# N926FD: 1985 Boeing 757-2S7

- Status: Valid registration
- Airframe: [Boeing 757-2S7](https://openairdocs.org/model/boeing-757-2s7) (registry code 1384962, 178 seats)
- Engine: [Rolls-Royce RB-211 series](https://openairdocs.org/engine/rolls-royce-rb-211-series) (registry code 54555)
- Serial number: 23323
- Year built: 1985
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 19, 1985
- Certificate issued: September 27, 2010
- Expires: May 31, 2028
- Mode S code: ACD4F5
- 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=926FD
- Page: https://openairdocs.org/aircraft/N926FD

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. The registry lists only the engine series, so ADs for every Rolls-Royce RB-211 model are included.

## ADs that may apply (OpenAirDocs): 140 in force

### Matched by airframe (Boeing 757-2S7)

None in force.

### Matched by engine (Rolls-Royce RB-211 series)

- [AD 2026-20-11](https://openairdocs.org/ad/2026-20-11): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Nov 17, 2026
- [AD 2026-18-04](https://openairdocs.org/ad/2026-18-04): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Oct 16, 2026
- [AD 2026-18-52](https://openairdocs.org/ad/2026-18-52): Turbine Engine Oil System · Rolls-Royce Deutschland RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Sep 21, 2026
- [AD 2026-18-51](https://openairdocs.org/ad/2026-18-51): Turbine Engine Oil System · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Sep 21, 2026
- [AD 2026-10-06](https://openairdocs.org/ad/2026-10-06): Turbine Section · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Jun 12, 2026
- [AD 2025-05-04](https://openairdocs.org/ad/2025-05-04): Engine Drains · Rolls-Royce Deutschland RB211-TRENT 970-84 and RB211-TRENT 972-84. Effective Apr 1, 2025
- [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 2024-07-04](https://openairdocs.org/ad/2024-07-04): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-524H-36 and RB211-524H-T-36. Effective Apr 15, 2024
- [AD 2023-23-13](https://openairdocs.org/ad/2023-23-13): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Jan 4, 2024
- [AD 2023-22-01](https://openairdocs.org/ad/2023-22-01): Turbine Section · Rolls-Royce Deutschland RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19 and 5 more. Effective Dec 26, 2023
- [AD 2023-21-03](https://openairdocs.org/ad/2023-21-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19 and 5 more. Effective Dec 11, 2023
- [AD 2023-18-05](https://openairdocs.org/ad/2023-18-05): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-535C-37. Effective Oct 30, 2023
- [AD 2023-18-01](https://openairdocs.org/ad/2023-18-01): Engine Fuel Pump · Rolls-Royce Deutschland RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Oct 30, 2023
- [AD 2023-17-12](https://openairdocs.org/ad/2023-17-12): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Oct 26, 2023
- [AD 2022-09-10](https://openairdocs.org/ad/2022-09-10): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Jun 23, 2022
- [AD 2021-08-01](https://openairdocs.org/ad/2021-08-01): Turbine Engine Combustion Section · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Apr 30, 2021
- [AD 2020-25-04](https://openairdocs.org/ad/2020-25-04): Engine Fireseals · Rolls-Royce Deutschland RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Jan 8, 2021
- [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 2019-11-07](https://openairdocs.org/ad/2019-11-07): Turbine Engine Compressor Section · Rolls-Royce RB211-524G3-19, RB211-524G3-T-19, RB211-524H-36 and 3 more. Effective Jun 28, 2019
- [AD 2018-18-15](https://openairdocs.org/ad/2018-18-15): Turbine Engine Compressor Section · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Nov 1, 2018
- [AD 2018-18-06](https://openairdocs.org/ad/2018-18-06): Turbine Section · Rolls-Royce RB211-TRENT 970-84, RB211-TRENT 970B-84, RB211-TRENT 972-84 and 4 more. Effective Sep 20, 2018
- [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 2017-19-16](https://openairdocs.org/ad/2017-19-16): Turbine Engine Compressor Section · Rolls-Royce RB211 Trent 553-61, RB211 Trent 553A2-61, RB211 Trent 556-61 and 5 more. Effective Oct 13, 2017
