# N910AW: 1989 Boeing 757-2G7

- Status: Valid registration
- Airframe: [Boeing 757-2G7](https://openairdocs.org/model/boeing-757-2g7) (registry code 1384963, 178 seats)
- Engine: [Rolls-Royce RB-211 series](https://openairdocs.org/engine/rolls-royce-rb-211-series) (registry code 54555)
- Serial number: 24523
- Year built: 1989
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 29, 1989
- Certificate issued: March 9, 2017
- Expires: March 31, 2027
- Mode S code: AC96C0
- Registered owner: [Sundown Aircraft LLC](https://openairdocs.org/faa-owner/SUNDOWN%20AIRCRAFT%20LLC)
- Location: [Knoxville, TN](https://openairdocs.org/faa-place/TN/Knoxville)
- Owner type: LLC
- Owner's area on the map: 35.9763° N, 84.1263° W: Placed by OpenAirDocs at the center of ZIP code 37931, 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=910AW
- Page: https://openairdocs.org/aircraft/N910AW

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 757-2G7)

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/N910AW/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 (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB LAX00LA146](https://openairdocs.org/ntsb/LAX00LA146), Apr 3, 2000: Boeing 757-2G7 (N910AW), Dallas, TX, no damage. Probable cause: The en route cruise encounter with forecast moderate turbulence.
- [NTSB LAX99LA322](https://openairdocs.org/ntsb/LAX99LA322), Jul 24, 1999: Boeing 757-2G7 (N910AW), Phoenix, AZ, substantial damage. Probable cause: The failure of the flight crew and the tug driver to verify that the aircraft was properly configured for pushback. Factors in the accident were the left wing walker's failure to notify the tug…

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20000402006529A](https://openairdocs.org/incident/20000402006529A), Apr 2, 2000: Boeing 7572G7 (N910AW), Las Vegas, NV, No damage. (-23) Awe 563 B757-200, 910AW, orlando, FL. To Las Vegas encountered severe turbulence at FL350 over abilene, TX at 022100 PDT. 190 passengers, no injuries.…

## Service difficulty reports (157, 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 AALA201608299005](https://openairdocs.org/sdr/AALA201608299005), Aug 28, 2016: SLIDE. DISLODGED. AIRCRAFT WAS NOT GROUNDED: CABIN SERVICE REPORTS L4 DOOR HARD TO CLOSE. FOUND SLIDE PACK TO BE DISLODGED. SAFETY PIN INSTALLED ON INFLATION CYLINDER, REINSTALLE
- [SDR AALA201603299007](https://openairdocs.org/sdr/AALA201603299007), Mar 28, 2016: UNKNOWN. ODOR. AIRCRAFT WAS GNDED. DURING DESCENT THE AFT CABIN FLIGHT ATTENDANT REPORTED SMELL OF SMOKE, NO SOURCE FOUND. DISAPPEARED AFTER 30 SECONDS. DECLARED AN EMER & LAN
- [SDR AALA201603159019](https://openairdocs.org/sdr/AALA201603159019), Mar 14, 2016: FLASHLIGHT. DEFECTIVE. AIRCRAFT WAS NOT GNDED. AFT FLIGHT ATTENDANT FLASHLIGHT NOT BLINKING. REPLACED FLASHLIGHT.
- [SDR AALA201602159004](https://openairdocs.org/sdr/AALA201602159004), Feb 12, 2016: WIRE HARNESS. DAMAGED. RETURNED, ACFT WAS GNDED. CREW NOTED A STATUS MSG, R ENG OH LP1, RESULTING IN THE ACFT RETURNING WHERE IT LANDED SAFELY WITH NO INCIDENTS REPORTED. NO EMER WAS 
- [SDR AALA201602159003](https://openairdocs.org/sdr/AALA201602159003), Feb 12, 2016: DETECTOR. DEFECTIVE. RETURNED, ACFT WAS GNDED. CREW NOTED A STATUS MSG, RT ENG OH LP1, RESULTING IN THE ACFT RETURNING WHERE IT LANDED SAFELY WITH NO INCIDENTS REPORTED. NO EMER WAS
- [SDR AALA201510159009](https://openairdocs.org/sdr/AALA201510159009), Oct 13, 2015: SLAT. DELAMINATED. LEFT WING NR 4 SLAT HAS DELAMINATION AT INBD TE BOTTOM SIDE. REPLACED SLAT IAW 19L52027002.
