# N469UP: 1997 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: 25485
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 29, 1997
- Certificate issued: November 18, 2005
- Expires: November 30, 2028
- Mode S code: A5BCDA
- 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=469UP
- Page: https://openairdocs.org/aircraft/N469UP

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/N469UP/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 N469UP.

## FAA accident and incident reports

None matched to N469UP.

## Service difficulty reports (207, 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 IPXA2026010883023](https://openairdocs.org/sdr/IPXA2026010883023), Jan 7, 2026: CONTROL UNIT. FAULTED. AT CRUISE FLT AT FL380. L SIDE WINDOW HAD STARTED TO DELAMINATE THE HEATING ELEMENT. FOLLOWED QRH CHECKLIST & WINDOW WAS EXTREMELY HOT TO TOUCH AND APPROX 5IN A
- [SDR IPXA2026010783023](https://openairdocs.org/sdr/IPXA2026010783023), Jan 7, 2026: WINDOW. DELAMINATED. AT CRUISE FLT AT FL380. L SIDE WINDOW HAD STARTED TO DELAMINATE THE HEATING ELEMENT. FOLLOWED QRH CHECKLIST & WINDOW WAS EXTREMELY HOT TO TOUCH AND APPROX 5IN A
- [SDR IPXA2025122247034](https://openairdocs.org/sdr/IPXA2025122247034), Dec 19, 2025: ENGINE. VIBRATION. DIVERSION, NR 2 ENG HIGH N1 VIBRATION ON CLIMB AT 36,000. KEPT OUT OF YELLOW BAND BELOW 67% N1 POWER SETTING. POWERPLANT ENGINEERING REVIEWED ECM/OCM DATA. CLE 
- [SDR IPXA2025111093190](https://openairdocs.org/sdr/IPXA2025111093190), Nov 10, 2025: ELEC CONNECTOR. DAMAGED. AIR TURN BACK DUE TO RIGHT ENG TAI INOP LIGHT & EICAS MSG. ENG. A/I CHECKLIST WAS RUN W/NO RELIEF. ICING CONDITIONS AT DESTINATION THIS OCCURRED ON CLIMB-OUT. R
- [SDR IPXA2025081246933](https://openairdocs.org/sdr/IPXA2025081246933), Aug 1, 2025: LATCH. INOPERATIVE. CREW ENTRY DOOR UPPER LATCH IS OUT OF LIMITS. INSTALLED CREW ENTRY DOOR UPR LATCH, IAW CMM 52-11-08 AND AMM 20-11-00-912-001.
- [SDR IPXA202508046933](https://openairdocs.org/sdr/IPXA202508046933), Aug 1, 2025: LATCH. OUT OF LIMITS. CREW ENTRY DOOR UPPER LATCH IS OUT OF LIMITS VERIFIED STEP 6. INSTALLATION OF CREW ENTRY DOOR UPPER LATCH.REMOVED CREW ENTRY DOOR UPPER LATCH, IAW B757-200 AMM 
- [SDR IPXA2025080310676](https://openairdocs.org/sdr/IPXA2025080310676), Jul 30, 2025: FRAME. CRACKED. DURING OK TO INSTALL, FOUND AT STA 1200, BTW RBL 5 TO RBL 24, INTERCOSTAL DELAMINATED AND WITH CRACK. INSTALLED 1 EA INTERCOSTAL IAW SRM 51-40-02-0G.
