# N457UP: 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: 25478
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 25, 1996
- Certificate issued: September 26, 1996
- Expires: May 31, 2028
- Mode S code: A58DED
- 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=457UP
- Page: https://openairdocs.org/aircraft/N457UP

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/N457UP/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 N457UP.

## FAA accident and incident reports

None matched to N457UP.

## Service difficulty reports (307, 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 IPXA2026102374753](https://openairdocs.org/sdr/IPXA2026102374753), Oct 22, 2026: GUARD. MISSING. CAPT AND FO EVAS SPLASH GUARD MISSING. INSTALLED ALL SPLASHGUARDS AS REQUIRED MM 25-69-00-200-801-C3
- [SDR IPXA2025102280275](https://openairdocs.org/sdr/IPXA2025102280275), Oct 15, 2025: RETAINER. CORRODED. CORROSION FOUND AT MAIN CARGO COMPARTMENT ANGLE RETAINER SUPPORT FROM BS 1610 - 1681.80, LBL 60. REMOVED CORRODED ANGLE RETAINER IAW SRM 51-40-02. INSTALLED ANG
- [SDR IPXA2025102162001](https://openairdocs.org/sdr/IPXA2025102162001), Oct 8, 2025: SUPPORT. CRACKED. RH PYLON PANEL 443KL SUPPORT STRUCTURE HAS (1EA) CRACK. REMOVED RH PYLON PANEL 443KL SUPPORT STRUCTURE IAW B757-200PF SRM 51-40-02. ++INSTALLED NWE SUPPORT AT R
- [SDR IPXA2025101787567](https://openairdocs.org/sdr/IPXA2025101787567), Oct 4, 2025: TIE CLIP. CORRODED. CORRODED STRUCTURE FOUND AT BS 680, AFT SIDE OF FLOOR FRAME AT RIGHT SIDE OUTBD SEAT TRACK AS SEEN FROM THE FWD LOWER CARGO PIT. REMOVED CLIP ON AT STA 680, AFT
- [SDR IPXA2025101571181](https://openairdocs.org/sdr/IPXA2025101571181), Oct 3, 2025: FLOOR SUPPORT. CORRODED. MAIN CABIN COMPARTMENT FLOOR STRUCTURE, BS 1720, LBL 25 HAS (1EA) PLATE EXFOLIATED. REMOVED PLATE 1 EA AT MAIN CABIN COMPARTMENT FLOOR STRUCTURE STA 1720 LBL 25
- [SDR IPXA2025102734451](https://openairdocs.org/sdr/IPXA2025102734451), Oct 1, 2025: FLOOR SUPPORT. CRACKED. MAIN CABIN COMPARTMENT BS 880-900, RBL 70, FLOOR SUPPORT CRACKED. ACCOMPLISHED REPAIR IAW EO-95420-REQ1 AND VT-MAE EA 757-5330-27-A4177.
- [SDR IPXA2025102339051](https://openairdocs.org/sdr/IPXA2025102339051), Oct 1, 2025: SHEAR WEB. CORRODED. MAIN CABIN COMPARTMENT STA 1180-1200 RBL 70-75 WEB HAS CORROSION. REMOVED MAIN CABIN COMPARTMENT STA 1180-1200 RBL 70-75 WEB IAW SRM 51-40-02. INSTALLED DOUBLER
- [SDR IPXA2025100941015](https://openairdocs.org/sdr/IPXA2025100941015), Oct 1, 2025: SUPPORT ANGLE. CORRODED. TAIL CONE BELOW APU EXHAUST DUCT, SUPPORT ANGLE HAS CORROSION. REMOVED CORRODED SUPPORT ANGLE AT ZONE.TAIL CONE BELOW APU EXHAUST DUCT IAW B757-200 SRM 51-40-02
