# N461UP: 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: 28265
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 30, 1997
- Certificate issued: May 29, 2007
- Expires: May 31, 2027
- Mode S code: A59F22
- 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=461UP
- Page: https://openairdocs.org/aircraft/N461UP

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/N461UP/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 N461UP.

## FAA accident and incident reports

None matched to N461UP.

## Service difficulty reports (326, 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 IPXA2026090615170](https://openairdocs.org/sdr/IPXA2026090615170), Sep 6, 2026: BRACKET. CORRODED. APU COMPARTMENT FWD BULKHEAD STA 1885 ALL WIRE HARNESSES AND POWER CABLE CLAMP SUPPORT BRACKETS ATTACHED TO BULKHEAD HAVE CORROSION AND OR MISSING PROTECTIVE FI
- [SDR IPXA2026090615477](https://openairdocs.org/sdr/IPXA2026090615477), Sep 6, 2026: LONGERON. CORRODED. LONGERON 17L LOWER SURFACE BETWEEN BS 1885 & 1963, ATTACHED TO SKIN PANELS TO INCLUDE ALL ADJACENT STRUCURE HAS AREAS OF CORROSION AND MISSING PROTECTIVE FINISH
- [SDR IPXA2026090615708](https://openairdocs.org/sdr/IPXA2026090615708), Sep 6, 2026: SUPPORT FITTING. CORRODED. CANOE PANEL 571BB HAS CORROSION INSIDE THE PIN HOLE. CLEANED AREA AT CANOE PANEL 571BB FOR EVLUATION DAMAGE IAW0 SRM 51-10-02-0G-0. PROCURED FAIRING ASSY. EFFEC
- [SDR IPXA2026090486275](https://openairdocs.org/sdr/IPXA2026090486275), Sep 4, 2026: SKIN. DEBONDED. APU COMPARTMENT, RT SIDE HONEYCOMB SKIN PANEL DISBONDED AREA BETWEEN FRAME STA 1918 AND 1941 AND 24" ABOVE LONGERON 17R. REMOVED DAMAGE AREA SKIN IAW SRM 53-80-
- [SDR IPXA2026090420255](https://openairdocs.org/sdr/IPXA2026090420255), Aug 4, 2026: GUSSET. CORRODED. APU COMPARTMENT FWD BULKHEAD FWD SIDE BS 1885.2, LBL-12 & RBL-9. EXTENSIVE CORROSION. INSTALLED ONE SPLICE RING, ONE LOWER FRAME, ONE INNER TEE CHORD & TWO BRAC
- [SDR IPXA2026082620255](https://openairdocs.org/sdr/IPXA2026082620255), Aug 4, 2026: BULKHEAD. CORRODED. APU COMPARTMENT FWD BULKHEAD FWD SIDE BS 1885.2, LBL 12 & RBL 9. EXTENSIVE CORROSION.
- [SDR IPXA2026080421673](https://openairdocs.org/sdr/IPXA2026080421673), Jul 29, 2026: FLOORBEAM. CORRODED. BULK CARGO MAIN CABIN FLOOR 2EA NUTPLATE RETAINERS CORRODED BS 1681 BL0 TO RBL6. INSTALLED 2EA NUTPLATE RETAINERS AT 1681 BL0 TO RBL6 IAW SRM 51-40-02-0G-0. AND
- [SDR IPXA2026090403739](https://openairdocs.org/sdr/IPXA2026090403739), Jul 28, 2026: DOUBLER. CORRODED. RIGHT FUSELAGE, INSIDE TUNNEL OF TORQUE BOX NLG, WASTE PAN CORRODED. INSTALLED -81, -84, & -88 DOUBLERS, 4EA. GUSSETS, 6EA. TEECLIPS, 2EA. INTERCOSTAL CHANNELS,
