# N459UP: 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: 25480
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 30, 1996
- Certificate issued: November 1, 1996
- Expires: November 30, 2028
- Mode S code: A5955B
- Registered owner: [Cc & Ei LLC](https://openairdocs.org/faa-owner/CC%20%26%20EI%20LLC)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: LLC
- 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=459UP
- Page: https://openairdocs.org/aircraft/N459UP

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/N459UP/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 N459UP.

## FAA accident and incident reports

None matched to N459UP.

## Service difficulty reports (266, 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 IPXA2026072758829](https://openairdocs.org/sdr/IPXA2026072758829), Jul 25, 2026: ENGINE. FAILED. EMERGENCY DECLARED, IN FLIGHT SHUT DOWN DURING CLIMB THRU FL220, LTT ENG FAILED WITHOUT WARNING. AIRSPEED WAS APPROX 310 KTS. N2 ROTATION NORMAL AFTER SHUTDOWN.
- [SDR IPXA2025112636097](https://openairdocs.org/sdr/IPXA2025112636097), Nov 25, 2025: FLAP SYSTEM. INOPERATIVE. TE FLAPS DISAGREE POSITIONING FLAPS 1 ON LANDING C/W FIM 27-51 FT 814. MSG CLEARED NO FUALTS NOTED. OPS CK REF AMM 27-51-00. NO MSG. OK TO CONTINUE.
- [SDR IPXA2025103173256](https://openairdocs.org/sdr/IPXA2025103173256), Oct 9, 2025: STRINGER. CORRODED. WHILE WORKING CORROSION AT AFT CARGO COMP. FOUND CORROSION BETWEEN STRINGER 29R AND FUSELAGE SKIN AT STA 1560-1580. INSTALLED (1EA) REPAIR STRINGER SECTION AND 
- [SDR IPXA2025102833199](https://openairdocs.org/sdr/IPXA2025102833199), Oct 7, 2025: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO BELOW ACCESS PANEL 241XHF HAS CORROSION, FLL-026, INSTALLED FLOOR SUPPORT 144N5005-3 UNDER FLOOR PANEL 241XHF IAW SRM 51-40-02-OG-0.
- [SDR IPXA2025103131819](https://openairdocs.org/sdr/IPXA2025103131819), Oct 7, 2025: STRAP. CORRODED. STRUCTURES, MAIN DECK CARGO BELOW ACCESS PANEL 252XFF FROM STA 1400 TO STA 1420, RBL 45.5 HAS CORROSION ON SUPPORT CEILING PANEL, FLL-012, ATA 53. NSTALLED 1EA 
- [SDR IPXA2025102930140](https://openairdocs.org/sdr/IPXA2025102930140), Oct 7, 2025: ANGLE. CORRODED. STRUCTURES, MAIN DECK CARGO AFT SHEAR WEB, FROM STA 1681 TO 1720, LBL 54.9 TO RBL 54.9 UNDER METALLIC FLOOR (ACCESS BY CARGO BAY) HAS CORROSION, FLL-005, ATA 53
- [SDR IPXA2025103132465](https://openairdocs.org/sdr/IPXA2025103132465), Oct 7, 2025: STRAP. CORRODED. STRUCTURES, MAIN DECK CARGO BELOW ACCESS PANEL 251XBF FROM STA 1220 TO STA 1240, LBL 24.75 HAS CORROSION , FLL-018, ATA 53. FABRICATED STABILIZER STRAP MAIN CAB
- [SDR IPXA2025103034768](https://openairdocs.org/sdr/IPXA2025103034768), Oct 7, 2025: STRUCTURE. CORRODED. MAIN DECK CABIN BELOW FLOOR PANEL 241XKF HAS CORROSION, FLL-023, ATA 53. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95488-REQ1 AND VT-SAA EA 757-5310-01-B0583, R
- [SDR IPXA2025102633251](https://openairdocs.org/sdr/IPXA2025102633251), Oct 7, 2025: SEAT TRACK. CORRODED. MAIN DECK CARGO BELOW ACCESS PANEL 242XGF SEAT TRACK HAS CORROSION, FLL-028. OPEN
- [SDR IPXA2025102133199](https://openairdocs.org/sdr/IPXA2025102133199), Oct 7, 2025: FLOOR SUPPORT. CORRODED. STRUCTURES, MAIN DECK CARGO BELOW ACCESS PANEL 241XHF HAS CORROSION, FLL-026, ATA 53.