- [AD 2017-10-13](https://openairdocs.org/ad/2017-10-13): Low-pressure (LP) fuel return tube · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Jul 10, 2017
- [AD 2017-10-06](https://openairdocs.org/ad/2017-10-06): Turbine Engine Compressor Section · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Jun 9, 2017
- [AD 2017-08-11](https://openairdocs.org/ad/2017-08-11): Engine · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective May 30, 2017
- [AD 2017-08-10](https://openairdocs.org/ad/2017-08-10): Engine · Rolls-Royce RB211-TRENT 970-84, RB211-TRENT 970B-84, RB211-TRENT 972-84 and 4 more. Effective May 9, 2017
- [AD 2017-03-03](https://openairdocs.org/ad/2017-03-03): Engine Oil Cooler · Rolls-Royce RB211 Trent 553-61, RB211 Trent 553A2-61, RB211 Trent 556-61 and 5 more. Effective Mar 17, 2017
- [AD 2016-25-10](https://openairdocs.org/ad/2016-25-10): High-pressure compressor (HPC) · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Jan 20, 2017
- [AD 2016-08-07](https://openairdocs.org/ad/2016-08-07): LPT support roller bearing · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 22 more. Effective May 16, 2016
- [AD 2016-04-13](https://openairdocs.org/ad/2016-04-13): Sealing sleeve · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Apr 19, 2016
- [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 2015-16-03](https://openairdocs.org/ad/2015-16-03): High-pressure turbine (HPT) blades · Rolls-Royce RB211-524B-02, RB211-524B2-19, RB211-524B3-02 and 6 more. Effective Sep 15, 2015
- [AD 2015-07-01](https://openairdocs.org/ad/2015-07-01): Low-pressure turbine (LPT) stage 3 turbine blades · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 4 more. Effective May 8, 2015
- [AD 2015-04-06](https://openairdocs.org/ad/2015-04-06): Electronic engine control (EEC) · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Apr 8, 2015
- [AD 2015-02-20](https://openairdocs.org/ad/2015-02-20): Intermediate-pressure compressor (IPC) rotor shaft · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 22 more. Effective Mar 11, 2015
- [AD 2014-14-01](https://openairdocs.org/ad/2014-14-01): Electronic engine control (EEC) · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Aug 15, 2014
- [AD 2014-13-02](https://openairdocs.org/ad/2014-13-02): LP turbine bearing support and exhaust case assembly · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Aug 5, 2014
- [AD 2014-13-03](https://openairdocs.org/ad/2014-13-03): Electronic engine control (EEC) software · Rolls-Royce RB211 Trent 553-61, RB211 Trent 553A2-61, RB211 Trent 556-61 and 5 more. Effective Jul 14, 2014
- [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 2013-23-12](https://openairdocs.org/ad/2013-23-12): Low-pressure (LP) compressor fan blade set · Rolls-Royce RB211 Trent 553-61, RB211 Trent 553A2-61, RB211 Trent 556-61 and 5 more. Effective Dec 11, 2013
- [AD 2013-19-21](https://openairdocs.org/ad/2013-19-21): Cracks in the HP compressor stage 1 and 2 disc posts · Rolls-Royce RB211-524G2-T-19, RB211-524G3-T-19, RB211-524H-T-36 and 19 more. Effective Nov 6, 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 2013-05-04](https://openairdocs.org/ad/2013-05-04): Piston ring · Rolls-Royce RB211-TRENT 970-84, RB211-TRENT 970B-84, RB211-TRENT 972-84 and 4 more. Effective Apr 30, 2013
- [AD 2013-04-01](https://openairdocs.org/ad/2013-04-01): Thrust reverser units (TRUs) · Rolls-Royce RB211-524D4-19, RB211-524D4-39, RB211-524D4-B-19 and 11 more. Effective Mar 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 2013-02-03](https://openairdocs.org/ad/2013-02-03): Fuel oil heat exchanger (FOHE) · Rolls-Royce RB211-TRENT 970-84, RB211-TRENT 970B-84, RB211-TRENT 972-84 and 4 more. Effective Jan 24, 2013
- [AD 2012-25-08](https://openairdocs.org/ad/2012-25-08): High pressure/ intermediate pressure (HP/IP) turbine bearing support oil feed tube outer heat shield · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Jan 10, 2013
- [AD 2012-24-05](https://openairdocs.org/ad/2012-24-05): Oil transfer tube · Rolls-Royce RB211-TRENT 970-84 and RB211-TRENT 972-84. Effective Dec 26, 2012
- [AD 2012-18-07](https://openairdocs.org/ad/2012-18-07): Low-pressure (LP) compressor blades · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Oct 29, 2012