- [SDR IPXA2026090803020](https://openairdocs.org/sdr/IPXA2026090803020), Jul 28, 2026: INTERCOSTAL. BENT. INTERCOSTAL UPPER FLANGE IS BENT IN THE AFT LOWER CARGO BAY BS 1366 BETWEEN STR S24R-S25R. REMOVED 2EA STOP FITTINGS AT STA 1380 S24R 1EA CLIP AT STA 1360 S24R 
- [SDR IPXA2026082401195](https://openairdocs.org/sdr/IPXA2026082401195), Jul 28, 2026: SKIN. MISREPAIRED. MAJOR REPAIR. MAJOR REPAIR F1-008 HAS WHAT APPEARS TO BE 2 SETS OF RIVET SET MARKS STA 1540-1580 STGR 28R-29R. VERIFIED STEP 34 ITEM HAS A REPETITIVE INSPECTION
- [SDR IPXA2026090186382](https://openairdocs.org/sdr/IPXA2026090186382), Jul 27, 2026: WEB. CRACKED. MAIN CABIN STA.515 APROX 10" RH FROM BUTTLINE HAS A CRACKED FLOOR SUPPORT WEB. INSTALLED FABRICATED FLOOR SUPPORT IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026090386203](https://openairdocs.org/sdr/IPXA2026090386203), Jul 27, 2026: DECK PLATE. CORRODED. MAJOR REPAIR, MAIN CABIN FLOOR BS 1680 FOUND CORRODED APROX 12" LT FROM BUTTLINE. PERFORMED REPAIR PER SRM 53-60-51-2R-8, REPAIR 8, ALTERNATIVE 1. REFERENCE TAB
- [SDR IPXA2026083180847](https://openairdocs.org/sdr/IPXA2026083180847), Jul 27, 2026: TORQUE BOX. DELAMINATED. MAJOR REPAIR, LT LOWER VERTICAL STABILIZER LOWER FWD TORQUE BOX PANEL HAS AREA OF DELAMINATION AROUND CIRCULAR PATCH/ PLUG NEAR UPPER FWD CORNER. ACCOMPLISHED R
- [SDR IPXA2026090186371](https://openairdocs.org/sdr/IPXA2026090186371), Jul 27, 2026: SPLICE PLATE. CORRODED. MAJOR REPAIR, MAIN CABIN BS 550 APROX 40" LT FROM BUTTLINE AT MAIN CARGO ENTRY SUB FLOOR HAS CORROSION. ACCOMPLISHED THE REPAIR PER EO-98496-REQ1 AND STE-SAA EA
- [SDR IPXA2026080486334](https://openairdocs.org/sdr/IPXA2026080486334), Jul 27, 2026: SUPPORT STRAP. CORRODED. AFT CARGO COMP AS SEEN FROM MAIN CABIN STA.1580 APROX 40" LH FROM BUTTLINE SUPPORT STRAP IS CORRODED. INSTALLED SUPPORT STRAP AND SPLICE ON AFT CARGO COMP. AT B
- [SDR IPXA2026080486315](https://openairdocs.org/sdr/IPXA2026080486315), Jul 27, 2026: SUPPORT STRAP. CORRODED. AFT CARGO COMP AS SEEN FROM MAIN CABIN BS 1580 APROX 20" LH FROM BUTTLINE SUPPORT STRAP IS CORRODED. INSTALLED SUPPORT STRAP AND SPLICE ON AFT CARGO AT STA 1540
- [SDR IPXA2026090468550](https://openairdocs.org/sdr/IPXA2026090468550), Jul 26, 2026: WEDGE. CHAFED. MAJOR REPAIR, LT WING SLAT NR 4 T/E WEDGE LOWER SURFACE CHAFED AT OTBD TRACK AREA. REPAIRED IAW SRM 57-43-02-2R-1 FIG 201, ALL SHEETS AND TABLE 201
- [SDR IPXA2026090468612](https://openairdocs.org/sdr/IPXA2026090468612), Jul 26, 2026: WEDGE. CHAFED. MAJOR REPAIR, LT WING SLAT NR 3 T/E WEDGE LOWER SURFACE CHAFED AT INBD TRACK. ACCOMPLISHED PERMANENT REPAIR IAW SRM 57-43-02-2R-1 FIGURE 201
- [SDR IPXA2026082169457](https://openairdocs.org/sdr/IPXA2026082169457), Jul 26, 2026: SLAT TRACK. CORRODED. NUMBER 9 SLAT INBD MAIN TRACK HAS SIGNS OF PITTING. INSTALLED NR 9 SLAT INBD MAIN TRACK IAW AMM 27-81-12-424-011.
