# N467UP: 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: 25483
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 29, 1997
- Certificate issued: September 28, 2007
- Expires: May 31, 2028
- Mode S code: A5B56C
- 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=467UP
- Page: https://openairdocs.org/aircraft/N467UP

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/N467UP/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 N467UP.

## 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 19980513013829I](https://openairdocs.org/incident/19980513013829I), May 13, 1998: Boeing 757200 (N467UP), Dallas-Ft Worth, TX, Substantial damage. Narrative: inspectors hudson and getso were dispatched to the ups ramp and took pictures of the damaged area of the aircraft. The ups chief pilot, Mr. Larry…

## Service difficulty reports (156, 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 IPXA2024112906836](https://openairdocs.org/sdr/IPXA2024112906836), Nov 5, 2024: FLOORBEAM. CORRODED. CORROSION FOUND ON EXISTING REPAIR AT MAIN CARGO COMPARTMENT FLOOR BEAM STA 1200 BL 0 TO LBL 25. VERIFIED REPAIR WAS ACCOMPLISHED PER EA 757-5360-27-A3734 AND U
- [SDR IPXA2024112978354](https://openairdocs.org/sdr/IPXA2024112978354), Nov 4, 2024: TEE ANGLE. CORRODED. WTB TEE CHORD SUPPORT FROM STA 1180 TO STA 1240 RBL 63 IS CORRODED. INSTALLED TEE CHORD AT STA 1180 TO STA 1240 RBL 63 PER SRM 51-40-02.
- [SDR IPXA2024120348337](https://openairdocs.org/sdr/IPXA2024120348337), Nov 3, 2024: LATCH. GOUGED. CREW ENTRY DOOR LWR FWD LOCK FITTING IS GOUGE AND BARE METAL. DOT 142-001. REF STEP 6. VERIFED STEP 4 WAS ACCOMPLISHED PER SRE0-14721-REQ001. MEASURES AT CREW E
- [SDR IPXA2024110448337](https://openairdocs.org/sdr/IPXA2024110448337), Nov 3, 2024: FITTING. GOUGED. CREW ENTRY DOOR LWR FWD LOCK FITTING IS GOUGE AND BARE METAL. DOT 142-001 APPROVED
- [SDR IPXA2024112644825](https://openairdocs.org/sdr/IPXA2024112644825), Nov 2, 2024: TEE FITTING. CORRODED. FAULT : STR TEE CHORD SUPPORT FOR WTB FAIRINGS AT STA 900 HAS CORROSION FROM LBL 20 TO RBL 20 APPROX. INSTALLED 4EA PLATES-5, 4EA PLATES-6 AND 1EA OUTBOARD CHOR
- [SDR IPXA2024111541838](https://openairdocs.org/sdr/IPXA2024111541838), Nov 2, 2024: FLOOR PANEL. BROKEN. FLOOR PANEL 242XCF IS BROKEN. FABRICATED FLOOR PANEL 242XCF USING MATERIAL P/N:5024N400001SS-G BATCH#:0004055277 INSERTS:BOTTOM P/N: G2002B-3S BATCH#:0003290203
- [SDR IPXA2024111338411](https://openairdocs.org/sdr/IPXA2024111338411), Nov 2, 2024: SKIN. CORRODED. #2 PYLON, LEFT SIDE SKIN, INSIDE PANEL 443GL WITH CORROSION (RED MARKS). DOT 73-015. INSTALLED 1EA SKIN, 1EA FAIRING SKIN, 1EA CHANNEL AND 1EA BRACKET IAW B757-