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

- [AD 2021-26-11](https://openairdocs.org/ad/2021-26-11) (historical): Engine Fuel Pump · Rolls-Royce Deutschland RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Jan 3, 2022
- [AD 2020-24-08](https://openairdocs.org/ad/2020-24-08) (historical): Turbine Section · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Jan 4, 2021
- [AD 2020-15-07](https://openairdocs.org/ad/2020-15-07) (historical): Turbine Section · Rolls-Royce Deutschland RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19 and 5 more. Effective Aug 4, 2020
- [AD 2020-06-16](https://openairdocs.org/ad/2020-06-16) (historical): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective May 5, 2020
- [AD 2019-05-02](https://openairdocs.org/ad/2019-05-02) (historical): Powerplant/Engine Drains · Rolls-Royce RB211-TRENT 970-84 and RB211-TRENT 972-84. Effective Mar 27, 2019
- [AD 2017-22-13](https://openairdocs.org/ad/2017-22-13) (historical): Powerplant/Engine Drains · Rolls-Royce RB211-TRENT 970-84 and RB211-TRENT 972-84. Effective Nov 22, 2017
- [AD 2017-03-02](https://openairdocs.org/ad/2017-03-02) (historical): LP compressor blade · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Mar 22, 2017
- [AD 2017-01-01](https://openairdocs.org/ad/2017-01-01) (historical): Engine (Turbine/Turboprop) · Rolls-Royce RB211-TRENT 970-84, RB211-TRENT 970B-84, RB211-TRENT 972-84 and 4 more. Effective Jan 26, 2017
- [AD 2016-24-08](https://openairdocs.org/ad/2016-24-08) (historical): Upper bifurcation fairing · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Jan 5, 2017
- [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 2015-17-19](https://openairdocs.org/ad/2015-17-19) (historical): Fan case low-pressure (LP) fuel tube · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Oct 20, 2015
- [AD 2015-04-03](https://openairdocs.org/ad/2015-04-03) (historical): High- pressure/intermediate-pressure (HP/IP) turbine support internal oil feed tube · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Mar 30, 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 2014-16-10](https://openairdocs.org/ad/2014-16-10) (historical): LP compressor blades · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Sep 23, 2014
- [AD 2014-05-25](https://openairdocs.org/ad/2014-05-25) (historical): Low-pressure turbine exhaust case and support assembly or tail bearing housing · Rolls-Royce RB211-TRENT 970-84, RB211-TRENT 970B-84, RB211-TRENT 972-84 and 4 more. Effective Apr 7, 2014
- [AD 2013-26-10](https://openairdocs.org/ad/2013-26-10) (historical): High-pressure (HP) compressor rotor stage 1 and stage 2 discs · Rolls-Royce RB211-524G2-19, RB211-524G3-19, RB211-524H-36 and 1 more. Effective Jan 23, 2014
- [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 2013-15-10](https://openairdocs.org/ad/2013-15-10) (historical): Cracking on the IP compressor rotor shaft rear balance land · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 22 more. Effective Oct 8, 2013
- [AD 2013-12-01](https://openairdocs.org/ad/2013-12-01) (historical): LP compressor blades · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Jul 29, 2013
- [AD 2013-05-18](https://openairdocs.org/ad/2013-05-18) (historical): Fuel tubes and fuel tube clips · Rolls-Royce RB211 Trent 553-61, RB211 Trent 553A2-61, RB211 Trent 556-61 and 5 more. Effective Apr 5, 2013
- [AD 2013-02-04](https://openairdocs.org/ad/2013-02-04) (historical): Low-pressure turbine (LPT) stage 2 disk interstage seal material loss and increased low-pressure rotor vibration while in flight · Rolls-Royce RB211-TRENT 970-84, RB211-TRENT 970B-84, RB211-TRENT 972-84 and 4 more. Effective Feb 14, 2013
- [AD 2012-10-12](https://openairdocs.org/ad/2012-10-12) (historical): Compressor rotor shafts · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 15 more. Effective Jun 29, 2012
- [AD 2012-06-23](https://openairdocs.org/ad/2012-06-23) (historical): LP compressor blades · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Apr 20, 2012
- [AD 2012-04-13](https://openairdocs.org/ad/2012-04-13) (historical): HP compressor stage 1 and 2 disc posts · Rolls-Royce RB211-524G2-T-19, RB211-524G3-T-19, RB211-524H-T-36 and 19 more. Effective Apr 11, 2012
- [AD 2012-04-01](https://openairdocs.org/ad/2012-04-01) (historical): Critical engine parts · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Mar 28, 2012