- [SDR IPXA2025102198394](https://openairdocs.org/sdr/IPXA2025102198394), Oct 5, 2025: STRAP. CORRODED. APU INLET DOOR SUPPORT STRUCTURE AFT STRAP SHOWS SIGNS OF CORROSION. INSTALLED 4EA NEW REPAIR PARTS, DOUBLER (-1), STRAP (-2), FILLER (-3), FILLER (-4), 1 EA EX
- [SDR IPXA2025103160829](https://openairdocs.org/sdr/IPXA2025103160829), Oct 2, 2025: STRINGER. CORRODED. STRUCTURES, AFT LOWER FUSELAGE FROM STA 1480 TO STA 1500, S-30, HAS PROTUBERANT DENT, FLL-018, ATA 53. INSTALLED FABRICATED STRINGER SECTION, NEW HAT SECTION AN
- [SDR IPXA2025103060968](https://openairdocs.org/sdr/IPXA2025103060968), Oct 2, 2025: SKIN. CORRODED. AFT LOWER FUSELAGE FROM STA 1480 TO STA 1500, S-27R TO S-28R, HAS PROTUBERANT DENT, FLL-018, ATA 53. REINSTALLED RH FLOOR PANEL AT AFT CARGO COMP STA 1440 TO ST
- [SDR IPXA2025102661012](https://openairdocs.org/sdr/IPXA2025102661012), Oct 2, 2025: SKIN. CORRODED. AFT LOWER FUSELAGE FROM BS 1560 - 1580, S29R, HAS PROTRUDING DENT, FLL-018, ACCOMPLISH REPAIR PER SRM 53-00-01-2R REPAIR 28 REV. 124 REQUIREMENTS.
- [SDR IPXA2025102254371](https://openairdocs.org/sdr/IPXA2025102254371), Oct 2, 2025: STRAP. CORRODED. TAILCONE. APU INLET DOOR CUTOUT HAS CORROSION ON THE FWD EDGE.REMOVED FWD STRAP LOWER MIDDLE ANGLE AND FWD LOWER ANGLE AT APU INLET DOOR STRUCTURE IAW SRM 51-40
- [SDR IPXA2025051420889](https://openairdocs.org/sdr/IPXA2025051420889), May 11, 2025: EVAS UNIT. FAILED. CAPTAINS EVAS FAILED BLOWER CHECK R&R CAPTS EVAS REF AMM 25-69-00
- [SDR IPXA2025051220889](https://openairdocs.org/sdr/IPXA2025051220889), May 11, 2025: EVAS UNIT. NO TEST. CAPTAINS EVAS FAILED BLOWER CHECK R&R CAPTS EVAS REF AMM 25-69-00.
- [SDR IPXA2024123020240](https://openairdocs.org/sdr/IPXA2024123020240), Dec 27, 2024: LANDING GEAR. WARNING MESSAGE. AFTER SELECTING GEAR DOWN THE GEAR DISAGREE MSG ILLUMINATED. PERFORMED QRH AND LANDED NORMALLY. IT WAS THE RIGHT MAIN GEAR THAT DID NOT EXTEND USING NORMAL METH
- [SDR IPXA202412270001](https://openairdocs.org/sdr/IPXA202412270001), Dec 27, 2024: LANDING GEAR. FAULTED. AFTER SELECTING GEAR DOWN THE GEAR DISAGREE MSG ILLUMINATED. PERFORMED QRH AND LANDED NORMALLY. IT WAS THE RIGHT MAIN GEAR THAT DID NOT EXTEND USING NORMAL METH
- [SDR IPXA2024092433591](https://openairdocs.org/sdr/IPXA2024092433591), Sep 11, 2024: WINDOW. WARNING MESSAGE. ON PREFLIGHT L SIDE WINDOW EICAS MESSAGE DISPLAYED. FINISHED REMOVAL OF L/H #2 WINDOW IAW B757 AMM 56-11-02-004-010. INSTALLED L/H #2 WINDOW IAW B757 AMM 56-11-
- [SDR IPXA2024091133591](https://openairdocs.org/sdr/IPXA2024091133591), Sep 11, 2024: WARNING MESSAGE. ILLUMINATED. SDR FILED OPEN, ON PREFLIGHT L SIDE WINDOW EICAS MESSAGE DISPLAYED STARTED REMOVAL OF #2 WINDOW IAW B757 AMM 56-11-02-004-010 UP TO STEP 5(G) 2).
