ECI) · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Nov 17, 2009
- [AD 2008-20-04](https://openairdocs.org/ad/2008-20-04): HP turbine discs · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 26 more. Effective Nov 3, 2008
- [AD 2006-11-05 R2](https://openairdocs.org/ad/2006-11-05-R2): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 21, 2008
- [AD 2007-14-07](https://openairdocs.org/ad/2007-14-07): Fluorescent penetrant inspections (FPI) · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 21 more. Effective Aug 16, 2007
- [AD 2006-17-12](https://openairdocs.org/ad/2006-17-12): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Sep 27, 2006
- [AD 2004-19-04](https://openairdocs.org/ad/2004-19-04): Critical Life-Limited Rotating Engine Parts · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Nov 1, 2004
- [AD 2004-01-21](https://openairdocs.org/ad/2004-01-21): Frount engine mount housing · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 27, 2004
- [AD 2003-10-03 R1](https://openairdocs.org/ad/2003-10-03-R1): High pressure (HP) turbine discs · Rolls-Royce RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jun 20, 2003
- [AD 2001-19-05](https://openairdocs.org/ad/2001-19-05): High Speed Gearbox Drive · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Oct 11, 2001
- [AD 2000-09-14](https://openairdocs.org/ad/2000-09-14): Radial Drive Steady Bearings · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Jul 11, 2000
- [AD 97-02-12](https://openairdocs.org/ad/97-02-12): Fuel Flow Governor (FFG) · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Apr 4, 1997
- [AD 87-25-04](https://openairdocs.org/ad/87-25-04): Fuel Quantity Indication System · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Dec 8, 1987

