# N440UP: 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: 25471
- Year built: 1994
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 23, 1994
- Certificate issued: October 31, 1994
- Expires: August 31, 2028
- Mode S code: A54C6D
- 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=440UP
- Page: https://openairdocs.org/aircraft/N440UP

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/N440UP/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 N440UP.

## FAA accident and incident reports (1)

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

- [Incident 20030124006669I](https://openairdocs.org/incident/20030124006669I), Jan 24, 2003: Boeing 75724APF (N440UP), West Palm Beach, FL, Minor damage. (-23) First officer flying aircraft to landing at kpbi. Aircraft aft fuselage contacted ground during touchdown. Aircraft taxied to parking after landing…

## Service difficulty reports (229, 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 IPXA2026050839220](https://openairdocs.org/sdr/IPXA2026050839220), Apr 29, 2026: CHANNEL. CRACKED. LEFT AFT MLG W/W 1180 BULKHEAD INBD LOWER SUPPORT CHANNEL SHOWS EVIDENCE OF A CRACK.
- [SDR IPXA2026050990937](https://openairdocs.org/sdr/IPXA2026050990937), Apr 26, 2026: TORQUE BOX. DAMAGED. THE R/H LWR FWD TORQUE BOX PANEL HAS A DELAMINATED / DISBONDED AREA (1EA) NEAR THE BOTTOM OF THE PANEL. ALL DAMAGE MARKED IN RED.ACCOMPLISH REPAIR IAW SRM REV 1
- [SDR IPXA2026051490733](https://openairdocs.org/sdr/IPXA2026051490733), Apr 26, 2026: PANEL. DELAMINATED. THE L/H LWR FWD TORQUE BOX PANEL HAS 5EA DISBONDED / DELAMINATED AREAS FROM TOP TO BOTTOM. INSTALLED 1 EA TORQUE BOX PANEL IAW SRM 51-40-02.
- [SDR IPXA2026042984389](https://openairdocs.org/sdr/IPXA2026042984389), Apr 26, 2026: PANEL. CORRODED. NR 1 PYLON PANEL 433FL AFT VERTICAL ATTACHMENT HAS FRETTING CORROSION.
- [SDR IPXA2026051481074](https://openairdocs.org/sdr/IPXA2026051481074), Apr 25, 2026: STRAP. CORRODED. MAJOR REPAIR. APU INLET DOOR AFT STRAP AT STA 1825.00 S-3R TO S-6R HAS CORROSION INSTALLED PARTS OF REPAIR (STRAP 1, STRAP 2, FILLER 3, FILLER 4 AND OUTER STRAP
- [SDR IPXA2026050381104](https://openairdocs.org/sdr/IPXA2026050381104), Apr 25, 2026: STRAP. CORRODED. APU INLET DOOR FWD STRAP AT BS 1787.45 FROM S-3R TO S-6R HAS CORROSION INSTALLED NEW FWD STRAP IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026050681325](https://openairdocs.org/sdr/IPXA2026050681325), Apr 25, 2026: ANGLE. CORRODED. APU INLET DOOR LOWER CORNER ANGLE AT STA 1787.45 S-R6 HAS EVIDENCE OF CORROSION. INSTALLED NEW LOWER CORNER ANGLE I.A.W. SRM 51-40-02-0G-0.
- [SDR IPXA2026050681237](https://openairdocs.org/sdr/IPXA2026050681237), Apr 25, 2026: ANGLE. CORRODED. APU INLET DOOR UPPER CORNER ANGLE AT STA 1787.45 S-3R HAS EVIDENCE OF CORROSION. INSTALLED NEW UPPER CORNER ANGLE I.A.W. SRM 51-40-02-0G-0.
- [SDR IPXA2026050681291](https://openairdocs.org/sdr/IPXA2026050681291), Apr 25, 2026: ANGLE. CORRODED. APU INLET DOOR LOWER ANGLE AT STA 1787.45 TO STA 1825.00 S6R HAS EVIDENCE OF CORROSION. INSTALLED NEW LOWER ANGLE I.A.W. SRM 51-40-02-0G-0.