- [SDR IPXA2025102887933](https://openairdocs.org/sdr/IPXA2025102887933), Sep 28, 2025: FLOORBEAM. CORRODED. MAJOR REPAIR - MDC, BS 1680, FLOOR STR HAS EVIDENCE OF CORROSION AROUND 3EA SCREW HOLES, BTW BL0 AND LBL 24.75. PERMANENT REPAIR ACCOMPLISHED IAW UPS EO: EO-954
- [SDR IPXA2025100979085](https://openairdocs.org/sdr/IPXA2025100979085), Sep 28, 2025: SKIN. DELAMINATED. TAIL CONE STA1963-1992 BOTTOM SKIN INTERNAL BELOW THE APU EXHAUST MANIFOLD CORRODED/DELAMINATED. REMOVED SKIN BELOW APU EXHAUST MANIFOLD IAW SRM 51-40-02. INSTA
- [SDR IPXA2025102273248](https://openairdocs.org/sdr/IPXA2025102273248), Sep 27, 2025: FRAME. DENTED. FAULT Z-100 STR: FWD CARGO COMPARTMENT AT STA 820 R/H BETWEEN STR 23 TO STR 24 FRAME HAS A DENT. INSTALLED PANEL 122KW IAW B757-200 AMM 25-50-02 404-006. ACCOMP
- [SDR IPXA2025102977740](https://openairdocs.org/sdr/IPXA2025102977740), Sep 27, 2025: SKIN. CRACKED. NR 2 ENG OUTBD T/R AFT OF SECOND FROM TOP BLOCKER DOOR HAS A CRACK AT PERFORATED SKIN AREA. WORK ACCOMPLISHED PER UPS EO: EO-95442-REQ1 AND VT MAE EA 757-7831-2
- [SDR IPXA2025102176477](https://openairdocs.org/sdr/IPXA2025102176477), Sep 27, 2025: CREASE BEAM. CORRODED. MAIN CABIN UPPER FLIGHT DECK STA 320 AT LBL 62.225 INNER CHORD HAS A SEVERE CORROSION. ACCOMPLISHED PER UPS EO-95416-REQ 1 AND VT MAE 757-5310-27-A4172 REV- .
- [SDR IPXA2025101373232](https://openairdocs.org/sdr/IPXA2025101373232), Sep 27, 2025: FLOORBEAM. CORRODED. MAIN CARGO COMPARTMENT FLOORBEAM STA 1200 RBL 45-60 LOWER SURFACE HAS CORROSION AT NUTPLATE. INSTALLED REPAIR PARTS IAW SRM 51-40-02. ACCOMPLISH PERMANENT REPAI
- [SDR IPXA2025102168027](https://openairdocs.org/sdr/IPXA2025102168027), Sep 27, 2025: DOOR FRAME. DAMAGED. CREW ENTRY DOOR FRAME UPPER FWD ROLLER GUIDE FITTING HAS DEEP SCRATCH/GOUGE. CREW ENTRY DOOR LATCH REWORKED PER SREO-14721-REQ001.
- [SDR IPXA2025101372331](https://openairdocs.org/sdr/IPXA2025101372331), Sep 27, 2025: FLOORBEAM. CORRODED. MAIN CARGO COMPARTMENT FLOORBEAM STA 1100 RBL 25-45 HAS (4EA) AREAS WITH CORROSION. DOT 28-712. REMOVED CORROSION ON 4 AREAS IAW SRM 51-10-02. ACCOMPLISHED A DV
- [SDR IPXA2025100972261](https://openairdocs.org/sdr/IPXA2025100972261), Sep 27, 2025: FLOORBEAM. CORRODED. MAIN CARGO COMPARTMENT FLOOR BEAM STA 1100 LBL 25-45 HAS (4EA) AREAS WITH CORROSION. REMOVED CORROSION ON 4 AREAS IAW SRM 51-10-02. ACCOMPLISHED A DVI IAW SRM 5
- [SDR IPXA2025100972265](https://openairdocs.org/sdr/IPXA2025100972265), Sep 27, 2025: FLOORBEAM. CORRODED. MAIN CARGO COMPARTMENT FLOORBEAM BS 1100 LBL 0-25 HAS (3EA) AREAS WITH CORROSION. REMOVED CORROSION ON 4 AREAS IAW SRM 51-10-02. ACCOMPLISHED A DVI IAW SRM 51-1