- [SDR IPXA2025080308094](https://openairdocs.org/sdr/IPXA2025080308094), Jul 24, 2025: FLOORBEAM. CORRODED. MAIN DECK FLOORBEAM BELOW FLOOR PANEL 242XGF AT BS 1100 RBL 24.75, HAS EXFOLIATED CORROSION, DOT 78-20, FABRICATED 01 EA REPAIR UPPER CHORD SECTION PER E.A.# 75
- [SDR IPXA2025080303268](https://openairdocs.org/sdr/IPXA2025080303268), Jul 24, 2025: TEE ANGLE. CORRODED. AT STA 1040 TO 1060 LEFT, UNDER THE RAM AIR DOOR ACTUATOR, T-CHORD HAS EXFOLITATION CORROSION ON UPPER FLANGE, DOT 8-018.RECEIVED NEW INTERCOSTAL FROM TRAVELER 
- [SDR IPXA2025080383490](https://openairdocs.org/sdr/IPXA2025080383490), Jul 23, 2025: SKIN. CORRODED. CORROSION FOUND AT SKIN AREA STA 1885.20 S-17L JUST ABOVE APU LEFT DOOR. PERFORMED EO-94659-REQ1 AND VT-MAE EA 757-5380-27-A4073, REV -.
- [SDR IPXA2025080708252](https://openairdocs.org/sdr/IPXA2025080708252), Jul 23, 2025: TEE ANGLE. CORRODED. AT STA 1200 LOWER T-CHORD SUUPORT CLIP HAS CORROSION ON INNER FLANGE. DOT 8-015.CLEANED INTRECOSTAL AT STA 1200 NO CORROSION NOTED FOUND TO BE PAINT DAMAGED ONL
- [SDR IPXA2025072588319](https://openairdocs.org/sdr/IPXA2025072588319), Jul 23, 2025: PAINT. DAMAGED. INTRECOSTAL AT BS 1090, RBL 50 HAS SURFACE CORROSION ON INNER SURFACES. CLEANED INTRECOSTAL AT BS 1190, NO CORROSION NOTED FOUND TO BE PAINT DAMAGED ONLY IAW B7
- [SDR IPXA2025080560795](https://openairdocs.org/sdr/IPXA2025080560795), Jul 22, 2025: SKIN. CORRODED. NUMBER 2 PYLON INBD SIDE, FWD INNER SKIN HAS CORROSION AROUND CUTOUT OF PANEL 443GL. INSTALLED PYLON #2 I/B FWD FAIRING IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2025080265076](https://openairdocs.org/sdr/IPXA2025080265076), Jul 22, 2025: TEE ANGLE. CORRODED. TEE CHORD BS 900 RBL 0 HAVE CORROSION. INSTALLED TEE CHORD AND 8 PLATES, IAW SRM 51-70-12-0G-0, SRM 51-40-02.
- [SDR IPXA2025080366377](https://openairdocs.org/sdr/IPXA2025080366377), Jul 22, 2025: SKIN. DENTED. EXTERNAL FUSELAGE SKIN BETWEEN STA 560 TO 580 AND S-27R TO S-28R HAS A DENT. ACCOMPLISH REPAIR PER EO-94639-REQ1 AND VT-MAE EA 757-5330-27-A4080, REV-.
- [SDR IPXA2025080361106](https://openairdocs.org/sdr/IPXA2025080361106), Jul 22, 2025: SKIN. CORRODED. NR 2 PYLON INBD SIDE, AFT INNER SKIN HAS CORROSION BETWEEN PANELS 443HL AND 443JL AT LOWER AREA. ACCOMPLISH REPAIR PER EO-94655-REQ1 AND VT-MAE EA 757-5450-27-A
- [SDR IPXA2025080706343](https://openairdocs.org/sdr/IPXA2025080706343), Jul 22, 2025: SUPPORT BRACKET. CORRODED. BETWEEN T-CHORD 860 AND LOWER SKIN OF FUSELAGE, LOWER SUPPORT BRACKET HAS CORROSION.REMOVED CORROSION T-CHORD 860 RBL 0 IAW B757-200PF SRM 51-10-02.TREATED AND 
- [SDR IPXA2025080766917](https://openairdocs.org/sdr/IPXA2025080766917), Jul 22, 2025: SUPPORT ANGLE. CORRODED. EVIDENCE CORROSION PANEL 192 DR UPPER SUPPORT R/H SIDE. CLEANED AREA AT PANEL 192 DR UPPER SUPPORT R/H SIDE IAW SOPM 20-30-03.TREATED AND PRIMED AREA IAW SRM 51
- [SDR IPXA2025080234385](https://openairdocs.org/sdr/IPXA2025080234385), Jul 21, 2025: STRAP. CORRODED. APU INLET DOOR FWD STRAP AT STA 1787.45 FROM STR 3R TO STR 6R HAS EXFOLIATION. INSTALLED NEW FWD STRAP IAW SRM 51-40-02-0G-0.