- [SDR IPXA2024112931133](https://openairdocs.org/sdr/IPXA2024112931133), Nov 1, 2024: FLOORBEAM. CORRODED. CORROSION FOUND AT MAIN CARGO COMPARTMENT FLOORBEAM BS 1100 RBL 15 APROX. INSTALLED IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2024111899922](https://openairdocs.org/sdr/IPXA2024111899922), Oct 31, 2024: SKIN. DENTED. LOWER FUSELAGE SKIN HAS DENT AT STA 440/456 AND STR 28/29. NO DOT TG-101. FABRICATED 1EA REPAIR DOUBLER AND 1EA FILLER TO ACCOMPLISHED E.A# 757-5330-27-A3725 PR
- [SDR IPXA2024090489688](https://openairdocs.org/sdr/IPXA2024090489688), Sep 2, 2024: ENGINE. MALFUNCTIONED. AIR TURNBACK DUE TO LEFT ENGINE INDICATIONS DEF PER MEL 77-11-1-1 DI # 2823227. PERFORMED TEST 13 TAKE-OFF POWER PER M/M REF 71-00-00-715-223-R03. OPS CK NORMAL
- [SDR IPXA2024090289688](https://openairdocs.org/sdr/IPXA2024090289688), Sep 2, 2024: ENGINE. INDICATION. AIR TURNBACK DUE TO LEFT ENGINE INDICATIONS DEF PER MEL 77-11-1-1. OPEN
- [SDR IPXA2024050689007](https://openairdocs.org/sdr/IPXA2024050689007), May 2, 2024: APU. INOPERATIVE. **SUPPLEMENTAL SDR** IN CRUISE @ FL 380 L ENG N3 BOUNCED BETWEEN 9-85. ON DECENT W/THROTTLES AT IDLE L ENG N3 INDICATED 0. L ENG SPEED CARD STATUS MESSAGE REPLA
- [SDR IPXA2024050389007](https://openairdocs.org/sdr/IPXA2024050389007), May 2, 2024: WARNING MESSAGE. ILLUMINATED. IN CRUISE @ FL 380 L ENG N3 BOUNCED BETWEEN 9-85. ON DECENT W/THROTTLES AT IDLE L ENG N3 INDICATED 0. L ENG SPEED CARD STATUS MESSAGE
- [SDR IPXA2023101044579](https://openairdocs.org/sdr/IPXA2023101044579), Oct 6, 2023: EVAS UNIT. UNKNOWN. CAPTAINS EVAS TEST TOOL MISSING FOUND CAPT. EVAS TEST TOOL AND INSTALLED IN POUCH ON EVAS UNIT REF IPC 25-60-00-90
- [SDR IPXA2023100644579](https://openairdocs.org/sdr/IPXA2023100644579), Oct 6, 2023: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** CAPTAINS EVAS TEST TOOL MISSING
- [SDR IPXA2023081710329](https://openairdocs.org/sdr/IPXA2023081710329), Aug 16, 2023: LIGHT. INOPERATIVE. EMER EXIT LIGHTS INOP REMOVED & REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY W/REF TO M/M 33-51-07-862-054, OPS CHECK GOOD
- [SDR IPXA2023060138762](https://openairdocs.org/sdr/IPXA2023060138762), May 29, 2023: BOLT. VIBRATION. *** SUPPLEMENTAL SDR *** HIGH N1 VIBE INDICATION IN LEFT ENGINE REMOVED ALL EXISTING TRIM BALANCE BOLT ASSEMBLIES AND REPLACED WITH STANDARD BOLTS IN POSITION 5
- [SDR IPXA202305308762](https://openairdocs.org/sdr/IPXA202305308762), May 29, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* *DIVERSION* HIGH N1 VIBE INDICATION IN LEFT ENGINE
- [SDR IPXA2023021691036](https://openairdocs.org/sdr/IPXA2023021691036), Feb 15, 2023: LEVER. INOPERATIVE. *ATB* *EMER DECL* DRING CL OUT ENGGED VNAV L ENG STCK IN TO POS. CAPT & FO TRIED TO PULL IT BACK RETRCTED FLPS LVLED OFF AT 500FT. AIRSPD INCREAS UNBLE TO CNTRL
