# N446UP: 1994 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: 27735
- Year built: 1994
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 2, 1994
- Certificate issued: January 31, 2026
- Expires: January 31, 2033
- Mode S code: A562B7
- 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=446UP
- Page: https://openairdocs.org/aircraft/N446UP

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/N446UP/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 N446UP.

## FAA accident and incident reports

None matched to N446UP.

## Service difficulty reports (184, 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 IPXA2026101326102](https://openairdocs.org/sdr/IPXA2026101326102), Oct 13, 2026: SMOKE GOGGLES. DETERIORATED. SECOND OBSERVERS SMOKE GOGGLES HAVE DETERIORATED FOAM SEAL. REMOVED AND REPLACED SECOND OBSERVERS SMOKE GOGGLES IAW AMM 25-64-00.
- [SDR IPXA2025032415186](https://openairdocs.org/sdr/IPXA2025032415186), Mar 17, 2026: UNKNOWN. ODOR. ON DEPARTURE, MAX PWR T/O , STRONG SMELL OF €ŒDIRTY SOCKS? ON FLT DECK. PERSISTED UNTILL LEVEL OFF AT FL 360. RIGHT ENGINE WAS R+R TO CORRECT STRONG ODOR OF DI
- [SDR IPXA2026031815186](https://openairdocs.org/sdr/IPXA2026031815186), Mar 17, 2026: UNKNOWN. ODOR. ON DEPARTURE, MAX PWR T/O , STRONG SMELL OF DIRTY SOCKS ON FLT DECK. PERSISTED UNTILL LEVEL OFF@ FL 360. REF FIM 21-00 TASK SUPPORT. REFERENCE: 21-00-01/301 ISO
- [SDR IPXA2026011613640](https://openairdocs.org/sdr/IPXA2026011613640), Jan 15, 2026: UNKNOWN. ODOR. AT APPLICATION OF TAKEOFF POWER AND DURING CLIMB-OUT, THE STRONG ODOR OF DIRTY WET SOCK EXISTED. THE SMELL LESSENED A BIT DURING CRUISE BUT WAS STILL NOTABLY PR
- [SDR IPXA2026011513640](https://openairdocs.org/sdr/IPXA2026011513640), Jan 15, 2026: UNKNOWN. ODOR. AT APPLICATION OF TAKEOFF POWER AND DURING CLIMB-OUT, THE STRONG ODOR OF DIRTY WET SOCK EXISTED. THE SMELL LESSENED A BIT DURING CRUISE BUT WAS STILL NOTABLY PR
- [SDR IPXA2025021215360](https://openairdocs.org/sdr/IPXA2025021215360), Feb 6, 2025: FUEL SYS. OUT OF BALANCE. IN FLIGHT FUEL IMBALANCE OF 2KLBS DEVELOPED WITH RIGHT SIDE LESS. WE BALANCED IT. 1HR LATER DURING ARRIVAL RIGHT SIDE WAS 1KLBS LESS THEN THE LEFT AGAIN ON SHOR
- [SDR IPXA2025020715360](https://openairdocs.org/sdr/IPXA2025020715360), Feb 6, 2025: FUEL SYS. OUT OF BALANCE. IN FLIGHT FUEL IMBALANCE OF 2KLBS DEVELOPED WITH RIGHT SIDE LESS. WE BALANCED IT. 1HR LATER DURING ARRIVAL RIGHT SIDE WAS 1KLBS LESS THEN THE LEFT AGAIN ON SHOR
- [SDR IPXA2024122093310](https://openairdocs.org/sdr/IPXA2024122093310), Dec 19, 2024: ANTI-ICE VALVE. FAULTED. **EMERGENCY DECLARED**AFTER TAKE OFF ,STATUS MESSAGE R ENG TAI VALVE CAME ON AND STAYED ON VERIFIED DMP IS C/W PER MEL 30-21-1-1
