# N912FD: 1988 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: 24260
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 19, 1993
- Certificate issued: June 5, 2008
- Expires: July 31, 2027
- Mode S code: AC9E9A
- 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=912FD
- Page: https://openairdocs.org/aircraft/N912FD

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/N912FD/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 N912FD.

## FAA accident and incident reports

None matched to N912FD.

## Service difficulty reports (154, 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 FDEA202608141125](https://openairdocs.org/sdr/FDEA202608141125), Aug 14, 2026: SLAT SYSTEM. ASYMETRIC. LE SLAT ASYM. COMPLIED WITH THE QRH. EMERGENCY DECLARED. TROUBLSHOT THE LE SLAT SYSTEM AND FOUND A SINGLE TORQUE TUBE COUPLING DICONNECTED ON THE RT WING. POSIT
- [SDR FDEA202606190785](https://openairdocs.org/sdr/FDEA202606190785), Jun 19, 2026: COLLAR. DAMAGED. DURING RAMP TRAINING L1 DOOR GUST LOCK WOULD NOT RELEASE. AMM 52-11-08-8 INSTALLED SERVICEABLE SPLIT COLLAR IN REF TO AMM. CLEARED MEL.
- [SDR FDEA202606010661](https://openairdocs.org/sdr/FDEA202606010661), Jun 1, 2026: SKIN. CRACKED. RH WING SLAT # 9 LOWER SURFACE O/N MAIN TRACK BRACKET AREA WITH CRACK APPLIED PERMANENT REPAIR AT RH WING SLAT # 9 LOWER FLEXIBLE SKIN PANEL BTW OSS 675 TO OSS 
- [SDR FDEA202605290653](https://openairdocs.org/sdr/FDEA202605290653), May 29, 2026: SKIN. DENTED. SEC 48 UPPER FUSELAGE BETWEEN BS 1941 AND BS 1963 WITH 03 DENTS APPLIED PERMANENT REPAIR AT SEC 48 UPPER FUSELAGE BTW STA 1941 TO 1963 IAW B757 SRM 51-70-10-2R 
- [SDR FDEA202605290652](https://openairdocs.org/sdr/FDEA202605290652), May 29, 2026: SKIN. DELAMINATED. APU COMPARTMENT INTERNAL SKIN AT BS 1900 DELAMINATED APPLIED PERMANENT AT APU COMPARTMENT INTERNAL SKIN IAW B757 SRM 51-70-10-2R AND PERFORMED TAP TEST AFTER RE
- [SDR FDEA202605290651](https://openairdocs.org/sdr/FDEA202605290651), May 29, 2026: SKIN. DENTED. SEC 48 UPPER FUSELAGE BETWEEN BS 1896 AND BS 1918 HAS A CUSTER OF 04 DENTS (TWO ARE LOCATED AROUND THE AREA, AND TWO ARE LOCATED OVER A PREVIOUS REPAIR) APPLIED
- [SDR FDEA202605270639](https://openairdocs.org/sdr/FDEA202605270639), May 27, 2026: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK BETWEEN BS 660.0 TO 885.0 RBL 58.22 WITH CORROSION EVALUATED SEAT TRACK FOUND DATA NOT ALLOWED DAMAGE OUT OF LIMITS IAW SRM 53- 00-52-1A F
- [SDR FDEA202605230629](https://openairdocs.org/sdr/FDEA202605230629), May 23, 2026: SKIN. CORRODED. PYLON NR 1 AROUND THE CUT OUT FOR ACCESS PANEL 433JR INTERNAL SKIN SHOWS CORROSION. REMOVED AND REPLACED INBD PYLON SKIN PANEL IAW B DWG 012N8774 REV A AND SRM 
- [SDR FDEA202605230628](https://openairdocs.org/sdr/FDEA202605230628), May 23, 2026: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK BETWEEN BS 660 TO 885 RBL 58.22 WITH CORROSION.