- [SDR IPXA2025100972378](https://openairdocs.org/sdr/IPXA2025100972378), Sep 27, 2025: FLOORBEAM. CORRODED. MAIN CARGO COMPARTMENT FLOOR BEAM STA 1100 RBL 0-25 HAS (2EA) AREAS WITH CORROSION. REMOVED CORROSION ON 2 AREAS IAW SRM 51-10-02. ACCOMPLISHED A DVI IAW SRM 51
- [SDR IPXA2025100972465](https://openairdocs.org/sdr/IPXA2025100972465), Sep 27, 2025: FLOORBEAM. CORRODED. MAIN CARGO COMPARTMENT FLOORBEAM BS 1100, RBL 45-60 HAS (1EA) AREA WITH CORROSION. REMOVED CORROSION ON 1 AREA IAW SRM 51-10-02. ACCOMPLISHED A DVI IAW SRM 51-1
- [SDR IPXA2025100665445](https://openairdocs.org/sdr/IPXA2025100665445), Sep 27, 2025: SUPPORT BRACKET. CORRODED. ACCESS DOOR 313AL LH AND RH LATCH STOPS AT THE CUT-OUT 4EA SUPPORT BRACKETS ARE CORRODED. REMOVED 2EA SUPPORTS AND 4 ANGLES IN ACCESS DOOR 313AL I.A.W. B757-200
- [SDR IPXA2025092968027](https://openairdocs.org/sdr/IPXA2025092968027), Sep 27, 2025: FITTING. GOUGED. CREW ENTRY DOOR FRAME UPPER FWD ROLLER GUIDE FITTING HAS DEEP SCRATCH/GOUGE.
- [SDR IPXA2025102158712](https://openairdocs.org/sdr/IPXA2025102158712), Sep 26, 2025: CAM. DAMAGED. CREW ENTRY DOOR UPPER CAM LATCH HAS A GOUGE. CREW ENTRY DOOR LATCH REWORKED PER SREO-14721-REQ001.
- [SDR IPXA2025102158881](https://openairdocs.org/sdr/IPXA2025102158881), Sep 26, 2025: CAM. DAMAGED. CREW ENTRY DOOR LOWER CAM LATCH HAS A GOUGE. CREW ENTRY DOOR LATCH REWORKED PER SREO-14721-REQ001.
- [SDR IPXA2025100857008](https://openairdocs.org/sdr/IPXA2025100857008), Sep 26, 2025: SKIN. DAMAGED. RIGHT EXTERNAL UPPER FUSELAGE, STA 700-720 BETWEEN STR 6R-7R HAS (1EA) HOLE CAUSED BY LIGHTNING STRIKE AT SKIN PREVIOUS REPAIR. REMOVED 1 EA RIVET AT RH EXTERNA
- [SDR IPXA2025101463121](https://openairdocs.org/sdr/IPXA2025101463121), Sep 26, 2025: TEE ANGLE. CORRODED. RIGHT MIDDLE LOWER FUSELAGE STA 900 RBL 25 TEE CHORD HAS CORROSION. REMOVED THE DAMAGED PORTION OF THE TEE CHORD IAW SRM 51-70-12-0G-0. INSTALLED ALL REPAIR PAR
- [SDR IPXA2025100955989](https://openairdocs.org/sdr/IPXA2025100955989), Sep 26, 2025: SKIN. DAMAGED. EXTERIOR RT FUSELAGE STA 1320-1340, BETWEEN STR 7R-8R HAS (1EA) HOLE AT SKIN CAUSED BY LIGHTNING STRIKE. EVALUATED DAMAGE: ORIGINAL TICKNESS: 0.045 IN, 100% MAT
- [SDR IPXA2025100857342](https://openairdocs.org/sdr/IPXA2025100857342), Sep 26, 2025: SKIN. DAMAGED. RIGHT EXTERNAL UPPER FUSELAGE, STA 540-560 BETWEEN STR 7R-8R HAS (1EA) HOLE CAUSED BY LIGHTNING STRIKE AT SKIN.PERFORMED HFEC SURFACE INSPECTION ON EXTERNAL SKI
- [SDR IPXA2025092908881](https://openairdocs.org/sdr/IPXA2025092908881), Sep 26, 2025: LATCH. GOUGED. CREW ENTRY DOOR LOWER CAM LATCH HAS A GOUGE APPROVED.