- [SDR IPXA2026050572367](https://openairdocs.org/sdr/IPXA2026050572367), Apr 25, 2026: BRACKET. CORRODED. ACCESS DOOR 313AL LT AND RT LATCH STOPS AT THE CUT-OUT 4EA BRACKETS ARE CORRODED. INSTALLED 4EA BRACKETS ND RT AND LT LATCH STOP IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026050281431](https://openairdocs.org/sdr/IPXA2026050281431), Apr 25, 2026: SKIN. CRACKED. NR 1 ENGINE AFT STRUT FAIRING LOWER AFT EXTERIOR OTBD SHOWS EVIDENCE OF A CRACK NEAR FASTENER. INSTALLED AFT STRUT FAIRING NR 1 ENGINE IAW SRM 51-40-02-0G.
- [SDR IPXA2025091632906](https://openairdocs.org/sdr/IPXA2025091632906), Sep 16, 2025: ACM. ODOR. LEFT PACK MODERATE BURNT ODOR RIGHT PACK MODERATE ODOR NOT BURNT SOME EYE IRRITATION AWARENESS BOTH CA AND F/O. R & R AIR CYCLE MACHINE I.A.W B757 MM 21-51-03. 
- [SDR IPXA2025091962906](https://openairdocs.org/sdr/IPXA2025091962906), Sep 16, 2025: A/C PACK. ODOR. LEFT PACK MODERATE BURNT ODOR RIGHT PACK MODERATE ODOR NOT €ŒBURNT€? SOME EYE IRRITATION AWARENESS BOTH CA AND F/O T/S AND FOUND LEFT PACK TO BE CAUSE OF SMEL
- [SDR IPXA2025091629291](https://openairdocs.org/sdr/IPXA2025091629291), Sep 11, 2025: INDICATION SYS. FALSE INDICATION. DESCENDING THRU 12,00 MSL, FLAPS 1, EICAS MESSAGE FOR GEAR NOT DOWN, DISPLAYED FOR APPROXIATELY 2 SECONDS. PERFORMED OPS CHECK OF RADIO ALT SYS IAW AMM 34-33-00
- [SDR IPXA2025091129291](https://openairdocs.org/sdr/IPXA2025091129291), Sep 11, 2025: WARNING MESSAGE. ILLUMINATED. DESCENDING THRU 12,00 MSL, FLAPS 1, EICAS MESSAGE GEAR NOT DOWN DISPLAYED FOR APPROXIATELY 2 SECONDS. PERFORMED GPWS FAULT/BITE CHECK .BITE FAULT OF LEFT RADIO 
- [SDR IPXA2025013162143](https://openairdocs.org/sdr/IPXA2025013162143), Jan 29, 2025: WARNING MESSAGE. FALSE ACTIVATION. L FWD ENT DOOR EICAS WITH DOOR CLOSED. REVERSED DMP. TROUBLESHOT IAW 757 FIM 52-71 FAULT TREE 802. ADJUSTED THE SENSOR FOR THE CREW ENTRY DOOR. CREW ENTRY DOOR 
- [SDR IPXA2025012962143](https://openairdocs.org/sdr/IPXA2025012962143), Jan 29, 2025: WARNING MESSAGE. FALSE INDICATION. L FWD ENT DOOR EICAS WITH DOOR CLOSED DEFERRED CREW ENTRY DOOR IND SYS IAW MEL 52-71-1. DMP CW. PLACARD INSTALLED. OPEN
- [SDR IPXA2024071536808](https://openairdocs.org/sdr/IPXA2024071536808), Jun 29, 2024: TRANSITION PANEL. CORRODED. AFT CARGO PIT TRANSITION PANEL BS 1480-1500 HAS CORROSION. INSTALLED TRANSITION PANEL BS 1480 - 1500 IAW SRM 51-40-02-0G-0.
