# N943FD: 1987 Boeing 757-2G5

- Status: Valid registration
- Airframe: [Boeing 757-2G5](https://openairdocs.org/model/boeing-757-2g5) (registry code 1384912, 239 seats)
- Engine: [Rolls-Royce RB-211 series](https://openairdocs.org/engine/rolls-royce-rb-211-series) (registry code 54555)
- Serial number: 23929
- Year built: 1987
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 3, 2004
- Certificate issued: June 8, 2010
- Expires: July 31, 2027
- Mode S code: AD18CE
- Registered owners: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Attn:  Michael Wilson](https://openairdocs.org/faa-owner/ATTN%3A%20%20MICHAEL%20WILSON)
- 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=943FD
- Page: https://openairdocs.org/aircraft/N943FD

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 757-2G5)

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/N943FD/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 N943FD.

## FAA accident and incident reports

None matched to N943FD.

## Service difficulty reports (118, 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 FDEA202610121559](https://openairdocs.org/sdr/FDEA202610121559), Oct 12, 2026: SKIN. CORRODED. LEFT WING INBD FLAP UPPER SURFACE O/B SIDE EXTERNAL SKIN SOME AREA WITH CORROSION. LT WING I/B FLAP UPPER SURFACE O/B SIDE WAS REPAIRED IAW B757 SRM 57-53-01-2R
- [SDR FDEA202610091536](https://openairdocs.org/sdr/FDEA202610091536), Oct 9, 2026: FLOORBEAM. CORRODED. MAIN CARGO COMPARTMENT FLOORBEAM BS 1200 BETWEEN 24LBL TO 0BL SOME AREAS WITH CORROSION. AREA OUT OF LIMITS WAS REPAIRED AT MAIN CARGO COMPARTMENT FLOORBEAM BS 
- [SDR FDEA202610051478](https://openairdocs.org/sdr/FDEA202610051478), Oct 5, 2026: SKIN. DELAMINATED. TWO INDICATIONS OF DISBOND WERE FOUND OVER TWO DENTS ON THE UPPER SKIN OF THE LEFT ELEVATOR: ONE AT ELEV STA 107.360, 1.800 INCHES IN DIAMETER AND 13.5 INCHES F
- [SDR FDEA202607030828](https://openairdocs.org/sdr/FDEA202607030828), Jul 3, 2026: DOOR. UNSECURE. COULD NOT GET R1 DOOR SLIDE LIGHT TO ILLUMINATE WHEN CLOSING DOOR. WHILE APPROACHING AIRCRAFT NOTED R1 DOOR NOT COMPLETELY CLOSED. CYCLED DOOR AND ARMED SLIDE, 
- [SDR FDEA202602060138](https://openairdocs.org/sdr/FDEA202602060138), Feb 6, 2026: BULB. FAILED. FOUND L1 OVERHEAD EMERGENCY LIGHT DIM DURING MX PRE-FLIGHT CHECK. AMM: 33-51-01-2 REMOVED AND REPLACED 11 FAULTY BULBS AT THE L1 EMERGENCY EXIT SIGN AS PER ABOV
- [SDR FDEA202507151221](https://openairdocs.org/sdr/FDEA202507151221), Jul 15, 2025: ACTUATOR. FAILED. AFTER ROTATE THE AIRCRAFT BEGAN TO SHAKE IN THE RUDDER PEDALS THEN ENTERED INTO A SUSTAINED DUTCH ROLL THAT CONTINUED TO WORSEN AS WE ACCELERATED. EMERGENCY DEC