- [SDR AALA201510159008](https://openairdocs.org/sdr/AALA201510159008), Oct 13, 2015: SLAT. DELAMINATED. RIGHT WING NR 8 SLAT HAS DELAMINATION AT PREVIOUS REPAIRS, 3 EACH, AREA 1. APPROX 70" FROM INBD EDGE. AREA 2, 19" FROM INBD EDGE. AREA 3, 13" FROM OTBD END & 2"
- [SDR AALA201504229008](https://openairdocs.org/sdr/AALA201504229008), Apr 21, 2015: LIGHT. INOPERATIVE. ROW 26 LT EMERGENCY LIGHT INOPERATIVE. REPLACED SEAT 26 LT EMERGENCY LIGHT.
- [SDR AALA201504149030](https://openairdocs.org/sdr/AALA201504149030), Apr 11, 2015: ACCESS PANEL. CRACKED. RIGHT WING FUEL ACCESS PANEL 641GB CRACKED & LEAKING FUEL. REPLACED RT WING FUEL ACCESS PANEL 641GB IAW AMM 28-11-00. LEAK CHECKED GOOD.
- [SDR USAA2015012300002](https://openairdocs.org/sdr/USAA2015012300002), Jan 22, 2015: LOCK. LACK OF LUBE. EN-ROUTE, CAPTAIN`S SEAT TRACK LOCK FAILED ON TAKEOFF, SEAT ROLLED BACK. LUBED THE SEAT TRACK LOCK MECHANISM.
- [SDR USAA2015011200012](https://openairdocs.org/sdr/USAA2015011200012), Dec 26, 2014: AILERON. DEBONDED. C2 CHECK, DISBONDING ON LT AILERON AT MOST INBD END & 12 INCHES FWD OF TE. REPLACED LT AILERON IAW JOB CARD 19L56827001.
- [SDR USAA2015011200013](https://openairdocs.org/sdr/USAA2015011200013), Dec 24, 2014: SKIN PANEL. DELAMINATED. C2 CHECK, DELAMINATION ON APU COMPARTMENT RT INTERIOR SKIN PANEL AT BS 1926, WL 247.6. REPAIRED APU COMPARTMENT RT INTERIOR SKIN PANEL AT BS 1926, WL 247.6 IAW 
- [SDR USAA2014122600003](https://openairdocs.org/sdr/USAA2014122600003), Dec 24, 2014: SKIN PANEL. DELAMINATED. C2 CHECK DELAMINATION & CRACK AT APU COMPARTMENT TAIL CONE RT INTERIOR FUSELAGE SKIN PANEL AT STATION 1925 ON BACK SIDE OF ELEVATOR INDEX. ACCOMPLISHED TIME LIM
- [SDR USAA2015011200014](https://openairdocs.org/sdr/USAA2015011200014), Dec 11, 2014: PANEL. CRACKED. C2 CHECK, CRACK AT FASTENER HOLE OF LT WING NR 3 LE COVE PANEL AT APPROX 354 INCHES FROM INBD EDGE & 14 INCHES DOWN FROM TE. REPLACED LT WING NR 3 LE COVE PANEL
- [SDR USAA2015011200016](https://openairdocs.org/sdr/USAA2015011200016), Dec 10, 2014: PANEL. CRACKED. C2 CHECK, CRACK AT FASTENER HOLE OF LT WING NR 1 LE COVE PANEL AT APPROX 30 INCHES FROM OTBD EDGE & 13 INCHES DOWN FROM TE. REPLACED LT WING NR 3 LE COVE PANEL 
- [SDR USAA2015011200015](https://openairdocs.org/sdr/USAA2015011200015), Dec 10, 2014: PANEL. CRACKED. C2 CHECK, CRACK AT FASTENER HOLE OF LT WING NR 1 LE COVE PANEL AT APPROX 54 INCHES FROM INBD EDGE & 11.250 INCHES DOWN FROM TE. REPLACED LT WING 1 LE COVE PANEL
- [SDR USAA2014052300003](https://openairdocs.org/sdr/USAA2014052300003), May 22, 2014: WIRE HARNESS. BROKEN. PHX SEAT ROW 6 EMERGENCY LIGHT HAS BROKEN WIRE AT CONNECTOR. REPLACED WIRE HARNESS, OPERATIONS GOOD.