- [SDR IPXA2025080534561](https://openairdocs.org/sdr/IPXA2025080534561), Jul 21, 2025: SKIN. CORRODED. APU INLET DOOR AFT STRAP AT STA 1826 FROM STR 3R TO STR 6R HAS EXFOLIATION CORROSION. ACCOMPLISH REPAIR PER EO-94632-REQ1 AND VT-MAE EA 757-5380-27-A4072, REV-,
- [SDR IPXA2025080234761](https://openairdocs.org/sdr/IPXA2025080234761), Jul 21, 2025: ANGLE. CORRODED. APU INLET DOOR UPPER ANGLE FROM STA 1787.45 TO STA 1826 AT STR 3R HAS CORROSION. INSTALLED NEW UPPER ANGLE IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2025080234656](https://openairdocs.org/sdr/IPXA2025080234656), Jul 21, 2025: ANGLE. CORRODED. APU INLET DOOR LOWER ANGLE FROM STA 1787.45 TO STA 1826 AT STR 6R HAS EXFOLIATION CORROSION. INSTALLED 1EA LOWER ANGLE IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2025080337337](https://openairdocs.org/sdr/IPXA2025080337337), Jul 21, 2025: TEE ANGLE. CORRODED. EVIDENCE OF CORROSION ON T-CHORD UPPER R/H SECTION STA 1200. REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.063''. AFTER BLENDED FOUND FOLLOWING ME
- [SDR IPXA2025080700384](https://openairdocs.org/sdr/IPXA2025080700384), Jul 21, 2025: STIFFENER. CORRODED. EVIDENCE OF CORROSION ON CHANNEL UPPER L/H STA 1120. REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.050''. AFTER BLENDED FOUND FOLLOWING MEASUREMEN
- [SDR IPXA2025080237575](https://openairdocs.org/sdr/IPXA2025080237575), Jul 21, 2025: TEE ANGLE. CORRODED. EVIDENCE OF CORROSION ON T-CHORD NEAR TO RAM AIR R/H STA 1220 RBL50. .REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.071''. AFTER BLENDED FOUND FOL
- [SDR IPXA2025080737989](https://openairdocs.org/sdr/IPXA2025080737989), Jul 21, 2025: TEE ANGLE. CORRODED. EVIDENCE OF CORROSION ON T-CHORD L/H STA 1180 TO 1240 LBL50.DOT 5846-12. REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.080''. AFTER BLENDED FOUND 
- [SDR IPXA2025080738248](https://openairdocs.org/sdr/IPXA2025080738248), Jul 21, 2025: TEE ANGLE. CORRODED. EVIDENCE OF CORROSION ON T-CHORD NEAR TO RAM AIR LT STA 1220 LBL50. REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.071''. AFTER BLENDED FOUND FOLLO
- [SDR IPXA2025080239097](https://openairdocs.org/sdr/IPXA2025080239097), Jul 21, 2025: SUPPORT ANGLE. CORRODED. APU INLET DOOR UPPER CORNER ANGLE AT STA 1787.45 S3R HAS CORROSION. REMOVED UPPER CORNER ANGLE WITH CORROSION IAW B757-200 SRM 51-40-02-0G.REMOVED AND REPLACED 
- [SDR IPXA2025080239271](https://openairdocs.org/sdr/IPXA2025080239271), Jul 21, 2025: ANGLE. CORRODED. APU INLET DOOR LOWER CORNER ANGLE AT BS 1787.45 STR 6R HAS CORROSION.REMOVED LOWER CORNER ANGLE WITH CORROSION IAW B757-200 SRM 51-40-02-0G.REMOVED AND REPLACED
- [SDR IPXA2025081314120](https://openairdocs.org/sdr/IPXA2025081314120), Jul 19, 2025: CAM. DAMAGED. CREW DOOR LOWER LATCH CAM HAS A GOUGE ON OUTER SIDE. ACCOMPLISHED JOB IN SREO-14721-REQ001 ((APPX A) CREW ENTRY DOOR UPPER AND LOWER LATCH CAMS REWORK INSTRUCTI
- [SDR IPXA202507214120](https://openairdocs.org/sdr/IPXA202507214120), Jul 19, 2025: CAM. GOUGED. CREW DOOR LOWER LATACH CAM HAS A GOUGE ON OUTER SIDE.