- [SDR IPXA2024102974638](https://openairdocs.org/sdr/IPXA2024102974638), Oct 17, 2024: ANGLE. CORRODED. UPON OK TO INSTALL FOUND LH ELEVATOR O/B BONDING JUMPER ATTACHMENT POINT TO HAVE EXFOLIATED CORROSION ON HORIZONTAL STAB. DOT 142-501. INSTALLED NEW L/H ELEVATO
- [SDR IPXA2024101981219](https://openairdocs.org/sdr/IPXA2024101981219), Oct 5, 2024: STRINGER SPLICE. CORRODED. HEAVY CORROSION FOUND AT STR 20LH PRODUCTION SPLICE, BETWEEN STA 1620 TO STA 1640. INSTALLED STRINGER CLIP AND NEW PRODUCTION SPLICE USING FASTENER PN: BACR15FV
- [SDR IPXA2024101574000](https://openairdocs.org/sdr/IPXA2024101574000), Oct 5, 2024: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL 242 XBF LOWER SURFACE PROTECTION MATERIAL SHOWS A BLOWN SPOT. DOT 75-014 HA-75. FABRICATED MCD FLOOR PANEL 242 XBF P/N:144N5361-19 USING M
- [SDR IPXA2024102941447](https://openairdocs.org/sdr/IPXA2024102941447), Oct 3, 2024: SKIN. CORRODED. RH ELEVATOR TIP, LOWER SURFACE SKIN HAS CORROSION. DOT 28-02. FABRICATED NEW SPLICE PLATE I.A.W. SRM 55-20-01-OI-1, DETAIL 1. MATERIAL: P/N 6061-T4.025B, BTCH# 
- [SDR IPXA2023122069443](https://openairdocs.org/sdr/IPXA2023122069443), Dec 17, 2023: FUEL TANK. OUT OF BALANCE. DEVELOPED 1.4K FUEL IMBALANCE. T/O PLUS 45 MINUTES LEFT MAIN 1.4K HEAVIER THAN RIGHT MAIN. ACCOMPLISHED FUEL MIGRATION CHECK FROM RIGHT MAIN TANK TO CENTER MAIN
- [SDR IPXA2023121869443](https://openairdocs.org/sdr/IPXA2023121869443), Dec 17, 2023: UNKNOWN. UNKNOWN. DEVELOPED 1.4K FUEL IMBALANCE. T/O PLUS 45 MINUTES LEFT MAIN 1.4K HEAVIER THAN RIGHT MAIN.
- [SDR IPXA2023011789993](https://openairdocs.org/sdr/IPXA2023011789993), Jan 16, 2023: FUEL CELL. UNKNOWN. INFLIGHT DIVERSION TO STL DUE TO INDICATIONS OF FUEL LEAK IN RT TANK. ONCE CTR FUEL USED THE RT FUEL TANK TOTAL SLIGHTLY DECREASED AT A GREATER RATE THAN THE LT
- [SDR IPXA2022111788188](https://openairdocs.org/sdr/IPXA2022111788188), Nov 16, 2022: A/C PACK. ODOR. WHEN RIGHT PACK OPERATED STRONG WET DOG SMELL IN FLIGHT DECKOPERATD RIGHT AND LEFT PACK COULD NOT DUPLICATE SMELL. NO DEFECTS NOTED. PER AMM 21-00-00-862-001
- [SDR IPXA2022101987246](https://openairdocs.org/sdr/IPXA2022101987246), Oct 16, 2022: DOOR. INOPERATIVE. INSPECTION TYPE:N/A**ATB**CAUTION "RUDDER RATIO" AFTER T/O PASSING 1500' REQUIRED ATBRH RRCM SHOWS HARD CVDT FAULT. OPEN VERT STAB TE PANELS AS REQUIRED. REPLAC
- [SDR IPXA2022101087030](https://openairdocs.org/sdr/IPXA2022101087030), Sep 27, 2022: FRAME. DENTED. INSPECTION TYPE:SEG3FWD CARGO FRAME AT STA 740, BETWEEN S-24R AND S-25R HAS A DENTREPAIRED IAW SRM 53-00-07-2R-5 DETAIL III AND RCD 287458