- [SDR FDEA202605210626](https://openairdocs.org/sdr/FDEA202605210626), May 21, 2026: SKIN. DELAMINATED. L/H WING INB MAIN FLAP TRAILING EDGE PREVIOUS REPAIR IS DEBONDED REMOVED PREVIOUS REPAIR LOWER SKIN FOUND DEBONDED AND INSTALLED PERMANENT REPAIR AT LH WING I/B
- [SDR FDEA202604090419](https://openairdocs.org/sdr/FDEA202604090419), Apr 9, 2026: LAMP. FAILED. R1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. AMM: 33-51-06-2 RELAMPED R1 DOOR EXTERIOR SLIDE LIGHT IAW ABOVE REF. OPS CHK SERVICEABLE.
- [SDR FDEA202603060325](https://openairdocs.org/sdr/FDEA202603060325), Mar 6, 2026: BATTERY PACK. FAULTED. RIGHT ENTRY SLIDE LIGHT REMAINS ON AFTER DISARMING. REPLACED BATTERY AT M730. REMOVED SOURCE MANUFACTURING BATTERY ASSEMBLY MPN 2013-1ASMI S/N 3341. TEST GOOD.
- [SDR FDEA202603030306](https://openairdocs.org/sdr/FDEA202603030306), Mar 3, 2026: LIGHT. INOPERATIVE. WHEN ARMING THE SLIDES FOR DEPARTURE, RT SLIDE LIGHT DID NOT ILLUMINATE. RELEASED FOR SERVICE IAW MEL 25-66-04-B, CATEGORY C. VERIFIED SLIDE ARMED LT DOES NOT I
- [SDR FDEA202601160063](https://openairdocs.org/sdr/FDEA202601160063), Jan 16, 2026: BATTERY PACK. FAILED. COURIER AREA CENTER OVERHEAD EMERGENCY EXIT LIGHT, R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT AND EXTERIOR R1 SLIDE LIGHT INOP. AMM: 33-51-07-2 REMOVED AND REPLACED 
- [SDR FDEA202511122167](https://openairdocs.org/sdr/FDEA202511122167), Nov 12, 2025: CIRCUIT BREAKER. FAULTED. R1 DOOR INTERIOR EMERGENCY EXIT LIGHT WILL NOT TEST. TROUBLESHOT RT EMERGENCY EXIT SIGN FAULT IAW WDM 33-51-12. RESET EMERGENCY LIGHT CIRCUIT BREAKER IAW MM 20-
- [SDR FDEA202511112156](https://openairdocs.org/sdr/FDEA202511112156), Nov 11, 2025: LIGHT. NO TEST. R1 DOOR INTERIOR EMERGENCY EXIT LIGHT WILL NOT TEST. TROUBLESHOT RT EMERGENCY EXIT SIGN FAULT IAW WDM 33-51-12. RESET EMERGENCY LIGHT CIRCUIT BREAKER IAW MM 20-
- [SDR FDEA202506281073](https://openairdocs.org/sdr/FDEA202506281073), Jun 28, 2025: GUST LOCK. STUCK. LEFT MAIN AIRCRAFT DOOR GUST LOCK STUCK. CANNOT CLOSE THE DOOR. REPLACED L1 DOOR HOLD OPEN LOCK PER ABOVE REF. OPS CHECKS GOOD.