### Historical (superseded or no longer in force)

- [AD 2022-08-12](https://openairdocs.org/ad/2022-08-12) (historical): Wings · Boeing 757-200 Series, 757-200PF Series, 757-200CB Series and 1 more. Effective Jun 10, 2022
- [AD 2022-04-05](https://openairdocs.org/ad/2022-04-05) (historical): Navigation · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 6 more. Effective Feb 14, 2022
- [AD 2020-21-17](https://openairdocs.org/ad/2020-21-17) (historical): Wings · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Jan 14, 2021
- [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 2019-23-06](https://openairdocs.org/ad/2019-23-06) (historical): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective Jan 13, 2020
- [AD 2019-20-03](https://openairdocs.org/ad/2019-20-03) (historical): Information systems · Airbus A340-312, A340-313, A318-111 and 48 more. Effective Nov 19, 2019
- [AD 2019-12-13](https://openairdocs.org/ad/2019-12-13) (historical): Flight controls · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Jul 12, 2019
- [AD 2018-26-03](https://openairdocs.org/ad/2018-26-03) (historical): Equipment/furnishings · Boeing 757-200 Series. Effective Jan 31, 2019
- [AD 2018-16-05](https://openairdocs.org/ad/2018-16-05) (historical): Wings · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Sep 10, 2018
- [AD 2018-06-07](https://openairdocs.org/ad/2018-06-07) (historical): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective May 3, 2018
- [AD 2017-24-10](https://openairdocs.org/ad/2017-24-10) (historical): Fuselage · Boeing 757-200 Series, 757-200PF Series and 757-300 Series. Effective Jan 9, 2018
- [AD 2017-26-10](https://openairdocs.org/ad/2017-26-10) (historical): Flight controls · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Jan 3, 2018
- [AD 2015-08-01](https://openairdocs.org/ad/2015-08-01) (historical): Flight Controls · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective May 26, 2015
- [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 2013-01-02](https://openairdocs.org/ad/2013-01-02) (historical): Doors · Boeing 747-100 Series, 747-100B Series, 747-100B SUD Series and 12 more. Effective Feb 22, 2013
- [AD 2012-15-15](https://openairdocs.org/ad/2012-15-15) (historical): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective Oct 3, 2012
- [AD 2011-01-15](https://openairdocs.org/ad/2011-01-15) (historical): Fuselage · Boeing 757-200 Series, 757-200CB Series and 757-300 Series. Effective Jan 25, 2011
- [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 2009-22-08](https://openairdocs.org/ad/2009-22-08) (historical): Control switches · Boeing 747-100 Series, 747-100B Series, 747-100B SUD Series and 12 more. Effective Dec 3, 2009
- [AD 2008-23-19](https://openairdocs.org/ad/2008-23-19) (historical): Left and right main fuel tanks · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Dec 30, 2008
- [AD 2008-13-20](https://openairdocs.org/ad/2008-13-20) (historical): Aft hinge fittings · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Aug 6, 2008
- [AD 2008-10-11](https://openairdocs.org/ad/2008-10-11) (historical): Fuel tank systems · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Jun 12, 2008
- [AD 2008-09-07](https://openairdocs.org/ad/2008-09-07) (historical): Fuel filter · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 4 more. Effective May 8, 2008
- [AD 2008-05-10](https://openairdocs.org/ad/2008-05-10) (historical): Vertical flange and bulkhead · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 9 more. Effective Mar 18, 2008
- [AD 2007-16-13](https://openairdocs.org/ad/2007-16-13) (historical): Shim installation · Boeing 757-200 Series, 757-200CB Series and 757-200PF Series. Effective Aug 24, 2007
- [AD 2007-03-01](https://openairdocs.org/ad/2007-03-01) (historical): Power feeder wire bundles · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Mar 5, 2007
- [AD 2006-20-11](https://openairdocs.org/ad/2006-20-11) (historical): Rivet inspection · Boeing 757-200 Series, 757-200CB Series and 757-200PF Series. Effective Nov 8, 2006
- [AD 2006-11-11](https://openairdocs.org/ad/2006-11-11) (historical): Fatigue cracking of PSEs · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Jun 30, 2006
- [AD 2005-18-18](https://openairdocs.org/ad/2005-18-18) (historical): Left and right engine-to-wing aft fairings · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Oct 14, 2005
- [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 2005-12-04](https://openairdocs.org/ad/2005-12-04) (historical): Aft torque bulkhead · Boeing 757-200 Series, 757-200CB Series and 757-200PF Series. Effective Jun 29, 2005
- [AD 2005-04-14](https://openairdocs.org/ad/2005-04-14) (historical): Joint of the mid-bulkhead and the upper link fittings · Boeing 757-200 Series, 757-200CB Series and 757-200PF Series. Effective Mar 15, 2005
- [AD 2004-12-07](https://openairdocs.org/ad/2004-12-07) (historical): Nacelle strut and wing structure · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Jul 21, 2004
- [AD 2004-09-32](https://openairdocs.org/ad/2004-09-32) (historical): Fuselage skin · Boeing 757-200 Series. Effective May 24, 2004
- [AD 2003-18-05](https://openairdocs.org/ad/2003-18-05) (historical): Nacelle Strut and Wing Structure · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 1 more. Effective Oct 16, 2003
- [AD 94-01-10 R1](https://openairdocs.org/ad/94-01-10-R1) (historical): Engine thrust reverser system · Boeing 757-200 Series and 757-200PF Series. Effective Sep 18, 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 2003-07-08](https://openairdocs.org/ad/2003-07-08) (historical): Upper link fittings · Boeing 757-200 Series, 757-200CB Series and 757-200PF Series. Effective Apr 18, 2003
- [AD 2001-24-02](https://openairdocs.org/ad/2001-24-02) (historical): Shoulder Restraint Harness Attachment · Boeing 707-100 Long Body, 707-100B Long Body, 707-300 Series (all) and 20 more. Effective Jan 4, 2002
- [AD 99-27-06](https://openairdocs.org/ad/99-27-06) (historical): Thrust Reverser Cable · Boeing 757-200 Series, 757-200CB Series and 757-200PF Series. Effective Feb 7, 2000
- [AD 99-18-16](https://openairdocs.org/ad/99-18-16) (historical): Modular Avionics Warning Electronic Assembly or Warning Electronics Unit · Boeing 747-400 Series, 747-400D Series, 747-400F Series and 6 more. Effective Sep 16, 1999
- [AD 99-09-13](https://openairdocs.org/ad/99-09-13) (historical): Forward Lavatory · Boeing 757-200 Series, 757-200CB Series and 757-200PF Series. Effective Jun 1, 1999
- [AD 97-06-04](https://openairdocs.org/ad/97-06-04) (historical): Lower Spar Chord · Boeing 757-200 Series, 757-200CB Series and 757-200PF Series. Effective Mar 28, 1997
- [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 2015-17-21](https://openairdocs.org/ad/2015-17-21) (historical): High-pressure turbine (HPT) disks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Dec 2, 2015
- [AD 2014-24-08](https://openairdocs.org/ad/2014-24-08) (historical): Fuel leaks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 6, 2015
- [AD 2013-19-18](https://openairdocs.org/ad/2013-19-18) (historical): LPT stage 2 disc failure · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Nov 7, 2013
- [AD 2013-19-17](https://openairdocs.org/ad/2013-19-17) (historical): Failure of rotating life limited parts · Rolls-Royce RB211-535E4-B-37. Effective Nov 7, 2013
- [AD 2011-11-08](https://openairdocs.org/ad/2011-11-08) (historical): LP Turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Jun 30, 2011
- [AD 2008-22-24](https://openairdocs.org/ad/2008-22-24) (historical): Low pressure compressor (LPC) fan blade · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Dec 9, 2008