- [SDR IPXA2023012090082](https://openairdocs.org/sdr/IPXA2023012090082), Jan 10, 2023: STIFFENER. CORRODED. INSPECTION TYPE:SEG1DURING THE REMOVAL OF THE RIGHT WING AILERON PANEL FOUND STIFFENER ASSY WITH CORROSION. REMOVED THE STIFFENER IAW SRM 51-40-02-0G, FABRICATE
- [SDR IPXA2023011990063](https://openairdocs.org/sdr/IPXA2023011990063), Jan 4, 2023: FRAME. DENTED. INSPECTION TYPE:SEG1, FRAME BS 1280 IN THE AFT CARGO COMPT, HAS A DENT ON TOP OF THE FRAME FLANGE, S26R, ACCOMPLISHED REPAIR IAW SRM REV 115.00, 53-00-07-2R-6 T
- [SDR IPXA2023011990062](https://openairdocs.org/sdr/IPXA2023011990062), Jan 4, 2023: FRAME. DAMAGED. INSPECTION TYPE:SEG1, AFT CARGO FRAME AT STA 1500.0 S25-L - S26-L HAS AN EXISTING REPAIR. COMPLY WITH IN BOUND EO B757-5310-79051-A. R & R EXISTING FRAME REPAIR
- [SDR IPXA2023012090085](https://openairdocs.org/sdr/IPXA2023012090085), Jan 4, 2023: SKIN. CORRODED. INSPECTION TYPE:SEG1#1 ENGINE INSIDE O/B FWD PYLON DOOR 433BL BOTTOM RIM IS BULGINGREMOVED SKIN PANEL PER SRM 51-40-02-0G, REMOVED CORROSION AT SKIN PANEL PER S
- [SDR IPXA2023011990059](https://openairdocs.org/sdr/IPXA2023011990059), Jan 4, 2023: SKIN. CORRODED. INSPECTION TYPE:SEG1#1 ENGINE INSIDE O/B PYLON (PPS 124.76) IS SHOWING SIGNS OF CORROSION. REPAIRED PER RCD 264950 AND EA 757-5450-27-A3114 REV-
- [SDR IPXA2021021065542](https://openairdocs.org/sdr/IPXA2021021065542), Feb 9, 2021: INDICATOR. UNRELIABLE. INSPECTION TYPE:NA**ATB - EMERG DECLARED - NO EMERG EQUP USED** UNREALIABLE AIRSPEED INDICATIONREMOVED PITOT TUBE COVERS, INSPECTED PITOT TUBES, REF AMM 34-11-0
- [SDR IPXA2021011964666](https://openairdocs.org/sdr/IPXA2021011964666), Jan 19, 2021: FRAME. DENTED. INSPECTION TYPE: SEF 4 AFT CARGO STA 1500 S26L-S25L HAS DENT. REPAIRED PER EO B757-5310-79051-A.
- [SDR IPXA2021011564461](https://openairdocs.org/sdr/IPXA2021011564461), Jan 15, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG4, MAIN CARGO COMPT FLOOR PANEL 241XGF IS DAMAGED.FABBED PANEL 241XGF IAW SREO B757-5320-9692-K.
- [SDR IPXA2021011560461](https://openairdocs.org/sdr/IPXA2021011560461), Jan 15, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE: SEG 4 MAIN EQUIPMENT CENTER WALKWAY PANEL 119AF IS DAMAGED. FABBED PANEL 119AF FROM 5024N400001SS-G BATCH 354653, PER SREO B757-5320-9692-K.
- [SDR IPXA2021011564463](https://openairdocs.org/sdr/IPXA2021011564463), Jan 14, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE: SEG 4 MAIN EQUIPMENT CENTER WALKWAY PANEL 119AF IS DAMAGED. FABBED PANEL 191AF FROM 5024N400001SS-G BATCH 354653, PER SREO B757-5320-9692-K.
- [SDR IPXA2019040534756](https://openairdocs.org/sdr/IPXA2019040534756), Apr 3, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 231XJF IS DELAMINATED.FABRICATED PNL 231XJF FROM 5024N400001SS-G BATCH# 3441868 PER SREO B757-5320-9692-K.