- [SDR FDEA202507011087](https://openairdocs.org/sdr/FDEA202507011087), Jul 1, 2025: IDG. FAULTED. IN FLIGHT L GEN OFF AND ASSOCIATED EICAS. L AC BUS OFF. RESET IN FLIGHT. OPERATED NORMALLY FOR 20 MINUTES. SAME MALFUNCTION AGAIN DURING DESCENT. EMERGENCY DECL
- [SDR FDEA202412201823](https://openairdocs.org/sdr/FDEA202412201823), Dec 20, 2024: GUST LOCK. WORN. L1 DOOR GUST LOCK COLLAR BROKEN. INSTALLED SERVICEABLE L1 DOOR LOCK COLLAR. DOOR LOCKS AND UNLOCKS NORMAL. MEL REMOVED
- [SDR FDEA202405010582](https://openairdocs.org/sdr/FDEA202405010582), May 1, 2024: WINDOW. WORN. AT F.L. 330 R FWD WINDOW STARTED TO ARCH. WE RAN THE QRH, AND THEN ONE OF THE PANES SHATTERED. DECLARED AN EMERGENCY INTO BOISE. OFF MPN: 141T4801-50 POS: RH SR
- [SDR FDEA202404230275](https://openairdocs.org/sdr/FDEA202404230275), Apr 23, 2024: COLLAR. CRACKED. R1 DOOR HOLD-OPEN LOCK(GUST LOCK) BROKEN. R1 DOOR HOLD-OPEN LOCK (GUST LOCK) WAS REMOVED AND REPLACED REF 757 AMM 52-11-08-8. OPS CHECK GOOD. A/C OK FOR CONTINU
- [SDR FDEA202404230274](https://openairdocs.org/sdr/FDEA202404230274), Apr 23, 2024: COLLAR. CRACKED. L1 DOOR HOLD-OPEN LOC(GUST LOCK) BROKEN. L1 DOOR HOLD-OPEN LOCK (GUST LOCK) WAS REMOVED AND REPLACED REF 757 AMM 52-11-08-8. OPS CHECK GOOD. A/C OK FOR CONTINUE
- [SDR FDEA202302030204](https://openairdocs.org/sdr/FDEA202302030204), Feb 3, 2023: SKIN. CORRODED. L/H WING, THE LARGE FIXED UPPER SKIN PANEL MOST I/B, THE LEADING EDGE IS STARTING TO LIFT AND HAS FOUR EACH PULLED HI-LOKS AS MARKED. THE LEADING EDGE OF THE PA
- [SDR FDEA202301170123](https://openairdocs.org/sdr/FDEA202301170123), Jan 17, 2023: FLOORBOARD. DELAMINATED. COURIER AREA FLOORBOARD 221 MBF IS DELAMINATED. FABRICATED COURIER FLOORBOARD 221 MBF ON VTMAE TRAVELER # T23/1654447 IAW DWG # SRZ-25-005 REVISION R. MAJOR REP
- [SDR FDEA202208051902](https://openairdocs.org/sdr/FDEA202208051902), Aug 5, 2022: LIGHT. INOPERATIVE. MDIS 943 33-50 0480 05AUG22 BNA OPEN U LT DOOR ESCAPE SLIDE LIGHT INOP RELAMPED LT DOOR ESCAPE SLIDE LIGHT REF B757 MM 33-51-06-2-1. OPS CHECK GOOD AT THIS TIME
- [SDR FDEA202204281085](https://openairdocs.org/sdr/FDEA202204281085), Apr 28, 2022: GUST LOCK. CRACKED. MDIS 943 52-10 0286 28APR22 DAY OPEN U L1 DOOR HOLD OPEN LOCK COLLAR BROKEN MEL 28APR22 23:58 DAY U RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIR
- [SDR FDEA202203310794](https://openairdocs.org/sdr/FDEA202203310794), Mar 31, 2022: NONE. NONE. R1 DOOR SLIDE ARMED LIGHT WILL NOT ILLUMINATE. THE PUSH TO TEST LIGHT WILL NOT ILLUMINATE.
- [SDR FDEA202203310793](https://openairdocs.org/sdr/FDEA202203310793), Mar 31, 2022: NONE. NONE. L1 DOOR SLIDE LIGHT WILL NOT ILLUMINATE WITH THE DOOR IN THE ARMED POSITION. PUSH TO TEST OF THE LIGHT OPERATES NORMALLY.