- [SDR IPXA2024071134376](https://openairdocs.org/sdr/IPXA2024071134376), Jun 26, 2024: FRAME. DENTED. AFT CARGO PIT - FRAME STA 1340 HAS A DENT ON INNER CHORD BETWEEN STR 24R-25R. INSPECTED AND VERIFIED JOB WAS ACCOMPLISHED IAW UPS EO-90803-REQ1 AND VT MAE EA 75
- [SDR IPXA2024062734376](https://openairdocs.org/sdr/IPXA2024062734376), Jun 26, 2024: FRAME. DENTED. AFT CARGO PIT - FRAME STA 1340 HAS A DENT ON INNER CHORD BETWEEN STR 24R-25R APPROVED.
- [SDR IPXA2024071215595](https://openairdocs.org/sdr/IPXA2024071215595), Jun 25, 2024: TEE FITTING. CORRODED. KEEL BEAM AREA FOR PANEL 139CL STRUCTURE HAS CORROSION. INSTALLED NEW SUPPORT TEE I.A.W SRM 51-40-02-0G.
- [SDR IPXA2024062486868](https://openairdocs.org/sdr/IPXA2024062486868), Jun 23, 2024: LATCH. GOUGED. **SDR FILED OPEN** FAULT STR Z800 CREW CABIN DOOR UPPER/LOWER LATCHES ARE GOUGED.DOT 72-016 APPROVED
- [SDR IPXA2022062183346](https://openairdocs.org/sdr/IPXA2022062183346), Jun 10, 2022: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG3MAIN CABIN FLOOR PANEL 232XFF IS CRACKEDFABBED PANEL 232XFF FROM 5024N400001SSG, BATCH #3855547 PER UPS SREO B757-5320-9692-K
- [SDR IPXA2022062183345](https://openairdocs.org/sdr/IPXA2022062183345), Jun 9, 2022: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG3L/H MAIN CARGO COMP, FLOOR PANEL 251XFF, IS SPLIT IN HALFFABBED PANEL 251XFF FROM 5024N400001SS-G BAT# 0003855547 PER UPS SREO B757-5320-969
- [SDR IPXA2022062283366](https://openairdocs.org/sdr/IPXA2022062283366), Jun 7, 2022: SKIN. CORRODED. INSPECTION TYPE:SEG3#2 ENGINE PYLON OUTBD INNER SKIN AT APPROXIMATELY STA PPS 130 HAS SURFACE CORROSION FWD OF PRECOOLER OPENINGREPLACED PYLON SKIN PER BOEING D
- [SDR IPXA2022062083318](https://openairdocs.org/sdr/IPXA2022062083318), Jun 7, 2022: FRAME. DENTED. INSPECTION TYPE:SEG3THE TOP OF THE FRAME FLANGE AT STA 1360 L/H SIDE IS DENTED. LOCATED NEAR S-26LACCOMPLISHED REPAIR PER RCD 262735 AND SRM 53-00-07-2R 5 DETAI
- [SDR IPXA2022062383404](https://openairdocs.org/sdr/IPXA2022062383404), Jun 6, 2022: FRAME ANGLE. DAMAGED. INSPECTION TYPE:SEG3DURING ACCOMPLISHMENT OF EO B757-5310-73926-A FOUND AN EXISTING FRAME REPAIR AT STA 1320 BETWEEN S-23R AND S-27R. ALTERNATE INSPECTION REQUI
- [SDR IPXA2022061683167](https://openairdocs.org/sdr/IPXA2022061683167), Jun 6, 2022: FRAME. CORRODED. INSPECTION TYPE:SEG3DURING ACCOMPLISHMENT OF EO B757-5310-73926-A, EXISTING REPAIR FOUND AT STA 1240, S-24R TO S-26R. ALTERNATE INSPECTION METHODS REQUIREDACCOM
