# N465UP: 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: 28269
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 15, 1997
- Certificate issued: September 22, 1997
- Expires: May 31, 2028
- Mode S code: A5ADFE
- 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=465UP
- Page: https://openairdocs.org/aircraft/N465UP

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/N465UP/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 N465UP.

## FAA accident and incident reports

None matched to N465UP.

## Service difficulty reports (208, 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 IPXA2026061235641](https://openairdocs.org/sdr/IPXA2026061235641), Jun 12, 2026: DOUBLER. CORRODED. TOILET/WASTE PANEL DRAIN VALVE ASSEMBLY, PAN ASSY (INTERNAL AND EXTERNAL DOUBLER) CORRODED
- [SDR IPXA2026060510499](https://openairdocs.org/sdr/IPXA2026060510499), Jun 4, 2026: VALVE. FAULTED. DURING REQUEST OF LEAK CHECK VERIFICATION. FOUND FWD RHS TOILET/WASTE PANEL DRAIN VALVE ASSEMBLY, PAN ASSY (INTERNAL AND EXTERNAL DOUBLER) CORRODED, INSTALLED N
- [SDR IPXA2025090405528](https://openairdocs.org/sdr/IPXA2025090405528), Sep 4, 2025: SEAL. DIRTY. L1 DOOR IS VERY DIFFICULT TO OPEN. ADJUSTED AND CLEANED L1 DOOR SEAL AND DOOR LINING REF. AMM 52-12-00. DOOR OPS CHECKS NORMAL.
- [SDR IPXA2025052810387](https://openairdocs.org/sdr/IPXA2025052810387), May 28, 2025: HYDRAULIC SYSTEM. WARNING MESSAGE. **ATB** ON TAKE OFF AFTER- 80 KTS , LEFT HYD QTY IN FLIGHT PROGRESSED TO (L) HYD SYS PRESS, ALT GEAR EXTEND, AND ALT FLAP EXTEND. FOUND FLAP/SLAT DEPRESSURIZATI
- [SDR IPXA2025022783755](https://openairdocs.org/sdr/IPXA2025022783755), Feb 21, 2025: RETAINER. CORRODED. FAULT: Z193 LH MLG WW DOOR TANG FWD BULB SEAL RETAINER IS EXFOLIATED. VERIFIED REMOVAL OF CORROSION FROM WW DOOR TANG BULB SEAL RETAINER PN 1496016-41. ORIGINAL
- [SDR IPXA2025030354337](https://openairdocs.org/sdr/IPXA2025030354337), Feb 14, 2025: FASTENER. MISSING. FAULT-STR-ZONE 400. ENG #2 O/B T/R FWD UPPER CHANNEL HAS (1EA) FASTENER MISSING. DOT 28-81. INSTALLED FASTENER (1EA) AT ENG #2 O/B T/R FWD UPPER CHANNEL, IAW B7
- [SDR IPXA2025030636262](https://openairdocs.org/sdr/IPXA2025030636262), Feb 13, 2025: ACCESS DOOR. DELAMINATED. PANEL 532HZ IS DELAMINATED.ACCOMPLISHED REPAIR PER 757-200PF SRM REV 122 CHAPTER 51-70-07 (250 DEGREE CURE), PER SRM 57-20-09-2R-1.CLEANED & EVALUATED PANEL 532
- [SDR IPXA2025030636145](https://openairdocs.org/sdr/IPXA2025030636145), Feb 13, 2025: PANEL. DELAMINATED. COMP DRY BAY DOOR CUT OUT HAS COMPOSITE DELAM. ACCOMPLISHED REPAIR PER VT-MAE EA 757-5720-27-A3804.