- [SDR FDEA202503070338](https://openairdocs.org/sdr/FDEA202503070338), Mar 7, 2025: WARNING MESSAGE. ILLUMINATED. PRIOR TO DESCENT, L AFT FUEL PUMP EICAS MESSAGE AND PRESS LIGHT IN L AFT PUMP SWITCH. COMPLIED WITH QRH PROCEDURE. WHILE DEBRIEFING CREW, FOUND "L AFT FUEL BOOS
- [SDR FDEA202412141804](https://openairdocs.org/sdr/FDEA202412141804), Dec 14, 2024: GUST LOCK. BROKEN. L1 DOOR GUST LOCK IS BROKE. STUCK IN THE UP POSITION. REPLACED L1 DOOR HOLD-OPEN LOCK COLLAR
- [SDR FDEA202407201038](https://openairdocs.org/sdr/FDEA202407201038), Jul 20, 2024: MODULE. INOPERATIVE. CLIMBING THROUGH FL200; EICAS R HYD QTY MSG FOLLOWED BY R HYD SYS PRESS MSG. COMPLETED QRH. AMM 29-18-04-4 FOUND BLOWN O-RING IN RT IN/BO ENG PYLON ON HYD FILTE
- [SDR FDEA202406040768](https://openairdocs.org/sdr/FDEA202406040768), Jun 4, 2024: WIRE. DISCONNECTED. NLG EMERGENCY LIGHT SWITCH INOP. REPLACED ONE TERMINAL ON WIRE W2052-0013-18 IAW WDM 33-51-11 SHEET 1 AND SWPM 20-30- 11, OP. TEST SATISFACTORY IAW AMM 33-51-00
- [SDR FDEA202405260729](https://openairdocs.org/sdr/FDEA202405260729), May 26, 2024: SEAT TRACK. CORRODED. DOT #106-10; MAIN CABIN BETWEEN STA. 1620 & STA. 1640, LBL 45.5 SEAT TRACK HAS CORROSION. CUT OUT SECTION SEAT TRACK, INSTALLED SEAT TRACK REPAIR SPLICE P/N BAC
- [SDR FDEA202405260728](https://openairdocs.org/sdr/FDEA202405260728), May 26, 2024: SEAT TRACK. CORRODED. MAIN CABIN STA. 1320, LBL 24.75 SEAT TRACK HAS CORROSION. REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN STA 1320 TO STA 1350 LBL 24.75 PER SRM 53-00-52-2R FIG
- [SDR FDEA202405200708](https://openairdocs.org/sdr/FDEA202405200708), May 20, 2024: FLOORBOARD. DAMAGED. MAIN DECK CARGO COMPT FLOORBOARD PANEL 252MVF IS DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 252MVF ON VTMAE TRAVELER #T24/1752843 IAW DWG SRZ-25-005 REVISION
- [SDR FDEA202405200707](https://openairdocs.org/sdr/FDEA202405200707), May 20, 2024: FLOORBOARD. DAMAGED. MAIN DECK CARGO COMPT FLOORBOARD PANEL 232MEF DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 232MEF ON VTMAE TRAVELER #T24/1752792 IAW DWG SRZ-25-005 REVISION R 
- [SDR FDEA202405200706](https://openairdocs.org/sdr/FDEA202405200706), May 20, 2024: FLOORBOARD. DAMAGED. MAIN DECK CARGO COMPT FLOORBOARD PANELS 252MUF IS DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 252MUF ON VTMAE TRAVELER #T24/1752842 IAW DWG SRZ-25-005 REVISIO
- [SDR FDEA202405200705](https://openairdocs.org/sdr/FDEA202405200705), May 20, 2024: FLOORBOARD. DAMAGED. MAIN DECK CARGO COMPT FLOORBOARD PANELS 251MWF IS DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 251MWF ON VTMAE TRAVELER #T24/1752837 IAW DWG SRZ-25-005 REVISIO
- [SDR FDEA202405200704](https://openairdocs.org/sdr/FDEA202405200704), May 20, 2024: FLOORBOARD. DAMAGED. MAIN DECK CARGO COMPT FLOORBOARD PANELS 252MRF IS DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 252MRF ON VTMAE TRAVELER #T24/1752840 IAW DWG SRZ-25-005 REVISIO
- [SDR FDEA202405200703](https://openairdocs.org/sdr/FDEA202405200703), May 20, 2024: FLOORBOARD. DAMAGED. MAIN DECK CARGO COMPT FLOORBOARD PANEL 232 MYF IS DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 232 MYF ON VTMAE TRAVELER #T24/1752806 IAW DWG SRZ-25-005 REVISI