- [AD 2012-02-04](https://openairdocs.org/ad/2012-02-04) (historical): Engine fuel leaks · Rolls-Royce RB211 Trent 553-61, RB211 Trent 553A2-61, RB211 Trent 556-61 and 5 more. Effective Feb 24, 2012
- [AD 2011-13-01](https://openairdocs.org/ad/2011-13-01) (historical): Rivets · Rolls-Royce RB211-524D4-19, RB211-524D4-39, RB211-524D4-B-19 and 11 more. Effective Aug 12, 2011
- [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 2011-09-07](https://openairdocs.org/ad/2011-09-07) (historical): High-pressure compressor (HPC) Stage 1 and 2 disc posts · Rolls-Royce RB211-524G2-T-19, RB211-524G3-T-19, RB211-524H-T-36 and 19 more. Effective Jun 7, 2011
- [AD 2011-08-07](https://openairdocs.org/ad/2011-08-07) (historical): LP compressor blades · Rolls-Royce RB211-Trent 884B-17, RB211-Trent 892B-17, RB211-Trent 895-17 and 4 more. Effective Jun 7, 2011
- [AD 2010-16-07](https://openairdocs.org/ad/2010-16-07) (historical): IP turbine · Rolls-Royce RB211-TRENT 970-84, RB211-TRENT 970B-84, RB211-TRENT 972-84 and 4 more. Effective Sep 17, 2010
- [AD 2009-24-05](https://openairdocs.org/ad/2009-24-05) (historical): Fuel pipes · Rolls-Royce RB211-Trent-884B-17, RB211-Trent-892B-17, RB211-Trent-895-17 and 4 more. Effective Jan 4, 2010
- [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
- [AD 2008-18-08](https://openairdocs.org/ad/2008-18-08) (historical): IP Compressor rotor · Rolls-Royce RB211-Trent 884B-17, RB211-Trent 892B-17, RB211-Trent 895-17 and 14 more. Effective Oct 14, 2008
- [AD 2007-19-10](https://openairdocs.org/ad/2007-19-10) (historical): Intermediate Pressure Compressor (IP Compressor) Drums · Rolls-Royce RB211 Trent 553-61, RB211 Trent 553A2-61, RB211 Trent 556-61 and 5 more. Effective Oct 3, 2007
- [AD 2006-11-05 R1](https://openairdocs.org/ad/2006-11-05-R1) (historical): Disc assemblies · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective May 1, 2007
- [AD 2007-02-05](https://openairdocs.org/ad/2007-02-05) (historical): High pressure-and-intermediate pressure (HP-IP) turbine internal and external oil 
vent tubes · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Feb 6, 2007
- [AD 2006-23-11](https://openairdocs.org/ad/2006-23-11) (historical): High pressure (HP)/intermediate pressure (IP) turbine bearing oil feed tube 
heat shield · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Dec 19, 2006
- [AD 2006-11-05](https://openairdocs.org/ad/2006-11-05) (historical): High pressure compressor (HPC) stage 3 disc assemblies · Rolls-Royce RB211-22B-02, RB211-524B-02, RB211-524B-B-02 and 24 more. Effective Jun 27, 2006
- [AD 2006-05-03](https://openairdocs.org/ad/2006-05-03) (historical): High pressure-intermediate pressure (HP- IP) turbine · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Mar 27, 2006
- [AD 2005-15-13](https://openairdocs.org/ad/2005-15-13) (historical): Intermediate pressure (IP) compressor stage 5 disks · Rolls-Royce RB211-524 Series (all). Effective Aug 30, 2005
- [AD 2005-02-05](https://openairdocs.org/ad/2005-02-05) (historical): Low Pressure Compressor (LPC) Fan Blade Roots · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Feb 11, 2005
- [AD 2004-26-05](https://openairdocs.org/ad/2004-26-05) (historical): Head section and meterpanel assembly of the combustion liner · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 20 more. Effective Feb 9, 2005
- [AD 2005-01-15](https://openairdocs.org/ad/2005-01-15) (historical): Fan blade dovetail roots · Rolls-Royce RB211-Trent-844B-17, RB211-Trent-884B-17, RB211-Trent-892B-17 and 5 more. Effective Jan 28, 2005
- [AD 2004-26-03](https://openairdocs.org/ad/2004-26-03) (historical): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Jan 13, 2005
- [AD 2004-23-03](https://openairdocs.org/ad/2004-23-03) (historical): High pressure-and-intermediate pressure (HP-IP) turbine internal and external oil vent tubes shaft · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Nov 23, 2004
- [AD 2004-15-02](https://openairdocs.org/ad/2004-15-02) (historical): LP Compressor Fan Blade · Rolls-Royce RB211-Trent-884B-17, RB211-Trent-892B-17, RB211-Trent-895-17 and 4 more. Effective Sep 1, 2004
- [AD 2004-01-20](https://openairdocs.org/ad/2004-01-20) (historical): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 24, 2004
- [AD 2003-17-15](https://openairdocs.org/ad/2003-17-15) (historical): Low pressure (LP) turbine stage 2 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Oct 2, 2003

