# N971FD: 1995 Boeing 757-28A

- Status: Valid registration
- Airframe: [Boeing 757-28A](https://openairdocs.org/model/boeing-757-28a) (registry code 1384976, 249 seats)
- Engine: [Rolls-Royce RB-211 series](https://openairdocs.org/engine/rolls-royce-rb-211-series) (registry code 54555)
- Serial number: 26277
- Year built: 1995
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 27, 1995
- Certificate issued: April 26, 2012
- Expires: April 30, 2028
- Mode S code: AD87DD
- 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=971FD
- Page: https://openairdocs.org/aircraft/N971FD

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 757-28A)

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/N971FD/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 N971FD.

## FAA accident and incident reports

None matched to N971FD.

## Service difficulty reports (116, 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 FDEA202307181240](https://openairdocs.org/sdr/FDEA202307181240), Jul 18, 2023: LAMP. FAILED. MDIS 971 33-50 9241 18JUL23 BMI FACT U R1 DOOR EXTERIOR SLIDE LIGHT INOP FACT 18JUL23 15:12 BMI U AMM: 33-51-06-2-1 REMOVED AND REPLACED R1 DOOR EXT SLIDE LIGHT
- [SDR FDEA202302280353](https://openairdocs.org/sdr/FDEA202302280353), Feb 28, 2023: FITTING. CRACKED. WHILE PERFORMING OPEN HOLE HFEC INSP OF RH WING UPPER SKIN AND DRAG FITTING FOUND HOLE #3 TO HAVE A CRACK INDICATION AT APPROX O'CLOCK FACING FWD. REMVOED RH IB
- [SDR FDEA202302280352](https://openairdocs.org/sdr/FDEA202302280352), Feb 28, 2023: FITTING. CRACKED. WHILE ACCOMPLISHING OPEN HFEC OF LH WING UPPER SKIN AND AROUND DRAG FITTING FOUND HOLE #18 TO HAVE A CRACK INDICATION AT APPROX. 1 O'CLOCK FACING FWD. REMOVED L
- [SDR FDEA202302280351](https://openairdocs.org/sdr/FDEA202302280351), Feb 28, 2023: FITTING. CRACKED. WHILE PERFORMING OPEN HOLE HFEC INSP FO RH WING UPPER SKIN AND DRAG FITTING FOUND HOLE #5 TO HAVE CRACK INDICATIONS AT APPROX 7 O'CLOCK. REMOVED RH OB DRAG FITT
- [SDR FDEA202302280350](https://openairdocs.org/sdr/FDEA202302280350), Feb 28, 2023: FITTING. CRACKED. WHILE ACCOMPLISHING OPEN HOLE HFEC INSP OF LH WING UPPER SKIN AND DRAG FITTING FOUND HOLE #3 TO HAVE A CRACK INDICATION AT APPROX 3 O'CLOCK FACING FWD. REMOVED 
- [SDR FDEA202211162798](https://openairdocs.org/sdr/FDEA202211162798), Nov 16, 2022: ACTUATOR. FAILED. SELECTED FLAPS 1 AT 5500 FEET AND ABOUT 200 KNOTS. RECEIVED LE SLAT DISAGREE EICAS MESSAGE. COMPLIED WITH QRH. MESSAGE REMAINED. QRH DIRECTED US TO RUN LE SLAT 
- [SDR FDEA202208121974](https://openairdocs.org/sdr/FDEA202208121974), Aug 12, 2022: IDG. FAILED. DURING CLIMB OUT AT 600 FEET L GEN OFF ILLUMINATED. RAN QRH AND ABLE TO RESET L GEN. STARTED APU FOR BACKUP AND APU RAN FOR ABOUT 5 MINUTES AND GOT AN APU FAULT
- [SDR FDEA202104271051](https://openairdocs.org/sdr/FDEA202104271051), Apr 27, 2021: FSEU. FAILED. ON ILS 11 KPWM GOT LE SLAT DISAG AUDIBLE WARNING, BUT NO EICAS MESSAGE DISPLAYED. WHEN FLAPS POSITIONED TO FLAPS 15 THEN RECEIVED EICAS MESSAGE LE SLAT DISAG. N
- [SDR FDEA202102120344](https://openairdocs.org/sdr/FDEA202102120344), Feb 12, 2021: SENSOR. BINDING. R1 DOOR LEVER PHYSICALLY MOVED ABOVE THE PANEL THAT COMES OUT WHEN THE DOOR IS CLOSED, UPON LANDING BLOCK IN MESSAGE/SUMMARY CAME UP BEFORE LEAVING THE RUNWAY. 
