# N922FD: 1989 Boeing 757-23A

- Status: Valid registration
- Airframe: [Boeing 757-23A](https://openairdocs.org/model/boeing-757-23a) (registry code 1384967, 178 seats)
- Engine: [Rolls-Royce RB-211 series](https://openairdocs.org/engine/rolls-royce-rb-211-series) (registry code 54555)
- Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM) (The Boeing Company) (OpenAirDocs)
- Serial number: 24293
- Year built: 1989
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 21, 2009
- Certificate issued: August 6, 2008
- Expires: February 29, 2028
- Mode S code: ACC619
- 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=922FD
- Page: https://openairdocs.org/aircraft/N922FD

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 757-23A)

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/N922FD/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 N922FD.

## FAA accident and incident reports

None matched to N922FD.

## Service difficulty reports (195, 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 FDEA202407211036](https://openairdocs.org/sdr/FDEA202407211036), Jul 21, 2024: BATTERY PACK. NO TEST. ON SERVICE CHECK FOUND EMERGENCY EXIT AISLE SIGN NOT ILLUMINATING WHEN EMERGENCY LIGHTS TEST PERFORMED. AMM: 33-51-07-2-0, REMOVED AND REPLACED EMERGENCY LIGHT 
- [SDR FDEA202404010430](https://openairdocs.org/sdr/FDEA202404010430), Apr 1, 2024: SKIN. CORRODED. R / WING DRY BAY ACCESS PANEL 644AB WING NUT PLATES DAMAGED WITH POSSIBLE EXFOLIATION ON WING SKIN. COMPLIED WITH EA F-5730-T0378521 P1 WINGS-PLATE AND SKIN COR
- [SDR FDEA202403290410](https://openairdocs.org/sdr/FDEA202403290410), Mar 29, 2024: WEB. CORRODED. FWD CARGO COMPARTMENT F. STA BETWEEN 600-620 RBL 64.5 SHEAR WEB HAS CORROSION AFTER EVALUATED SHEAR WEB AT F.STA 600 TO 620 AND BTW RBL 62.89 - 64.5 FOUND OUT O
- [SDR FDEA202403290408](https://openairdocs.org/sdr/FDEA202403290408), Mar 29, 2024: FAIRING. GOUGED. SEC 48 F.ST 1862.2 S.14BL HAS TYPICAL GOUGE CAUSED BY STAB BLADE SEAL L/H CLEANED GOUGED AREA ON TWO DIFERENT PARTS AFFECTED ( PANEL FAIRING) IAW B-SOPM 20-30-0
- [SDR FDEA202403280399](https://openairdocs.org/sdr/FDEA202403280399), Mar 28, 2024: SEAT TRACK. CORRODED. MAIN CABIN FOUND CORROSION ON SEAT TRACK STA 1180-1200 RBL45.50 REMOVED CORROSION AT SEAT TRACK FLANGE BETWEEN STA. 1180-1200 RBL 45.50, EVALUATED AREA FOUND TO
- [SDR FDEA202403270388](https://openairdocs.org/sdr/FDEA202403270388), Mar 27, 2024: SEAT TRACK. CORRODED. SEAT TRACK HAS EVIDENCE OF CORROSION ALONG FLANGE UNDER CRACKED PAINT BETWEEN STA 1320-1420 RBL-44 REMOVED CORROSION AT SEAT TRACK I\B FLANGE BETWEEN STA 1320-1
- [SDR FDEA202403270387](https://openairdocs.org/sdr/FDEA202403270387), Mar 27, 2024: SEAT TRACK. CORRODED. MAIN CABIN FOUND CORROSION ON SEAT TRACK STA 1180-1200 RBL 24.75 REMOVED CORROSION AT SEAT TRAK BEWEEN STA 1180-1200 RBL 24.75 IAW B757 SRM 51-10-02- OG, EVALUA
- [SDR FDEA202403270386](https://openairdocs.org/sdr/FDEA202403270386), Mar 27, 2024: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK FLANGE BETWEEN STA 1100-1180 RBL-45.5 REMOVED CORROSION AT SEAT TRACK STA 1075-1180, RBL 455 IAW B757 SRM 51-10-02-0G, EVALUATED AREA FO