- [SDR IPXA2022061683166](https://openairdocs.org/sdr/IPXA2022061683166), Jun 6, 2022: FRAME. CORRODED. INSPECTION TYPE:SEG3DURING ACCOMPLISHMENT OF EO B757-5310-73926-A, EXISTING REPAIR FOUND AT STA 1300, S-26L. ALTERNATE INSPECTION METHODS REQUIREDACCOMPLISH WOR
- [SDR IPXA2020072097952](https://openairdocs.org/sdr/IPXA2020072097952), Jul 19, 2020: PANEL. DELAMINATED. INSPECTION TYPE:CCK, RT TORQUE BOX PANEL HAD TWO DELAMINATED DENTS ON THE LWR SKIN SURFACE OF PANEL. REPAIRED IAW SRM 51-70-10-2R, REPAIR 5, AND 2 IAW EO B757-5
- [SDR IPXA2020072097951](https://openairdocs.org/sdr/IPXA2020072097951), Jul 19, 2020: PANEL. DELAMINATED. INSPECTION TYPE:CCKRH LWR FWD TORQUE BOX PANEL HAS 2EA DELAMINATIONS ON UPPER SKINREPAIR PER SRM B757-51-70-10-2R-2 REPAIR 2 PER EO B757-5530-77187-A
- [SDR IPXA2019071644531](https://openairdocs.org/sdr/IPXA2019071644531), Jul 16, 2019: CONTROL PANEL. DEFECTIVE. INSPECTION TYPE:N/A SPRING WIRE ON EMERGENCY EXIT LIGHT SWITCH FELL OUT. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL PANEL IAW AMM 33 51 08. OPS CHECK GOOD ESR
- [SDR IPXA2019030839838](https://openairdocs.org/sdr/IPXA2019030839838), Mar 7, 2019: BRACKET. BROKEN. INSPECTION TYPE:N/A CREW ENTRY DOOR INDICATION PROX SENSOR BRACKET BROKEN. DEFERRED PER E.O. B757-5270-71852-A SENSOR REMOVED AND WIRES CAPPED AND STOWED PARTS 
- [SDR IPXA2018073032112](https://openairdocs.org/sdr/IPXA2018073032112), Jul 26, 2018: ROLLER. OUT OF ADJUST. CAPT REPORTS ENTRY DOOR NOT LOCKING CLOSED EICAS MSG ON LANDING. ADJUSTED CREW ENTRY DOOR LATCH ROLLERS IAW MM 52-112-00-825-007. C/W CREW ENTRY DOOR WARNING SY
- [SDR IPXA2018040328153](https://openairdocs.org/sdr/IPXA2018040328153), Apr 3, 2018: WIRE. DETACHED. EMERGENCY LIGHT GUARDED SWITCH WIRE SEPARATED. INSTALLED THE WIRE. CHECKED GOOD.
- [SDR IPXA2017071019144](https://openairdocs.org/sdr/IPXA2017071019144), Jul 8, 2017: POWER SUPPLY. INOPERATIVE. EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-07-201. OPS CHECKED GOOD.
- [SDR IPXA2016092708694](https://openairdocs.org/sdr/IPXA2016092708694), Sep 27, 2016: EVAS UNIT. UNSERVICEABLE. F/O CSVS EMERGENCY VISION ASSURANCE SYSTEM MOUNTING BRACKET LOOSE. REATTACHED MOUNTING BRACKET IAW EO B757-2560-45127-E. REINSTALLED SERVICEABLE EVAS UNIT IAW M
- [SDR IPXA2016092008469](https://openairdocs.org/sdr/IPXA2016092008469), Sep 19, 2016: SWITCH. INOPERATIVE. EMERGENCY LIGHT UNARMED INDICATION LIGHT INOPERATIVE. REMOVED & REPLACED EMERGENCY LIGHT UNARMED INDICATOR SWITCH IAW MM 33-13-00. OPS CHECKED GOOD.
