# N456UP: 1996 Boeing 757-24APF

- Status: Valid registration
- Airframe: [Boeing 757-24APF](https://openairdocs.org/model/boeing-757-24apf) (registry code 1384969, 178 seats)
- Engine: [Rolls-Royce RB-211 series](https://openairdocs.org/engine/rolls-royce-rb-211-series) (registry code 54555)
- Serial number: 25477
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 8, 1999
- Certificate issued: September 18, 1996
- Expires: May 31, 2028
- Mode S code: A58A36
- Registered owner: [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: Corporation
- Owner's area on the map: 38.2585° N, 85.5398° W: Placed by OpenAirDocs at the center of ZIP code 40223, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=456UP
- Page: https://openairdocs.org/aircraft/N456UP

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 757-24APF)

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/N456UP/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 N456UP.

## FAA accident and incident reports

None matched to N456UP.

## Service difficulty reports (269, 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 IPXA2026081830212](https://openairdocs.org/sdr/IPXA2026081830212), Aug 18, 2026: ACTUATOR. FAULTED. ATB, GEAR DISAGREE EICAS AND GEAR LIGHT. RAN CHECKLIST RETURN TO CAE & CAUTION LIGHT TOO. REVERSED DMP 32-30-1. REPLACED PROX SWITCH 065 REF FIM 32-09 FAULT TRE
- [SDR IPXA2026073088683](https://openairdocs.org/sdr/IPXA2026073088683), Jul 28, 2026: LANDING GEAR. WARNING MESSAGE. AIR TURN BACK, AFTER TK-OFF LANDING GEAR HANDLE IN UP POSITION AMBER GEAR DISCREET LIGHT ON AND EICAS GEAR DISAGREE MSG. QRH PROCEDURE COMPLETED AIR TURN BACK T
- [SDR IPXA2026072888683](https://openairdocs.org/sdr/IPXA2026072888683), Jul 28, 2026: WARNING LIGHT. FALSE ACTIVATION. AIR TURN BACK, AFTER TAKE-OFF LANDING GEAR HANDLE IN UP POSITION AMBER GEAR DISCREET LIGHT ON AND EICAS GEAR DISAGREE MSG. QRH PROCEDURE COMPLETED AIR TURN BACK
- [SDR IPXA2026070256697](https://openairdocs.org/sdr/IPXA2026070256697), Jul 1, 2026: WARNING MESSAGE. ILLUMINATED. AIR TURN BACK, GEAR DISAGREE EICAS MSG AND GEAR LIGHT PRESENT AFTER T/O. ATB AS DIRECTED BY FLIGHT CONTROL. GEAR OPERATED NORMALLY DURING EXTENSION. FOUND FAULT
- [SDR IPXA2025112157102](https://openairdocs.org/sdr/IPXA2025112157102), Oct 31, 2025: STRAP. CORRODED. WORKING FAULT T3F18E007KJYV LINE 920 STA 879 FLOOR BEAM FOUND CORROSION ON LWR. FWD STRAP ATA-53-05.FABRICATED STRAP P/N 143N5553-1SAAU FOR LWR FWD FLOOR BEAM, 
- [SDR IPXA2025110357102](https://openairdocs.org/sdr/IPXA2025110357102), Oct 31, 2025: FLOOR SUPPORT. CORRODED. WORKING FAULT T3F18E007KJYV LINE 920 STA 879 FLOOR BEAM FOUND CORROSION ON LWR. FWD STRAP ATA-53-05 INSP VERIFIED STEP 16 OUT OF SEQUENCE INSTALLED REPLACEMENT 
- [SDR IPXA2025111264443](https://openairdocs.org/sdr/IPXA2025111264443), Oct 14, 2025: STRUT. CRACKED. FOUND DURING DVI NR 1 PYLON OTBD SIDE HAS A CRACKED PANEL LANDING UNDER PANEL P/N 311N5049-139. INSTALL REPAIR DOUBLER, FILLERS 2 EACH /ALL REPAIR PARTS AT # 1 
- [SDR IPXA2025111897577](https://openairdocs.org/sdr/IPXA2025111897577), Oct 10, 2025: SEAT TRACK. CORRODED. MAIN DECK CABIN FLOOR SEAT TRACK HAS 2 EA AREAS WITH CORROSION AT APPROX FROM BS 1660 TO BS 1681, RBL 45.50, ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-95706-REQ1 