All 211: https://openairdocs.org/aircraft/N926FD/ads.md

## Information bulletins (advisory) (1 in force)

- [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 N926FD.

## FAA accident and incident reports

None matched to N926FD.

## Service difficulty reports (95, 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 FDEA202304130639](https://openairdocs.org/sdr/FDEA202304130639), Apr 13, 2023: UNKNOWN. UNKNOWN. UPON SELECTING FLAPS 25, TE FLAP DISAGREE MESSAGE. COMPLIED WITH QRH. LANDED WITH FLAPS 20, LANDING SPEED 138. EMERGENCY DECLARED. ACCOMPLISHED FSEU BITE CHECKS
- [SDR FDEA202208061907](https://openairdocs.org/sdr/FDEA202208061907), Aug 6, 2022: CONNECTOR. NOT SEATED. PDIS 926 27-50 0370 06AUG22 FAT OPEN U WHEN SELECTING FLAPS 25 FOR LANDING WE RECEIVED THE TE FLAP DISAGREE EICAS MESSAGE. WE INITIATED A GO AROUND, COMPLIED WI
- [SDR FDEA202204060880](https://openairdocs.org/sdr/FDEA202204060880), Apr 6, 2022: COLLAR. DAMAGED. ON ARRIVAL FOUND R1 DOOR GUST LOCK BROKEN. COLLAR ASSY MPN: 654N0244-7 CPN: 5214377 QTY: 1 REMOVED AND REPLACED R1 DOOR GUST LOCK DOOR HOLD OPEN COLLAR WITH ANO
- [SDR FDEA202203260700](https://openairdocs.org/sdr/FDEA202203260700), Mar 26, 2022: NONE. UNKNOWN. TE FLAP DISAGREE ON FINAL. QRH COMPLIED WITH. PERFORMED BITE OF ALL 3 FSEU'S FOUND NO CURRENT FAULTS. ATTEMPTED TO DUPLICATE FAULT, OPERATED FLAP/SLATS FROM FAI
- [SDR FDEA202108202048](https://openairdocs.org/sdr/FDEA202108202048), Aug 20, 2021: FRAME. DAMAGED. REPAIR INSTRUCTIONS REQUIRED FOR THE ACCOMPLISHMENT OF FEDEX E.A. F-5310-147693, PART 10, SPLICE REPAIR AT STA 1640, S9R TO S20R COMPLIED WITH E.A F-5310-147693
- [SDR FDEA202108112001](https://openairdocs.org/sdr/FDEA202108112001), Aug 11, 2021: SKIN. DENTED. FUSELAGE SKIN @ STA 1730, BETWEEN STR 29L - STR 29R, HAS 2EA DENTS. REPAIRED SKIN IAW FEDEX EA # F-5330-146539-P3
- [SDR FDEA202105081161](https://openairdocs.org/sdr/FDEA202105081161), May 8, 2021: LINE. LEAKING. A SLOW LOSS OF RIGHT HYDRAULIC SYSTEM FLUID LED TO RIGHT HYDRAULIC SYSTEM FAILURE. COMPLIED WITH QRH, DECLARED AN EMERGENCY. AIRCRAFT WAS AIRBORNE FOR APPROXIMA
- [SDR FDEA202103090608](https://openairdocs.org/sdr/FDEA202103090608), Mar 9, 2021: DRIVE UNIT. FAILED. WHEN CONFIGURING TO LAND AT SLC IT WAS VERY DIFFICULT TO MOVE FLAP LEVER FROM 20 TO 25 DETENT. WHEN I FINALLY WAS ABLE TO MOVE FLAP LEVER TO 25, WE RECEIVED A T
- [SDR FDEA202101290236](https://openairdocs.org/sdr/FDEA202101290236), Jan 29, 2021: ACTUATOR. INOPERATIVE. MAIN CARGO DOOR WILL NOT CLOSE. FOUND BOTH LINKS ON AFT MAIN CARGO DOOR ACTUATOR BROKEN. RAISED CARGO DOOR WITH SLING REF B757 AMM CH 52-32-00-4 SO CARGO COULD 
- [SDR FDEA202012063050](https://openairdocs.org/sdr/FDEA202012063050), Dec 6, 2020: SKIN. DAMAGED. LOWER FUSELAGE SKINS BETWEEN STA 1540 AND STA 1640 STRINGERS S-30 TO S-26L HAS NUMEROUS PLACES OF DAMAGE. COMPLIED WITH EA F-5330-T0358203 TITLED: FUSELAGE-SECT
- [SDR FDEA202012063049](https://openairdocs.org/sdr/FDEA202012063049), Dec 6, 2020: STRAP. DAMAGED. AFT CARGO COMPARTMENT FUSELAGE CIRCUMFERENTIAL STRAP AT STA 1620 FROM STRINGER S-28L TO S-29R PUNCTURED, DEFORMED WITH SURFACE CORROSION. REMOVED AND REPLACED C
- [SDR FDEA202012063048](https://openairdocs.org/sdr/FDEA202012063048), Dec 6, 2020: STRINGER CLIP. DAMAGED. AFT CARGO COMPARTMENT STRINGER CLIP AT S30 STA 1616 TO STA 1623 SEPARTED FROM SKIN AND HAS SHEARED FASTENERS AND SURFACE CORROSION. REMOVED AND REPLACED SPLICE 