- [SDR FDEA202101170142](https://openairdocs.org/sdr/FDEA202101170142), Jan 17, 2021: FLOOR PANEL. DELAMINATED. MAIN CABIN FWD WET AREA FLOOR PANEL 222BF DELAMINATED. FABRICATED MAIN CABIN FWD WET AREA FLOOR PANEL 222BF, IAW B757 AMM 53-01-01-7 AND FEDEX DWG SRZ-25-005.
- [SDR FDEA202101110051](https://openairdocs.org/sdr/FDEA202101110051), Jan 11, 2021: PANEL. CRACKED. RT WING NR 10 SLAT LOWER COVE PANEL HAS EVIDENCE OF CRACK ON OUTBOARD SIDE OF OUTBOARD MAIN TRACK. REPAIRED RT WING NR 10 SLAT LOWER COVE PANEL ON OUTBOARD SIDE
- [SDR FDEA202101110050](https://openairdocs.org/sdr/FDEA202101110050), Jan 11, 2021: PANEL. CRACKED. RT WING NR 10 SLAT LOWER COVE PANEL HAS EVIDENCE OF CRACK ON INBOARD SIDE OF OUTBOARD MAIN TRACK. REPAIRED RT WING NR 10 SLAT LOWER COVE PANEL ON INBOARD SIDE O
- [SDR FDEA202101030002](https://openairdocs.org/sdr/FDEA202101030002), Jan 3, 2021: FLOOR SUPPORT. CORRODED. MAIN CARGO FLOOR SUPPORT CHANNEL HAS CORROSION AT RBL-58 BETWEEN STA 324 AND STA 345. REMOVED CORROSION ON SUPPORT CHANNEL STA 324 AND STA 345 RBL 58, IAW B757 
- [SDR FDEA202101030006](https://openairdocs.org/sdr/FDEA202101030006), Jan 3, 2021: WEB. CORRODED. MAIN CABIN FLOOR SUPPORT WEB HAS MULTIPLE AREAS OF CORROSION AT LBL 58 BETWEEN STA 1635 AND STA 1681. REMOVED CORR ON WEB LBL 58 STA 1635-1681, IAW B757 SRM 51-
- [SDR FDEA202101030004](https://openairdocs.org/sdr/FDEA202101030004), Jan 3, 2021: CREASE BEAM. CORRODED. MAIN CABIN FLOOR CREASE BEAM STA 876 RT SIDE CORRODED. REMOVED CORROSION ON CREASE BEAM STA 876 RT SIDE, IAW B757 SRM 51-10-02. ORIG MAT .071 REM .046 LOSS .025
- [SDR FDEA202012293217](https://openairdocs.org/sdr/FDEA202012293217), Dec 29, 2020: PANEL. CRACKED. MAIN CARGO DOOR FWD PRESSURE DOOR INTERNAL DAMAGED (CRACK) AT THE WEB. REMOVED, FABRICATED AND INSTALLED NEW FWD PANEL (WEB) ON MAIN CARGO DOOR, IAW B757 SRM 51
- [SDR FDEA202012293218](https://openairdocs.org/sdr/FDEA202012293218), Dec 29, 2020: PANEL. DENTED. MAIN CARGO DOOR AFT PRESSURE DOOR INTERNAL PROTRUDING DENTS AT THE WEB. REMOVED, FABRICATED, AND INSTALLED NEW AFT PANEL (WEB) ON MAIN CARGO, IAW B757 SRM 51-40
- [SDR FDEA202012213193](https://openairdocs.org/sdr/FDEA202012213193), Dec 21, 2020: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK FLANGE HAS COORSION @ RBL-57 BETWEEN STA. 1180 AND STA. 1300 REMOVED CORR ON SEAT TRACK STA 1180-1300 RBL58 IAW B757 SRM 51-10-02 ORIG MAT
- [SDR FDEA202003270609](https://openairdocs.org/sdr/FDEA202003270609), Mar 27, 2020: WARNING SYSTEM. FALSE ACTIVATION. PDIS 971 27-30 6467 ON CLIMB IN CLEAR CONFIGURATION RECIVED EICAS MSG RUDDER RATIO AND MACH / SDD TRIM (AND OVERHEAD LT) ALONG WITH ELEV ASYM ON STATUS PAGE, NO