All 398: https://openairdocs.org/aircraft/N950FD/ads.md

## Information bulletins (advisory) (14 in force)

- [SAIB 2026-09](https://openairdocs.org/saib/2026-09): HYDRAULIC POWER, Hydraulic Power Transfer Unit System. Issued Apr 6, 2026
- [SAIB 2025-02](https://openairdocs.org/saib/2025-02): DOORS, Main Deck Cargo Door. Issued Feb 21, 2025
- [SAIB 2025-01](https://openairdocs.org/saib/2025-01): HYDRAULIC POWER SYSTEM, Fatigue Failure of Hydraulic Flexible Hoses. Issued Jan 14, 2025
- [SAIB NM-20-07](https://openairdocs.org/saib/NM-20-07): Navigation - Glideslope System. Issued Apr 16, 2020
- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [SAIB NM-18-33](https://openairdocs.org/saib/NM-18-33): Engine Fuel and Control. Issued Dec 17, 2018
- [SAIB NM-17-17](https://openairdocs.org/saib/NM-17-17): Oxygen System. Issued Jun 19, 2017
- [SAIB NM-17-10](https://openairdocs.org/saib/NM-17-10): Maintenance Practices. Issued Apr 13, 2017
- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [SAIB NM-10-24](https://openairdocs.org/saib/NM-10-24): Hydraulic Motors: Hydraulic Motor Generator (HMG) Inadvertent Lock-out. Issued Mar 31, 2010
- [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-07-14](https://openairdocs.org/saib/NM-07-14): M10444 APU/Cargo Fire Control Panel (APU/CFCP). Issued Jan 3, 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 2026-11](https://openairdocs.org/saib/2026-11): Theft of Turbofan Engine Parts before Mutilation. Issued Jun 8, 2026

## NTSB investigations

None matched to N950FD.

## FAA accident and incident reports

None matched to N950FD.

## Service difficulty reports (97, newest 50)

As reported by operators and repair stations.

