# N454UP: 1995 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: 25475
- Year built: 1995
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 6, 1995
- Certificate issued: September 11, 1995
- Expires: May 31, 2028
- Mode S code: A582C8
- 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=454UP
- Page: https://openairdocs.org/aircraft/N454UP

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/N454UP/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 N454UP.

## FAA accident and incident reports

None matched to N454UP.

## Service difficulty reports (250, 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 IPXA2026042225183](https://openairdocs.org/sdr/IPXA2026042225183), Apr 22, 2026: TRANSITION PANEL. CORRODED. FWD CARGO RH OTBD TRANSITION PANEL CORRODED AT BS 620. REMOVED CORROSION ON FWD CARGO RT OTBD TRANSITION PANEL AT BS 620. TREATED AND PRIMED AREA AND APPLIED TO
- [SDR IPXA2026043081790](https://openairdocs.org/sdr/IPXA2026043081790), Apr 13, 2026: RETAINER. CORRODED. UPON SEAL REMOVAL- AFTER CARGO DOOR FRAME SEAL RETAINER LOWER HAS CORROSION THE INTERIOR LENGTH. LOCATED AND DRILLED NEW SEAL RETAINER AT AFT CARGO DOOR FRAME L
- [SDR IPXA2026043042646](https://openairdocs.org/sdr/IPXA2026043042646), Apr 10, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOOR STRINGER HAS CORROSION APPROX BTW BS 1445 AND BS 1497.5, RBL 10.45. REMOVED 1EA DAMAGED FLOOR STRINGER IN AFT CARGO COMPARTMENT BTW 
- [SDR IPXA2026043042676](https://openairdocs.org/sdr/IPXA2026043042676), Apr 10, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOOR STRINGER HAS CORROSION APPROX BTW BS 1445 AND BS 1497.5, LBL 7.55. REMOVED 1EA DAMAGED FLOOR STRINGER IN AFT CARGO COMPARTMENT BTW B
- [SDR IPXA2026042142676](https://openairdocs.org/sdr/IPXA2026042142676), Apr 10, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOOR STRINGER HAS CORROSION APPROX BTW BS 1445 AND BS 1497.5, LBL 7.55,
- [SDR IPXA2026041742646](https://openairdocs.org/sdr/IPXA2026041742646), Apr 10, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOOR SUPPORT HAS CORROSION APPROX BTW BS 1445 AND BS 1497.5, RBL 10.45
- [SDR IPXA2026050107936](https://openairdocs.org/sdr/IPXA2026050107936), Apr 9, 2026: ATTACH ANGLE. CORRODED. LEFT ELEVATOR OB BONDING JUMPER ATTACHMENT HAS CORROSION. REMOVED INTERCOSTAL TO GAIN ACCESS AT LH STABILIZER HORIZONTAL TIP AREA REF SRM 51-40-02-0G-0. INSTALL
- [SDR IPXA2026050588833](https://openairdocs.org/sdr/IPXA2026050588833), Apr 8, 2026: SUPPORT TRAY. CORRODED. APU FIRE BOTTLE SUPPORT TRAY HAS UPPER SURFACE CORROSION AND FWD INBD CORNER CRACKED. INSTALLED NEW REPLACEMENT APU FIRE BOTTLE SUPPORT TRAY IN AFT INTERNAL FUS
- [SDR IPXA2026050190796](https://openairdocs.org/sdr/IPXA2026050190796), Apr 8, 2026: ATTACH ANGLE. CORRODED. RIGHT ELEVATOR OB BONDING JUMPER BRACKET HAS CORROSION. REMOVED 1EA DAMAGE BRACKET AND DAMAGE BONDING WIRE AT R/H ELEVATOR T/E IAW SRM 51-40-02-0G-0. INSTALLED 