- [SDR FDEA2019102422726](https://openairdocs.org/sdr/FDEA2019102422726), Oct 22, 2019: COVER. UNSECURE. NOTICED LEFT FORWARD ENTRYDOOR WAS BINDING. HAD MAINTENANCE OPEN DOOR FROM THE OUTSIDE. KMEM WHILE PERFORMING INSPECTION CHECK IN REF. TO AMM 52-11-01-6. FOUND 
- [SDR FDEA201909122213](https://openairdocs.org/sdr/FDEA201909122213), Sep 12, 2019: PROBE. OBSTRUCTED. PDIS 971 77-00 6015 12SEP19 RIC OPEN U LOGPAGES:3180701 CONTINUED FROM LOG PAGE 2966550, CONTINUED OPERATION OF RT ENG AT IDLE TO LANDING. FIRST INDICATION OF P
- [SDR FDEA2019081541866](https://openairdocs.org/sdr/FDEA2019081541866), Aug 14, 2019: WARNING MESSAGE. FALSE ACTIVATION. ON TAKEOFF ROLL,WHEN ENGINES WERE SET TO TAKEOFF THRUST AND ABOUT 30 KNOT AIRSPEED RECEIVED A SPOILER EICAS WITH CORRESPONDING MASTER WARNING LIGHTS AND TONE. R
- [SDR FDEA201802220469](https://openairdocs.org/sdr/FDEA201802220469), Feb 22, 2018: SWITCH. FAILED. DURING FINAL APPROACH, RECEIVED A LEADING EDGE SLAT ASSYMETRY EICAS AND ASSOCIATED CUE LIGHT. RAN QRH PROCEDURES, FLAPS 20 LANDING. LANDING NORMAL. R & R THE RT
- [SDR FDEA201711243302](https://openairdocs.org/sdr/FDEA201711243302), Nov 24, 2017: SEAT TRACK. DAMAGED. FOUND A BROKEN LOCK AT POS 3 MAIN DECK CENTER LINE. LOCK D611. FOUND DAMGED SEAT TRACK AT SAME LOCATION. COMPLIED WITH EA F-5320-T0336761 PART 1. REPAIRED THE S
- [SDR FDEA201709062464](https://openairdocs.org/sdr/FDEA201709062464), Sep 6, 2017: TRANSMITTER. OUT OF ADJUST. RECEIVED EICAS MSG "TE FLAP ASYM" RAN QRH LANDED WITH MAX AUTO BRAKES LANDING WEIGHT 167.0LB. R&R LT TE FLAP POSITION XMITTER PER MM 27-58-03-4 AND PERFORM ADJ/
- [SDR FDEA201703280999](https://openairdocs.org/sdr/FDEA201703280999), Mar 28, 2017: GIRT BAR. INOPERATIVE. R1 DOOR SLIDE ARM LIGHT WOULD NOT ARM. REMOVED AND REPLACED R1 GIRT BAR IAW MM 25-66-10-2. SLIDE ARM LIGHT OPS CHECKED GOOD. OPS CHECKED GOOD. ACFT OK FOR SERVI
- [SDR FDEA201609143219](https://openairdocs.org/sdr/FDEA201609143219), Sep 14, 2016: INDICATOR. READS LOW. PRESSURE REGULATOR GAUGE ON R1 DOOR SHOWS RED. R & R THE R1 DOOR SLIDE IAW MM 25-66-01-4.
- [SDR FDEA201509303007](https://openairdocs.org/sdr/FDEA201509303007), Sep 30, 2015: VALVE. LEAKING. LEFT HYD SYS LEAK & LOW FLUID FAILURE. SEVERAL ASSOCIATED EICAS & STATUS MSGS. LT HYD QTY WENT TO .12, FOLLOWED BY A LT QTY LOW EICAS MSG, LT RESERVOIR PSI LIGH
- [SDR FDEA201509303006](https://openairdocs.org/sdr/FDEA201509303006), Sep 30, 2015: BYPASS VALVE. LEAKING. LEFT HYD SYS LEAK & LOW FLUID FAILURE. SEVERAL ASSOCIATED EICAS & STATUS MESSAGES. LT HYD QTY WENT TO .12, FOLLOWED BY A LT QTY LOW EICAS MESSAGE, LT RESERVOIR 
- [SDR FDEA201508232690](https://openairdocs.org/sdr/FDEA201508232690), Aug 23, 2015: LIGHT. INOPERATIVE. R1 DOOR EXTERNAL EMER LIGHT INOPERATIVE. RELAMPED R1 SLIDE LIGHT & CHECKED OK IAW AMM 33-51-06-2-1.