- [SDR FDEA202604140446](https://openairdocs.org/sdr/FDEA202604140446), Apr 14, 2026: BULB. FAILED. DURING MX PRE-FLIGHT EMERGENCY LIGHT TEST, FOUND L1 DOOR EXIT SIGN SEEMS DIM. REMOVED AND REPLACED 9 FAULTY BULBS AT THE L1 EXIT SIGN IAW AMM 33-51-01-2. OPS CH
- [SDR FDEA202505070724](https://openairdocs.org/sdr/FDEA202505070724), May 7, 2025: LAMP. FAILED. R SLIDE LIGHT INOP. AMM: 33-51-06-2-1 RELAMPED R/H SLIDE LIGHT I/A/W AMM REFERENCED ABOVE, GOOD FOE SERVICE.
- [SDR FDEA202411221716](https://openairdocs.org/sdr/FDEA202411221716), Nov 22, 2024: HANDLE. NO DISCREPANCY. L1 DOOR EXTERNAL DOOR HANDLE NOT OPERATING PROPERLY. INSPECTED AND OPERATED DOOR MULTIPLE TIMES PER AMM 12-21-18-13. DOOR OPERATES AS IT SHOULD. NO FAULTS FOUND
- [SDR FDEA202403180307](https://openairdocs.org/sdr/FDEA202403180307), Mar 18, 2024: SEAL. FAILED. R FWD WINDOW SHATTERED AT 360 AFTER ST ELMO FIRE. DIDN T HEAR AIR LEAK. STARTED R/R OF F/O`S WINDSHIELD IAW AMM 56-11-01-4. NEW WINDOW INSTALLED AND FIRST TORQU
- [SDR FDEA202312151941](https://openairdocs.org/sdr/FDEA202312151941), Dec 15, 2023: GUST LOCK. CRACKED. DURING POST FLIGHT, FOUND L1 DOOR GUST LOCK COLLAR BROKEN. REMOVED BROKEN COLLARS. PLACARD INSTALLED. A/C OK TO CONTINUE USING R1 DOOR. L1 DOOR INOP. REMOVED BR
- [SDR FDEA202306211074](https://openairdocs.org/sdr/FDEA202306211074), Jun 21, 2023: DRAG FITTING. UNKNOWN. LT PYLON HAS 2 CRACK INDICATIONS AT #6 HOLE, 2 O'CLOCK & 7 O'CLOCK POSITIONS IN THE FITTING. 0.850 DEPTH. COMPLIED WITH EA# F-5730-T0374640 PART 1 (P1) LH WING 
- [SDR FDEA202306211073](https://openairdocs.org/sdr/FDEA202306211073), Jun 21, 2023: DRAG FITTING. UNKNOWN. LT PYLON HAS 1 CRACK INDICATION AT #3 HOLE, 6 O'CLOCK POSITION IN THE SKIN, 0.250 DEPTH. COMPLIED WITH EA# F-5730-T0374640 PART 1 (P1) LH WNG UPPER SKIN AT IB P
- [SDR FDEA202306211072](https://openairdocs.org/sdr/FDEA202306211072), Jun 21, 2023: DRAG FITTING. UNKNOWN. LT PYLON HAS 1 CRACK INDICATION AT #8 HOLE 3 O'CLOCK POSITION IN THE FITTING 0.850 DEPTH. COMPLIED WITH EA# F-5730-T0374640 PART 1 (P1) LH WING UPPER SKIN AT IB
- [SDR FDEA202306211071](https://openairdocs.org/sdr/FDEA202306211071), Jun 21, 2023: DRAG FITTING. UNKNOWN. LT PYLON HAS 2 CRACK INDICATIONS AT #7 HOLE, 12 O'CLOCK POSITION IN THE FITTING 0.850 DEPTH. COMPLIED WITH EA# F-5730-T0374640 PART 1 (P1) LH WING UPPER SKIN AT
- [SDR FDEA202302030200](https://openairdocs.org/sdr/FDEA202302030200), Feb 3, 2023: TRANSMISSION. FAILED. PDIS 950 27-51 9670 03FEB23 MEM OPEN U TE FLAP DISAGREE DURING APPROACH. RAN QRH. ALTERNATE FLAP EXTENSION WORKED AS ADVERTISED. DIVERTED TO MEM. LANDED FLAPS 2