- [SDR FDEA202403270385](https://openairdocs.org/sdr/FDEA202403270385), Mar 27, 2024: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK FLANGE, BETWEEN STA 1100-1180 RBL-24.5 REMOVED CORROSION AFT FLANGE SEAT TRACK A STA 1075-1180 RBL 24.5 IAW B57 SRM 51-10-02- 0G , FOUND
- [SDR FDEA202403270384](https://openairdocs.org/sdr/FDEA202403270384), Mar 27, 2024: CREASE BEAM. CORRODED. MAIN DECK, RIGHT CREASE BEAM HAS CORROSION BETWEEN STA.1260-1280. REMOVED CORROSION CREASE BEAM AT STA 1260 TO 1280 IAW B757 SRM 51-10-02-0G, EVALUATED AREA FOU
- [SDR FDEA202403270383](https://openairdocs.org/sdr/FDEA202403270383), Mar 27, 2024: CREASE BEAM. CORRODED. LH AFT MAIN CABIN CREASE BEAM HAS POSSIBLE CORROSION BETWEEN BS 1420 THRU BS 1640 REMOVED CORROSION AT CREASE BEAM BETWEEN STA. 1520 - 1605 IAW B757 SRM 51-10-0
- [SDR FDEA202403260380](https://openairdocs.org/sdr/FDEA202403260380), Mar 26, 2024: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK FLANGE, BETWEEN STA 1320-1340, RBL-57 REMOVED CORROSION IAW B757 SRM 51-10-02-0G, NO LIMITS REPLACEMENT REQ. IAW B757 SRM 53-00-52-1A FI
- [SDR FDEA202403260375](https://openairdocs.org/sdr/FDEA202403260375), Mar 26, 2024: ANGLE. CORRODED. AFT CARGO COMPARATMENT ON STA 1440 S-27 R\H CLIP ANGLE CORRODED. REMOVED, EVALUATED FOUND OUT OF LIMTIS, FABRICATE, TREATED, PRIMED, TOP COAT AND INSTALLED AFT 
- [SDR FDEA202403250371](https://openairdocs.org/sdr/FDEA202403250371), Mar 25, 2024: BRACKET. CORRODED. AFT CARGO COMPARTMENT F.STA 1440 S.27 R BRAKET SUPPOR CORRODED REMOVED, INSPECTED FOUND OUT OF LIMIT, FABRICATED, TREATED, PRIMED TOP COATED AND INSTALLED AFT C
- [SDR FDEA202403250370](https://openairdocs.org/sdr/FDEA202403250370), Mar 25, 2024: CREASE BEAM. CORRODED. MAIN DECK RIGHT SIDE CREASE BEAM, HAS CORROSION BETWEEN STA 1580-1620. REMOVED CORROSION ON CREASE BEAM IAW B757 SRM 51-10-02-0G FOUND TO BE OUT OF LIMITS AT AR
- [SDR FDEA202403240359](https://openairdocs.org/sdr/FDEA202403240359), Mar 24, 2024: SEAT TRACK. WORN. MAIN CABIN, FOUND SEAT TRACK DAMAGED ON CROWN AREAS STA 1580 RBL 24.75. REWORKED DAMAGED AREAS AT SEAT TRACK CROWN AREA AT BETWEEN STA 1570-1590 RBL 24.5 IAW B7
- [SDR FDEA202403240358](https://openairdocs.org/sdr/FDEA202403240358), Mar 24, 2024: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK FLANGE BETWEEN STA 1320-1340, RBL-57.
- [SDR FDEA202403220350](https://openairdocs.org/sdr/FDEA202403220350), Mar 22, 2024: SEAT TRACK. CORRODED. AFT CARGO COMPARTMENT BETWEEN F. STA 1280-1300 RBL 45.50 SEAT TRACK HAVE CORROSION REMOVED CORROSION AT SEAT TRACK SECTION BETWEEN STA. 1280-1300 RBL 45.50 IAW 
- [SDR FDEA202403220349](https://openairdocs.org/sdr/FDEA202403220349), Mar 22, 2024: SEAT TRACK. CORRODED. MAIN DECK,SEAT TRACK HAS CORROSION AT FLANGE, STA 1537 RBL-57 REMOVED CORROSION AT SEAT TRACK I/B FLANGE IAW B757 SRM 51-10-02-0G, AREA NO LIMITS IAW B757 SRM 5
- [SDR FDEA202403220348](https://openairdocs.org/sdr/FDEA202403220348), Mar 22, 2024: SEAT TRACK. CORRODED. SEAT TRACK HAS CORROSION, ON LOWER SURFACE OF CLIPS NUTS HOLES, BETWEEN STA/ 1300 - 1320 , RBL24.5 REMOVED CORROSION AT SEAT TRACK SECTION BETWEEN STA/ 1300-132