- [SDR IPXA2016072206165](https://openairdocs.org/sdr/IPXA2016072206165), Jul 3, 2016: PLATE. CORRODED. INSPECTION TYPE: SEG4, LEFT ELEVATOR OB LOWER PLATE HAS CORROSION. REMOVED AND REPLACED THE PLATE IAW SRM 55-20-01-0I-1, AND DWG 183N2007.
- [SDR IPXA2016072006095](https://openairdocs.org/sdr/IPXA2016072006095), Jul 3, 2016: PLATE. CORRODED. INSPECTION TYPE: SEG4, RT ELEVATOR O/B UPPER AND LOWER PLATE IS CORRODED.FOUND TWO SPLICE PLATES TO BE OUT OF LIMITS IAW SRM 55-20-01-1A-1 FABRICATED 2 EA NEW S
- [SDR IPXA2016071505923](https://openairdocs.org/sdr/IPXA2016071505923), Jul 2, 2016: ATTACH FITTING. WORN. INSPECTION TYPE: SEG4, LEFT WING FLAP TRACK NR 3 IB ATTACH FITTING MOUNT HOLES WORN AND FASTENERS SHEARED. REPAIRED IAW SRM 57-53-02-2R-3 REPAIR 3 WITH NO DEVIA
- [SDR IPXA2016070805583](https://openairdocs.org/sdr/IPXA2016070805583), Jul 2, 2016: FLOOR PANEL. PUNCTURED. INSPECTION TYPE: SEG4, MAIN DECK FLOOR PANEL 241XAF HAD NUMEROUS PUNCTURES. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
- [SDR IPXA2016071906059](https://openairdocs.org/sdr/IPXA2016071906059), Jul 1, 2016: SKIN. DENTED. INSPECTION TYPE: SEG4, SKIN DENTED BS 360, STRINGERS 15-16L. REPAIRED IAW EA 757-5311-27A2226 AND EO B757-5330-61249-A.
- [SDR IPXA2015111795907](https://openairdocs.org/sdr/IPXA2015111795907), Nov 17, 2015: LIFE VEST. TORN. CAPTAIN`S LIFE VEST BAG TORN SEVERAL PLACES. R & R LIFE VEST LOCATED IN CAPTAIN SEAT POUCH REF AMM 25-64-00.
- [SDR IPXA2014072383711](https://openairdocs.org/sdr/IPXA2014072383711), Jul 10, 2014: FLOOR PANEL. DELAMINATED. INSPECTION 11C3, MAIN DECK FLOOR PANEL 231XHF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
- [SDR IPXA2014072583734](https://openairdocs.org/sdr/IPXA2014072583734), Jul 9, 2014: FLOOR PANEL. DELAMINATED. INSPECTION 11S3, MAIN DECK FLOOR PANEL 231XCF IS DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SREO 5320-9692-H.
- [SDR IPXA2014072583733](https://openairdocs.org/sdr/IPXA2014072583733), Jul 9, 2014: FLOOR PANEL. DELAMINATED. INSPECTION 11S3, MAIN DECK FLOOR PANEL 231XMF IS DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SREO 5320-9692-H.
- [SDR IPXA2014072583732](https://openairdocs.org/sdr/IPXA2014072583732), Jul 9, 2014: FLOOR PANEL. DAMAGED. INSPECTION 11S3, MCD FLOOR PANEL 252XUF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO 5320-9692-H.
- [SDR IPXA2014072583731](https://openairdocs.org/sdr/IPXA2014072583731), Jul 9, 2014: FLOOR PANEL. DELAMINATED. INSPECTION 11S3, MAIN CARGO DECK FLOOR PANEL 251XRF IS DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SREO 5320-9692-H.
- [SDR IPXA2014072583730](https://openairdocs.org/sdr/IPXA2014072583730), Jul 9, 2014: FLOOR PANEL. DELAMINATED. INSPECTION 11S3, MAIN CARGO DECK FLOOR PANEL 231XFFR IS DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SREO 5320-9692-H.

All 229: https://openairdocs.org/aircraft/N440UP/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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.