- [SDR FDEA202209132339](https://openairdocs.org/sdr/FDEA202209132339), Sep 13, 2022: BEARING. FAILED. TE FLAP ASYM EICAS MSG AFTER SELECTING FLAPS 20. SPEED WAS 170 KTS AT 2000 FT. FLAP INDICATORS ARE SPLIT AT FLAPS 15. RIGHT WING WANTED TO COME UP. EMERGENCY DE
- [SDR FDEA202112083047](https://openairdocs.org/sdr/FDEA202112083047), Dec 8, 2021: NONE. NONE. AFTER TAKEOFF AND RAISING GEAR HANDLE WE RECEIVED EICAS: GEAR DISAGREE & GEAR DOORS ALONG WITH GEAR AND DOORS LIGHTS. RETURNED TO IND AND GEAR EXTENDED NORMALLY
- [SDR FDEA202012223196](https://openairdocs.org/sdr/FDEA202012223196), Dec 22, 2020: LINE. OUT OF POSITION. RT FWD ENTRY DOOR WILL NOT ARM, NO SLIDE LIGHT. FOUND STATIC LINE INTERFERE WITH GIRT BAR. REPOSITION STATIC LINE AS REQUIRED. OPERATIONS CHECK NORMAL, REF B757
- [SDR FDEA2020090311872](https://openairdocs.org/sdr/FDEA2020090311872), Aug 13, 2020: LIGHT. MALFUNCTIONED. RT CABIN DOOR SLIDE ARMED LIGHT NOT ILLUMINATING WHEN DOOR ARMED. OPERATED DOOR PER AMM 25-66-00-5. OK FOR SERVICE.
- [SDR FDEA2020081431872](https://openairdocs.org/sdr/FDEA2020081431872), Aug 13, 2020: UNKNOWN. UNKNOWN. R CABIN DOOR SLIDE ARMED LIGHT NOT ILLUMINATING WHEN DOOR ARMED. OPERATED DOOR PER AMM 25-66-00-5. OK FOR SERVICE
- [SDR FDEA2020041750748](https://openairdocs.org/sdr/FDEA2020041750748), Apr 15, 2020: ELEMENT. FAILED. APU WHEN PUT ON LINE FIRE BOTTLE BLEW, APU FIRE WARNING LIGHT HORN ON CONSTANT, SHUT OFF APU RESET THE HORN FIRE WARNING. LIGHT OUT BUT FIRE BOTTLE SQUIBS FIRED
- [SDR FDEA2020032980612](https://openairdocs.org/sdr/FDEA2020032980612), Mar 28, 2020: WARNING SYSTEM. FALSE ACTIVATION. INTERMITTANT R EMER DOOR ADVISORY AT BLOCK - IN HAD NO "R EMER DOOR" ADVISORY. VISUALLY CHECKED DOOR AND VERIFED IT WAS CLOSED WITH HANDLE LOCK PLATED STILL INS
- [SDR FDEA201901160151](https://openairdocs.org/sdr/FDEA201901160151), Jan 16, 2019: WARNING SYSTEM. ACTIVATED. PDIS 950 27-80 6538 16JAN19 LOGPAGES:3084577 WHEN CONFIGURING FOR APPROACH RECEIVED MASTER CAUTION AND EICAS MASSAGE LE SLAT DISAGREE. RAN QRH, DECLARED EMERGEN
- [SDR FDEA201708182273](https://openairdocs.org/sdr/FDEA201708182273), Aug 18, 2017: FLOORBEAM. CRACKED. MAIN CARGO BAY STUB FLOORBEAM AT BS 580, LBL 45.5 - 58.22, AFT FLANGE IS CRACKED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-02, AND DWG 657N4311, REV -.
- [SDR FDEA201708102173](https://openairdocs.org/sdr/FDEA201708102173), Aug 10, 2017: SHEAR PLATE. CRACKED. MAIN CARGO BAY SHEAR PLATE IS CRACKED AT BS 580, LBL 45.5. REPAIRED THE SHEAR PLATE IAW EA F-5310-T0334835 P1.
- [SDR FDEA201708082148](https://openairdocs.org/sdr/FDEA201708082148), Aug 8, 2017: SEAT TRACK. CORRODED. CORROSION ON COURIER SEAT TRACK R1 DOOR ENTRY BS 345 TO 377, LBL 5. REMOVED CORROSION, HAD 100% MATERIAL LOSS AND IS OUT OF LIMITS. FABRICATED A NEW SEAT TRACK.