- [SDR IPXA2025110597614](https://openairdocs.org/sdr/IPXA2025110597614), Oct 10, 2025: RETAINER. CORRODED. STR, MAIN DECK CABIN FLOOR STRUCTURE STRAP HAS CORROSION AT APPROX FROM BS 1660 TO BS 1681, RBL 61, ID STICKER NUM. (061-002). ATA 53-05. INSTALLED NEW RETAINER
- [SDR IPXA2025110593368](https://openairdocs.org/sdr/IPXA2025110593368), Oct 10, 2025: FLOORBEAM. CORRODED. MAIN DECK CARGO COMPARTMENT BELOW ACCESS PANNEL FLOOR 231XSF HAS CORROSION. ACCOMPLISHED REPAIR PER EO-95804-REQ1 AND VT-SAA EA 757-5310-01-B0586, REV. IR, PRIO
- [SDR IPXA2025110593910](https://openairdocs.org/sdr/IPXA2025110593910), Oct 10, 2025: FLOORBEAM. CORRODED. MAIN DECK CARGO COMPARTMENT STA 620 RBL-45.5 TO RBL-54.9 BELOW ACCESS PANNEL FLOOR 232XPF HAS CORROSION ON FLOORBEAM LOWER AREA, INSTALLED REPAIR PARTS AND TWO 
- [SDR IPXA2025110597577](https://openairdocs.org/sdr/IPXA2025110597577), Oct 10, 2025: SEAT TRACK. CORRODED. MAIN DECK CABIN FLOOR SEAT TRACK HAS 2 EA AREAS WITH CORROSION AT APPROX FROM BS 1660 TO BS 1681, RBL 45.50.
- [SDR IPXA2025110598112](https://openairdocs.org/sdr/IPXA2025110598112), Oct 10, 2025: FLOORBEAM. CORRODED. MAIN DECK CABIN FLOORBEAM UPPER CHORD HAS CORROSION AT APPROX BS 1600, LBL 45.50 THRU LBL 62.22, ACCOMPLISHED REPAIR PER VT-SAA EA 757-5300-01-B0603, REV IR.
- [SDR IPXA2025110598146](https://openairdocs.org/sdr/IPXA2025110598146), Oct 10, 2025: FLOORBEAM. CORRODED. MAIN DECK CABIN FLOORBEAM LOWER CHORD HAS CORROSION ONTO SEVERAL AREAS AT APPROX BS 1360, BL 0 THRU LBL 45.50, ACCOMPLISH REPAIR PER EO-95790-REQ1 AND VT-SAA EA
- [SDR IPXA2025110581619](https://openairdocs.org/sdr/IPXA2025110581619), Oct 9, 2025: SUPPORT FITTING. CORRODED. MAIN DECK CARGO COMPARTMENT BELOW FLOOR ACCESS PANEL 222XAF HAS CORROSION. REMOVED AND REPLACED FITTING P/N 141N5131-35 PER BOEING DRAWINGS 141N5131 AND 141N525
- [SDR IPXA2025110540630](https://openairdocs.org/sdr/IPXA2025110540630), Oct 7, 2025: STRAP. CORRODED. RT ELEV TIP HAS CORROSION ON UPPER AND LOWER STRAPS, FLL-003, INSTALL CONDUCTIVE FRAME AT R/H ELEVATOR TIP UPPER SURFACE REF. B-757-200 SRM 51-40-02-OG-0. INSTA
- [SDR IPXA2025111315848](https://openairdocs.org/sdr/IPXA2025111315848), Oct 6, 2025: SUPPORT. CORRODED. RT APU DOOR SUPPORT LONGERON HAS MULTIPLE AREAS OF CORROSION. ACCOMPLISHED REPAIR PER EA 757-5330-01-B0582, REV IR.
- [SDR IPXA2025111395107](https://openairdocs.org/sdr/IPXA2025111395107), Oct 5, 2025: SKIN. CORRODED. SECTION 48 CORRODED FUSELAGE SKIN BET. STA.1885.20 TO 1918.90 LH SIDE JUST ABOVE THE APU LH DOOR FWD HINGE AS MARKED (059-07). ACCOMPLISHED REPAIR IN ACCORDANCE
- [SDR IPXA2025061164148](https://openairdocs.org/sdr/IPXA2025061164148), Jun 11, 2025: PLATE. MISSING. ATB GEAR DOORS EICAS MESSAGE. CYCLED FROM OFF TO UP PER QRH.MESSAGE CLEARED. UPON TROUBLESHOOTING FOUND LFT MAIN GEAR DOOR PROXIMITY SWITCH S10242 DAMAGED. R & 
- [SDR IPXA2024111362738](https://openairdocs.org/sdr/IPXA2024111362738), Nov 8, 2024: HEATER. FAULTED. R WINDOW HEAT EICAS MSG. NO HEAT ON #3 RT SIDE WINDOW R/R #3 RT SIDE WINDOW IAW AMM 56-11-10-424-015. WINDOW HEAT OPS CHECK AND LEAK CHECK CW. NO FAULTS NOTED. 