- [SDR FDEA202403220347](https://openairdocs.org/sdr/FDEA202403220347), Mar 22, 2024: FLOOR SUPPORT. CORRODED. REWORK REQUIRED ON NR# N00383 FOR NOT PERFORMING REQUIRED HARDNESS TEST FOR FLOOR SUPPORT LOCATED AT STA 339 LBL 60. PERFORMED REQUIRE HARDNESS TEST ON FABRICAT
- [SDR FDEA202403210336](https://openairdocs.org/sdr/FDEA202403210336), Mar 21, 2024: DECK PLATE. GOUGED. MAIN CABIN AFT DECK PLATE FOUND GOUGE OUT OF LIMITS AT STA 1682 LBL 7. REPAIRED AREA OUT OF LIMITS ON DECK PLATE AT STA. 1682 LBL 7 IAW B-757 SRM 53-60-51-2R RE
- [SDR FDEA202403210335](https://openairdocs.org/sdr/FDEA202403210335), Mar 21, 2024: DECK PLATE. GOUGED. MAIN CABIN AFT DECK PLATE FOUND GOUGE OUT OF LIMITS AT STA 1711, LBL 7. REPAIRED AREA OUT OF LIMITS ON DECK PLATE AT STA 1711 LBL 7 IAW B-757 SRM 53-60-51-2R RE
- [SDR FDEA202403210334](https://openairdocs.org/sdr/FDEA202403210334), Mar 21, 2024: CREASE BEAM. CORRODED. R/H MAIN CABIN CREASE BEAM HAS CORROSION BETWEEN BS 840 THRU BS 880. MAIN CABIN CREASE BEAM BETWEEN BS 733-900 REMOVED CORROSION IAW B757 SRM 51-10-02- 0G, FOUN
- [SDR FDEA202403170305](https://openairdocs.org/sdr/FDEA202403170305), Mar 17, 2024: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK FLANGE STA 1195 LBL-26. AFTER EVALUATED CORROSION AREA ON SEAT TRACK FLANGE AT STA. 1195, LBL 26 FOUND OUT OF LIMITS IAW B757 SRM 53-00-
- [SDR FDEA202403170304](https://openairdocs.org/sdr/FDEA202403170304), Mar 17, 2024: SEAT TRACK. CORRODED. SEAT TRACK HAS CORROSION, AT STA 1427 RBL-25. AFTER EVALUATED CORROSION AREA ON SEAT TRACK STA 1427 RBL25 FOUND OUT OF LIMTIS IAW B757 SRM 53-00-51-1A FIG 101 S
- [SDR FDEA202403150293](https://openairdocs.org/sdr/FDEA202403150293), Mar 15, 2024: CREASE BEAM. CORRODED. CREASE BEAM HAS CORROSION, BETWEEN STA 1320-1350 NEXT TO R-3 DOOR. REMOVED CORROSION IAW B757 SRM 51-10-02-0G AT CHORD, OUT OF LIMTIS IAW B757 SRM 53-60- 13-1A 
- [SDR FDEA202403120278](https://openairdocs.org/sdr/FDEA202403120278), Mar 12, 2024: FLOOR SUPPORT. CORRODED. L-1 ENTRY DOOR UPPER SIDE OF THE FLOOR SUPPORT AT STA 339 LBL 60 FOUND CORROSION. REMOVED CORROSION AT L-1 ENTRY DOOR STA 339 LBL 60 ON FLOOR SUPPORT IAW B757 S
- [SDR FDEA202402130160](https://openairdocs.org/sdr/FDEA202402130160), Feb 13, 2024: UNKNOWN. ODOR. AT GATE, STATUS MESSAGES EQT CLG TEST AND WARN ELEX APPEARED, AT THE SAME TIME A STRONG FOUL RUBBER/ELECTRICAL ODOR PRESENTED ITSELF. EQUIPMENT COOLING SYSTEM T
- [SDR FDEA202310271801](https://openairdocs.org/sdr/FDEA202310271801), Oct 27, 2023: CONTAINER. FAILED. POB AT COURIER AREA FOUND DAMAGE (PROTECTIVE BAG LOST VACUUM) PROTECTIVE BREATHING EQUIPMENT, NOT POB MEL 27OCT23 07:49 BCN U RELEASED FOR SERVICE PER MEL : 35-
- [SDR FDEA202304240757](https://openairdocs.org/sdr/FDEA202304240757), Apr 24, 2023: PANEL. DELAMINATED. DURING OPEN UP FOR ELEVATOR LUBRICATION FOUND ACCESS PANEL 345BB EDGE DELEMINATED PERFORMED WET LAYUP REPAIR FOR MENTIONED PANEL PER SRM 51-70-17,PAR. 4.G. REF.