- [SDR FDEA201708042116](https://openairdocs.org/sdr/FDEA201708042116), Aug 4, 2017: SEAT TRACK. CRACKED. MAIN CARGO COMPARTMENT SEAT TRACK AT BS 580 LBL 45.5 IS CRACKED ON IB FLANGE AT FLOORBEAM. REMOVED THE SEAT TRACK . FABRICATED A REPLACEMENT SEAT TRACK AND INST
- [SDR FDEA201708022097](https://openairdocs.org/sdr/FDEA201708022097), Aug 2, 2017: DOOR FRAME. PUNCTURED. TOP OF LOWER FRAME PUNCTURED BS 231 AT THE FORWARD ACCESSORY DOOR CUTOUT. COMPLIED WITH FED EX EA F-5310-T0334685 P1. REPAIRED THE DOOR FRAME IAW SRM 53-00-00-0
- [SDR FDEA201704111133](https://openairdocs.org/sdr/FDEA201704111133), Apr 11, 2017: SLIDE. MALFUNCTIONED. AFTER SHUTDOWN ON ACFT EXIT FAILED TO DRM LEFT DOOR STOPPED BEFORE BLOWING SLIDE. REMOVED AND REPLACED L1 DOOR ESAPE SLIDE, OP CHECKED GOOD IAW MM 25-66-01-4-0.
- [SDR FDEA201610273723](https://openairdocs.org/sdr/FDEA201610273723), Oct 27, 2016: LIGHT. INOPERATIVE. L1 DOOR SLIDE LIGHT WILL NOT ILLUMINATE. RELAMPED L1 DOOR SLIDE LIGHT IAW AMM 25-66-00-5. OPS CHECK GOOD. A/C OK TO CONTINUE.
- [SDR FDEA201607062295](https://openairdocs.org/sdr/FDEA201607062295), Jul 6, 2016: UNKNOWN. MALFUNCTIONED. ON INITIAL TAKEOFF AT APPROXIMATELY 30 KTS, LT GENERATOR OFF, LT BUSS TIE IS LN. LEFT BUSS OFF, RETURNED TO GATE. RELEASED FOR SERVICE IAW MEL 24-00-01, CATEGOR
- [SDR FDEA201606252138](https://openairdocs.org/sdr/FDEA201606252138), Jun 25, 2016: SWITCH. INOPERATIVE. RIGHT IRS DC FAIL ILLUMINATED MOMENTARILY AND EXTINGUISHED IN CRUISE; NO OTHER LIGHTS BUT SOME NOISE LIKE A RELAY OPENING AND CLOSING OCCURED ON THE F/O SIDE NE
- [SDR FDEA201604291427](https://openairdocs.org/sdr/FDEA201604291427), Apr 29, 2016: FAN. OUT OF BALANCE. EXCESSIVE N1 VIBRATION ON LT ENG DURING TAKEOFF & CLIMB. N1 STAYED IN AMBER BAND. RAN QRH PROCEDURE & UNABLE TO OBTAIN CLIMB POWER. RETARDED THROTTLE TO OPERATE
- [SDR FDEA201601260327](https://openairdocs.org/sdr/FDEA201601260327), Jan 26, 2016: HOUSING. BROKEN. FIRST OFFICERS SIDE, ESCAPE ROPE COVER WILL NOT STAY IN UPPER LATCH, HOUSING BROKEN. R & R FIRST OFFICERS SIDE ESCAPE ROPE COVER IAW AMM 25-61-00-4. COMPLIED WI
- [SDR FDEA201510233331](https://openairdocs.org/sdr/FDEA201510233331), Oct 23, 2015: LIGHT. INOPERATIVE. SERVICE CHECK, L1 DOOR ESCAPE SLIDE LIGHT INOPERATIVE. RELAMPED L1 DOOR EMER ESCAPE SLIDE LIGHT IAW AMM 33-51-06-2-1, USING BULB PN 767 LAMP, 6VDC 2 AMP. OPERAT
- [SDR FDEA201508102525](https://openairdocs.org/sdr/FDEA201508102525), Aug 10, 2015: SKIN. GOUGED. FUSELAGE SKIN DENTED WITH GOUGE IN THE CENTER AT STRINGER 19L, BS 460. COMPLIED WITH EA F-5330-T0319367 P1.