- [SDR IPXA2024110862738](https://openairdocs.org/sdr/IPXA2024110862738), Nov 8, 2024: HEATER. FAULTED. *** SDR FILED OPEN *** R WINDOW HEAT EICAS MSG. NO HEAT ON #3 RT SIDE WINDOW DEFERRED RT #3 SIDE WINDOW HEAT IAW MEL 30-41-1-3. C/W DMP.
- [SDR IPXA2023112705282](https://openairdocs.org/sdr/IPXA2023112705282), Nov 22, 2023: TEE ANGLE. CORRODED. FAULT: R/H WTB T-CHORDS STA 1240 FOUND EXFOLIATED CORROSION, BETWEEN RBL 57.50 TO RBL 63. INSTALLED NEW T-CHORD AND 4 E/A PLATES I.A.W SRM 51-40-02-0G.- REVIEWE
- [SDR IPXA2023112605348](https://openairdocs.org/sdr/IPXA2023112605348), Nov 22, 2023: TEE ANGLE. CORRODED. FAULT: R/H WTB T-CHORD STA 1220, FOUND EXFOLIATED CORROSION. INSTALLED NEW PART P/N UP536071D1-1 IAW B757 SRM 51-40-02-0G. REVIEWED
- [SDR IPXA2023112605270](https://openairdocs.org/sdr/IPXA2023112605270), Nov 22, 2023: TEE ANGLE. CORRODED. FAULT: R/H WTB T-CHORD, RBL 63, FOUND EXFOLIATED CORROSION. INSTALLED T-CHORD AT RBL 63 BETWEEN FS 1180 TO FS 1240 IAW SRM 51-40-02-0G. REF, STEP 14 WORK VERIFI
- [SDR IPXA2023112413955](https://openairdocs.org/sdr/IPXA2023112413955), Nov 16, 2023: SKIN. CORRODED. *MAJOR REPAIR* FAULT: #1 ENGINE PYLON O/B AFT. SKIN HAS CORROSION AT INNER SKIN APP. STA 154. NO DOT. VERIFIED COMPLIED WITH FINAL EA 757-5450-27-A3447 REV -. A
- [SDR IPXA2023120195921](https://openairdocs.org/sdr/IPXA2023120195921), Nov 11, 2023: TEE ANGLE. CORRODED. *SUPPLEMENTAL SDR* FAULT: R/H WTB T-CHORD, RBL 67, FOUND EXFOLIATED CORROSION, BET STA 1037 TO 1060. INSTALLED T- CHORD RBL 67 STA 1037 TO 1060 IAW SRM 51-40-02
- [SDR IPXA2023112750267](https://openairdocs.org/sdr/IPXA2023112750267), Nov 11, 2023: TEE ANGLE. CORRODED. FAULT: WTB STRUCTURE - FRAME WTB STRUCTURE STA. 1240 BETWEEN RBL 57 AND RBL 63 IS EXFOLIATED. INSTALLED CHANNEL STA.1240 RBL 63 I.A.W. SRM 51-40-02-0G STEP. 4,7
- [SDR IPXA2023112750323](https://openairdocs.org/sdr/IPXA2023112750323), Nov 11, 2023: FRAME. CORRODED. FAULT: WTB STRUCTURE - FRAME WTB STRUCTURE BETWEEN STA. 1180 AND 1240. RBL 63 IS EXFOLIATED. INSTALLED WEB STA.1180 TO 1240 RH, 6 EA STIFFENERS BETWEEN STA.1187
- [SDR IPXA2023112637854](https://openairdocs.org/sdr/IPXA2023112637854), Nov 10, 2023: FAIRING. CORRODED. FAULT-FUS BELLY FAIRING AFT W/W CUTOUT SUPPORT FITTING WITH CORROSION SEVERAL PLACES. INSTALLED T-CHORD AT LBL 5750 BETWEEN STA 1180 TO 1240 IAW SRM 51-40-02-0G
- [SDR IPXA2023112919701](https://openairdocs.org/sdr/IPXA2023112919701), Nov 9, 2023: TEE ANGLE. CORRODED. *** SUPPLEMENTAL SDR *** FAULT: WTB STRUCTURE - T-CHORD STA 1037.67 IS CORRODED BETWEEN LBL 20 TO LBL 65 REVIEWED