- [SDR FDEA202012063047](https://openairdocs.org/sdr/FDEA202012063047), Dec 6, 2020: STRINGER SPLICE. DAMAGED. AFT CARGO COMPARTMENT STRINGER S-29L STRINGER SPLICE AT STA 1620 PUNCTURED AND STRINGER FROM STA 1623 TO STA 1630 DEFORMED. REMOVED AND REPLACED STRINGER SPLICE
- [SDR FDEA202012053034](https://openairdocs.org/sdr/FDEA202012053034), Dec 5, 2020: STRINGER. BENT. AFT CARGO COMPARTMENT STRINGER S-27L BETWEEN STA 1588 TO STA 1600 BENT AND DEFORMED. REPAIRED STRINGER S-27L AT STA 1570, IAW SRM 53-00-03-2R. REPAIR BETWEEN ST
- [SDR FDEA202012043030](https://openairdocs.org/sdr/FDEA202012043030), Dec 4, 2020: SKIN. DAMAGED. FUSELAGE SKIN HAS DENT AND CREASE DAMAGE BETWEEN STA 1520 AND STA 1540 STRAINGERS S-25L TO S-26L. COMPLIED WITH EA F-5330-T0358196 PART 1 TITLE: FUSELAGE-SECTIO
- [SDR FDEA202012043029](https://openairdocs.org/sdr/FDEA202012043029), Dec 4, 2020: SHEAR TIE. CRACKED. AFT CARGO COMPARTMENT SHEAR TIE AT STA 1600 STRINGER S-27L TO S-28L SHEARED/CRACKED. REMOVED AND REPLACED SHEAR TIE STA 1600 S-27L TO S-28L, IAW SRM 51-40-02. F
- [SDR FDEA202012043028](https://openairdocs.org/sdr/FDEA202012043028), Dec 4, 2020: SHEAR TIE. CRACKED. AFT CARGO COMPARTMENT SHEAR TIE AT STA 1620 FROM STRINGER S-28L TO S-29L SHEARED, CRACKED. REMOVED AND REPLACED SHEAR TIE STA 1620 S-28L TO S-29L, IAW SRM 51-40
- [SDR FDEA202012043027](https://openairdocs.org/sdr/FDEA202012043027), Dec 4, 2020: SHEAR TIE. BENT. AFT CARGO COMPARTMENT SHEAR TIE AT STRINGER S-29L TO S-30 DEFORMED WITH SURFACE CORROSION. REMOVED AND REPLACED SHEAR TIE, IAW SRM 51-40-02. FABED ON VTMAE TRAV
- [SDR FDEA202007171565](https://openairdocs.org/sdr/FDEA202007171565), Jul 17, 2020: CREASE BEAM. CORRODED. MAIN DECK, BS 765 RT INBD CREASE BEAM WAS CORRODED. REMOVED THE CORROSION IAW SRM 51-10-02. EVALUATED 100% MATERIAL LOSS, AND OUT OF LIMITS IAW SRM 53-30-13, FI
- [SDR FDEA2020030970501](https://openairdocs.org/sdr/FDEA2020030970501), Mar 7, 2020: UNKNOWN. MALFUNCTIONED. PDIS 926 27-50 8236 07MAR20 RNO FACT U LOGPAGES:3215684 EXTENDING FLAPS FROM 15*- 20* RECEIVED TE FLAP DISAGREE CAUTIN MESSAGE. FLAPS STOPPED MOVING AT 17*. COM
- [SDR FDEA202001110158](https://openairdocs.org/sdr/FDEA202001110158), Jan 11, 2020: SKIN. DAMAGED. THE LH SIDE OF THE FUSELAGE FROM STA 510-515 2"-4" DOWN FROM STR 26L HAS SEVERAL DEEP PITS FROM LIGHTNING STRIKE. REPAIRED DAMAGE IN FUSELAGE SKIN CAUSED BY LIG
- [SDR FDEA201907251695](https://openairdocs.org/sdr/FDEA201907251695), Jul 25, 2019: FRAME. CRACKED. FORWARD CARGO COMPARTMENT, BS 740 JUST ABOVE STRINGER 22R FRAME IS CRACKED AT TOOLING HOLE. VERIFIED BY HFEC (OPEN HOLE) INSPECTION, CIRCLED HOLE IN BLACK.
- [SDR FDEA201907241678](https://openairdocs.org/sdr/FDEA201907241678), Jul 24, 2019: DOOR. CRACKED. POSSIBLE CRACK ON L2 DOOR UPPER HINGE CUTOUT ALL WORK ACCOMPLISHED IAW EA F-5210-T0348085 P1 DOORS - PASSENGER/CREW - CARGO - L -2 DOOR FORWARD FRAME UPPER HING
- [SDR FDEA201907231668](https://openairdocs.org/sdr/FDEA201907231668), Jul 23, 2019: FILLER. CORRODED. AFT CARGO COMPT STA 1440 AT STR 29R TAPERED FILLER ON STRINGER HAS EXFOLIATING CORROSION. FOUND TAPERED FILLER AT STA 1440 STR 29R OUT OF LIMITS DUE TO 100% MAT
- [SDR FDEA201907111527](https://openairdocs.org/sdr/FDEA201907111527), Jul 11, 2019: STRINGER. CORRODED. AFT PIT - BS 1440, STR. 29 RT HAS CORROSION ON I/B SIDE.
- [SDR FDEA201907101520](https://openairdocs.org/sdr/FDEA201907101520), Jul 10, 2019: SEAT TRACK. CORRODED. MAIN CABIN BETWEEN STA 1180-1200 LBL44.5 SEAT TRACK FANGE CORRODED EVALUATED SEAT TRACK STA 1180-1200 LBL 44.5 ORIG MAT .070 REM .00 LOSS .070 OUT OF LIMITS IAW