- [SDR FDEA202203230649](https://openairdocs.org/sdr/FDEA202203230649), Mar 23, 2022: GUST LOCK. FAILED. MDIS 943 52-10 0190 23MAR22 RST OPEN U DURING SERV CK FOUND L1 ENTRY DOOR GUST LOCK COLLAR BROKEN MEL 23MAR22 00:18 RST U RELEASED FOR SERVICE PER MEL : 52-11-0
- [SDR FDEA202110282647](https://openairdocs.org/sdr/FDEA202110282647), Oct 28, 2021: FLAP SYSTEM. MALFUNCTIONED. WHEN SELECTING FLAPS 25, GOT TE FLAP DISAGREE ON EICAS. USED QRH TO SELECT FLAPS 20 WITH ALTERNATE SYSTEM AND LANDED UNEVENTFULLY. UPON BLOCK IN TO GATE FLAPS W
- [SDR FDEA202105201321](https://openairdocs.org/sdr/FDEA202105201321), May 20, 2021: IDG. FAILED. R GEN OFF CAUTION WITH ASSOCIATED R HYD ELEC 2, R UTIL BUS, AND L UTIL BUS ADVISORIES AT 40 KTS DURING TAKEOFF JUST AFTER PRESSING THR BUTTON FOR TAKEOFF THRUST
- [SDR FDEA202103040556](https://openairdocs.org/sdr/FDEA202103040556), Mar 4, 2021: ACTUATOR. INOPERATIVE. UPON GEAR RETRACTION ON THE AFTER TAKEOFF PHASE THE NOSE GEAR DID NOT RETRACT. WE HAD A --NOSE GEAR GREEN LIGHT-- WITH --DOORS AMBER LIGHT-- ACCOMPANNIED BY --A
- [SDR FDEA202102120340](https://openairdocs.org/sdr/FDEA202102120340), Feb 12, 2021: GUIDE VANE. DAMAGED. #1 ENGINE I/B GUIDE VANES COMPOSITE COVERINGS IS DAMAGED IN SEVERAL PLACES REPAIRED DAMAGE ON A-FRAMES IAW B757 AMM 72-34-10-6-4 AND RR EM 72-34-13-300-001
- [SDR FDEA202102110332](https://openairdocs.org/sdr/FDEA202102110332), Feb 11, 2021: SKIN. CORRODED. R/H WING #8 SLAT HAS CORROSION AT THE UPPER SURFACE AT BULLNOSE AREA APPROX 32.8" FROM I/B SIDE REPLACED SLAT PER B757 AMM 27-81-02-4
- [SDR FDEA202102110333](https://openairdocs.org/sdr/FDEA202102110333), Feb 11, 2021: COVER. CRACKED. L1 DOOR PRISM COVER CRACKED REMOVED AND REPLACED IAW B757 DWG 411N2044 REV A
- [SDR FDEA202102110331](https://openairdocs.org/sdr/FDEA202102110331), Feb 11, 2021: RING. CRACKED. L1 DOOR TRIM RING ASSY CRACKED REPAIRED L1 DOOR TRIM IAW B757-2 AMM 25-00-00-8 STEP 7,E, METHOD 2 AND BAC 5010 TYPE 70
- [SDR FDEA202102050294](https://openairdocs.org/sdr/FDEA202102050294), Feb 5, 2021: SUPPORT. CORRODED. #1 PYLON FIXED AFT FAIRING I/B FWD UPPER SUPPORT FOR PANEL 433MR IS FRETTED AT MATING SURFACE REMOVED AND FABRICATED NEW PLATE IAW B757-2 DWG 313N5033 REV AP, I
- [SDR FDEA202102030285](https://openairdocs.org/sdr/FDEA202102030285), Feb 3, 2021: STRUCTURE. CRACKED. MAIN CABIN R1 DOOR LOWER HINGE CUTOUT UPPER CORNER CRACKED TRIMMED OUT DAMAGED AREA PER BDWG 141N6200 SHEET 2 REVISION M AND B757 SRM 51-10- 02. HFEC ACCOMPLISH
- [SDR FDEA202102030283](https://openairdocs.org/sdr/FDEA202102030283), Feb 3, 2021: SKIN. CRACKED. #2 PYLON PANEL 443KL IS CRACKED. REPAIRED #2 PYLIN PNL 443KL CRACK IAW B757 SRM 54-50-70-2R FIG 201, 51-70-04-0G, B757AMM 51-24-02
- [SDR FDEA202012023017](https://openairdocs.org/sdr/FDEA202012023017), Dec 2, 2020: GUST LOCK. BROKEN. L1 ENTRY DOOR GUST LOCK COLLAR BROKEN. REMOVED BROKEN PIECES OF GUST LOCK AND HARDWARE FROM DOOR HINGE AREA. REMOVED AND REPLACED L1 DOOR HOLD OPEN LOCK COLLAR,
- [SDR FDEA2020091422189](https://openairdocs.org/sdr/FDEA2020091422189), Sep 12, 2020: LAMP. INOPERATIVE. LT FUSELAGE EMERGENCY ESCAPE LIGHT BY L1 DOOR INOP. RELAMPED, REF AMM 33-51-06-2-1. GOOD FOR SERVICE.