- [SDR IPXA2023120134182](https://openairdocs.org/sdr/IPXA2023120134182), Nov 30, 2023: RELIEF VALVE. MALFUNCTIONED. AT 37000FT CABIN ALT AUTO 2 CABIN ALT AUTO 1 MASTER WARNING CABIN AUTO INOP ALL APPEARED. UNABLE TO CONTROL CABIN INITIATED DECENT MANUAL CONTROL BECAME EFFECTI
- [SDR IPXA2023112859902](https://openairdocs.org/sdr/IPXA2023112859902), Nov 12, 2023: STRAKE. CORRODED. FAULT: LH HORIZONTAL LOWER STRAKELET HAS EVIDENCE OF CORROISON DOT: 107-002. INTALLED STRAKAKELET IAW SRM 51-40-02. REVIEWED
- [SDR IPXA2023120543755](https://openairdocs.org/sdr/IPXA2023120543755), Nov 11, 2023: TEE ANGLE. CORRODED. *** SUPPLEMENTAL SDR *** FAULT: R/H WTB, T-CHORD STA 1220, FOUND EXFOLIATED CORROSION. FAULT WROTE UP FOR OTHER A/C, PLEASE REFER TO T3F18E00CTLT
- [SDR IPXA2023120543694](https://openairdocs.org/sdr/IPXA2023120543694), Nov 11, 2023: TEE ANGLE. CORRODED. R/H WTB, T-CHORD, RBL 63, FOUND EXFOLIATED CORROSION. FAULT CREATED FOR OTHER A/C (N456UP), PLEASE REFER TO T3F18E003CTKV
- [SDR IPXA2023120543467](https://openairdocs.org/sdr/IPXA2023120543467), Nov 11, 2023: TEE ANGLE. CORRODED. *** SUPPLEMENTAL SDR *** FAULT: R/H WTB, T-CHORD, STA 1240, FOUND EXFOLIATED CORROSION, BETWEEN RBL 57.50 T0 RBL 63 FAULT WRITTEN FOR WRONG AIRCRAFT (N456UP), P
- [SDR IPXA2023111343755](https://openairdocs.org/sdr/IPXA2023111343755), Nov 11, 2023: UNKNOWN. UNKNOWN. R/H WTB, T-CHORD STA 1220, FOUND EXFOLIATED CORROSION. REMOVED T-CHORD STA 1220 IAW SRM 51-40-02-0G. VERIFIED T-CHORD AT STA. 1220 REMOVED.