- [SDR IPXA2022101187052](https://openairdocs.org/sdr/IPXA2022101187052), Sep 26, 2022: FRAME. DENTED. INSPECTION TYPE:SEG3FRAME 1360 ON THE R/H SIDE HAS A DENT ON TOP OF THE FLANGE BY S26RACCOMPLISHED REPAIR PER 757-200PF SRM REV 115.0 CHAPTER 53-00-07-2R-5 DETA
- [SDR IPXA2022101287074](https://openairdocs.org/sdr/IPXA2022101287074), Sep 24, 2022: DOUBLER. CORRODED. INSPECTION TYPE:SEG3#2 PYLON O/B AFT SKIN, INTERNAL DOUBLER HAS CORROSION BETWEEN PP STA 144-425 AN 153.90 THAT WAS FOUND TO BE OUT OF LIMITSREPAIRED IAW UPS EO
- [SDR IPXA2022101187063](https://openairdocs.org/sdr/IPXA2022101187063), Sep 24, 2022: DOUBLER. CORRODED. INSPECTION TYPE:SEG3#2 PYLON IB AFT SKIN INTERNAL DOUBLER HAS CORROSION BETWEEN PP STA 153.960 - PP STA 163.10ACCOMPLISHED REPAIR PER UPS EO B757-5430-84941-A A
- [SDR IPXA2022100686899](https://openairdocs.org/sdr/IPXA2022100686899), Sep 23, 2022: NONE. NONE. INSPECTION TYPE:SEG3DURING INSPECTION PER EO B757-5310-73926-A FOUND AN EXISTING REPAIR AT STA 1320 S26R-S25RACCOMPLISHED PER EO B757-5310-84517-A AND VT MAE EA
- [SDR IPXA2022100586872](https://openairdocs.org/sdr/IPXA2022100586872), Sep 23, 2022: PANEL. DELAMINATED. INSPECTION TYPE:SEG3R/H VERT. STAB. LWR FWD TORQUE BOX PANEL HAS 1 EA. AREA OF DELAMINATION/DISBOND.REPAIRED PANEL IAW B757 SRM 51-70-10-2R-4, PER SRM 55-30-01-
- [SDR IPXA2022100486840](https://openairdocs.org/sdr/IPXA2022100486840), Sep 23, 2022: NONE. NONE. INSPECTION TYPE:SEG3DURING INSPECTION PER EO B757-5310-73926-A FOUND AN EXISTING REPAIR AT STA 1280 S26R-S25RACCOMPLISHED ALTERNATE INSPECTION PER UPS EO B757-5
- [SDR IPXA2021111976143](https://openairdocs.org/sdr/IPXA2021111976143), Nov 18, 2021: NONE. NONE. INSPECTION TYPE:N/A*DIVERSION*NO EMERGENCY DECLARED*LANDED WITHOUT INCIDENT* NO POSSIBLE FUEL MIGRATION FROM R FUEL TANK TO L MAIN FUEL TANK. AFTER CENTER TANK 
- [SDR IPXA2021110375571](https://openairdocs.org/sdr/IPXA2021110375571), Nov 2, 2021: NONE. NONE. INSPECTION TYPE:N/A**DIVERSION - EMERGENCY DECLARED** - CENTER HYDRAULIC QUANTITY LOW LIGHT MSG. RAN CHECKLISTR&R C HYD QUANTITY TRANSMITTER PER AMM 29-33-01. O
- [SDR IPXA2021071371648](https://openairdocs.org/sdr/IPXA2021071371648), Jul 13, 2021: EVAS UNIT. INOPERATIVE. CAPT'S L/H EVAS, COCKPIT SMOKE VISION SYSTEM , INOP. DEFERRED CAPT'S EVAS IAW MEL 25-60-01, DMP C/W, PLACARD INSTALLED,PARTS ORDERED ON REQ# 359345, A/C OK TO C
- [SDR IPXA2021022265932](https://openairdocs.org/sdr/IPXA2021022265932), Feb 22, 2021: SKIN. DENTED. INSPECTION TYPE: SEG 2 FUSELAGE SKIN AT STA 500-530 STR 19L-20L HAS INCOMING DENT DAMAGE. REPAIRED PER EA 757-5330-27-A2548 REV-.