- [SDR USAA2014042100021](https://openairdocs.org/sdr/USAA2014042100021), Apr 21, 2014: SWITCH. NO TEST. PHX IAW OVERNIGHT CHECK STEP 4, EMERGENCY LIGHTING TEST SWITCH OVER L3 DOOR ESCAPE WILL NOT TEST. R & R EMERGENCY LIGHT TEST SWITCH AT L3 DOOR.
- [SDR USAA2014031800001](https://openairdocs.org/sdr/USAA2014031800001), Mar 17, 2014: SLIDE. MULTIPLE FAIL. DOOR 4L GIRT BAR CAME OUT FROM SLIDE ASSEMBLY. 4L SLIDE REMOVED & REINSTALLED. PROBLEM WITH ARM & DISARM RIG. REPLACED THE L4 DOOR GIRT BAR OPERATING MECHANISM 
- [SDR USAA2014013100004](https://openairdocs.org/sdr/USAA2014013100004), Jan 29, 2014: GIRT BAR. DEFECTIVE. PHX 4L DOOR ARMED LIGHT WOULD NOT ILLUMINATE WHEN ARMED. REINSTALLED GIRT BAR FOOT, OPERATIONS CHECKED GOOD.
- [SDR USAA2013121700002](https://openairdocs.org/sdr/USAA2013121700002), Dec 15, 2013: TRANSCEIVER. FAULTY. FLIGHT 694 ENROUTE. HF NR 1 WILL NOT TUNE. DETECTED SMOKE & TURNED OFF HF NR 1 RADIO UNTIL SMOKE ODOR WENT AWAY. LEFT OFF REMAINDER OF FLIGHT. HF NR 2 TUNE & WO
- [SDR USAA2013120200016](https://openairdocs.org/sdr/USAA2013120200016), Nov 7, 2013: FRAME. DAMAGED. C1 CHECK ELEC ARCING DAMAGE AT TERMINAL LUG BRACKET & FRAME ATTACH POINTS AT BS 1480 BETWEEN STRINGER 23R TO STRINGER 24R. REPAIRED FUSELAGE FRAME AT BS 1480 BE
- [SDR USAA2013110800010](https://openairdocs.org/sdr/USAA2013110800010), Nov 6, 2013: SKIN. CRACKED. DURING C1 CHECK, CRACK FOUND ON NR 2 OTBD SLAT COVE PANEL AT APPROX. 29 INCHES INBD FROM OTD EDGE & 3 INCHES UP FROM LOWER SIDE. REPLACED LT WING 2 OTBD SLAT CO
- [SDR USAA2013110800011](https://openairdocs.org/sdr/USAA2013110800011), Nov 5, 2013: SKIN. CRACKED. DURING C1 CHECK, CRACK FOUND ON NR 3 SLAT COVE PANEL AT APPROX 5 INCHES INBD FROM OTBD PANEL EDGE & 2 INCHES UP FROM BOTTOM EDGE. REPLACED LT WING NR 3 SLAT COV
- [SDR USAA2013030100004](https://openairdocs.org/sdr/USAA2013030100004), Feb 26, 2013: STATOR. FAILED. HNL - FLT 22 EN ROUTE PHX TO HNL. SMOKE SMELL IN CABIN, EICAS R RECIRC FAN, OVERHEAD RIGHT RECIRC FAN INOP. REPLACED THE RIGHT CABIN AIR RECIRCULATION FAN. FOUN
- [SDR USAA2012112300014](https://openairdocs.org/sdr/USAA2012112300014), Nov 22, 2012: LENS. DAMAGED. PHX - SEAT MOUNTED EMERGENCY EXIT LIGHT (RED) LENSES DAMAGED 2 EA ROW 10ABC. REPLACED LENSES AS NEEDED.
- [SDR USAA2012092100001](https://openairdocs.org/sdr/USAA2012092100001), Sep 18, 2012: SOLENOID. FAILED. PHX FLT 125 EN ROUTE HNL TO PHX. WHEN AUTOPILOT WAS DISCONNECTED AT 6000FT ON APPROACH THE ROLL YOKE CONTROL WAS VERY HEAVY (ABOUT 3X NORMAL FORCE). IT WAS THE 
- [SDR USAA2012091400065](https://openairdocs.org/sdr/USAA2012091400065), Sep 13, 2012: MEGAPHONE. INOPERATIVE. PHX - AFT MEGAPHONE INOP. REPLACED AFT EMERGENCY MEGAPHONE.