- [SDR IPXA2025021397102](https://openairdocs.org/sdr/IPXA2025021397102), Feb 12, 2025: STRIP. CRACKED. FAULT-STR- ZONE 420, ACCESS PANEL 425BL METAL STRIP EDGE CRACKED. DOT 68-16.REMOVED SEAL, HINGE-REAR WITH CRACK IAW SRM B757-200 TASK: 51-40-02.INSTALLED NEW SE
- [SDR IPXA2025022693724](https://openairdocs.org/sdr/IPXA2025022693724), Feb 11, 2025: FLOOR PANEL. CRACKED. FAULT-STR-ZONE 100. AFT CARGO COMPT FLOOR PANEL 153BF HAS A CRACK. DOT 28-57.FABRICATED NEW FLOOR PANEL 153BF IAW GMM 09.08.01.03.
- [SDR IPXA2025021378219](https://openairdocs.org/sdr/IPXA2025021378219), Feb 11, 2025: BRACKET. CRACKED. FAULT: STR Z800 FWD LWR CARGO DOOR HAS A CRACK IN AN "L" BRACKET LOCATED IN THE FWD UPPER CORNER. DOT 06677-03.INSTALLED BRACKET WITH (3EA) BACR15FT6D6C, BATCH:
- [SDR IPXA2025021271069](https://openairdocs.org/sdr/IPXA2025021271069), Feb 10, 2025: SKIN. CRACKED. LH WING LEADING EDGE UPPER SURFACE AT SLAT #4 LOCATION, HAS 1 CRACK. DOT 28-38. MADE A REPLACEMENT SKIN FROM 2024-T3 CLAD SHEET, 0.100''. PER E.A. #: 757-5741-2
- [SDR IPXA2025021577164](https://openairdocs.org/sdr/IPXA2025021577164), Feb 10, 2025: FLOORBEAM. CORRODED. FAULT-STR- ZONE 142 MAIN CARGO COMPARTMENT RIGHT SIDE STA 1020, BL 0 TO RBL 24.5 FLOOR BEAM SUPPORT CHANNEL SPOTS WITH CORROSION. CLEANED MAIN CARGO COMPARTMENT
- [SDR IPXA2025021577074](https://openairdocs.org/sdr/IPXA2025021577074), Feb 10, 2025: SUPPORT CHANNEL. CORRODED. MAIN CARGO COMPARTMENT LEFT SIDE STA 1050 BL 0 TO LBL 24.5 FLOOR BEAM SUPPORT CHANNEL SPOTS WITH CORROSION. DOT 68-02 FR-68. LOCATED AND DRILLED NEW TEE SUPORT 
- [SDR IPXA2025022576954](https://openairdocs.org/sdr/IPXA2025022576954), Feb 10, 2025: FLOORBEAM. CORRODED. MAIN CARGO COMPARTMENT LEFT SIDE STA 1050 LBL 45.5 TO LBL 65.5 FLOOR BEAM SUPPORT CHANNEL SPOTS WITH CORROSION. DOT 68-01 FR-68. REMOVE AND REPLACE 1 EACH FLOOR
- [SDR IPXA2025021760646](https://openairdocs.org/sdr/IPXA2025021760646), Feb 9, 2025: CAM. GOUGED. MAIN CREW DOOR LWR CAMLATCH HAS GOUGE ON OUTER SURFACE. DOT 69/006. EL-69. BLEND OUT GOUGE ON MAIN CREW DOOR LWR CAMLATCH IAW B757-200PF, SRM 51-10-02. SURFACE 
- [SDR IPXA2025021760600](https://openairdocs.org/sdr/IPXA2025021760600), Feb 9, 2025: LATCH. GOUGED. MAIN CREW DOOR UPPER CAMLATCH HAS GOUGE ON OUTER SURFACE. DOT 69/005. EL-69. SURFACE HFEC PERFORMED ON MAIN CREW DOOR UPPER CAM LATCH BLENDED AREA. NO DEFECTS F
- [SDR IPXA2025021060646](https://openairdocs.org/sdr/IPXA2025021060646), Feb 9, 2025: CAM. GOUGED. MAIN CREW DOOR LWR CAMLATCH HAS GOUGE ON OUTER SURFACE.
- [SDR IPXA2025021060600](https://openairdocs.org/sdr/IPXA2025021060600), Feb 9, 2025: CAM. GOUGED. MAIN CREW DOOR UPPER CAMLATCH HAS GOUGE ON OUTER SURFACE.