- [SDR IPXA2026050102987](https://openairdocs.org/sdr/IPXA2026050102987), Apr 8, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOOR STRINGER UPPER FLANGE HAS EVIDENCE OF CORROSION APPROX BTW BS 1460 AND BS 1480, LBL 7.55 AND RBL 7.55, INSTALLED NEW REPLACEMANT STR
- [SDR IPXA2026050103053](https://openairdocs.org/sdr/IPXA2026050103053), Apr 8, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOOR STRINGER UPPER FLANGE HAS EVIDENCE OF CORROSION APPROX BTW BS 1460 AND BS 1480, LBL 10.45 AND RBL 10.45, REMOVED CORROSION AT AFT CA
- [SDR IPXA2026050103176](https://openairdocs.org/sdr/IPXA2026050103176), Apr 8, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOOR STRINGER UPPER FLANGE HAS CORROSION APPROX BTW BS 1460 AND BS 1480, RBL 16.10, REMOVED SPLICE STRAP AT AFT CARGO COMPARTMENT FLOOR S
- [SDR IPXA2026042200417](https://openairdocs.org/sdr/IPXA2026042200417), Apr 8, 2026: FRAME ANGLE. CRACKED. BULK CGO COMP STA 1640 LBL 16" FLOOR AREA ANGLE FRAME HAS CRACKED. REMOVED FLOOR ANGLE FRAME AT AFT CARGO COMP AT STA 1640 LBL 16" IAW B757 SRM 51-40-02-0G-0. I
- [SDR IPXA2026041203053](https://openairdocs.org/sdr/IPXA2026041203053), Apr 8, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOOR SUPPORT UPPER FLANGE HAS EVIDENCE OF CORROSION APPROX BTW BS 1460 AND BS 1480, LBL 10.45 AND RBL 10.45, ID STICKER NUM, (085-040) AT
- [SDR IPXA2026041202987](https://openairdocs.org/sdr/IPXA2026041202987), Apr 8, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOOR SUPPORT UPPER FLANGE HAS EVIDENCE OF CORROSION APPROX BTW BS 1460 AND BS 1480, LBL 7.55 AND RBL 7.55, ID STICKER NUM, (085-039) ATA 
- [SDR IPXA2026041803176](https://openairdocs.org/sdr/IPXA2026041803176), Apr 8, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOOR STRINGER UPPER FLANGE HAS CORROSION APPROX BTW BS 1460 AND BS 1480, RBL 16.10, ID STICKER NUM, (085-041) ATA 53-10 VERIFIED STEP 6. 
- [SDR IPXA2026041984059](https://openairdocs.org/sdr/IPXA2026041984059), Apr 7, 2026: ANGLE. CORRODED. RIGHT WTB PANEL LANDING, 2ND FROM FWD, AT UPPER WING ROOT HAS SURFACE CORROSION. 83-021. ATA 53-030 INSTALLED (3EA) NUTPLATES ON FWD SUPPORT ANGLE AND (3EA) NUT
- [SDR IPXA2026043078576](https://openairdocs.org/sdr/IPXA2026043078576), Apr 7, 2026: ANGLE. CRACKED. AFT CARGO R/H AFT. WALL ANGLE SUPPORT ZONE 164 FOUND CRACK. ES-009. REMOVED CRACKED AFT CARGO RT AFT. WALL ANGLE SUPPORT AT STA 1640 RBL 24.8 IAW SRM 51-40-02-0
- [SDR IPXA2026042382776](https://openairdocs.org/sdr/IPXA2026042382776), Apr 7, 2026: TIE DOWN. CORRODED. FWD CARGO RH OTBD TRANSITION HAS CORROSION BS 770 - 800. REMOVED CORROSION AT R/H STA. 780 ON TIE DOWN FITTING RBL 20R IAW 51-10-02-0G-0. INSTALLED NEW TIE DOWN