- [SDR IPXA2019040340755](https://openairdocs.org/sdr/IPXA2019040340755), Apr 3, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PNL 232XJF IS DELAMINATED.FABRICATED PNL FROM 5024N400001SS-G BATCH # 3441868 PER SREO B757-5320-9692-K.
- [SDR IPXA2019040340744](https://openairdocs.org/sdr/IPXA2019040340744), Apr 3, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 231 XFF IS DELAMINATEDFABRICATED PNL 231XFF FROM 5024N400001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019040240709](https://openairdocs.org/sdr/IPXA2019040240709), Apr 2, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 232XCF IS DELAMINATED. FABRICATED PNL 232XCF FROM 5024N40001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019040324708](https://openairdocs.org/sdr/IPXA2019040324708), Apr 2, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 231XCF IS DELAMINATEDFABRICATED PNL FROM 5024N400001SS-G, BATCH # 3441869 PER SREO B757-5320-9692-K
- [SDR IPXA2019040324707](https://openairdocs.org/sdr/IPXA2019040324707), Apr 2, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 211XAFF IS DELMINATED. FABRICATED PNL 211XAFF FROM 5024N400001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019040324706](https://openairdocs.org/sdr/IPXA2019040324706), Apr 2, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 212XAF IS DELAMINATEDFABRICATED PNL 212XF FROM 5024N00001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019040140639](https://openairdocs.org/sdr/IPXA2019040140639), Mar 21, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 232XGF IS DELAMINATEDFABRICATED PNL 232XGF FROM 5024N400001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019040140638](https://openairdocs.org/sdr/IPXA2019040140638), Mar 21, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 232XHF IS DELAMINATEDFABRICATED PNL 232XHF FROM 5024N400001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019040140637](https://openairdocs.org/sdr/IPXA2019040140637), Mar 21, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 232XFF IS DELAMINATEDFABRICATED PNL 232XFF FROM 5024N400001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019040140636](https://openairdocs.org/sdr/IPXA2019040140636), Mar 21, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 232XEF IS DELAMINATEDFABRICATED PNL 232XEF FROM 5024N400001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019040140635](https://openairdocs.org/sdr/IPXA2019040140635), Mar 21, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 232XDF IS DELAMINATEDFABRICATED PNL 232XDF FROM 5024N400001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019040140634](https://openairdocs.org/sdr/IPXA2019040140634), Mar 21, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 232XBF IS DELAMINATEDFABRICATED PNL 232XBF FROM 5024N400001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019040140633](https://openairdocs.org/sdr/IPXA2019040140633), Mar 21, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 232XAF IS DELAMINATEDFABRICATED PNL 232XAF FROM 5024N400001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019040140632](https://openairdocs.org/sdr/IPXA2019040140632), Mar 21, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 231XHF IS DELAMINATEDFABRICATED PNL 231XHF FROM 5024N400001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019040140631](https://openairdocs.org/sdr/IPXA2019040140631), Mar 21, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 231XGF IS DELAMINATEDFABRICATED PNL 231XGF FROM 5024N400001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019040140630](https://openairdocs.org/sdr/IPXA2019040140630), Mar 21, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 231XEF IS DELAINATEDFABRICATED PNL 231XEF FROM 5024N400001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019033140629](https://openairdocs.org/sdr/IPXA2019033140629), Mar 21, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 231XDF IS DELAMINATEDFABRICATED PNL 231XDF FROM 5024N400001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019040140628](https://openairdocs.org/sdr/IPXA2019040140628), Mar 21, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 231XBF IS DELAMINATEDFABRICATED PNL 231XBF FROM 5024N400001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019040140627](https://openairdocs.org/sdr/IPXA2019040140627), Mar 21, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 222XCF IS DELAMINATEDFABRICATED PNL 221SCF FROM 5024N400001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K
- [SDR IPXA2019040140626](https://openairdocs.org/sdr/IPXA2019040140626), Mar 21, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 222XBF IS DELAMINATEDFABRICATED PNL 222XBF FROM 5024N400001SS-G, BATCH # 3441868 PER SREO B757-5320-9692-K

All 156: https://openairdocs.org/aircraft/N467UP/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.
