# N466UP: 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: 25482
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 29, 1997
- Certificate issued: September 27, 2007
- Expires: May 31, 2028
- Mode S code: A5B1B5
- 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=466UP
- Page: https://openairdocs.org/aircraft/N466UP

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/N466UP/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 N466UP.

## FAA accident and incident reports

None matched to N466UP.

## Service difficulty reports (193, 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 IPXA2026040311723](https://openairdocs.org/sdr/IPXA2026040311723), Apr 2, 2026: OVERHEAT SYS. FALSE ACTIVATION. EMERGENCY DECLARED, EQUIP OVRHT MSG @ FL 390. DID QRH CHECKLIST YET MSG REMAINED. WENT AWAY @ 1200" AGL. ALSO REF 21-58-00-710-802-011 STEP D. AND STEP E. NO OV
- [SDR IPXA2026030541774](https://openairdocs.org/sdr/IPXA2026030541774), Mar 5, 2026: ADC. INOPERATIVE. AIR TURN BACK - UNRELIABLE AIRSPEED DURING CLIMB OUT. R&R L/H ADC , OPS CHECK GOOD IAW 757 AMM 34-12-01. WORK DONE BY CAT QUALIFIED MECHANIC.
- [SDR IPXA2025083196619](https://openairdocs.org/sdr/IPXA2025083196619), Aug 15, 2025: FLOORBEAM. CORRODED. MDC BETWEEN STA 1100 AND LBL 62 CROSSBEAN WITH CORROSION. ACCOMPLISHED REPAIR PER EO-94866-REQ1 AND VT-MAE 757-5340-27-A4101, REV-.
- [SDR IPXA2025090270617](https://openairdocs.org/sdr/IPXA2025090270617), Aug 14, 2025: STRAP. CORRODED. FWD CARGO COMPT, BS 800-820 CEILING DECOMPRESSION PANEL SUPPORT HAS CORROSION AND (1EA) NUTPLATE LOOSE. STRAP INSTALLED ACCORDING TO IAW SRM 51-40-02. INSTALLED
- [SDR IPXA2025090271962](https://openairdocs.org/sdr/IPXA2025090271962), Aug 14, 2025: TEE FITTING. CORRODED. LOWER CENTER FUSELAGE, STA 1040-1060 LBL 40, LT PACK EXHAUST SUPPORT INTERCOSTAL TEE FITTING HAS EXFOLIATION. INSTALLED 1 NEW TEE FITTING IAW SRM-51-40-02.
- [SDR IPXA2025082770574](https://openairdocs.org/sdr/IPXA2025082770574), Aug 14, 2025: SUPPORT. CORRODED. FWD CARGO COMPT, BS 580 - 600 CEILING DECOMPRESSION PANEL SUPPORT HAS CORROSION. INSTALLED NEW SUPPORT PANEL IN FWD CARGO COMPT BS 580 - 600 CEILING DECOMPRESSI
- [SDR IPXA2025090270230](https://openairdocs.org/sdr/IPXA2025090270230), Aug 14, 2025: TEE FITTING. CORRODED. LEFT AFT BODY FAIRING BS 1220, LBL 65, TEE FITTING HAD CORROSION. INSTALLED A NEW TEE FITTING IAW SRM 51-40-02-0G.