- [SDR FDEA202405200702](https://openairdocs.org/sdr/FDEA202405200702), May 20, 2024: FLOORBOARD. DAMAGED. MAIN CABIN CARGO COMPT FLOORBOARD PANEL 241MNF IS DAMAGED. FABRICATED ZONE 240 FLOORBOARD PANEL 241MNF ON VTMAE TRAVELER #T24/1752825 IAW DWG SRZ-25-005 REVISIO
- [SDR FDEA202405200701](https://openairdocs.org/sdr/FDEA202405200701), May 20, 2024: FLOORBOARD. DAMAGED. MAIN DECK CARGO COMPT FLOORBOARD PANEL 241MRF IS DAMAGED. FABRICATED ZONE 240 FLOORBOARD PANEL 241MRF ON VTMAE TRAVELER #T24/1752834 IAW DWG SRZ-25-005 REVISION
- [SDR FDEA202405200700](https://openairdocs.org/sdr/FDEA202405200700), May 20, 2024: FLOORBOARD. DAMAGED. MAIN DECK CARGO COMPT FLOORBOARD PANEL 232MJF IS DAMAGED. FABRICATED ZONE 230 FLOORBOARD 232MJF ON VTMAE TRAVELER #T24/1752794 IAW DWG SRZ- 25-005 REVISION R MA
- [SDR FDEA202405200699](https://openairdocs.org/sdr/FDEA202405200699), May 20, 2024: FLOORBOARD. DAMAGED. MAIN CABIN CARGO COMPT FLOORBOARD PANEL 231 MYF IS DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 231 MYF ON VTMAE TRAVELER #T24/1752802 IAW DWG SRZ25-005 REVISI
- [SDR FDEA202405200698](https://openairdocs.org/sdr/FDEA202405200698), May 20, 2024: FLOORBOARD. DAMAGED. MAIN DECK CARGO CMPT FLOORBOARD 231 MRF IS DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 231 MRF ON VTMAE TRAVELER #T24/1752801 IAW DWG SRZ25-005 REVISION R, MA
- [SDR FDEA202405200697](https://openairdocs.org/sdr/FDEA202405200697), May 20, 2024: FLOORBOARD. DAMAGED. FLOORBOARD PANEL 222MEF DAMAGED FABRICATED ZONE 220 FLOORBOARD PANEL 222MEF ON VTMAE TRAVELER #T24/1753851 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR
- [SDR FDEA202405180685](https://openairdocs.org/sdr/FDEA202405180685), May 18, 2024: CREASE BEAM. CORRODED. MAIN DECK CREASE BEAM CORRODED BETWEEN STA 860-880 LH. REMOVED AND REPLACED CREASE BEAM BETWEEN STA 860-880 LH P/N BAC1515-553 (143N5540-9) BATCH 0002677936 IAW
- [SDR FDEA202405160679](https://openairdocs.org/sdr/FDEA202405160679), May 16, 2024: FLOORBOARD. DAMAGED. FLOORBOARD PANEL 222AF DAMAGED. FABRICATED ZONE 220 FLOORBOARD PANEL 222AF ON VTMAE TRAVELER # T24/1753759 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202405160678](https://openairdocs.org/sdr/FDEA202405160678), May 16, 2024: FLOORBOARD. DAMAGED. FLOORBOARD 221MAF IS DAMAGED. FABRICATED ZONE 220 FLOORBOARD PNL 221MAF ON VTMAE TRAVELER #24/1753757 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202405160677](https://openairdocs.org/sdr/FDEA202405160677), May 16, 2024: FLOORBOARD. DAMAGED. FLOORBOARD PANEL 221MBF IS DAMAGED. FABRICATED ZONE 220 FLOOR PANEL 221MBF ON VTMAE TRAVELER # T24/1753758 IAW DWG SRZ- 25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202405160676](https://openairdocs.org/sdr/FDEA202405160676), May 16, 2024: FLOORBOARD. DAMAGED. FLOORBOARD PANELS 221AF DAMAGED FABRICATED ZONE 220 FLOORBOARD PANEL 221AF ON VTMAE TRAVELER #T24/1753756 IAW DWG. SRZ-25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202405160675](https://openairdocs.org/sdr/FDEA202405160675), May 16, 2024: FLOORBOARD. DAMAGED. FLOORBOARD PANEL 222MAF IS DAMAGES FABRICATE ZONE 220 FLOORBOARD PANEL 222MAF ON VTMAE TRAVELER # T24/1753760 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAAIR.