- [SDR FDEA201508102524](https://openairdocs.org/sdr/FDEA201508102524), Aug 10, 2015: SKIN. CRACKED. LIGHTNING STRIKE ON FUSELAGE SKIN BS 558, BETWEEN STRINGERS 28 & 29L. CUT OUT DAMAGED AREA IAW SRM 53-00-01-2 R16. FABRICATED REPAIR DOUBLER IAW SRM 53-00-01-2R
- [SDR FDEA201501220260](https://openairdocs.org/sdr/FDEA201501220260), Jan 22, 2015: LIGHT. INOPERATIVE. 1R SLIDE ARM LIGHT INOPERATIVE. RELAMPED R1 SLIDE ANNUNCIATOR IAW AMM P2F1 25-6 6-00. OPERATIONS CHECKED NORMAL. ACFT OK FOR SERVICE.
- [SDR FDEA201408052082](https://openairdocs.org/sdr/FDEA201408052082), Aug 5, 2014: SKIN. DAMAGED. RIGHT OTBD AFT FLAP BOTTOM PUNCTURED & TOP CRACKED OTBD OF OTBD FAIRING. REPAIRED OTBD AFT FLAP TE IAW SRM 57-53-01 & SRM 51-70-04 PARA B & PARA G FIG 9. TOP SU
- [SDR FDEA201406171477](https://openairdocs.org/sdr/FDEA201406171477), Jun 17, 2014: SEAL. UNSECURE. FIRST OFFICER`S WINDOW WILL NOT CLOSE. WINDOW CONTACTING UPPER AFT WINDOW SEAL. SECURED SEAL, WINDOW OPS NORMAL IAW AMM 56-11-04-4.
- [SDR FDEA201401150120](https://openairdocs.org/sdr/FDEA201401150120), Jan 15, 2014: CONTROL ROD. BENT. R1 ARMING INDICATOR RETRACTABLE DOOR STICKY & HAS A WEAK SPRING. RELEASED FOR SERVICE IAW MEL 52-11-01-B. IDENTIFY L1 & OR R1 DOOR SLIDES, INOPERABLE OR MISSING
- [SDR FDEA201311152792](https://openairdocs.org/sdr/FDEA201311152792), Nov 15, 2013: BEARING. BROKEN. FOUND L1 DOOR HARD TO CLOSE. DISCOVERED BROKEN BEARING ON CRANK ROLLER IN UPPER CORNER. INSTALLED BEARING, DOOR OPERATES NORMAL.
- [SDR FDEA201309272334](https://openairdocs.org/sdr/FDEA201309272334), Sep 27, 2013: CONTROL UNIT. FAILED. FL 400, CAPTAIN`S LT FWD WINDOW CRACKED, EICAS MESSAGE LT FWD WINDOW. NO DEFORMATION OR AIR LEAKAGE NOTED. REMOVED AND REPLACED WINDOW HEAT CONTROL UNIT MM 30-4
- [SDR FDEA201307241645](https://openairdocs.org/sdr/FDEA201307241645), Jul 24, 2013: SKIN. DAMAGED. LIGHTNING STRIKE ON FUSELAGE SKIN BS 585 BETWEEN S29 - 30L. BLENDED OUT AREA AND FOUND AREA CRACKED. CUTOUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER AND FABRI
- [SDR FDEA201206202276](https://openairdocs.org/sdr/FDEA201206202276), Jun 20, 2012: TERMINAL. LOOSE. RT INTERIOR EMERGENCY EXIT LIGHT DOES NOT TEST. FOUND GROUND GD498-DC LOOSE AT TERMINAL STUD. TIGHTENED TERMINAL AT GROUND STUD REF SMP. PERFORMED OPS TEST OF I
- [SDR FDEA201206192270](https://openairdocs.org/sdr/FDEA201206192270), Jun 19, 2012: TERMINAL. LOOSE. RT INTERIOR EMERGENCY EXIT LIGHT DOES NOT TEST. FOUND GROUND GD498-DC LOOSE AT TERMINAL STUD. TIGHTENED TERMINAL AT GROUND STUD REF SMP. PERFORMED OPS TEST OF I