- [SDR IPXA2026042382902](https://openairdocs.org/sdr/IPXA2026042382902), Apr 7, 2026: SIDEWALL SUPPORT. CORRODED. FWD CARGO LH LOWER SIDEWALL SUPPORT FRAME CORRODED STA 740 STR. REMOVED CORROSION ON L/H LOWER SIDEWALL SUPPORT AT BS 740 BTW STR 22R-26R IAW B757-200PF SRM 51-
- [SDR IPXA2026042783844](https://openairdocs.org/sdr/IPXA2026042783844), Apr 7, 2026: SUPPORT CHANNEL. CORRODED. AFT WTB LOWER FAIRING PANEL LANDING CHORD AT APPROX. BS 1217 HAS EXFOLIATED CORROSION. 83-015. REMOVED 1EA EXFOLIATED CHORD (CHANNEL) AT AFT WTB LOWER FAIRING A
- [SDR IPXA2026043083949](https://openairdocs.org/sdr/IPXA2026043083949), Apr 7, 2026: SUPPORT ANGLE. CRACKED. STR- RH AFT WTB LOWER FAIRING PNL LANDING SUPPORT BRACKET HAS EVIDENCE OF A CRACK. 83-018. REMOVED SUPPORT BRACKET AT RH AFT WTB LOWER FAIRING PNL IAW B757-200P
- [SDR IPXA2026042884007](https://openairdocs.org/sdr/IPXA2026042884007), Apr 7, 2026: ANGLE. CORRODED. RIGHT WTB FWD PANEL LANDING AT UPPER WING ROOT HAS SURFACE CORROSION. 83-020. REMOVED (1EA) FWD SUPPORT ANGLE AND (1EA) AFT SUPPORT ANGLE FROM RH WTB UPPER WING
- [SDR IPXA2026042982498](https://openairdocs.org/sdr/IPXA2026042982498), Apr 7, 2026: STRAP. CORRODED. AFT CARGO RT OTBD CEILING PROFILE CORRODED BS 1420 - 1440, REMOVED CORROSION ON CEILING PROFILE STABILIZATION STRAP AT BS1420, RBL 24.75 ON BOTH UPPER AND LOWER
- [SDR IPXA2026042384007](https://openairdocs.org/sdr/IPXA2026042384007), Apr 7, 2026: ANGLE. CORRODED. RH WTB FWD PANEL LANDING AT UPPER WING ROOT HAS SURFACE CORROSION.
- [SDR IPXA2026042383844](https://openairdocs.org/sdr/IPXA2026042383844), Apr 7, 2026: SUPPORT CHANNEL. CORRODED. AFT WTB LOWER FAIRING PANEL LANDING CHORD AT APPROX. STA. 1217 HAS EXFOLIATED CORROSION.
- [SDR IPXA2026042383814](https://openairdocs.org/sdr/IPXA2026042383814), Apr 7, 2026: TEE ANGLE. CORRODED. AFT WTB LOWER FAIRING PANEL LANDING CHORD AT STA. 1220 HAS EXFOLIATED CORROSION. REMOVED EXFOLIATED CHORD FROM AFT WTB LOWER FAIRING AREA AT STA 1220 BTW RBL 30
- [SDR IPXA2026042382439](https://openairdocs.org/sdr/IPXA2026042382439), Apr 7, 2026: TRANSITION PANEL. CORRODED. AFT CARGO RH OTBD TRANSITION PANEL CORRODED STA 1440-1500. REMOVED CORROSION AT RT BS 1440 ON TIE DOWN FITTING RBL 20R IAW 51-10-02-0G-0. INSTALLED NEW RT OTBD 
- [SDR IPXA2026042176560](https://openairdocs.org/sdr/IPXA2026042176560), Apr 7, 2026: STRAP. CORRODED. WHILE EVALUATING CORROSION AT APU INLET SURROUND STRUCTURE FOUND CORROSION AT APU INLET AFT STRAP AT STA 1825 BETWEEN STR 3R-6R. CORROSION FOUND ON MIDDLE STRAP
- [SDR IPXA2026042280199](https://openairdocs.org/sdr/IPXA2026042280199), Apr 7, 2026: SKIN. CORRODED. AFT CARGO DOOR INNER SKIN LOWER WEB CORRODED IN SEVERAL PLACES. REMOVED 36 E/A FASTENERS AND CORROSION ON AFT CARGO DOOR INNER SKIN LOWER WEB BETWEEN BS 1380-14
- [SDR IPXA2026041882776](https://openairdocs.org/sdr/IPXA2026041882776), Apr 7, 2026: TRANSITION PANEL. CORRODED. FWD CARGO RT OTBD TRANSITION HAS CORROSION STA 770-800.