- [SDR IPXA2026082169452](https://openairdocs.org/sdr/IPXA2026082169452), Jul 26, 2026: SLAT TRACK. CORRODED. NUMBER 8 SLAT OTBD MAIN TRACK HAS SIGNS OF PITTING ATA 57 INSTALLED NR 8 SLAT OTBD MAIN TRACK IAW AMM 27-81-12-424-011.
- [SDR IPXA2026081872380](https://openairdocs.org/sdr/IPXA2026081872380), Jul 26, 2026: SKIN. CORRODED. AFTER CLEANING, FOUND CORROSION ON APU TAIL CONE SKIN PANEL AT STA.1963.8 VERIFIED STEP 13 NO REPEAT INSPECTION. REPAIR DOUBLERS FROM MATERIAL REF SRM 53-80-01-
- [SDR IPXA2026091153076](https://openairdocs.org/sdr/IPXA2026091153076), Jul 25, 2026: LONGERON. CORRODED. LONGERON 17L UPPER SURFACE AREA BETWEEN STA 1885 AND 1963 AND ATTACHMENT TO SKIN PANELS TO INCLUDE ALL ADJACENT STRUCURE HAS AREAS OF CORROSION AND MISSING PROT
- [SDR IPXA2026091153193](https://openairdocs.org/sdr/IPXA2026091153193), Jul 25, 2026: ANGLE. CORRODED. LONGERON 17L LOWER SURFACE BETWEEN STA 1885 AND 1963 AND ATTACHMENT TO SKIN PANELS TO INCLUDE ALL ADJACENT STRUCURE HAS AREAS OF CORROSION AND MISSING PROTECTIV
- [SDR IPXA2026090462271](https://openairdocs.org/sdr/IPXA2026090462271), Jul 25, 2026: SKIN. CORRODED. COMP-RH WING I/B FLAP UPPER SKIN SURFACE HAS CORROSION. FLAP BEING REPLACED ON TASK CARD # T3F18E009B8KN LINE 1088
- [SDR IPXA2026091154285](https://openairdocs.org/sdr/IPXA2026091154285), Jul 25, 2026: BRACKET. CORRODED. APU COMPARTMENT FWD BULKHEAD STA 1885 ALL WIRE HARNESSES AND POWER CABLE CLAMP SUPPORT BRACKETS ATTACHED TO BULKHEAD HAVE CORROSION AND OR MISSING PROTECTIVE FI
- [SDR IPXA2026090153257](https://openairdocs.org/sdr/IPXA2026090153257), Jul 25, 2026: SKIN PANEL. DEBONDED. APU COMPARTMENT RT SIDE HONEYCOMB SKIN PANEL LOWER END DISBONDED BETWEEN FRAME STA 1941 AND 1963 JUST ABOVE LONGERON 17R. RL046 PERFORMED REPAIR PER B757-200PF 
- [SDR IPXA2026091153139](https://openairdocs.org/sdr/IPXA2026091153139), Jul 25, 2026: SKIN. DEBONDED. APU COMPARTMENT R/H SIDE HONEYCOMB SKIN PANEL DISBONDED AREA BETWEEN FRAME STA 1918 AND 1941 AND 24" ABOVE LONGERON 17R. RL045 REPAIRED PER SRM 51-70-10-2R-4 RE
- [SDR IPXA2026082254285](https://openairdocs.org/sdr/IPXA2026082254285), Jul 25, 2026: SUPPORT BRACKET. CORRODED. APU COMPARTMENT, FWD BULKHEAD BS 1885, ALL WIRE HARNESSES AND POWER CABLE CLAMP SUPPORT BRACKETS ATTACHED TO BULKHEAD HAVE CORROSION AND OR MISSING PROTECTIVE F
- [SDR IPXA2026090530479](https://openairdocs.org/sdr/IPXA2026090530479), Jul 24, 2026: STIFFENER. CORRODED. APU COMPARTMENT STA-1885 LIGHT SWITCH/ INTERPHONE SUPPORT BRACKET AND ATTACHED HORZ STIFFINER HAS CORROSION AND FILLET SEALANT MISSING IN AREAS. RL013 INSTALLED
- [SDR IPXA2026090432341](https://openairdocs.org/sdr/IPXA2026090432341), Jul 24, 2026: SKIN PANEL. DAMAGED. AFT SIDE OF FRAME STA 1963 AND LOWER METAL HONEYCOMB SKIN PANEL LEVELING COMPOUND AROUND DRAIN HOLES SEPERATED FROM CORRODED STRUCTURE. RL038 INSTALLED SKIN AT 
- [SDR IPXA2026090431507](https://openairdocs.org/sdr/IPXA2026090431507), Jul 24, 2026: DOUBLER. CORRODED. TAIL CONE STA 1992 FRAME FWD AND AFT SIDES HAVE AREAS OF CORROSION AND AREAS OF PROTECTIVE FINISH BLISTERING UP AND PEELING OFF CIRCUMFERENTIALLY AROUND FRAME. 