- [SDR IPXA2055092908712](https://openairdocs.org/sdr/IPXA2055092908712), Sep 26, 2025: LATCH. GOUGED. CREW ENTRY DOOR UPPER CAM LATCH HAS A GOUGE APPROVED.
- [SDR IPXA2024020896523](https://openairdocs.org/sdr/IPXA2024020896523), Jan 16, 2024: TRANSITION PANEL. CORRODED. *SUPPLEMENTAL SDR* FAULT: AFT CARGO COMPT, R/H SIDE PANELS, BETWEEN STA 1380 TO STA 1440, FOUND EXFOLIATED CORROSION. INSTALLED SIDE PANEL IAW SRM 51-40-02-0G-0
- [SDR IPXA2024012446523](https://openairdocs.org/sdr/IPXA2024012446523), Jan 16, 2024: PANEL. CORRODED. **SDR FILED OPEN**FAULT: AFT CARGO COMPT, R/H SIDE PANELS, BETWEEN STA 1380 TO STA 1440, FOUND EXFOLIATED CORROSION. REVIEWED.
- [SDR IPXA2024012943372](https://openairdocs.org/sdr/IPXA2024012943372), Jan 15, 2024: TRANSITION PANEL. CORRODED. *SUPPLEMENTAL SDR* FAULT: AFT CARGO COMPT, R/H TRANSITION PANEL, BETWEEN STA 1440 TO STA 1520, FOUND EXFOLIATED CORROSION. INSTALLED DOUBLER (06) AND INSTALLED 
- [SDR IPXA2024012443372](https://openairdocs.org/sdr/IPXA2024012443372), Jan 15, 2024: TRANSITION PANEL. CORRODED. **SDR FILED OPEN**FAULT: AFT CARGO COMPT, R/H TRANSITION PANEL, BETWEEN STA 1440 TO STA 1520, FOUND EXFOLIATED CORROSION. REF STEP 20 AND 21. INSPECTED AND VERI
- [SDR IPXA2024020844456](https://openairdocs.org/sdr/IPXA2024020844456), Jan 9, 2024: SUPPORT BRACKET. CRACKED. FAULT - AFT CARGO PIT SIDE LH FR 1540 UNDER PANEL 161AW, BRAKET SUPPORT AIR CONDITION DUCT BOTH SIDE CRACKED. INSTALLED BRACKETS-APU DUCT SUPPORT WITH P/N BACB3
- [SDR IPXA2024020844406](https://openairdocs.org/sdr/IPXA2024020844406), Jan 9, 2024: PANEL. CRACKED. FAULT - AFFT CARGO PIT FWD BULKHEAD AIR CONDITION DUCT WITH CRACKED UNDER PANEL 151BZ. REPAIRED AIR CONDITION DUCT WHITH CRACKED IAW 757-AMM, TASK 21-23-01-308-
- [SDR IPXA2024011053278](https://openairdocs.org/sdr/IPXA2024011053278), Jan 9, 2024: UNKNOWN. UNKNOWN. PROTRUDING DENT AFT OF FRAME STA 1460 R.H SIDE NEAR STRINGER 17R. DOT 142-99
- [SDR IPXA202401104406](https://openairdocs.org/sdr/IPXA202401104406), Jan 9, 2024: UNKNOWN. UNKNOWN. AFT CARGO PIT FWD BULKHEAD AIR CONDITION DUCT WITH CRACKED UNDER PANEL 151BZ APPROVED.
- [SDR IPXA202401104456](https://openairdocs.org/sdr/IPXA202401104456), Jan 9, 2024: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - AFT CARGO PIT SIDE LH FR 1540 UNDER PANEL 161AW, BRAKET SUPPORT AIR CONDITION DUCT BOTH SIDE CRACKED. APPROVED.