- [SDR FDEA202405130659](https://openairdocs.org/sdr/FDEA202405130659), May 13, 2024: CREASE BEAM. CORRODED. RBL 63 STATION 860 TO 880 CREASE BEAM HAS AREAS OF CORROSION. CORROSION FOUND OUT OF LIMITS. REMOVED AND REPLACED CREASE BEAM P/N BAC 1515 553124 BATCH NUMBER 0
- [SDR FDEA202402160165](https://openairdocs.org/sdr/FDEA202402160165), Feb 16, 2024: DUCT. DAMAGED. DURING SVC WHILE DOING A LEAK INSPECTION ON APU AREA FOUND APU SURGE DUCT CASING BROKEN AND MISSING MATERIAL RELEASED FOR SERVICE PER MEL : 49-11-01. REMOVED AN
- [SDR FDEA202401240116](https://openairdocs.org/sdr/FDEA202401240116), Jan 24, 2024: LOCK. WORN. WHILE WORKING ON TSI 25-60/5212, FOUND RH DOOR ARMED LIGHT WORKING INTERMITTENTLY. RELEASED FOR SERVICE PER MEL : 25-66-05-A CATEGORY : C EXPIRATION : 03FEB24 "
- [SDR FDEA202401190090](https://openairdocs.org/sdr/FDEA202401190090), Jan 19, 2024: GIRT BAR. FOD. RIGHT ENTRY DOOR SLIDE LIGHT INOP. REPEAT GRIPE. REFER TO ATTACHED PICTURES: SLIDE ARMED THREE TIMES IN A ROW: SLIDE LIGHT COMES UP EVERY TIME. FOLLOWED FIM 25-
- [SDR FDEA202401170088](https://openairdocs.org/sdr/FDEA202401170088), Jan 17, 2024: LAMP. FAILED. SLIDE LIGHT ON RIGHT ENTRY DOOR BURNED OUT. AMM: 33-16-02-2 RELAMPED PER MM 33-16-02-2.OPS CHECK OK.
- [SDR FDEA202401040038](https://openairdocs.org/sdr/FDEA202401040038), Jan 4, 2024: GIRT BAR. DIRTY. RIGHT SIDE ENTRY DOOR SLIDE LIGHT NOT ILLUMINATING WHEN ARMED. AMM: 25-66-11-02. DEBRIS FOUND BETWEEN PROX SWITCH AND GIRT BAR SLIDER, AREA CLEANED, "SLIDE" LIG
- [SDR FDEA202210062563](https://openairdocs.org/sdr/FDEA202210062563), Oct 6, 2022: SKIN. TORN. DURING PUSH BACK FROM HANGAR L/H VERTICAL STABILIZER SKIN BETWEEN FIN STA 375-400 AND BETWEEN REAR SPAR AND STR-3 WAS DAMAGED WORK ACCOMPLISHED IN ACCORDANCE WI
- [SDR FDEA202209182554](https://openairdocs.org/sdr/FDEA202209182554), Sep 18, 2022: SKIN. NONE. FOUND CORROSION IN FASTENER HOLE #3 UPPER SKIN STRUT AREA L/H WING ACCOMPLISHED IAW FEDEX E.A #F-5730-T0370691 P1 MAJOR REPAIR
- [SDR FDEA202209162555](https://openairdocs.org/sdr/FDEA202209162555), Sep 16, 2022: SKIN. CRACKED. FOUND CRAKES CORROSION ,DAMGE IN HOLES #2,#4,#5,#7,#10,#12 AT UPPER SKIN R/H WING STRUT ATTACH AREA ACCOMPLISHED IAW FEDEX E.A # F-5730-T0370683 P1

All 154: https://openairdocs.org/aircraft/N912FD/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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