- [SDR IPXA2020123063969](https://openairdocs.org/sdr/IPXA2020123063969), Dec 29, 2020: FLAP SYSTEM. MALFUNCTIONED. INSPECTION TYPE: N/A EMERGENCY DECLARED. FLIGHT LANDED UNEVENTFUL, FAA NOTIFIED. WHEN SELECTING FLAPS 20, TRAILING EDGE FLAP DISAGREE EICAS & LIGHT ILLUMINATED 
- [SDR IPXA2020090960035](https://openairdocs.org/sdr/IPXA2020090960035), Sep 8, 2020: WARNING MESSAGE. ILLUMINATED. INSPECTION TYPE: SDR FILED OPEN, EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. EMERGENCY TRUCKS WERE WAITING DURING LANDING, UPON SELECTION OF FLAPS 20 EICAS TE 
- [SDR IPXA2019060762897](https://openairdocs.org/sdr/IPXA2019060762897), Jun 4, 2019: FMC. INOPERATIVE. ATB - LEFT FMC FAIL.R/R LEFT FMC PER AMM 34-61-01/401.
- [SDR IPXA2019041214962](https://openairdocs.org/sdr/IPXA2019041214962), Apr 11, 2019: BULB. INOPERATIVE. EMERGENCY LIGHT HAS THREE INOP BULBS.R&R THREE BULBS IN EMERGENCY LIGHT PEN AMM 33-51-01-2.
- [SDR IPXA2018060630358](https://openairdocs.org/sdr/IPXA2018060630358), Jun 3, 2018: TRANSCEIVER. FAILED. WEATHER RADAR FAILED. AIR TURNBACK, PERFORMED WX RADAR BITE PROCEDURE IAW FIM 34-43-00. R & R THE WEATHER RADAR TRANSCIEVER IAW AMM 34-43-01, OPS CHECKED GOOD.
- [SDR IPXA2018040528232](https://openairdocs.org/sdr/IPXA2018040528232), Apr 4, 2018: UNKNOWN. ODOR. STRONG DIRTY SOCK ODOR FROM RIGHT PACK, OPERATED THE RIGHT PACK FOR 30 MINUTES IAW MM 21-00-00-862-001. COULD NOT DUPLICATE THE ODOR. OKAY TO CONTINUE FLIGHT.
- [SDR IPXA2017060117779](https://openairdocs.org/sdr/IPXA2017060117779), Jun 1, 2017: SMOKE GOGGLES. CRACKED. COURIER SMOKE GOGGLES CRACKED. REPLACED THE SMOKE GOGGLES.
- [SDR IPXA2017060117756](https://openairdocs.org/sdr/IPXA2017060117756), May 17, 2017: FLOOR SUPPORT. DENTED. INSPECTION TYPE: C-12, AFT CARGO, RT SIDE BY UPPER DOOR SILL, RT OTBD FLOOR SUPPORT IS DENTED ON THE TOP FLANGE. REPAIRED IAW SRM 53-00-53-2R.
- [SDR IPXA2017040515826](https://openairdocs.org/sdr/IPXA2017040515826), Apr 4, 2017: LAMP. INOPERATIVE. EMERGENCY LIGHT ASSY HAS FOUR INOPERATIVE LAMPS. REPLACED THE LAMPS IAW AMM 33-51-01-2.
- [SDR IPXA2017030914909](https://openairdocs.org/sdr/IPXA2017030914909), Mar 8, 2017: WARNING LIGHT. FALSE ACTIVATION. PRIOR TO DEPARTURE AND ENGINE START, AN EICAS MESSAGE FOR THE LT FWD ENTRY DOOR AND ASSOCIATED OVERHEAD LIGHT ON. CYCLED THE DOOR SEVERAL TIMES, LIGHT WENT OUT.
- [SDR IPXA2017030614801](https://openairdocs.org/sdr/IPXA2017030614801), Mar 2, 2017: INDICATION SYS. MISMATCHED. WITH TROTTLES MATCHED LT EPR 1.40 & RT EPR 1.16. REST OF ENGINE GAUGES SAME. PERFORMED ENGINE RUN IAW MM 71-00-00, INDICATIONS GOOD, NO DEFECTS NOTED
- [SDR IPXA2017030114558](https://openairdocs.org/sdr/IPXA2017030114558), Feb 15, 2017: SUPPORT. CORRODED. INSPECTION TYPE: C12, FORWARD CARGO COMPARTMENT DOOR TEE SUPPORT CORRODEDREPLACED TEE SUPPORT.