- [SDR FDEA201905171088](https://openairdocs.org/sdr/FDEA201905171088), May 17, 2019: COLLAR. BROKEN. UNABLE TO CLOSE LEFT ENTRY DOOR L1 DOOR GUSLOCK HOLD OPEN COLLAR BROKEN INSTALLED SERVICEABLE HOLD OPEN LOCK COLLAR ON L1 DOOR CPN 5217125 REF; AMM 52-11-08-8, 
- [SDR FDEA201902150425](https://openairdocs.org/sdr/FDEA201902150425), Feb 15, 2019: SHOULDER BELT. MALFUNCTIONED. FIRST OFFICER SHOULDER HARNESS WILL NOT RETRACT ALL THE WAY. TRY TO ENGAGE & DISENGAGE SHOULDER LOCK BUT NO HELP. REMOVED & REPLACED FIRST OFFICERS SEAT ASSY. R
- [SDR FDEA201901210187](https://openairdocs.org/sdr/FDEA201901210187), Jan 21, 2019: SKIN. CRACKED. LEFT O/B MAIN FLAP HAS A PUNCTURE IN COMPOSITE SKIN ON UPPER SURFACE INBD OF 2ND AFT FLAP TRACK. REPAIRED LEFT O/B MAIN FLAP PUNCTURE IN COMPOSITE SKIN ON UPPER
- [SDR FDEA201901210188](https://openairdocs.org/sdr/FDEA201901210188), Jan 21, 2019: STRUCTURE. PUNCTURED. LT WING INBD MAIN FLAP INTERNAL STRUCTURE HAS 4EA PUNCTURES IN THE HONEYCOMB, VIEW THRU OUTBD UPPER ACCESS PNL, INTERNAL INBD LOWER END AREA. REPAIRED LT WING I
- [SDR FDEA201901190173](https://openairdocs.org/sdr/FDEA201901190173), Jan 19, 2019: STRINGER. CORRODED. WHILE REMOVING A DOMENUT AT BS1340 STR23L FOUND STRINGER TO BE CORRODED. EVALUATED STRINGER AT BS 1340 STR 23L FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE AREA IA
- [SDR FDEA201901150136](https://openairdocs.org/sdr/FDEA201901150136), Jan 15, 2019: STRINGER. CRACKED. CABIN BS 1440 STR 4LT. UPPER EDGE IS CRACKED PERFORMED STRINGER REPAIR AT STR 4L FROM BS 1424 TO BS 1456 IAW SRM 53-00-03 03-2R FIG 201 DETAIL II REPAIR 2. DAMA
- [SDR FDEA201901100083](https://openairdocs.org/sdr/FDEA201901100083), Jan 10, 2019: FLOORBEAM. CRACKED. CRACK FORWARD CARGO CEILING LBL 45 STA 580 MAIN CABIN FLOORBEAM "T" CAP ON THE RADIUS. DOT 88-001 REMOVED DAMAGED SECTION OF THE LT BS580 LBL45 "T" CORD. FABRIC
- [SDR FDEA201810162904](https://openairdocs.org/sdr/FDEA201810162904), Oct 16, 2018: LIGHT. INOPERATIVE. EMER LIGHTS "UNARMED" LIGHT DOES NOT ILLUMINATE WHEN SWITCH IS OFF. REMOVED AND REPLACED UNARMED LIGHT BASE ASSY MANUFACTURER PN 434-1031-2001 CPN 3312041 REF A
- [SDR FDEA201802130379](https://openairdocs.org/sdr/FDEA201802130379), Feb 13, 2018: COLLAR. CRACKED. L1 DOOR HOLD-OPEN LOCK COLLAR CRACKED. REMOVED AND REPLACED THE L1 DOOR HOLD OPEN LOCK COLLAR AND CATCH IAW AMM 52-11-08-08.
- [SDR FDEA201706201720](https://openairdocs.org/sdr/FDEA201706201720), Jun 20, 2017: COLLAR. BROKEN. L1 HOLD OPEN LOCK IS BROKEN. REPLACED HOLD OPEN COLLAR HALVES AND CATCH ASSEMBLY IAW AMM 52-11-08-8. OK FOR SERVICE.