- [SDR IPXA2025090276350](https://openairdocs.org/sdr/IPXA2025090276350), Aug 14, 2025: SKIN. GROUND DAMAGE. FAULT-COMP-Z500- LH WING, SLAT 4 AREA, FIXED L/E SKIN, BY I/B MAIN TRACK, HAS COMPOSITE BROKEN. INSTALLED NEW PANEL ASSY-UPPER SKIN OTBD FIXED L/E. IAW B757-200
- [SDR IPXA2025082957732](https://openairdocs.org/sdr/IPXA2025082957732), Aug 13, 2025: STRAP. CORRODED. AFT CARGO COMPARTMENT CEILING DECOMPRESSION PANEL SUPPORT AT STA 1220 -1240 LBL 40 HAS EXFOLIATION CORROSION. INSTALLED AFT CARGO COMPARTMENT CEILING 153AC IAW 
- [SDR IPXA2025082757796](https://openairdocs.org/sdr/IPXA2025082757796), Aug 13, 2025: STRAP. CORRODED. AFT CARGO COMPARTMENT CEILING DECOMPRESSION PANEL SUPPORT AT STA 1580 LBL 40 HAS CORROSION. INSTALLED CEILING PANEL 161DC AFT CARGO PIT L/H STA 1520-1600 IAW B7
- [SDR IPXA2025082857775](https://openairdocs.org/sdr/IPXA2025082857775), Aug 13, 2025: STRAP. CORRODED. AFT CARGO COMPARTMENT CEILING DECOMPRESSION PANEL SUPPORT AT STA 1400-1420 RBL 45 HAS EXFOLIATION CORROSION. INSTALLED CEILING PANEL 154EC IAW B757-200 AMM 25-5
- [SDR IPXA2025082756968](https://openairdocs.org/sdr/IPXA2025082756968), Aug 13, 2025: TEE FITTING. CORRODED. FUSELAGE LOWER STA 1260 BL 0 TO RBL 50 TEE FITTING HAS SURFACE CORROSION. INSTALLED TEE FITTING AND ANGLES ON STA 1260 BL 0 TO RBL 50, IAW SRM 51-40-02, SRM 51-
- [SDR IPXA2025082944844](https://openairdocs.org/sdr/IPXA2025082944844), Aug 13, 2025: SUPPORT BRACKET. CRACKED. RH WW, FWD CUTOUT, STA. APPROX 1060, BRACKET #6 (I/B TO O/B) HAS A CRACK. INSTALLED NEW BRACKET AT RH WW, FWD CUTOUT, STA. APPROX 1060 IAW B757-200PF SRM 51-40-
- [SDR IPXA2025082741605](https://openairdocs.org/sdr/IPXA2025082741605), Aug 13, 2025: SUPPORT CHANNEL. CRACKED. RIGHT MLG WW FWD SEAL RETAINER ATTACHMENT FRAME CRACKED AT OTBD END. INSTALLED NEW SUPPORT CHANNEL AT RT MLG WW IAW SRM 51-40-02.
- [SDR IPXA2025082350589](https://openairdocs.org/sdr/IPXA2025082350589), Aug 13, 2025: TEE ANGLE. CORRODED. AFT BODY FAIRINGS RH SIDE AT STA 1180 TO 1240 AND RBL 62 T-CHORD EXFOLIATED. INSTALLED T-CHORD FROM STA 1180-1240 R/H IAW B757-200-SRM-51-40-02-OG.
- [SDR IPXA2025082143477](https://openairdocs.org/sdr/IPXA2025082143477), Aug 13, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR, MDC FLOOR, ACCESS PANEL 242XBF HAS EDGES DAMAGED. FABRICATION OF PANEL 242XBF IAW MAIN CARGO COMPARTMENT FLOOR PANAL REPLACEMENT (SREO-9692-RE001)
- [SDR IPXA2025082143382](https://openairdocs.org/sdr/IPXA2025082143382), Aug 13, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR, MDC FLOOR, ACCESS PANEL 242XDF HAS EDGE ANT EXTERNAL SURFACE DAMAGED. FABRICATION OF PANEL 242XBF IAW MAIN CARGO COMPARTMENT FLOOR PANEL REPLACEME
- [SDR IPXA2025082143354](https://openairdocs.org/sdr/IPXA2025082143354), Aug 13, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR, MDC FLOOR, ACCESS PANEL 242XAF HAS EDGES DAMAGED. FABRICATION OF PANAL 242XAF IAW MAIN CARGO COMPARTMENT FLOOR PANEL REPLACEMENT (SREO -9692-REQ00
- [SDR IPXA2025082143295](https://openairdocs.org/sdr/IPXA2025082143295), Aug 13, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR, MDC FLOOR, ACCESS PANEL 242XHF INNER SURFACE HAS SPOTS DAMAGED. FABRICATION OF PANEL 242XHF IAW MAIN CARGO COMPARTMENT FLOOR PANEL REPLACEMENT (SR
- [SDR IPXA2025082143203](https://openairdocs.org/sdr/IPXA2025082143203), Aug 13, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR, MDC FLOOR PANEL, ACCESS PANEL 242XJF EXTERNAL SURFACE HAS SPOTS DAMAGED IN 4 PLACES. FABRICATION OF PANEL 242XJF IAW MAIN CARGO COMPARTMENT FLOOR 
- [SDR IPXA2025082143158](https://openairdocs.org/sdr/IPXA2025082143158), Aug 13, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR, MDC FLOOR, ACCESS PANEL 242XFF HAS EDGE DAMAGE. FABRICATION OF PANEL 242XJF IAW MAIN CARGO COMPARTMENT FLOOR PANEL REPLACEMENT (SREO-9692-REQ001).