- [SDR FDEA201507022139](https://openairdocs.org/sdr/FDEA201507022139), Jul 2, 2015: LATCH. LOOSE. ESCAPE ROPE COVER ON CAPTAINS SIDE DOES NOT STAY LATCHED. BOTTOM LATCH LOOSE. SECURED BOTTOM LATCH ON CAPTAINS SIDE ESCAPE ROPE COVER & CLOSED PANEL.
- [SDR FDEA201412094087](https://openairdocs.org/sdr/FDEA201412094087), Dec 9, 2014: PANEL. CRACKED. MAIN DECK CARGO DOOR AFT PRESS RELIEF DOOR COVE PANEL IS CRACKED.
- [SDR FDEA201412084080](https://openairdocs.org/sdr/FDEA201412084080), Dec 8, 2014: SHEAR WEB. CORRODED. MAIN DECK SHEAR WEB HAS CORROSION AT RBL 25 BS 420. REMOVED CORROSION, FABRICATED, LOCATED, DRILLED & INSTALLED THE DOUBLER IAW SRM 51-40-02 & SRM 5 4 3.
- [SDR FDEA201412084079](https://openairdocs.org/sdr/FDEA201412084079), Dec 8, 2014: SHEAR WEB. CORRODED. MAIN DECK SHEAR WEB HAS CORROSION AT LBL 25 BS 420. REMOVED CORROSION, FABRICATED DOUBLER, LOCATED, DRILLED & INSTALLED THE DOUBLERIAW SRM 51-40-02 & SRM 5 4 3.
- [SDR FDEA201412044060](https://openairdocs.org/sdr/FDEA201412044060), Dec 4, 2014: SKIN. CRACKED. MAIN CARGO DOOR INNER SKIN CRACKED. FABRICATED & INSTALLED NEW ACCESS PANEL ON MAIN CARGO DOOR INNER SKIN BS 500 - 520 IAW SRM 51-40-02 & DWG 65-49309 REV D.
- [SDR FDEA201404100710](https://openairdocs.org/sdr/FDEA201404100710), Apr 10, 2014: FIRE WARNING. FALSE INDICATION. MOMENTARY WW FIRE EICAS ALERT & BELL ON TOUCHDOWN, LASTED 1 - 2 SECONDS, COULD NOT DUPLICATE. INSPECTED DETECTOR LOOPS & ELEC CONNECTIONS IN BOTH MLG WW, NO DEF
- [SDR FDEA201402040254](https://openairdocs.org/sdr/FDEA201402040254), Feb 4, 2014: TARGET. OUT OF ADJUST. ON TAKEOFF ROLL THE RT REVERSER ECAS MESSAGE CAME INTERMITTENT REJECT AT 80 KTS. REVERSER SECURED IN FWD THRUST POSITION. FOUND THE RIGHT LOCK PROX TARGET, TOO 
- [SDR FDEA201308292072](https://openairdocs.org/sdr/FDEA201308292072), Aug 29, 2013: GUARD. FAILED. THE OVERHEAD EMERGENCY LIGHT SWITCH GUARD SPRING IS WEAK AND NOT WORKING PROPERLY, MANUAL OPERATION OF THE SWITCH IS NOT EFFECTED. REMOVED BROKEN EMERGENCY LIGH
- [SDR FDEA201308021754](https://openairdocs.org/sdr/FDEA201308021754), Aug 2, 2013: CABLE. SHEARED. DURING OPENING OF RT SIDE ENTRY DOOR, GIRT BAR HUNG UP ON DOOR SILL, SLIDE PARTIALLY DISENGAGED AS WELL AS SAFETY CABLE SHEARED. R & R R1 DOOR SLIDE ASSY REF AM
- [SDR FDEA201305301140](https://openairdocs.org/sdr/FDEA201305301140), May 30, 2013: LATCH. BROKEN. DOOR ESCAPE SLIDE COVER LOWER STRAP LATCH BROKEN. REPLACED LATCH IAW AMM 25-66-01-4. ACFT OK FOR SERVICE.