- [SDR FDEA202212072888](https://openairdocs.org/sdr/FDEA202212072888), Dec 7, 2022: EXHAUST VALVE. STUCK. PDIS 922 21-30 3695 07DEC22 CDG FACT U RECEIVED CABIN ALT WARNING IN FLIGHT AT FL400. CABIN ALT WAS JUST OVER 10,000 . DIFFERENTIAL PRESSURE WAS APPROXIMATELY 7
- [SDR FDEA202211172814](https://openairdocs.org/sdr/FDEA202211172814), Nov 17, 2022: CONTROL PANEL. FAILED. JUST PRIOR TO TOP OF DESCENT, RECEIVED A FIRE LOOK UP LIGHT WITH ALL MAIN CARGO FIRE INDICATORS ILLUMINATED. QRH COMPLETED & AN EMERGENCY DECLARED. THERMO IMAGE
- [SDR FDEA202210272677](https://openairdocs.org/sdr/FDEA202210272677), Oct 27, 2022: OIL SYSTEM. LOW PRESSURE. APU SHUTDOWN AT CRUISE RESULTING IN SINGLE GENERATOR REMAINING. EMERGENCY DECLARED AND RETURNED TO LFPG FOR NORMAL LANDING. EMERGENCY DECLARED, APU SHUT DOWN IS
- [SDR FDEA202208071945](https://openairdocs.org/sdr/FDEA202208071945), Aug 7, 2022: SENSOR. LOOSE. PDIS 922 52-20 3302 07AUG22 MEM FACT U L EMER DOOR EICAS MESSAGE AFTER POWER TRANSFER T/S REF. B757 FIM 52-71 FT 802/805, NO FAULT CODES NOTED. TARGET TEST FAR 
- [SDR FDEA202208061944](https://openairdocs.org/sdr/FDEA202208061944), Aug 6, 2022: TARGET. FAULTED. PDIS 922 52-20 3299 06AUG22 MEM FACT U L EMER DOOR EICAS MESSAGE DISPLAYED CLIMBING THROUGH 9,500 MSL. CAIN DIFFERENTIAL WAS 4.4 AND CABIN ALTITUDE WAS 800 FEET
- [SDR FDEA202208041888](https://openairdocs.org/sdr/FDEA202208041888), Aug 4, 2022: SKIN. CRACKED. REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #15. #1 PYLON FITTING PERFORMED REPAIR ON EA F-5730-T0369120 P1 STEP 20 AND 23, WINGS-PLATES AND SKINS-LH WING, UPPE
- [SDR FDEA202208041887](https://openairdocs.org/sdr/FDEA202208041887), Aug 4, 2022: SKIN. CRACKED. REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #9 #1 PYLON FITTING PERFORMED REPAIR ON EA F-5730-T0369120 P1 STEP 10. TITLE: WINGS-PLATES AND SKINS-LH WING, UPPER 
- [SDR FDEA202208041886](https://openairdocs.org/sdr/FDEA202208041886), Aug 4, 2022: SKIN. CRACKED. REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #8. #1 PYLON FITTING PERFORMED REAIR ON EA F-5730-T0369120 P1 STEP 20 AND 23. TITLE: WINGS-PLATES AND SKINS- LH WING
- [SDR FDEA202208041885](https://openairdocs.org/sdr/FDEA202208041885), Aug 4, 2022: SKIN. CRACKED. REJECTABLE DAMAGE INDICATINS NOTED IN HOLE #4 #1 PYLON FITTING PERFORMED REPAIR ON EA F-5730-T0369120 P1 STEP 20 AND 23, TITLE: WINGS-PLATES AND SKINS-LH WING-U
- [SDR FDEA202208041884](https://openairdocs.org/sdr/FDEA202208041884), Aug 4, 2022: SKIN. CRACKED. REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #3 #1 PYLON FITTING. PERFORMED REPAIR ON EA F-5730-T0369120 P1 STEP 21, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN A
- [SDR FDEA202208041882](https://openairdocs.org/sdr/FDEA202208041882), Aug 4, 2022: SKIN. CRACKED. REJECTABLE DAMAGE NOTED ON HOLE #3 #2 PYLON PERFORMED REPAIR ON E.A. F-5730-T0369270 P1 (WINGS-PLATES AND SKINS-RH WING, UPPER SKIN AT DRAG FITTING, CORROSION R
- [SDR FDEA202208041878](https://openairdocs.org/sdr/FDEA202208041878), Aug 4, 2022: SKIN. CRACKED. REJECTABLE DAMAGE NOTED ON HOLE #4 #2 PYLON PERFORMED REPAIR ON EA F-5730-T0369270 P1 (WINGS-PLATES AND SKINS-RH WING,UPPER SKIN AT DRAG FITTING, CORROSION REPA