- [SDR IPXA2023111343694](https://openairdocs.org/sdr/IPXA2023111343694), Nov 11, 2023: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT: R/H WTB, T-CHORD, RBL 63, FOUND EXFOLIATED CORROSION. REMOVED T-CHORD AT RBL 63.0 BETWEEN FS 1180 TO FS 1240 IAW B757 SRM 51-40-02
- [SDR IPXA2023111343467](https://openairdocs.org/sdr/IPXA2023111343467), Nov 11, 2023: UNKNOWN. UNKNOWN. R/H WTB, T-CHORD, STA 1240, FOUND EXFOLIATED CORROSION, BETWEEN RBL 57.50 T0 RBL 63 PERFORMED CUT OUT AT T-CHORD FROM BL0 TO RBL63 STA 1240 I.A.W SRM 51-70-12-O
- [SDR IPXA2023112740899](https://openairdocs.org/sdr/IPXA2023112740899), Nov 10, 2023: SKIN. CORRODED. *MAJOR REPAIR* FAULT: EVIDENCE OF CORROSION INSIDE #2 PYLON SKIN FWD OF PANEL 443CR. DOT 140-13. ACCOMPLISH EO-88765-REQ1 AND EA 757-5450-27-A3442. SUBTASK UP T
- [SDR IPXA2023112533548](https://openairdocs.org/sdr/IPXA2023112533548), Nov 10, 2023: TEE ANGLE. CORRODED. FAULT:LOWER FUSELAGE WEBS BETWEEN BOTH AIR CONDITIONING ACCESS DOOR WITH SURFACE CORROSION.DOT119-065. INSTALLED T-CHORD IN LOWER FUSELAGE BTWN BOTH AIR CONDITI
- [SDR IPXA2023112718179](https://openairdocs.org/sdr/IPXA2023112718179), Nov 9, 2023: TEE ANGLE. CORRODED. FAULT:WING TO BODY LH STRUCTURE HAS CORROSION AT T CHORD STA 1.040.DOT119-060. INSTALLED NEW T-CHORD IN WING TO BODY LH STRUCTURE STA.1040 IAW SRM 51-40-02-0G.-
- [SDR IPXA2023112316833](https://openairdocs.org/sdr/IPXA2023112316833), Nov 9, 2023: WEB. CORRODED. FAULT:WING TO BODY FAIRING STA 1.200 WEB RH HAS CORROSION.DOT119-048. INSTALLED NEW WEB AT STA 1200 RH WTB IAW SRM 51-40-02-0G. REVIEWED.
- [SDR IPXA2023112989044](https://openairdocs.org/sdr/IPXA2023112989044), Nov 8, 2023: TEE ANGLE. CORRODED. FAULT: L/H WTB T-CHORD AT STA. 1200 HAS EXFOLIATING CORROSION. INSTALLED NEW T-CHORD AT FS 1200 LH IAW B757 SRM 51-40-02-0G. REVIEWED
- [SDR IPXA2023112867666](https://openairdocs.org/sdr/IPXA2023112867666), Nov 7, 2023: TEE ANGLE. CORRODED. FAULT: R/H WTB T-CHORD STA 1037, FOUND EXFOLIATED CORROSION AT NUT PLATE HOLES. INSTALLED T-CHORD AT STA 1037RH WTB IAW SRM 51-40-02-0G. REVIEWED
- [SDR IPXA2023112767770](https://openairdocs.org/sdr/IPXA2023112767770), Nov 7, 2023: TEE ANGLE. CORRODED. FAULT: R/H WTB, INTERCOSTAL, FOUND EXFOLIATE CORROSION, BETWEEN STA 1037 TO STA 1060. INSTALLED T-CHORD IAW SRM 51-40-02. REVIEWED
- [SDR IPXA2023111967834](https://openairdocs.org/sdr/IPXA2023111967834), Nov 7, 2023: TEE ANGLE. CORRODED. R/H WTB, T-CHORD STA 1220, AT RBL 63 FOUND EXFOLIATED CORROSION. INSTALLED T-CHORD IAW SRM 51-40-02-0G. REVIEWED
- [SDR IPXA2025022649962](https://openairdocs.org/sdr/IPXA2025022649962), Nov 6, 2023: SKIN. CORRODED. WING RH I/B FLAP SURFACE CORROSION AT LOWER SURFACE. DOT119-029 PLEASE REF BARCODE T3F18E0039JV1 FOR CORRECTIVE ACTION AND INSTALLATION OF NEW FLAP.