- [SDR FDEA201703160941](https://openairdocs.org/sdr/FDEA201703160941), Mar 16, 2017: PRESSURE SWITCH. DEFECTIVE. DURING DESCENT HAD SPOILERS EICAS WITH ASSOCIATED SPOILERS LIGHT OVERHEAD FELT SLIGHT ROLL TO RIGHT. REMOVED AND REPLACED HYDRAULIC PRESSURE SW (S27) PER AMM 27
- [SDR FDEA201612064327](https://openairdocs.org/sdr/FDEA201612064327), Dec 6, 2016: GUST LOCK. MALFUNCTIONED. FOUND THAT L1 DOOR GUST LOCK DOES NOT ENGAGE WHEN DOOR IS PLACED IN FULL OPEN POSITION. R & R THE L1 DOOR HOLD OPEN LOCK COLLAR IAW MM 52-11-08-4. OK FOR SERVIC
- [SDR FDEA201606262148](https://openairdocs.org/sdr/FDEA201606262148), Jun 26, 2016: TRANSMISSION. FAILED. RECEIVED T/E FLAP DISAGREE ON ECIAS WITH FLAPS 20 DEGREES AND 156 KIAS, RAN QRH FOR T/E FLAP DISAGREE AND LANDED WITH FLAPS 20 DEGREES, GROUND PROXIMITY TO OVER
- [SDR FDEA201606252137](https://openairdocs.org/sdr/FDEA201606252137), Jun 25, 2016: TRANSMISSION. INOPERATIVE. RECEIVED T/E FLAP DISAGREE ON ECIAS WITH FLAPS 20 DEGREES AND 156 KIAS, RAN QRH FOR T/E FLAP DISAGREE AND LANDED WITH FLAPS 20 DEGREES, GROUND PROXIMITY TO OVER
- [SDR FDEA201510243351](https://openairdocs.org/sdr/FDEA201510243351), Oct 24, 2015: COLLAR. BROKEN. L1 DOOR HOLD OPEN COLLAR BROKEN. COLLAR REMOVED, REPLACED L1 DOOR HOLD OPEN LOCK COLLAR IAW AMM 52-11-08-8. OPERATIONS CHECKED GOOD.
- [SDR FDEA201507292427](https://openairdocs.org/sdr/FDEA201507292427), Jul 29, 2015: LOCK. INOPERATIVE. LEFT ENTRY DOOR FORCED FROM OPEN POSITION, OVERRIDING LATCH. HOLD OPEN LATCH INOPERATIVE. DOOR CLOSES NORMALLY. R & R L1 HOLD OPEN LOCK ASSEMBLY IAW MM 52-11-08
- [SDR FDEA201506111771](https://openairdocs.org/sdr/FDEA201506111771), Jun 11, 2015: WINDSHIELD. CRACKED. DURING DECENT BELOW 210 WINDSCREEN ARCED THEN CRACKED. REMOVED AND REPLACED THE R1 WINDSHEILD IAW AMM 56-11-01-4 STEPS 1 THRU 3 (12)(A). PERFORMED WINDOW HEAT O
- [SDR FDEA201504181258](https://openairdocs.org/sdr/FDEA201504181258), Apr 18, 2015: CABLE. UNSECURE. JUMPSEATER SAID R1 DOOR HAD LOUD SQUEAL AT ALTITUDE, FL 350. COMPLETED A GVI OF R1 DOOR ASSEMBLY, FOUND BRADED ROPE FROM SLIDE ASSEMBLY EXTENDING TOO FAR OUT FR
- [SDR FDEA201504131218](https://openairdocs.org/sdr/FDEA201504131218), Apr 13, 2015: LIGHT. INOPERATIVE. L1 DOOR SLIDE LIGHT INOPERATIVE. RELAMPED IAW MM 33-51-06-2-1. OPERATIONS CHECKED GOOD.
- [SDR FDEA201412204156](https://openairdocs.org/sdr/FDEA201412204156), Dec 20, 2014: COVER. LOOSE. RAFT & SLIDE COVER FOR L1 DOOR IS LOOSE ON LOWER RT SIDE, IT GETS PUSHED OUT WHILE CLOSING THE DOOR. SECURED DOOR SLIDE COVER IAW AMM 25-66-00-2. NO FURTHER DEF

All 118: https://openairdocs.org/aircraft/N943FD/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 757-2G5 aircraft: https://openairdocs.org/model/boeing-757-2g5/aircraft.md
- The Rolls-Royce RB-211 series engine: https://openairdocs.org/engine/rolls-royce-rb-211-series.md

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