- [SDR FDEA202208041877](https://openairdocs.org/sdr/FDEA202208041877), Aug 4, 2022: SKIN. CRACKED. REJECTABLE DAMAGE NOTED ON HOLE #6 #2 PYLON PERFORMED REPAIR ON E.A. F-5730-T0369270 P1 (WINGS-PLATES AND SKINS-RH WING, UPPER SKIN AT DRAG FITTING,CORROSION RE
- [SDR FDEA202208041876](https://openairdocs.org/sdr/FDEA202208041876), Aug 4, 2022: SKIN. CRACKED. #1 PYLON INBD. FITTING #12 HOLE DAMAGED IN SKIN ONLY PERFORMED REPAIR ON EA F-5730-T0361920 PT STEP 10, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT DRAG FITTI
- [SDR FDEA202208041880](https://openairdocs.org/sdr/FDEA202208041880), Aug 4, 2022: DRAG FITTING. CRACKED. REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #4, #1 PYLON FITTING PERFORMED REPAIR ON EA F-5730-T0369120 PT1 STEP 20 AND 23. TITLE: WINGS - PLATES AND SKINS - LH
- [SDR FDEA202208031856](https://openairdocs.org/sdr/FDEA202208031856), Aug 3, 2022: DRAG FITTING. CRACKED. REJECTABLE DAMAGE NOTED ON HOLE #12 .593, #2 PYLON THRU SKIN AND FITTING TITLE-WINGS-PLATES AND SKINS-RH WING UPPER SKIN @ DRAG FITTING, CORROSION REPAIR- FEDEX
- [SDR FDEA202208031850](https://openairdocs.org/sdr/FDEA202208031850), Aug 3, 2022: DRAG FITTING. CRACKED. REJECTABLE DAMAGE INDICATIONS NOTED IN HOLE #10 #1 PYLON FITTING. PERFORMED REPAIR ON EA F-5730-T0369120 P1 STEP 10, WINGS-PLATES AND SKIN-LH WING, UPPER SKIN @
- [SDR FDEA202108172021](https://openairdocs.org/sdr/FDEA202108172021), Aug 17, 2021: LIGHT. INOPERATIVE. MDIS 922 33-50 2242 13AUG21 CDG FACT U FOUND L1 EMER DOOR GROUND ILLUMINATION LIGHT INOP. SHGN 13AUG21 19:28 CDG U RELAMPED AS PER MM:33-51-06-2-1. LIGHT TEST O
- [SDR FDEA202107271872](https://openairdocs.org/sdr/FDEA202107271872), Jul 27, 2021: DOOR. CRACKED. LMG BODY DOOR CRACKED AFT OF TANG REPAIRED LMG DOOR CRACKED AFT OF TANG IAW FEDEX B757 SRM: 52-80-02, 51-70-06-0G, DWG #149N6003 AND AMM 51-21-00. MINOR REPAIR

All 195: https://openairdocs.org/aircraft/N922FD/reports.md

## STCs that may be installed (OpenAirDocs) (8)

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 airframe (Boeing 757-23A)

- [STC ST01162NY](https://openairdocs.org/stc/ST01162NY): Installation of Literature Pockets. Magee Plastics Company. Lists 757 Series
- [STC ST01675CH](https://openairdocs.org/stc/ST01675CH): Installation of Butterfly Valve Ring AIR23028 in starter control valves, part number 775538 or 799700. Cook Airtomic. Lists 757 Series
- [STC ST02296AT](https://openairdocs.org/stc/ST02296AT): Upgrade existing HF Voice Communication System to provide HF datalink capability. ARINC, Inc. Lists 757 Series
- [STC SA01916AT](https://openairdocs.org/stc/SA01916AT): Manufacture of Tray Carrier P/N 1839-501. BFE Services. Lists 757 Series
- [STC SA1258EA](https://openairdocs.org/stc/SA1258EA): Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584). Miller Stuart R. Lists 757 Series

### 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 757-23A aircraft: https://openairdocs.org/model/boeing-757-23a/aircraft.md
- The Rolls-Royce RB-211 series engine: https://openairdocs.org/engine/rolls-royce-rb-211-series.md

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