- [SDR IPXA2025090435309](https://openairdocs.org/sdr/IPXA2025090435309), Aug 12, 2025: PANEL. CRACKED. NUMBER 2 PYLON VENT PANEL 443CR HAS A CRACK IN UPPER FWD CORNER. ACCOMPLISHED DVI IAW EO B757-5450-82780-A STEP 4(I). FASTENERS ARE IN SERVICEABLE CONDITION.
- [SDR IPXA2025090236564](https://openairdocs.org/sdr/IPXA2025090236564), Aug 12, 2025: TEE ANGLE. CORRODED. BODY FAIRINGS AREA T-COURD AT STA 900 WITH CORROSION. NSTALLED NEW T-CHORD AND SPLICES AT STA 900, IAW B757-200PF SRM 51-70-12-0G-0 PAG 7 FIGURE 1.
- [SDR IPXA2025082226871](https://openairdocs.org/sdr/IPXA2025082226871), Aug 12, 2025: SKIN. CORRODED. PYLON NR 1 OTBD AFT INNER SKIN CORROSION BETWEEN PANELS 433BL AND 433CL. ACCOMPLISHED REPAIR PER EO-94789-REQ1 AND VT-MAE EA 757-5450-27-A4098, REV- WITH NO DEV
- [SDR IPXA2025090233389](https://openairdocs.org/sdr/IPXA2025090233389), Aug 12, 2025: BRACKET. CORRODED. AFT CARGO BULKHEAD LOWER STRUCTURE OF MDC BETWEEN BS 1700 TO 1720 HAVE 5 BRACKETS OF THE NUTPLATE WITH CORROSION. INSTALLED 5EA BRACKETS AT AFT CARGO BULKHEAD L
- [SDR IPXA2025082337065](https://openairdocs.org/sdr/IPXA2025082337065), Aug 12, 2025: TEE FITTING. CORRODED. LEFT LOWER FUSELAGE, STA 1200-1260 LBL 70 T-CHORD HAS (2EA) AREAS WITH DELAMINATION. INSTALLED NEW T-CHORD IN LH LOWER FUSELAGE STA 1200-1260 LBL 70 T-CHORD IAW
- [SDR IPXA2025082135811](https://openairdocs.org/sdr/IPXA2025082135811), Aug 12, 2025: STIFFENER. CORRODED. CORROSION BETWEEN BS 1120 - 1140, LT CHANNEL UNDER PANEL 197EL. INSTALLED A NEW STIFFENER BETWEEN BS 1120-1140 LEFT.
- [SDR IPXA2025090214639](https://openairdocs.org/sdr/IPXA2025090214639), Aug 11, 2025: WEB. CORRODED. EVIDENCE OF CORROSION ON WEB LOWER SECTION STA 1180 TO STA 1240 R/H. INSTALLED WEB LOWER SECTION STA 1180 TO STA 1240 R/H IAW B757-200 SRM 51-40-02. FASTENERS I
- [SDR IPXA2025083014616](https://openairdocs.org/sdr/IPXA2025083014616), Aug 11, 2025: TEE ANGLE. CORRODED. EVIDENCE OF CORROSION ON TEE ANGLE UPPER SECTION STA 1220 RT. INSTALLED TEE ANGLE UPPER BS 1220 RT SIDE UPPER SECTION IAW B757-200 SRM 51-40-02.