- [SDR IPXA2025072113981](https://openairdocs.org/sdr/IPXA2025072113981), Jul 19, 2025: CAM. GOUGED. CREW DOOR UPPER LATACH CAM HAS A GOUGE ON OUTER SIDE. ACCOMPLISHMENT OF SREO-14721-REQ001.
- [SDR IPXA2025071153206](https://openairdocs.org/sdr/IPXA2025071153206), Jul 3, 2025: INDICATOR. INOPERATIVE. AIR TURN BACK DUE TO RIGHT SIDE FUEL QTY INDICATION INOP REMOVED AND REPLACED ON R/H WING TANK: FUEL PROBES: #1, #2, #3, #4, #5, #7, #8, #9, #10, #11 AND 12, AN
- [SDR IPXA2025070753206](https://openairdocs.org/sdr/IPXA2025070753206), Jul 3, 2025: INDICATOR. INOPERATIVE. AIR TURN BACK DUE TO RIGHT SIDE FUEL QTY INDICATION INOP ACCOMPLISHED DRY CAPACITANCE TEST PER AMM 28-41-00-735-080-002.<BR>RM TU 10 AND 11 CAPACITANCES WITHIN 
- [SDR IPXA2025040792925](https://openairdocs.org/sdr/IPXA2025040792925), Apr 2, 2025: INDICATOR. INOPERATIVE. **SUPPLEMENTAL SDR** DURING CLIMBOUT LEFT MAIN FUEL QTY AND TOTAL FUEL QTY BLANKED OUT. DEFUELED LH MAIN TANK AND PERFORMED FQIS DRY CAPACITANCE TEST PER FIM 28
- [SDR IPXA2025040792867](https://openairdocs.org/sdr/IPXA2025040792867), Apr 2, 2025: INDICATOR. INOPERATIVE. **SUPPLEMENTAL SDR** DURING CLIMBOUT RT MAIN FUEL QTY GAUGE BLANKED OUT TECH SUSPECTED POSSIBLE RH MAIN TANK HARNESS, REFERENCE BARCODE &NBSP;&NBSP;&NBSP;&NBSP;
- [SDR IPXA2025040292925](https://openairdocs.org/sdr/IPXA2025040292925), Apr 2, 2025: INDICATOR. INOPERATIVE. **SDR FILED OPEN** **DIVERSION** DURING CLIMBOUT LEFT MAIN FUEL QTY AND TOTAL FUEL QTY BLANKED OUT.
- [SDR IPXA2025040292867](https://openairdocs.org/sdr/IPXA2025040292867), Apr 2, 2025: INDICATOR. FAILED. **SDR FILED OPEN** **DIVERSION** DURING CLIMBOUT RT MAIN FUEL QTY GAUGE BLANKED OUT
- [SDR IPXA2025030526691](https://openairdocs.org/sdr/IPXA2025030526691), Feb 24, 2025: LIGHT. INOPERATIVE. *SUPPLEMENTAL SDR* INTERIOR EMERGENCY LIGHT INOP ACCOMPLISHED OPS CK OF INTERIOR EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CK GOOD. THIS CLEARS ITEM. PLACARD REMOV
- [SDR IPXA2025022426691](https://openairdocs.org/sdr/IPXA2025022426691), Feb 24, 2025: LIGHT. INOPERATIVE. **SDR FILED OPEN**INTERIOR EMERGENCY LIGHT INOP DEFERRED PER MEL 33-51-1-1. NO DMP, PLACARED INSTALLED.