- [SDR IPXA2015031987187](https://openairdocs.org/sdr/IPXA2015031987187), Mar 13, 2015: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:C, MCD FLOOR PANEL 231 XCF DELAMINATED, FABRICATED NEW FLOOR PANEL 231 XCF IAW SAMPLE IAW EO B757-5320-9692-H, MATERIAL A402H-48X144 BATCH 26645
- [SDR IPXA2015031386955](https://openairdocs.org/sdr/IPXA2015031386955), Mar 12, 2015: SKIN. CRACKED. INSPECTION TYPE:CRT, WING SLAT NR 9 INBD TRACK ON THE INBD COVE SKIN PANEL HAVE CRACKS. REMOVED AND INSTALLED NEW FABRICATED SKIN, COVE, PANEL IAW DWG 114N4003-
- [SDR IPXA2015031687077](https://openairdocs.org/sdr/IPXA2015031687077), Mar 5, 2015: FLOORBOARD. BROKEN. INSPECTION TYPE:C, MAIN DECK FLOORBOARD 251XFF BROKEN. 122-041, FABRICATED PANEL 251XFF, IAW SREO B757-5320-9692-H.
- [SDR IPXA2015031687062](https://openairdocs.org/sdr/IPXA2015031687062), Mar 5, 2015: FLOORBOARD. DELAMINATED. INSPECTION TYPE:C, MAIN DECK FLOORBOARD, 232XWF, DELAMINATED. 122-048, FABRICATED PANEL IAW SREO B757-5320-9692-H.
- [SDR IPXA2015031687061](https://openairdocs.org/sdr/IPXA2015031687061), Mar 5, 2015: FLOORBOARD. DELAMINATED. INSPECTION TYPE:C, PANEL RACK MAIN DECK FLOORBOARD 241XFF, DELAMINATED, 122-052. FABRICATED PANEL IAW SREO B757-5320-9692-H. 2.
- [SDR IPXA2015031687080](https://openairdocs.org/sdr/IPXA2015031687080), Mar 5, 2015: FLOORBOARD. DELAMINATED. INSPECTION TYPE:C, MAIN DECK FLOORBOARD 232XSF DELAMINATED. FABRICATED A NEW FLOORBOARD IAW SREO B757-5320-9692-H.
- [SDR IPXA2015031687084](https://openairdocs.org/sdr/IPXA2015031687084), Mar 5, 2015: FLOORBOARD. DAMAGED. INSPECTION TYPE:C, MAIN DECK FLOORBOARD 251XJF, HAS EDGE DAMAGE, FABRICATED A NEW FLOORBOARD IAW SREO B757-5320-9692-H.
- [SDR IPXA2015031687082](https://openairdocs.org/sdr/IPXA2015031687082), Mar 5, 2015: FLOORBOARD. DELAMINATED. INSPECTION TYPE:C, MAIN DECK FLOORBOARD, 231XWF, DELAMINATED. FABRICATED A NEW FLOORBOARD IAW SREO B757-5320-9692-H.
- [SDR IPXA2015031787139](https://openairdocs.org/sdr/IPXA2015031787139), Mar 5, 2015: FLOORBOARD. DAMAGED. INSPECTION TYPE:C, MAIN DECK FLOORBOARD 242XJF HAS EDGE DAMAGE, 122-046, FABBED PANEL 242XJF, PN 144N5361-55 FROM A402H-48X144, BATTERY, 2664589, IAW SREO B757-
- [SDR IPXA2015031787138](https://openairdocs.org/sdr/IPXA2015031787138), Mar 5, 2015: FLOORBOARD. DELAMINATED. INSPECTION TYPE:C, MAIN DECK FLOORBOARD 241XCF DELAMINATED, 122-050, FABBED PANEL 241XCF, PN 144N5361-54 FROM A402H-48X144, BATTERY 2664589 IAW SREO B757-5320-9

All 184: https://openairdocs.org/aircraft/N446UP/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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