- [SDR FDEA201907101519](https://openairdocs.org/sdr/FDEA201907101519), Jul 10, 2019: SEAT TRACK. CORRODED. MAIN CABIN BETWEEN STA 1040-1055 BLO CORROSION ON SEAT TRACK FLANGE. REMOVED CORR ON SEAT TRACK (FLANGE) SUPPORT STA 1040-1055 BL0 IAW SRM 51-10- 02. ORIG MAT.0
- [SDR FDEA201907101521](https://openairdocs.org/sdr/FDEA201907101521), Jul 10, 2019: SEAT TRACK. CORRODED. MAIN CABIN STA 1195 BL0 SEAT TRACK FLANGE CORRODED.
- [SDR FDEA201907091513](https://openairdocs.org/sdr/FDEA201907091513), Jul 9, 2019: SKIN. DENTED. LT FUSELAGE OUTER SKIN AT FS 215 AROUND S-21L HAS A DENT. EVALUATED DENT ON SKIN STA. 215 AROUND S-21L A\Y FOUND TO BE IN LIMITS IAW SRM 53-00-01-1A. HFEC IAW N
- [SDR FDEA201907061494](https://openairdocs.org/sdr/FDEA201907061494), Jul 6, 2019: SHEAR PLATE. CORRODED. MAIN CABIN BETWEEN STA. 1680 - 1720, BL0 RBL53 FLOOR WEB CORRODED ALL WORK ACCOMPLISHED IAW EA F-5310-T0348184 P1 FUSELAGE - MAINFRAME - AFT SHEAR DECK PLATE CO
- [SDR FDEA201907061492](https://openairdocs.org/sdr/FDEA201907061492), Jul 6, 2019: FLOORBEAM. CORRODED. MAIN CABIN BETWEEN STA. 920 - 1040 RBL 24.75 FLOOR BEAM T CHORD CORRODED REMOVED CORR ON T-CHORD STA 920-1040 RBL 24.75 IAW SRM 51-10-02. ORIG MAT .090 REM .045
- [SDR FDEA201907061491](https://openairdocs.org/sdr/FDEA201907061491), Jul 6, 2019: SEAT TRACK. CORRODED. MAIN CABIN BETWEEN STA. 1620 - 1640 RBL 44.5 SEAT TRACK FLANGE CORRODED REMOVED CORR ON SEAT TRACK FLANGE STA 1620-1640 RBL 44.5 IAW SRM 51-10-02. ORIG MAT. .07
- [SDR FDEA201907061493](https://openairdocs.org/sdr/FDEA201907061493), Jul 6, 2019: FLOORBEAM. CORRODED. MAIN CABIN BETWEEN STA. 1015 - 1021 BLB 24.75 FLOORBEAM T CHORD CORRODED.
- [SDR FDEA201901120106](https://openairdocs.org/sdr/FDEA201901120106), Jan 12, 2019: SEAT TRACK. GOUGED. REMOVE AND REPLACE LBL 45.50 SEAT TRACK FROM BS440 TO BS680 COMPLIED WITH - EQUIP AND FURNISH - CARGO - LOADING SYSTEM - INTERIM REPAIR FOR DAMAGE SEAT TRACK LO
- [SDR FDEA2018080321896](https://openairdocs.org/sdr/FDEA2018080321896), Aug 2, 2018: THERMAL SWITCH. FAILED. LT ENG STRUT OH DET 1 EICAS MESSAGE ON STATUS PAGE DURING CLIMB OUT TO 360. FOUND THERMAL SWITCH S10196 GIVING AN OVERHEAT DETECTION INDICATION BEFORE TEMPERATU
- [SDR FDEA2018080311873](https://openairdocs.org/sdr/FDEA2018080311873), Aug 1, 2018: CIRCUIT CARD. FAILED. WHILE CLIMBING THROUGH FL340 TO 360, LT ENGINE OVHT EICAS MESSAGE ON. PERFORMED QRH, LIGHT EXTINGUISHED AT 1.28 EPR. IAW FIM R&R AFOLDS CARD IAW AMM 26-10-01-4 
- [SDR FDEA201808171644](https://openairdocs.org/sdr/FDEA201808171644), Jul 7, 2018: UNKNOWN. MALFUNCTIONED. AT SPEEDBRAKE DEPLOYMENT A ROLE TO THE LEFT OCCURS WITH A DISPLACEMENT OF THE YOKE TO THE RIGHT. AT DEPLOYMENT YOKE DISPLACES 1.5 UNITS ON AILERON TRIM INDICATO
- [SDR FDEA201806071417](https://openairdocs.org/sdr/FDEA201806071417), Jun 7, 2018: POWER SUPPLY. INOPERATIVE. RT R1 DOOR EXTERIOR SLIDE LIGHT INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY M00730 PER MM CH 33-51-07-2. A/C READY FOR CONT SERVICE.
- [SDR FDEA201708172251](https://openairdocs.org/sdr/FDEA201708172251), Aug 17, 2017: BRACKET. LOOSE. FLAP FAIRING BRACKET FOR 573HB IS LOOSE. REPAIRED THE LT, INBD MAIN FLAP IAW SRM 57-53-02-2R, REPAIR 3, AND EA F-5750-T0334988, PI.