- [SDR IPXA2025020848485](https://openairdocs.org/sdr/IPXA2025020848485), Feb 8, 2025: FLOORBEAM. CORRODED. FAULT: Z100 STR FS 1240 RBL 22 TO RBL 30 FWD FLANGE OF LOWER TEE CHORD HAS SEVERE INTERGRANULAR CORROSION. INSTALLED T-CHORD AN ANGLES ON STR FS 1240 RBL IAW B7
- [SDR IPXA2025022851520](https://openairdocs.org/sdr/IPXA2025022851520), Feb 8, 2025: FLOORBEAM. CORRODED. FAULT: Z100 STR FS 900 BETWEEN RBL 12 TO RBL 16.5 LOWER TEE CHORD HAS CORROSION. INSTALLED OUTBOARD CHORD AND 8(EA) REPAIR PLATES AT STA 900 I.A.W SRM 51-70-12-
- [SDR IPXA2025022751440](https://openairdocs.org/sdr/IPXA2025022751440), Feb 8, 2025: FLOORBEAM. CORRODED. FS 1037 RBL 59 LOWER TEE CHORD HAS CORROSION FWD AND AFT FLANGE. RESTORED SURFACE PROTECTION AT NEW T-CHORD IAW B757-200PF SRM 51-20-01-0G-0. ALODINE P/N; ALODI
- [SDR IPXA2025020848535](https://openairdocs.org/sdr/IPXA2025020848535), Feb 8, 2025: TEE ANGLE. CORRODED. FS 1238- FS 1240 RBL 31 INBD LOWER TEE CHORD FLANGE HAS SEVERE INTERGRANULAR CORROSION. REMOVE AND REPLACE 1 EACH RBL 30.75 (P/N: 149N7633-14) LOWER TEE CHORD A
- [SDR IPXA2024060535801](https://openairdocs.org/sdr/IPXA2024060535801), May 31, 2024: IDG. FAULTED. **SUPPLEMENTAL SDR**L GEN DRIVE EICAS MESSAGE DURING DECENT PHASE OF FLIGHT. COMPLIED WITH QRH PROCEDURE R&R LH ENGINE IDG REF 757 AMM 24-11-01 OPS AND LEAK CK 
- [SDR IPXA2024053135801](https://openairdocs.org/sdr/IPXA2024053135801), May 31, 2024: WARNING LIGHT. ILLUMINATED. LEFT GEN DRIVE EICAS MESSAGE DURING DECENT PHASE OF FLIGHT. COMPLIED WITH QRH PROCEDURE DEFERRED LH IDG PER MEL 24-00-1. C/W DMP. VERIFIED IDG DISCONNECTED WITH
- [SDR IPXA2024012502634](https://openairdocs.org/sdr/IPXA2024012502634), Jan 24, 2024: DOOR. STUCK. CREW ENTRY DOOR JAMMED AND WAS UNABLE TO ENTER AIRCRAFT WITHOUT EFFORT OF SOMEONE INSIDE THE COCKPIT, WAS OPENED WITH GREAT DIFFICULTY CLEANED BOTTOM OF SEAL AF
- [SDR IPXA2023112998124](https://openairdocs.org/sdr/IPXA2023112998124), Nov 28, 2023: FLAP. WARNING MESSAGE. *EMERGENCY DECLARED* ON APPROACH LE FLAP DISAGREE LIGHT W/ EICAS CAUTION MESSAGE. WENT AROUND AND LANDED W/ FLAPS 20 USING ALTN FLAP EXTENSION CHECKLIST. PERFOR
- [SDR IPXA2023042793003](https://openairdocs.org/sdr/IPXA2023042793003), Apr 27, 2023: LANDING GEAR. INOPERATIVE. INSPECTION TYPE:NA*SDR FILED OPEN* *ATB* *EMERGENCY DECLARED* AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT- CHECKLIST COMPLETED GEAR SHOWED 3 GREE, LANDING UNEVENT
- [SDR IPXA2023050193059](https://openairdocs.org/sdr/IPXA2023050193059), Apr 23, 2023: LANDING GEAR. WARNING MESSAGE. INSPECTION TYPE:NA*ATB* AFTER SELECTING THE GEAR TO UP THE GREEN NOSE GEAR LIGHT REMAIN ILUMINATED AS DID THE AMBER DOORS AND GEAR LIGHT. EICAS SHOWED GEAR DISA