- [SDR IPXA2023112915514](https://openairdocs.org/sdr/IPXA2023112915514), Nov 9, 2023: FLOOR SUPPORT. CORRODED. *** SUPPLEMENTAL SDR *** FAULT: MAIN CARGO DECK - FLOOR BEAM STA 1057 BL 0 TO RBL 24.75 WITH CORROSION (UNDER FLOOR PANEL 242XGF) . DOT 07608-026 INSTALLED SUPP
- [SDR IPXA2023120119733](https://openairdocs.org/sdr/IPXA2023120119733), Nov 9, 2023: TEE ANGLE. CORRODED. WTB STRUCTURE - T-CHORD STA 1060 IS CORRODED BETWEEN LBL 50 TO LBL 65. INSTALLED NEW T-CHORD STA 1060 IAW SRM 51-40-02, STEP 4. REVIEWED
- [SDR IPXA2023112819755](https://openairdocs.org/sdr/IPXA2023112819755), Nov 9, 2023: TEE ANGLE. CORRODED. FAULT: WTB STRUCTURE - T-CHORD STA 1060 IS CORRODED BETWEEN LBL 20 TO LBL 30. INSTALLED T-CHORD SECTION I.A.W. B757-200 S.R.M. 51-40-02-OG. REVIEWED
- [SDR IPXA2023111315514](https://openairdocs.org/sdr/IPXA2023111315514), Nov 9, 2023: UNKNOWN. UNKNOWN. MAIN CARGO DECK - FLOOR BEAM STA 1057 BL 0 TO RBL 24.75 WITH CORROSION (UNDER FLOOR PANEL 242XGF) .
- [SDR IPXA2023111319733](https://openairdocs.org/sdr/IPXA2023111319733), Nov 9, 2023: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT: WTB STRUCTURE - T-CHORD STA 1060 IS CORRODED BETWEEN LBL 50 TO LBL 65 EVALUATED T-CHORD AT STA 1060 BETWEEN LBL 50 TO LBL 65, EXFO
- [SDR IPXA2023111319701](https://openairdocs.org/sdr/IPXA2023111319701), Nov 9, 2023: UNKNOWN. UNKNOWN. WTB STRUCTURE - T-CHORD STA 1037.67 IS CORRODED BETWEEN LBL 20 TO LBL 65 REF. STEP 3 , WORK VERIFIED. REMOVED T-CHORD STA 1037.67 BETWEEN LBL 20 TO LBL 65 INSPE
- [SDR IPXA2023112984644](https://openairdocs.org/sdr/IPXA2023112984644), Nov 7, 2023: ANGLE. CORRODED. *** SUPPLEMENTAL SDR *** FAULT RT WING TO BODY AREA ABOVE RAT DOOR INTERIOR AREA SHOWS EVIDENCE OF CORROSION DOT 47-09 INSTALLED T-CHORD I.A.W SRM 51-40-02-0G I
- [SDR IPXA2023112984377](https://openairdocs.org/sdr/IPXA2023112984377), Nov 7, 2023: ANGLE. CORRODED. *** SUPPLEMENTAL SDR *** FAULT LEFT WING TO BODY SUPPORT AREA FWD OF W/W SHOWS EVIDENCE OF CORROSION DOT 47-05 INSTALLED T-CHORD STA 1037,67 TO 1060 LH SIDE IAW
- [SDR IPXA2023112486155](https://openairdocs.org/sdr/IPXA2023112486155), Nov 7, 2023: SKIN. CORRODED. *MAJOR REPAIR* FAULT: #1 ENGINE PYLON I/B AFT. SKIN HAS CORROSION AT INNER SKIN APP. STA 154 . DOT 07308-005 (PLACED AT EXTERNAL SKIN) VERIFIED COMPLIED WITH EO
- [SDR IPXA2023111384377](https://openairdocs.org/sdr/IPXA2023111384377), Nov 7, 2023: UNKNOWN. UNKNOWN. LEFT WING TO BODY SUPPORT AREA FWD OF W/W SHOWS EVIDENCE OF CORROSION DOT 47-05 REMOVED T-CHORD FROM STA 1037.67 TO 1060 LH SIDE LBL 67 IAW SRM 51-40-02-0G. VER
- [SDR IPXA2023111384644](https://openairdocs.org/sdr/IPXA2023111384644), Nov 7, 2023: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT RT WING TO BODY AREA ABOVE RAT DOOR INTERIOR AREA SHOWS EVIDENCE OF CORROSION DOT 47-09 REMOVED T-CHORD AT AREA INTERIOR DOOR RAT I