- [SDR FDEA201708082146](https://openairdocs.org/sdr/FDEA201708082146), Aug 8, 2017: SKIN. DENTED. LEFT WING NR 3 SLAT UPPER SURFACE HAS A DENT AT CENTER OF SLAT AT T\E. REPAIRED THE LT WING SLAT IAW SRM 51-70-10-2R, PARAG 8 AND 20.
- [SDR FDEA201708082142](https://openairdocs.org/sdr/FDEA201708082142), Aug 8, 2017: SEAT TRACK. CORRODED. MAIN CABIN, BS 1640 - 1680, LBL45, SEAT TRACK HAS CORROSION ON FLANGE. REMOVED THE CORROSION IAW SRM 51-10-02 WITH 100 PERCENT MATERIAL LOSS. FABRICATED A NEW S
- [SDR FDEA201708082141](https://openairdocs.org/sdr/FDEA201708082141), Aug 8, 2017: SEAT TRACK. CORRODED. MAIN CABIN, BS 1640 - 1660, RBL 45, SEAT TRACK HAS CORROSION ON FLANGE. REMOVED CORROSION IAW SRM 51-10-02-0G, 100 PERCENT LOSS. FABRICATED A NEW SEAT TRACK IAW
- [SDR FDEA201708082140](https://openairdocs.org/sdr/FDEA201708082140), Aug 8, 2017: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK BS 365 - 345, LBL 6 HAS CORROSION. REMOVED THE CORROSION AND FOUND 100% LOSS IAW SRM 51-10-02, & 53-00-52-1A. REMOVED AND REPLACED THE SEA
- [SDR FDEA201705191457](https://openairdocs.org/sdr/FDEA201705191457), May 19, 2017: SIGHT GAUGE. CLOUDY. LEFT ENTRY DOOR INSPECTION WINDOW FOR SLIDE PRESSURE GAUGE IS HAZED, MAKING IT DIFFICULT TO READ. CLEANED THE SIGHT WINDOW IAW AMM: 20-30-02-2. OK FOR SERVICE.
- [SDR FDEA201702020380](https://openairdocs.org/sdr/FDEA201702020380), Feb 2, 2017: COMPUTER. OUT OF ADJUST. AIRCRAFT PITCH CONTROL HAS LAG ON PREFLIGHT CONTROL CHECK AND ON ARRIVAL PITCH AXIS WAS STIFF AND SEEMED TO HAVE A DELAY IN CONTROL. ADJUSTED AND TESTED OF ELEV
- [SDR FDEA201701050053](https://openairdocs.org/sdr/FDEA201701050053), Jan 5, 2017: WARNING BELL. FALSE ACTIVATION. TRIED TO SWITCH TO GROUND POWER AFTER BLOCKIN, THE FIRE BELL SOUNDED FOR 10 SECONDS. NO FIRE LIGHTS ILLUMINATED. NO OTHER INDICATIONS OF FIRE OR ANY OTHER MALFU
- [SDR FDEA201510283395](https://openairdocs.org/sdr/FDEA201510283395), Oct 28, 2015: CIRCUIT CARD. FAULTY. FIRE BELL ACTIVATED AT LIFTOFF, NO VISUAL INDICATIONS OF FIRE, COULD NOT CANCEL BELL. R & R BELL CHIME WARNING CARD AS REQUIRED.
- [SDR FDEA201507242380](https://openairdocs.org/sdr/FDEA201507242380), Jul 24, 2015: SKIN. DENTED. PROTRUDING DENTS, BS 630 STRINGER 26L. COMPLIED WITH EA F-5330-T0319058 PT 1.
- [SDR FDEA201507242379](https://openairdocs.org/sdr/FDEA201507242379), Jul 24, 2015: SKIN. DENTED. PROTRUDING DENTS, STATION 643, STRINGER 26L. COMPLIED WITH EA F-5330-T0319058 PT 1.
- [SDR FDEA201507242377](https://openairdocs.org/sdr/FDEA201507242377), Jul 24, 2015: SKIN. GOUGED. LEFT WING INBD FLAP, UPPER SURFACE HAS 2 EACH DEEP GOUGE AT WS 258. WORK ACCOMPLISHED IAW EA F-5750-T0318998 P 2.

All 95: https://openairdocs.org/aircraft/N926FD/reports.md

## STCs that may be installed (OpenAirDocs) (3)

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 engine (Rolls-Royce RB-211 series)

- [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc. Lists RB211-22B-02
- [STC SE00409LA](https://openairdocs.org/stc/SE00409LA): Installation of gas generator fairing thermal insulation blankets. Air New Zealand Limited. Lists RB211-524G2-19
- [STC SE1516CE](https://openairdocs.org/stc/SE1516CE): Modification of lower fuel control box assembly to incorporate vibration isolators. Trans World Airlines Inc. Lists RB211-22B-02

## Related

- Other Boeing 757-2S7 aircraft: https://openairdocs.org/model/boeing-757-2s7/aircraft.md
- The Rolls-Royce RB-211 series engine: https://openairdocs.org/engine/rolls-royce-rb-211-series.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.