- [SDR IPXA2024052305539](https://openairdocs.org/sdr/IPXA2024052305539), May 22, 2024: PROCESSOR. FAILED. *** ATB *** ON CLIMB OUT LEFT MAIN TANK FUEL BLANK, INDICATION CAME BACK 90 MINUTES INTO FLIGHT R/R FQIS PROCESSOR IAW AMM 28-41-08 . OPS CHECK GOOD.
- [SDR IPXA2024032045317](https://openairdocs.org/sdr/IPXA2024032045317), Mar 14, 2024: ENGINE. SLOW. LEFT ENGINE SLOW TO SPOOL WHEN POWER PUSHED UP ON TAKEOFF AND IN THE AIR. SLOW ENOUGH TO YAW AIRCRAFT IN THE AIR. ONCE CAUGHT UP ALL PARAMETERS APPEAR NORMAL + 
- [SDR IPXA2024031545317](https://openairdocs.org/sdr/IPXA2024031545317), Mar 14, 2024: GOVERNOR. SLOW. LEFT ENGINE SLOW TO SPOOL WHEN POWER PUSHED UP ON TAKEOFF AND IN THE AIR. SLOW ENOUGH TO YAW AIRCRAFT IN THE AIR. ONCE CAUGHT UP ALL PARAMETERS APPEAR NORMAL + 
- [SDR IPXA2024040259120](https://openairdocs.org/sdr/IPXA2024040259120), Mar 2, 2024: PANEL. DAMAGED. DAMAGE RUDDER HINGE PANEL VERY MOST TOP PANEL DEFERED PER EO-89694 CORRECTIVE ACTION. SPEED TAPE APPLIED TO THE AREA. ITEM CLOSED AND FAULT TRANSFERRED TO BARCO
- [SDR IPXA2024030459120](https://openairdocs.org/sdr/IPXA2024030459120), Mar 2, 2024: HINGE. DAMAGED. *SDR FILED OPEN* DAMAGE RUDDER HINGE PANEL VERY MOST TOP PANEL DAMAGED BONDED PANEL REMOVED. WAITING ON NEW PANEL
- [SDR IPXA2023120557614](https://openairdocs.org/sdr/IPXA2023120557614), Nov 18, 2023: DOOR SILL. DAMAGED. *** SUPPLEMENTAL SDR *** AFT LOWER CARGO COMP. HAS DAMAGE TO INNER SILL PROTECTOR AND UNDERLYING FITTINGS. INSTALLLED AFT LWR SILL PLATE AS REQUIRED REF AMM 20-
- [SDR IPXA2023112057614](https://openairdocs.org/sdr/IPXA2023112057614), Nov 18, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* *MAJOR REPAIR* AFT LOWER CARGO COMP. HAS DAMAGE TO INNER SILL PROTECTOR AND UNDERLYING FITTINGS. REMOVED CLOSEOUT ZEE ANGLE FROM STA 1380 TO ST
- [SDR IPXA61502](https://openairdocs.org/sdr/IPXA61502), Sep 15, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* GEAR DISAGREE EICAS WITH NO RIGHT MAIN GEAR DOWN
- [SDR IPXA2023090693849](https://openairdocs.org/sdr/IPXA2023090693849), Aug 22, 2023: SKIN. CRACKED. LEFT WING FIXED LEADING EDGE HAS CRACK BEHIND SLAT#4 OUTBOARD END REPAIR ACCOMPLISHED ON FAULT: T3F18E002792J. INSTALLED REPAIR PARTS I.A.W. B757-200 S.R.M. 51-
- [SDR IPXA202308230001](https://openairdocs.org/sdr/IPXA202308230001), Aug 22, 2023: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT: LEFT WING FIXED LEADING EDGE HAS CRACK BEHIND SLAT#4 OUTBOARD END

All 207: https://openairdocs.org/aircraft/N469UP/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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