- [SDR IPXA2024010803867](https://openairdocs.org/sdr/IPXA2024010803867), Jan 6, 2024: UNKNOWN. UNKNOWN. R/H HORIZONTAL STABILIZER UPPER SURFACE HAS MULTIPLE DENTS. APPROVED
- [SDR IPXA2024021679317](https://openairdocs.org/sdr/IPXA2024021679317), Jan 4, 2024: SKIN. CORRODED. NR 2 PYLON INBD SKIN, INNER SKIN FWD OF PANEL# 443HL OPENING HAS CORROSION. DOT 8-003. APPLIED TREAT AND PRIMER I.A.W SRM 51-20-01, PRIMER MIXED IN CUP P/N 02-0
- [SDR IPXA2024021679125](https://openairdocs.org/sdr/IPXA2024021679125), Jan 4, 2024: SEAL. DETERIORATED. CREW INNER DOOR SEAL DETERIORATING TOP. SEAL FOR CREW INNER DOOR REPLACED IN TASK CARD NUMBER T3F18E003P9EP. INSTALLED NEW CREW DOOR SEAL IAW AMM 52-09-02-404-0
- [SDR IPXA2024021679020](https://openairdocs.org/sdr/IPXA2024021679020), Jan 4, 2024: SEAL. TORN. CREW ENTRANCE DOOR SEAL TORN OUTER SEAL. INSTALLED NEW CREW DOOR SEAL IAW AMM 52-09-02-404-004. C/W.
- [SDR IPXA2024013079249](https://openairdocs.org/sdr/IPXA2024013079249), Jan 4, 2024: SKIN. CORRODED. NR 2 PYLON INBD SKIN, INNER SKIN FWD OF PANEL# 443JL HAS CORROSION. DOT 8-002. INSTALLED FILLER AND DOUBLER I.A.W. S.R.M. 51-40-02-OG AND EA 757-5450-27-A3485 S
- [SDR IPXA2024021679612](https://openairdocs.org/sdr/IPXA2024021679612), Jan 4, 2024: SKIN. CORRODED. NR 1 PYLON OUTBD SKIN, INNER SKIN FWD OF PANEL 433BL OPENING, HAS A LITTLE SPOT OF CORROSION. DOT 8-009. APPLIED PROTECTIVE TREATMENT, INNER SKIN FWD OF PANEL 4
- [SDR IPXA2024013079006](https://openairdocs.org/sdr/IPXA2024013079006), Jan 4, 2024: SKIN. CORRODED. MAJOR REPAIR. NR 2 OUTBD PYLON, INNER SKIN FWD OF PANEL #443CR OPNENING HAS EXFOLITATION CORROSION. DOT 8-001, PLACED ON THE OUTSIDE. JOB WAS ACCOMPLISHED IAW U
- [SDR IPXA2024013079351](https://openairdocs.org/sdr/IPXA2024013079351), Jan 4, 2024: SKIN. CORRODED. *SUPPLEMENTAL SDR* FAULT- #2 PYLON INBD FWD HINGE PANEL 443GL , INNER FRAME STRUCTURE HAS EXFOLITATION CORROSION. DOT 8-004. JOB ACCOMPLISHED PER UPS EO: EO-892
- [SDR IPXA2024020979580](https://openairdocs.org/sdr/IPXA2024020979580), Jan 4, 2024: DOUBLER. CORRODED. MAJOR REPAIR* FAULT- #1 PYLON OUTBD SKIN, INNER SKIN AFT OF PANEL#433BL OPENING, HAS EXFOLITATION CORROSION. DOT 8-008. JOB WAS ACCOMPLISHED PER UPS EO: EO-8922
- [SDR IPXA2024020979528](https://openairdocs.org/sdr/IPXA2024020979528), Jan 4, 2024: SKIN. CORRODED. NR 1 PYLON INBD SKIN, INNER SKIN FWD OF PANEL#433HR OPENING HAS CORROSION. DOT 8-007. REMOVED DAMAGE, IAW SRM 51-10-02, MATERIAL REMOVED 0.004, ORIGINAL MATERIA
- [SDR IPXA2024013079451](https://openairdocs.org/sdr/IPXA2024013079451), Jan 4, 2024: DOUBLER. CORRODED. *SUPPLEMENTAL SDR* *MAJOR REPAIR* FAULT- #1 PYLON INBD SKIN, INNER SKIN AFT OF PANEL# 433HR OPENING HAS EXFOLIATION CORROSION. DOT 8-004. JOB WAS ACCOMPLISHED P

All 307: https://openairdocs.org/aircraft/N457UP/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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