- [SDR IPXA2023042192952](https://openairdocs.org/sdr/IPXA2023042192952), Apr 21, 2023: WARNING MESSAGE. ILLUMINATED. INSPECTION TYPE:NA*SDR FILED OPEN* *ATB* GEAR DISAGREE AND GEAR DOOR EICAS
- [SDR IPXA2023030491513](https://openairdocs.org/sdr/IPXA2023030491513), Feb 22, 2023: FLOORBEAM. CORRODED. INSPECTION TYPE:SEG1*MAJOR REPAIR* MAIN CARGO COMPARTMENT, STA 1600 LBL 55, FLOOR BEAM UPPER CHORD HAS CORROSIONREPAIRED PER UPS RCD 271627 AND VT MAE EA 757-53
- [SDR IPXA2023030491514](https://openairdocs.org/sdr/IPXA2023030491514), Feb 20, 2023: SKIN. CORRODED. INSPECTION TYPE:SEG1#2 ENGINE PYLON INBD SKIN AT THE FWD HINGE DOOR INNER AFT LIP HAS A EXFOLIATION CORROSIONCORROSION FOUND TO BE OUT OF LIMITS, REMOVED AND RE
- [SDR IPXA2023030591540](https://openairdocs.org/sdr/IPXA2023030591540), Feb 18, 2023: SKIN. CORRODED. INSPECTION TYPE:SEG1*MAJOR REPAIR* #1 ENGINE OUTBD PYLON SKIN OF VENT 433CL OPENING HAS EXFOLIATION CORROSION ON THE INNER SKINREPAIR PER UPS RCD 271422 AND VT 
- [SDR IPXA2023030391502](https://openairdocs.org/sdr/IPXA2023030391502), Feb 18, 2023: SKIN. CORRODED. INSPECTION TYPE:SEG1#2 ENGINE PYLON OUTBD EXTERIOR SKIN BELLOW PANEL 443AR HAS BULDGING CORROSIONREPAIRED PER EA 757-5450-27-A3152 REV-
- [SDR IPXA2021082473088](https://openairdocs.org/sdr/IPXA2021082473088), Aug 22, 2021: RADAR. FAULTED. INSPECTION TYPE:N/A**AIR TURNBACK** ENROUTE RECIVED ON BOTH CAPT & F/O PFD EXR FAIC AND EXR WEAK AT FL340 ALSO RECEIVED A EXR SYS STATUS MESSAGE DUE TO ENROUTE 
- [SDR IPXA2021042468568](https://openairdocs.org/sdr/IPXA2021042468568), Apr 24, 2021: BARRIER. CRACKED. INSPECTION TYPE:SEG2 EA CRACKS ON THE LH WING DRY BAY BARRIER (P/N: 112N8004-15) COMMON TO DRY BAY ACCESS DOOR 532HZACCOMPLISHED WORK PER PRELIM 1 EA 757-5720-2
- [SDR IPXA2021042068451](https://openairdocs.org/sdr/IPXA2021042068451), Apr 20, 2021: FITTING. CRACKED. INSPECTION TYPE:SEGREMOVE O/B DRAG LINK FITTING P/N 653N0002-15 FROM #1 PYLON. REMOVED AND REPLACED IAW EA 757-5720-27-A2563 REV
- [SDR IPXA2021042068450](https://openairdocs.org/sdr/IPXA2021042068450), Apr 20, 2021: FITTING. CRACKED. INSPECTION TYPE:SEGREMOVE #1 PYLON I/B DRAG LINK FITTING P/N: 653N0002-13REMOVED AND REPLACED IAW EA# 757-5720-27-A2563 REV
- [SDR IPXA2021041368178](https://openairdocs.org/sdr/IPXA2021041368178), Apr 13, 2021: SEAT TRACK. CORRODED. INSPECTION TYPE:SEG4SEAT TRACK LOCATED AT STA 1060-1080 HAS CORROSIONREMOVED AND REPLACED SEAT TRACK IAW SRM 53-00-52-1A-1 DET VII
- [SDR IPXA2021033167573](https://openairdocs.org/sdr/IPXA2021033167573), Mar 31, 2021: SKIN. DELAMINATED. INSPECTION TYPE: SEG DELAMINATION ON THE UPPER SKIN SECTION 48. REPAIRED PANEL IAW B757 SRM 51-70-10-2R-2 350 DEG F CURE PER SRM 53-80-01-2R FIG 201.