- [SDR IPXA2026083141623](https://openairdocs.org/sdr/IPXA2026083141623), Jul 24, 2026: WEDGE. DENTED. MAJOR REPAIR, LT WING OTBD FLAP UPPER SURFACE OF T/E WEDGE HAD TWO DENTS INBD & OUTBD. FABRICATED REPAIR PLIES TO INSTALLED AT TWO DAMAGE AREA DAMAGE AREA NR 1 
- [SDR IPXA2026082728931](https://openairdocs.org/sdr/IPXA2026082728931), Jul 24, 2026: SKIN. CORRODED. MAJOR REPAIR, EXTERNAL FUSELAGE SKIN HAS CORROSION BS 1885, LONERON 17R. PERFORMED REPAIR PER SRM 53-80-01-2R-3, REPAIR 3.
- [SDR IPXA2026090342747](https://openairdocs.org/sdr/IPXA2026090342747), Jul 24, 2026: SKIN. DENTED. MAJOR REPAIR. LT WING OTBD MAIN FLAP UPPER SURFACE INBD T/E AREA DENTED. FABRICATED REPAIR PLIES TO INSTALLED AT DAMAGE AREA LOCATED 57" FORM INBD-OTBD AND 11" 
- [SDR IPXA2026072637225](https://openairdocs.org/sdr/IPXA2026072637225), Jul 24, 2026: STRAKE. CORRODED. EVIDENCE OF CORROSION AT BOTTOM SIDE OF RT HORIZ / ABOVE BANANA FAIRING. INSTALLED STRAKELET SUPT. AT BOTTOM SIDE OF RH HORIZ ABOVE BANANA FAIRING IAW SRM 51-40
- [SDR IPXA2026072425384](https://openairdocs.org/sdr/IPXA2026072425384), Jul 23, 2026: SHEAR TIE. CORRODED. AFT CARGO LOWER FRAME SHEAR TIE AT STGR 28L EXFOLIATED BS 1460. INSTALLED REPLACEMENT SHEAR TIE AT S-28L BS 1460 REF 757SRM 51-40-02-0G-0
- [SDR IPXA2026090225381](https://openairdocs.org/sdr/IPXA2026090225381), Jul 23, 2026: SKIN SPLICE. CORRODED. MAJOR REPAIR, AFT CARGO FUSELAGE LOWER SKIN SPLICE AT STR 28L EXFOLIATED BS 1460. ACCOMPLISHED THE REPAIR PER EO-98505-REQ1 AND STE-SAA EA 757-5360-01-B0799, RE
- [SDR IPXA2026090225321](https://openairdocs.org/sdr/IPXA2026090225321), Jul 23, 2026: STRINGER. CORRODED. MAJOR REPAIR, AFT CARGO STRINGER 28L EXFOLIATED BS 1460. ACCOMPLISHED THE PERMANENT REPAIR PER EO-98492-REQ1 AND STE-SAA EA 757-5360-01-B0796, REV. I/R.