- [SDR FDEA201203201035](https://openairdocs.org/sdr/FDEA201203201035), Mar 20, 2012: GUARD. DAMAGED. EMERGENCY LIGHTS ARMING SWITCH MUST BE MANUALLY ARMED. DOES NOT ARM OR TURN OFF WHEN CLOSING OR OPENING SWITCH HANDLE. REMOVED AND REPLACED PILOTS EMERGENCY LIG
- [SDR FDEA201108193375](https://openairdocs.org/sdr/FDEA201108193375), Aug 19, 2011: STRUCTURE. CORRODED. AFT LWR CARGO BAY, AFTER REMOVAL OF SUPPORT FITTING AT LOWER SILL NR 2 DOOR CUTOUT AREA. CORROSION FOUND UNDER SUPPORT FITTING ON LOWER CHORD STA 1415 - 1425. R
- [SDR FDEA201108113202](https://openairdocs.org/sdr/FDEA201108113202), Aug 11, 2011: FRAME. CORRODED. AFT LOWER CARGO COMP WHILE CARRYING OUT REPAIR CORROSION WAS EXPOSED WHILE REMOVING SEALANT AT STA 1400, FRAME LWR STRAP, BETWEEN STRINGERS S26L -26R. FRAME REM
- [SDR FDEA201108103180](https://openairdocs.org/sdr/FDEA201108103180), Aug 10, 2011: FAIRING. GOUGED. NR 1 NAC STRUT AFT FAIRING STRUCTURE LOWER EXTERNAL SKIN INBD SIDE FOUND WITH PUNCTURE HOLE AT PP STA 260.0. PUNCTURED SKIN REPAIRED IAW EA F-5480-150719. REPAI
- [SDR FDEA201108103179](https://openairdocs.org/sdr/FDEA201108103179), Aug 10, 2011: FAIRING. GOUGED. NR 2 NAC STRUT AFT FAIRING STRUCTURE LOWER EXTERNAL SKIN OTBD SIDE FOUND WITH GOUGE MARK AT PP STA 260.0. REPAIR CARRIED OUT ON GOUGED SKIN IAW EA F-5480-150720
- [SDR FDEA201108103178](https://openairdocs.org/sdr/FDEA201108103178), Aug 10, 2011: SKIN. GOUGED. NR 2 NAC STRUT AFT FAIRING STRUCTURE LOWER EXTERNAL SKIN INBD SIDE FOUND WITH PUNCTURE HOLE AT PP STA 260.0. PUNCTURED SKIN REPAIRED IAW EA F-5480-150720. (RT P
- [SDR FDEA201107112636](https://openairdocs.org/sdr/FDEA201107112636), Jul 11, 2011: SKIN. CORRODED. NR1 PYLON UPPER WEB DOUBLER EXTERNAL SKIN AT PPSTA 196.2 FOUND WITH CORROSION. R & R IAW SRM 51-40-02, REV 103. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201107112635](https://openairdocs.org/sdr/FDEA201107112635), Jul 11, 2011: BEAM. DENTED. FWD LWR CARGO NR1 DOOR CENTER EDGE BEAM LWR SURFACE SKIN HAS 2 EA DENTS. DENTS ARE APPROX 1 INCH IN DIAMETER. R & R BEAM IAW EA F-5230-152516. REPAIR IS CLASSIF
- [SDR FDEA201107092619](https://openairdocs.org/sdr/FDEA201107092619), Jul 9, 2011: SHIM. UNKNOWN. WHILE COMPLYING SSIP MOD TO NR 1 STRUT ASSY STRUCTURE, CLEARANCE OF MORE THAN 0.040" SHIMS THICKNESS REQUIRED BETWEEN LOWER SPAR FITTING AND AFT BULKHEAD. ACCOM

All 97: https://openairdocs.org/aircraft/N950FD/reports.md

## Related

- Other Boeing 757-236 aircraft: https://openairdocs.org/model/boeing-757-236/aircraft.md
- STCs for the Boeing 757-236: https://openairdocs.org/model/boeing-757-236/stcs.md
- The Rolls-Royce RB211-535E4 series engine: https://openairdocs.org/engine/rolls-royce-rb211-535e4-series.md

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