- [SDR IPXA2021030766499](https://openairdocs.org/sdr/IPXA2021030766499), Mar 6, 2021: A/C PACK. ODOR. INSPECTION TYPE:N/ASLIGHT OILY SMELL COMING FROM THE PACKS. MORE PRONOUNCED WITH THE LEFT PACK ON. AT ALTITUDE OIL PRESSURE LEFT ENGINE 51, RIGHT ENGINE 91.R+R 
- [SDR IPXA2020072097927](https://openairdocs.org/sdr/IPXA2020072097927), Jul 18, 2020: LINE. UNSECURE. EMERGENCY DECLARED, LANDED AND REQUIRED TOW FROM RUNWAY. LEFT HYD QTY EICAS C, LT HYD QTY DECREASED DURING FLIGHT TO 0.20. DRY MOTORED LT ENGINE, NO LEAKS NOTED
- [SDR IPXA2019042294243](https://openairdocs.org/sdr/IPXA2019042294243), Apr 19, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MAIN CARGO COMPARTMENT FLOOR PANEL 222XCF IS DAMAGEDFABBED PANEL 222XCF FROM 5024N400001SS-G, BATCH # 3467574 PER SREO B757-5320-9692-K
- [SDR IPXA2019042294241](https://openairdocs.org/sdr/IPXA2019042294241), Apr 19, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MAIN CARGO COMPARTMENT FLOOR PANEL 231XDF IS DAMAGEDFABBED PANEL 231XDF FROM 5024N400001SS-G, BATCH # 3467574 PER SREO B757-5320-9692-K
- [SDR IPXA2019042294240](https://openairdocs.org/sdr/IPXA2019042294240), Apr 19, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE: SEG3, MAIN CARGO COMPARTMENT FLOOR PANEL 231XEF IS DAMAGED. FABRICATED A NEW FLOOR PANEL PER SREO B757-5320-9692-K.
- [SDR IPXA2019041941239](https://openairdocs.org/sdr/IPXA2019041941239), Apr 19, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG3, MAIN CARGO COMPARTMENT FLOOR PANEL 231XHF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL PER SREO B757-53320-9692-K.
- [SDR IPXA2019041941237](https://openairdocs.org/sdr/IPXA2019041941237), Apr 19, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG3, MAIN CARGO COMPARTMENT FLOOR PANEL 222XAF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL PER SREO B757-5320-9692-K.
- [SDR IPXA2019041941236](https://openairdocs.org/sdr/IPXA2019041941236), Apr 19, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE: SEG3, MAIN CARGO COMPARTMENT FLOOR PANEL 221XCF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL PER SREO B757-5320-9692-K.
- [SDR IPXA2019041941235](https://openairdocs.org/sdr/IPXA2019041941235), Apr 19, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3, MAIN CARGO COMPARTMENT FLOOR PANEL 221XBF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL PER SREO B757-5320-9692-K.
- [SDR IPXA2019041941234](https://openairdocs.org/sdr/IPXA2019041941234), Apr 19, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG3, MAIN CARGO COMPARTMENT FLOOR PANEL 221XAF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL PER SREO B757-5320-9692-K.

All 208: https://openairdocs.org/aircraft/N465UP/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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