- [SDR USAA2012061400028](https://openairdocs.org/sdr/USAA2012061400028), Jun 13, 2012: DIODE. FAILED. PHX - FLT 26 EN ROUTE OGG TO PHX. FLAPS FAILED TO MOVE, TRAILING EDGE LIGHT ON, AND EICAS MSG TRAILING EDGE DISAGREE DISPLAYED. FLAPS NORMAL ON ALTERNATE SYS. T
- [SDR USAA2012061400003](https://openairdocs.org/sdr/USAA2012061400003), Jun 13, 2012: SYNCRONIZER. FAILED. PHX - FLT 26 EN ROUTE OGG TO PHX. FLAPS FAILED TO MOVE, TRAILING EDGE LIGHT ON, AND EICAS MSG TRAILING EDGE DISAGREE DISPLAYED. FLAPS NORMAL ON ALTERNATE SYS. T
- [SDR USAA2012051700028](https://openairdocs.org/sdr/USAA2012051700028), May 14, 2012: SURVIVAL KIT. UNSERVICEABLE. PHX - INFLIGHT CREW REPORTS SLIDE RAFT SURVIVAL KITS NOT SEALED. REPLACED 4 EA SLIDE RAFT SURVIVAL KITS ASSY.
- [SDR USAA2012040500001](https://openairdocs.org/sdr/USAA2012040500001), Mar 27, 2012: WEB. CORRODED. C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR WEB PANEL AT BS 1420, S17R. REPAIRED FLOOR WEB PANEL AT BS 1420, S17R IAW EA 103818.
- [SDR USAA2012032000002](https://openairdocs.org/sdr/USAA2012032000002), Mar 16, 2012: ANGLE. CRACKED. C4 CHECK - CRACK ON FORWARD SIDE OF FRAME L-ANGLE AT BS 350, S7L. REPLACED FRAME L-ANGLE AT BS 350, S7L IAW B757 SRM 51-40-10.
- [SDR USAA2012040500004](https://openairdocs.org/sdr/USAA2012040500004), Mar 14, 2012: PIN. CRACKED. C4 CHECK - CRACK IN LOWER FUSE PIN OF RIGHT ENGINE NACELLE STRUT DIAGONAL BRACE AT PPS 300, PPWL 161.70. REPLACED LOWER FUSE PIN OF DIAGONAL BRACE AT PPS 300, P
- [SDR USAA2012040900025](https://openairdocs.org/sdr/USAA2012040900025), Mar 9, 2012: WEDGE. DELAMINATED. C4 CHECK - DELAMINATION ON NR 7 SLAT TRAILING EDGE WEDGE AT WS 397.50, WBL 740.00, 6 INCHES FROM INBOARD END AT LOWER SKIN. REPAIRED NR 7 SLAT TRAILING EDGE WED
- [SDR USAA2012031300015](https://openairdocs.org/sdr/USAA2012031300015), Mar 9, 2012: SKIN. DAMAGED. C4 CHECK - SMALL 1 INCH SPLIT IN RIGHT INBOARD AFT FLAP ON OUTBOARD END AT WS 258.50, WBL 740. REPAIRED RIGHT INBOARD AFT FLAP SKIN IAW B757 SRM 51-70-17.
- [SDR USAA2012040500003](https://openairdocs.org/sdr/USAA2012040500003), Mar 6, 2012: STIFFENER. CRACKED. C4 CHECK - CRACK ON FLOORBEAM STIFFENER STRAP AT BS 718, RBL 48. REPAIRED FLOORBEAM STABILIZER STRAP AT BS 718, RBL 48 IAW EA 103787.
- [SDR USAA2012032200005](https://openairdocs.org/sdr/USAA2012032200005), Mar 6, 2012: STRAP. CRACKED. C4 CHECK - CRACK ON STRAP AT BS 720, LBL 24. REPAIRED STRAP AT BS 720, LBL 24 IAW TYPICAL REPAIR TR 757-5335-11-0334.