- [SDR IPXA2023112956677](https://openairdocs.org/sdr/IPXA2023112956677), Nov 6, 2023: TEE ANGLE. CORRODED. *** SUPPLEMENTAL SDR *** FAULT: WTB STRUCTURE - WEB FOR T-CHORD STA 900 HAS CORROSION AT APROX LBL 10 - DOT 07608-002 INSTALLED WEB AT STA 900 I.A.W. SRM 51-40-
- [SDR IPXA2023111360602](https://openairdocs.org/sdr/IPXA2023111360602), Nov 6, 2023: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT: RH RAM AIR INLET STRUCTURE AT APROX STA 880 HAS 2 ANGLES WITH CORROSION. DOT 07608-006 REMOVED RAM AIR INLET ASSY P/N: 149N7160-31
- [SDR IPXA2023111356677](https://openairdocs.org/sdr/IPXA2023111356677), Nov 6, 2023: UNKNOWN. UNKNOWN. WTB STRUCTURE - WEB FOR T-CHORD STA 900 HAS CORROSION AT APROX LBL 10 - DOT 07608-002 REMOVED WEB ON FRAME STA 900 L/H IAW B757 SRM 51-40-02. VERIFIED WEB ON FR
- [SDR IPXA2023110759388](https://openairdocs.org/sdr/IPXA2023110759388), Nov 6, 2023: UNKNOWN. UNKNOWN. WTB STRUCTURE - T-CHORD STA 900 HAS CORROSION AT APROX LBL 16 - DOT 07608-005 PERFORMED CUT OUT DAMGED T-CHORD L= 75.5" STA 900 IAW SRM 51-10-02.
- [SDR IPXA2023112532382](https://openairdocs.org/sdr/IPXA2023112532382), Nov 4, 2023: SHEAR TIE. DENTED. FAULT: AFT CARGO PIT - FRAME STA. 1460 RH SIDE BETWEEM STR. 25R AND 26R HAS A DENT AT UPPER FLANGE. DOT 07308-001. INSTALLED NEW CLIP I.A.W SRM 51-40-02-0G.- SU
- [SDR IPXA2023100410733](https://openairdocs.org/sdr/IPXA2023100410733), Sep 29, 2023: ENGINE. SURGES. ATB ON CLIMB OUT RT ENGINE HAD SOME SURGING WITH HIGHER GET THAN LEFT ENGINE. IN CRUISE, SETTLED DOWN NORMAL. DISPATCH INSTRUCTED US TO PERFORM AN AIR TURN BACK
- [SDR IPXA2023093000733](https://openairdocs.org/sdr/IPXA2023093000733), Sep 29, 2023: UNKNOWN. UNKNOWN. ATB, ON CLIMB OUT RT ENGINE HAD SOME SURGING WITH HIGHER GET THAN LEFT ENGINE. IN CRUISE, SETTLED DOWN NORMAL. DISPATCH INSTRUCTED US TO PERFORM AN AIR TURN BAC
- [SDR IPXA2023092126666](https://openairdocs.org/sdr/IPXA2023092126666), Sep 21, 2023: CONTROL UNIT. UNKNOWN. **ATB**RIGHT ENG EGT REMOVED AND REPLACED RT BVCU PER AMM 75-32-01-404-023 OPS CHK OK
- [SDR IPXA2022101787184](https://openairdocs.org/sdr/IPXA2022101787184), Oct 17, 2022: SKIN. DENTED. INSPECTION TYPE:N/AREF D779518 FUSELAGE TAILCONE UPPER SURFACE DENTREPAIRED PER EO B757-5330-83549-C

All 269: https://openairdocs.org/aircraft/N456UP/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 757-24APF aircraft: https://openairdocs.org/model/boeing-757-24apf/aircraft.md
- The Rolls-Royce RB-211 series engine: https://openairdocs.org/engine/rolls-royce-rb-211-series.md

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