- [SDR IPXA2025022651282](https://openairdocs.org/sdr/IPXA2025022651282), Nov 6, 2023: SKIN. CORRODED. WING RH I/B TRAILING EDGE FLAP SURFACE CORROSION AT LOWER SKIN. DOT119-031 INSTALLED RH IB TRAILING EDGE MAIN FLAP PER AMM 27-51-02-424-021. COMPLETED INSTALLAT
- [SDR IPXA2023112049962](https://openairdocs.org/sdr/IPXA2023112049962), Nov 6, 2023: SKIN. CORRODED. *SDR FILED OPEN* FAULT:WING RH I/B FLAP SURFACE CORROSION AT LOWER SURFACE. DOT119-029 PARTS ON ORDER IN BARCODE T3F18E0039JV1. 3 MECHANICS REQUIRED FOR 4 SHIFT
- [SDR IPXA2023112051282](https://openairdocs.org/sdr/IPXA2023112051282), Nov 6, 2023: SKIN. CORRODED. *SDR FILED OPEN* FAULT:WING RH I/B TRAILING EDGE FLAP SURFACE CORROSION AT LOWER SKIN. DOT119-031 PARTS ON ORDER. 3 MECHANICS REQUIRED FOR 4 SHIFTS ESTIMATED, C
- [SDR IPXA2023112865059](https://openairdocs.org/sdr/IPXA2023112865059), Nov 6, 2023: TEE ANGLE. CORRODED. FAULT: R/H WTB T-CHORD, RBL 57.50, FOUND EXFOLIATED CORROSION, BET STA 1180 TO STA 1240. INSTALLED T-CHORD I.A.W. B757-200 S.R.M. 51-40-02-OG. REVIEWED
- [SDR IPXA2023112759219](https://openairdocs.org/sdr/IPXA2023112759219), Nov 6, 2023: TEE ANGLE. CORRODED. FAULT: LH AFT WTB STRUCTURE T-CHORD AT STA 1220, UNDER PANEL 195CL HAS CORROSION. INSTALLED NUT PLATE 17 E/A IAW SRM 51-40-02-0G. INSTALLED T-CHORD AT STA 1220 
- [SDR IPXA2023112758827](https://openairdocs.org/sdr/IPXA2023112758827), Nov 6, 2023: UNKNOWN. CORRODED. FAULT: WTB STRUCTURE UNDER PANEL 198MR, FROM STA 1180-1240 ON TH RH SIDE HAS SEVERAL AREAS WITH CORROSION. INSTALLED T-CHORD UNDER PANEL 198MRFROM STA.1180 TO 1
- [SDR IPXA2023112265202](https://openairdocs.org/sdr/IPXA2023112265202), Nov 6, 2023: TEE ANGLE. CORRODED. FULT: R/H WTB T-CHORD STA 1240, FOUND EXFOLIATED CORROSION, BET RBL 57.50 TO RBL 63.0 INSTALLED T-CHORD I.A.W. SRM 51-40-02-0G. INSTALLED 4 E/A SPLICES AT R/H W
- [SDR IPXA2023111958867](https://openairdocs.org/sdr/IPXA2023111958867), Nov 6, 2023: TEE ANGLE. CORRODED. FAULT: RH WTB STRUCTURE UNDER PANEL 198AR, STA 1040-1060 HAS CORROSION. INSTALLED T- CHORD STA. 1040 TO STA.1060 IAW SRM 51-40-02-0G. REVIEWED
- [SDR IPXA2023111959108](https://openairdocs.org/sdr/IPXA2023111959108), Nov 6, 2023: TEE ANGLE. CORRODED. FAULT: RH WTB STRUCTURE T-CHORD AT STA 1060 HAS CORROSION. INSTALLED T-CHORD I.A.W. B757-200 S.R.M. 51-40-02-OG. REVIEWED
- [SDR IPXA2023120535508](https://openairdocs.org/sdr/IPXA2023120535508), Nov 4, 2023: FLOOR PANEL. BROKEN. MAIN CARGO COMPARTMENT FLOOR PANEL 232XVF BROKEN. DOT119-019 INSTALLED FLOOR PANEL 232XVF I.A.W. AMM 53-01-024-023.
- [SDR IPXA2023112732706](https://openairdocs.org/sdr/IPXA2023112732706), Nov 4, 2023: SKIN PANEL. DENTED. *MAJOR REPAIR* FAULT:#2 PYLON I/B HAS DENT AT OUTTER SKIN BETWEEN NAC STA 105.66 AND NAC STA 169.8. DOT119-009. ACCOMPLISH EO-88785-REQ1 AND EA 757-5450-27-A345
- [SDR IPXA2023111735508](https://openairdocs.org/sdr/IPXA2023111735508), Nov 4, 2023: FLOOR PANEL. BROKEN. FAULT:MAIN CARGO COMPARTMENT FLOOR PANEL 232XVF BROKEN. DOT119-019 VERIFIED INSTALLATION OF FLOOR PANEL 232XVF

All 266: https://openairdocs.org/aircraft/N459UP/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.