- [SDR IPXA2026090225374](https://openairdocs.org/sdr/IPXA2026090225374), Jul 23, 2026: FRAME. CORRODED. MAJOR REPAIR, AFT CARGO FLOOR FRAME AT STR 28L EXFOLIATED BS 1460. ACCOMPLISHED REPAIR PER EO-98508-REQ1 AND STE-SAA EA 757-5360-01-B0798, REV. I/R
- [SDR IPXA2026072725384](https://openairdocs.org/sdr/IPXA2026072725384), Jul 23, 2026: SHEAR TIE. CORRODED. AFT CARGO LOWER FRAME SHEAR TIE AT STGR 28L EXFOLIATED STA 1460 STR 28L GM009 AFTER FURTHER EVALUATION FOUND SHEAR TIE AT S28L BS 1460 WITH 100% MAT. LOSS AND R
- [SDR IPXA2025060801104](https://openairdocs.org/sdr/IPXA2025060801104), Jun 7, 2025: BLOWER. INOPERATIVE. F/O€™S EVAS FAILS BLOWER TEST. BLOWER DOES NOT COME ON. R&R RH (1ST OFFICER) EVAS UNIT IAW MM 25-69-00. OPS CK OK
- [SDR IPXA2025040730719](https://openairdocs.org/sdr/IPXA2025040730719), Mar 29, 2025: PANEL. DAMAGED. CORROSION ON LEFT APU DOOR FRAME NEAR FWD HINGE MARKED WITH TAPE. LH APU DOOR REPAIRED, REF BARCODE T3F18E006CWEK AND T3F18E006E00H. APU DOOR REINSTALLED THIS C
- [SDR IPXA2025033130719](https://openairdocs.org/sdr/IPXA2025033130719), Mar 29, 2025: DOOR FRAME. CORRODED. **SDR FILED OPEN** CORROSION ON LEFT APU DOOR FRAME NEAR FWD HINGE MARKED WITH TAPE MATERIALS:<BR>2024 T3 (.040) PO# SP2752491
- [SDR IPXA2025030751420](https://openairdocs.org/sdr/IPXA2025030751420), Mar 4, 2025: WARNING LIGHT. FALSE ACTIVATION. L FWD ENT DOOR EICAS AFTER BLOCK OUT. RERFORMED ADJUSTMENT AND TEST OF FWD ENTRY DOOR SWITCH PER AMM 52-71-00-825-223. OPS CHECK GOOD. THIS CLEARS DEFERRAL. PLA
- [SDR IPXA2025030451420](https://openairdocs.org/sdr/IPXA2025030451420), Mar 4, 2025: WARNING MESSAGE. ILLUMINATED. L FWD ENT DOOR EICAS AFTER BLOCK OUT DEFERRED CREW ENTRY DOOR INDICATION IAW MEL 52-71-1. DMP C/W PLACARD APPLIED. OPEN
- [SDR IPXA2025020576230](https://openairdocs.org/sdr/IPXA2025020576230), Feb 5, 2025: FLAP SYSTEM. FAULTED. *EMERGENCY DECLARED* TE DISAGREE ICAS MSG PERFORMED FIM TASK 27-51 FAULT TREE 808. NO FAULTS ON FSEU 1, 2 , & 3. OPERATED FLAPS AND SLATS SYS MULITPLE TIMES. CO
- [SDR IPXA2024122332898](https://openairdocs.org/sdr/IPXA2024122332898), Dec 21, 2024: WINDOW. LACK OF LUBE. L2 WINDOW IS HARD TO CLOSE. LUBRICATED L2 WINDOW SEAL. L2 WINDOW OPERATES NORMAL REF B757 AMM 56-11-02
- [SDR IPXA2024110418329](https://openairdocs.org/sdr/IPXA2024110418329), Nov 1, 2024: WARNING LIGHT. FALSE ACTIVATION. **AIR TURN BACK** DUE TO LEFT REVERSER LIGHT AT 10K FT LIGHT REMAINED ILLUMINATED FOR 15 MINUTES NO BUFFETING OR YAW LIGHT EXTINGUISHED AFTER 15 MINUTES. CLEANE
- [SDR IPXA2024091345662](https://openairdocs.org/sdr/IPXA2024091345662), Sep 11, 2024: SPLASH GUARD. MISSING. **SUPPLEMENTAL SDR** F/O EVAS SPLASH GUARD COVER MISSING. INSTALLED SPLASH GUARD AS NEEDED MM 25-60-00
- [SDR IPXA2024091345563](https://openairdocs.org/sdr/IPXA2024091345563), Sep 11, 2024: SPLASH GUARD. MISSING. **SUPPLEMENTAL SDR** CAPT EVAS SPLASH GUARD COVER MISSING. INSTALLED SPLASH GUARD AS NEEDED MM 25-60-00

All 326: https://openairdocs.org/aircraft/N461UP/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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