- [SDR IPXA2026041782902](https://openairdocs.org/sdr/IPXA2026041782902), Apr 7, 2026: SIDEWALL SUPPORT. CORRODED. FWD CARGO LH LOWER SIDEWALL SUPPORT FRAME CORRODED STA 740.
- [SDR IPXA2026042865233](https://openairdocs.org/sdr/IPXA2026042865233), Apr 6, 2026: FLOORBEAM. CORRODED. MAJOR REPAIR, FWD CARGO CEILING MAIN CABIN FLOORBEAM UPPER FLANGE LOWER SURFACE EXFOLIATED RT OTBD SIDE BS 879, ACCOMPLISHED REPAIR IAW EO-97324-REQ1 AND EA 757
- [SDR IPXA2026042965161](https://openairdocs.org/sdr/IPXA2026042965161), Apr 6, 2026: CREASE BEAM. DAMAGED. FWD CARGO COMP RT LOWER CUSP FITTING BS 760 HAS TOOL MARKS. REMOVED FWD CARGO COMP RT LOWER AFT CUSP FITTING AT BS 760 IAW SRM 51-40-02-0G-0. LOCATED, DRILLED A
- [SDR IPXA2026042265976](https://openairdocs.org/sdr/IPXA2026042265976), Apr 6, 2026: ANGLE. CORRODED. AFT CARGO RT AFT BULKHEAD PANEL STA. 1640 SUPPORT FOUND CORROSION. AFTER FURTHER EVALUATION REPORTED CORROSION FOUND ON AFT CARGO R/H AFT UPPER BULKHEAD PANEL L
- [SDR IPXA2026042265216](https://openairdocs.org/sdr/IPXA2026042265216), Apr 6, 2026: TRANSITION PANEL. CORRODED. FWD CARGO RH OTBD TRANSITION PANEL CORRED AT STA 620 STR ATA 53-00 GM028. REMOVED CORROSION ON FWD CARGO RH OTBD TRANSITION PANEL AT STA 620, ORIGINIGINAL THICH
- [SDR IPXA2026042065233](https://openairdocs.org/sdr/IPXA2026042065233), Apr 6, 2026: FLOORBEAM. CORRODED. FWD CARGO CEILING MAIN CABIN FLOOR BEAM UPPER FLANGE LOWER SURFACE EXFOLIATED RH OTBD SIDE STA 879. FABRICATED REPAIR PARTS AS SHOWN IN FIG. 2, -1 ANGLE (2 EACH
- [SDR IPXA2026042153361](https://openairdocs.org/sdr/IPXA2026042153361), Apr 5, 2026: STRAP. CORRODED. APU INLET SURROUND STRUCTURE FWD STRAP O/B CORNER HAS CORROSION. REMOVED 1EA FWD STRAP, 1EA UPPER SUPPORT ANGLE, 1EA UPPER CORNER ANGLE, 1EA LOWER SUPPORT ANGLE
- [SDR IPXA2026050134931](https://openairdocs.org/sdr/IPXA2026050134931), Apr 4, 2026: RETAINER. CORRODED. APU COMPARTMENT FWD BULKHEAD STA 1885 HORZ STRIFFENER JUST BELOW LIGHT SWITCH ASSY HAS AREAS OF LITE CORROSION, BENT AND DOOR HOOK DAMAGED WITH SEVERAL SHEARED 
- [SDR IPXA2026043035211](https://openairdocs.org/sdr/IPXA2026043035211), Apr 4, 2026: BRACKET. CORRODED. APU COMPARTMENT FWD BULKHEAD STA 1885 CEILING WIRE HARNESS CLAMP SUPPORT BRACKETS 6 EACH UPPER AND LOWER SIDES HAVE LITE CORROSION AND MISSING PROTECTIVE FINISH
- [SDR IPXA2026041134931](https://openairdocs.org/sdr/IPXA2026041134931), Apr 4, 2026: STIFFENER. INOPERATIVE. APU COMPARTMENT FWD BULKHEAD STA 1885 HORZ STRIFFENER JUST BELOW LIGHT SWITCH ASSY HAS AREAS OF LITE CORROSION, BENT AND DOOR HOOK DAMAGED WITH SEVERAL SHEARED 