- [SDR USAA2012032000003](https://openairdocs.org/sdr/USAA2012032000003), Mar 3, 2012: FLOORBEAM. CORRODED. C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT BS 377.7 & BETWEEN LBL 54 TO LBL 60. REPAIRED FLOORBEAM AT BS 377.7 & BETWEEN LBL 54 TO LBL 60 IAW B7
- [SDR USAA2012040500002](https://openairdocs.org/sdr/USAA2012040500002), Feb 29, 2012: FLOORBEAM. CORRODED. C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOOR BEAM T-CAP AT BS 365 BETWEEN RBL 36 TO RBL 59. REPAIRED FLOORBEAM T-CAP AT BS 365 BETWEEN RBL 36 TO RBL 59 I
- [SDR USAA2012030800005](https://openairdocs.org/sdr/USAA2012030800005), Feb 29, 2012: FLOOR SUPPORT. CORRODED. C4 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT AT BS 1316, RBL 18. REPLACED FLOOR SUPPORT AT BS 1316, RBL 18 IAW B757 SRM 51-10-02 & 51-40-00.
- [SDR USAA2012011700024](https://openairdocs.org/sdr/USAA2012011700024), Jan 16, 2012: FITTING. MISSING. PHX - GIRT BAR ENGAGEMENT LIGHT EXTIN WITH EVACUATION SLIDE ARMING LEVER IN ENGAGE POS AT ENTRY/SERVICE DOOR L-4. FOUND FWD GIRT BAR END FITTING MISSING. REPLAC
- [SDR USAA2011122300020](https://openairdocs.org/sdr/USAA2011122300020), Dec 22, 2011: GIRT BAR. MISSING. PHX - AFT LEFT SLIDE ARM DOOR LIGHT INOP. FOUND L4 DOOR, FWD GIRT BAR SLIDER MISSING. INSTALLED SLIDER. DOOR ARM LIGHT OPS GOOD.
- [SDR USAA2011080900011](https://openairdocs.org/sdr/USAA2011080900011), Aug 7, 2011: PIN. BACKED OUT. PHX - EMERGENCY LIGHT ON SEAT 7 INOP. RELAMP, NO HELP. RESEATED PUSHED PIN IN EMER LIGHT CONNECTOR FOR SEAT 7.
- [SDR USAA2011080200027](https://openairdocs.org/sdr/USAA2011080200027), Jul 31, 2011: WIRE HARNESS. INOPERATIVE. PHX - EMERGENCY LIGHT ON SEAT 23 INOP. MAINTENANCE REPLACED FLOOR TO LIGHT HARNESS. OPS GOOD.
- [SDR USAA20110204BB006](https://openairdocs.org/sdr/USAA20110204BB006), Feb 2, 2011: GIRT BAR. BENT. PHX - THE L4 DOOR GIRT BAR AFT SPRING TAB WAS BENT. REMOVED AND REPLACED THE L4 DOOR GIRT BAR.
- [SDR USAA2010111092583](https://openairdocs.org/sdr/USAA2010111092583), Nov 5, 2010: SUPPORT ANGLE. CORRODED. CLT - C3 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FORWARD CARGO LATERAL SUPPORT ANGLE AT BS 690, LBL 14. REPLACED FORWARD CARGO LATERAL SUPPORT ANGLE A
- [SDR USAA2010111192589](https://openairdocs.org/sdr/USAA2010111192589), Oct 20, 2010: SUPPORT ANGLE. CORRODED. CLT - C3 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON LOWER AFT CARGO BULKHEAD SUPPORT ANGLE AT BS 848, RBL 2. REPLACED LOWER AFT CARGO BULKHEAD SUPPORT AN
- [SDR USAA2010102992453](https://openairdocs.org/sdr/USAA2010102992453), Oct 16, 2010: FITTING. CORRODED. CLT - C3 - MAJOR REPAIR - NR I2D52602/007 - CORROSION ON SMALL CLIP ON AFT CARGO DOOR LOWER FORWARD CORNER INTERIOR. REPLACED SMALL CLIP ON AFT CARGO DOOR LOWER
- [SDR USAA20100604BB035](https://openairdocs.org/sdr/USAA20100604BB035), Jun 1, 2010: SLIDE. LOW PRESSURE. PHX - R3 EMERGENCY DOOR SLIDE HAS LOW PRESSURE. REPLACED R3 DOOR SLIDE.

All 157: https://openairdocs.org/aircraft/N910AW/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 757-2G7 aircraft: https://openairdocs.org/model/boeing-757-2g7/aircraft.md
- The Rolls-Royce RB-211 series engine: https://openairdocs.org/engine/rolls-royce-rb-211-series.md

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