- [SDR FDEA201304180801](https://openairdocs.org/sdr/FDEA201304180801), Apr 18, 2013: SLIDER. DISCONNECTED. RT FWD ENTRY DOOR SLIDE LIGHT DOES NOT ILLUMINATE WHEN DOOR ARMED. INSPECTED AND FOUND R1 DOOR GIRT BAR SLIDERS NOT ATTACHED TO DOOR MECHANISM. REINSTALLED GIRT
- [SDR FDEA201303040496](https://openairdocs.org/sdr/FDEA201303040496), Mar 4, 2013: LAMP. INOPERATIVE. EMERGENCY EXTERIOR LIGHT AFT OF R1 DOOR INOPERATIVE. REPLACED LAMP IAW SMP'S. OPS CHECKED GOOD.
- [SDR FDEA201301180134](https://openairdocs.org/sdr/FDEA201301180134), Jan 18, 2013: SKIN. CORRODED. FUSELAGE SKIN BS 1200 -1220 BETWEEN STRINGER 29 LT AND 29 RT. THERE IS CORROSION AROUND THE TOILET SERVICING HOLES IN THE SKIN. REPAIR CARRIED OUT AS PER EA F-3
- [SDR FDEA201301180133](https://openairdocs.org/sdr/FDEA201301180133), Jan 18, 2013: SKIN. CORRODED. AFT CARGO LOWER COMPARTMENT INTERIOR SKIN BETWEEN BS 1200 AND 1205 NEAR LBL 2. CUT OUT AREA WITH CORROSION. REPAIR CARRIED OUT IAW EA F-3830-163852. REPAIR CLAS
- [SDR FDEA201301180136](https://openairdocs.org/sdr/FDEA201301180136), Jan 18, 2013: CHANNEL. DAMAGED. MAIN DECK -DURING OK TO INSTALL, FOUND SPLICE CHANNEL WITH ELONGATED HOLE AT STR 1, BS 1620. REMOVED CHANNEL IAW SRM 51-40-02 REV 107. NEW CHANNEL FABRICATED IA
- [SDR FDEA201301130090](https://openairdocs.org/sdr/FDEA201301130090), Jan 13, 2013: STIFFENER. SHEARED. AFT CARGO COMPARTMENT RT SIDE LOWER FLOORBEAM STIFFENER STRAP IS BROKEN, BS 1640, RBL 45. COMPLIED PART 1 OF EA F-5330-163846. REPAIR CLASSIFIED MAJOR IAW GMM 6
- [SDR FDEA201301110067](https://openairdocs.org/sdr/FDEA201301110067), Jan 11, 2013: FLOORBEAM. CORRODED. BS 1320, FLOORBEAM UPPER TEE HAS CORROSION, LBL 56 TO LBL 64. COMPLIED WITH EA F-5310-163824, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201212244372](https://openairdocs.org/sdr/FDEA201212244372), Dec 24, 2012: SKIN. DENTED. FUSELAGE SKIN DENTED AT BS 1620, BELOW STR 24R. REPAIR CARRIED OUT IAW EA F-5330-163828. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201212144300](https://openairdocs.org/sdr/FDEA201212144300), Dec 14, 2012: CREASE BEAM. CORRODED. BS 1259, RBL 64 CREASE BEAM HAS CORROSION. CORROSION REMOVED IAW SRM 51-10-02, REV 107. FOUND EXCEED 10 PERCENT LIMIT IAW SRM 53-30-13, ALLOWABLE DAMAGE 1, FIG 
- [SDR FDEA201212124285](https://openairdocs.org/sdr/FDEA201212124285), Dec 12, 2012: SEAT TRACK. CORRODED. SEAT TRACK AT BS 1050 TO 1075, RBL 24 HAS DEEP DRILL MARK WITH CORROSION ON CHANNEL. SEAT TRACK REPAIRED IAW SRM 53-00-52 FIG.201 REPAIR 4 REV.107. REPAIR MAJOR

All 116: https://openairdocs.org/aircraft/N971FD/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 757-28A aircraft: https://openairdocs.org/model/boeing-757-28a/aircraft.md
- The Rolls-Royce RB-211 series engine: https://openairdocs.org/engine/rolls-royce-rb-211-series.md

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