- [SDR IPXA2026042143555](https://openairdocs.org/sdr/IPXA2026042143555), Apr 4, 2026: CLAMP. CRACKED. FWD CARGO O2 BOTTLE RETAINER IS CRACKED AND TENSION STRAP IS SECURED CORRECTLY. REMOVED FWD CARGO CRACKED O2 BOTTLE RETAINER FRONT HALF ASSY IAW BOEING 757-200P
- [SDR IPXA2026042142345](https://openairdocs.org/sdr/IPXA2026042142345), Apr 4, 2026: ANGLE. CORRODED. AFT CARGO. CORROSION ON 2 EA NUT PLATES AND STIFFNER BTWN STA 1715 AND AFT PRESS BULHEAD. BTWN 12 RBL AND 24 RBL. 61. REMOVED 2EA STIFFENER AT AFT CARGO BTW STA
- [SDR IPXA2026042142289](https://openairdocs.org/sdr/IPXA2026042142289), Apr 4, 2026: ANGLE. CORRODED. AFT CARGO. CORROSION ON NUT PLATE AND STIFFNER. BTWN STA 1715 AND AFT PRESS. BULKHEAD BTWN. 33 RBL AND 39 RBL. 61. REMOVED 1EA STIFFENER AT AFT CARGO BTWN STA 1
- [SDR IPXA2026042142204](https://openairdocs.org/sdr/IPXA2026042142204), Apr 4, 2026: ANGLE. CORRODED. AFT CARGO. CORROSION ON NUT PLATE AND STIFFNER BTWN BS 1715 AND AFT PRESS. BULKHEAD 45LBL - 24.74 LBL 61. REMOVED DAMAGED NUTPLATE ASSY FROM STIFFNER PER B757-2
- [SDR IPXA2026041735211](https://openairdocs.org/sdr/IPXA2026041735211), Apr 4, 2026: SUPPORT BRACKET. CORRODED. APU COMPARTMENT FWD BULKHEAD STA 1885 CEILING WIRE HARNESS CLAMP SUPPORT BRACKETS 6 EACH UPPER AND LOWER SIDES HAVE LIGHT CORROSION AND MISSING PROTECTIVE FINIS
- [SDR IPXA2026042143284](https://openairdocs.org/sdr/IPXA2026042143284), Apr 4, 2026: DOUBLER. CORRODED. RT FWD LAV DUMP VALVE ADAPTER PLATE CORRODED. REMOVED PLATE FOR ACCESS FROM R/H FWD LAV DUMP VALVE ADAPTER REF. B757-200PF SRM 51-40-02-OG-0, UPON FURTHER EVALU
- [SDR IPXA2025112581036](https://openairdocs.org/sdr/IPXA2025112581036), Nov 15, 2025: FUEL SYS. LEAKING. FUEL CONFIG MSG. C/W QRH PROCEDURE. FUEL LEAK NOT SUSPECTED. L QTY 6.6 R QTY 8.4 TOT 15.0 FUEL USED L13.4 FUEL USED R 14.0 TOTALIZER 15.0 CALCULATED 14.8 FF L3.
- [SDR IPXA2025111971036](https://openairdocs.org/sdr/IPXA2025111971036), Nov 15, 2025: VALVE. FAULTED. FUEL CONFIG MSG. C/W QRH PROCEDURE. FUEL LEAK NOT SUSPECTED. L QTY 6.6 R QTY 8.4 TOT 15.0 FUEL USED L13.4 FUEL USED R 14.0 TOTALIZER 15.0 CALCULATED 14.8 FF L3.
- [SDR IPXA2025060974825](https://openairdocs.org/sdr/IPXA2025060974825), Jun 6, 2025: FUEL SYS. OUT OF BALANCE. **SUPPLEMENTAL SDR** FUEL STARTED L13.0 USED 7.2 = 5.8. LEFT GAUGE READS 5.4. FUEL STARTED R13.2 USED 7.7 = 5.5. RT GAUGE READS 6.2. FUEL IMBALANCE DID NOT AGRE

All 250: https://openairdocs.org/aircraft/N454UP/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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