- [SDR IPXA2025082315088](https://openairdocs.org/sdr/IPXA2025082315088), Aug 11, 2025: TEE FITTING. CORRODED. EVIDENCE OF CORROSION ON VERTICA LT-CHORD STA 1220 RT. INSTALLED NEW T-CHORD IN STA 1200 R/H IAW B757-200 SRM 51-40-02-0G
- [SDR IPXA2025083098755](https://openairdocs.org/sdr/IPXA2025083098755), Aug 10, 2025: ANGLE. CORRODED. APU INLET DOOR LOWER CORNER ANGLE STA 1785.45 STR 6R HAS CORROSION. INSTALLED LOWER CORNER ANGLE IAW SRM 51-40-02-0G-0.
- [SDR IPXA2025083098735](https://openairdocs.org/sdr/IPXA2025083098735), Aug 10, 2025: ANGLE. CORRODED. APU INLET DOOR UPPER CORNER ANGLE STA 1785.45 STR 3R HAS CORROSION. INSTALLED UPPER CORNER ANGLE IAW SRM 51-40-02-0G-0.
- [SDR IPXA2025083000877](https://openairdocs.org/sdr/IPXA2025083000877), Aug 10, 2025: STRAP. CORRODED. MAJOR REPAIR, APU INLET DOOR AFT STRAP AT STA 1825 HAS EVIDENCE CORROSION. INSTALLED ALL REPAIR PARTS (3EA STRAPS AND 2EA FILLERS), 2 FITTINGS AND 4 ANGLES IAW 
- [SDR IPXA2025082798800](https://openairdocs.org/sdr/IPXA2025082798800), Aug 10, 2025: ANGLE. CORRODED. APU INLET DOOR UPPER ANGLE FROM STA 1785.45 TO STA 1826 AT STR 3R HAS CORROSION. INSTALLED UPPER ANGLE IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2025090298768](https://openairdocs.org/sdr/IPXA2025090298768), Aug 10, 2025: ANGLE. CORRODED. APU INLET DOOR LOWER ANGLE BS 1785.45 TO 1826, S6R HAD CORROSION. INSTALLED LOWER ANGLE IAW SRM 51-40-02-0G-0.
- [SDR IPXA2025082785917](https://openairdocs.org/sdr/IPXA2025082785917), Aug 9, 2025: STRAP. CORRODED. APU INLET DOOR FWD STRAP AT STA 1787.45 FROM STG 3R TO STG 6R HAS EXFOLIATION, CORROSION. INSTALLED FWD STRAP IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2024071750251](https://openairdocs.org/sdr/IPXA2024071750251), Jul 17, 2024: WINDOW. LEAKING. WATER DRIPPING FROM WINDOW INTO 02 MASK BETWEEN L1 AND L2. ADJUSTED THE LINK ARM TO PUSH WINDOW OUTBOARD TO MAKE CONTACT WITH SEAL. REF AMM 56-11-02-825-013.
- [SDR IPXA2024051065942](https://openairdocs.org/sdr/IPXA2024051065942), May 8, 2024: WINDSHIELD. LEAKING. LOUD SQUEAL FROM L1 WINDOW STARTED AT FL 380 NEAR DAYTONA BEACH. FL 210 6 PSI SQUEAL WENT AWAY. R/R L1 WINDSHIELD ASSY PER AMM 56-11-01.
- [SDR IPXA2023090377830](https://openairdocs.org/sdr/IPXA2023090377830), Aug 22, 2023: SHEAR TIE. DENTED. *** MAJOR REPAIR *** FAULT: AFT CARGO PIT STA 1500 AND STR 26 LH - STR 25 LH FRAME HAS A DENT. INSTALLED STRINGER CLIP (2E/A) AT AFT CARGO PIT STA 1500 IAW SRM 
- [SDR IPXA2023090298791](https://openairdocs.org/sdr/IPXA2023090298791), Aug 22, 2023: SHEAR TIE. DENTED. *** MAJOR REPAIR *** FAULT: AFT CARGO COMPT, FRAME, STA 1580 R/H, AT S-26R HAS A DENT. ACCOMPLISHED REINFORCING ANGLE REPAIR IAW PER 757-200PF SRM REV 117.00 CH
- [SDR IPXA2023083177842](https://openairdocs.org/sdr/IPXA2023083177842), Aug 22, 2023: SHEAR TIE. DENTED. AFT CARGO PIT STA 1500 AND STR 26 RH FRAME HAS A DENT. ACCOMPLISHED REINFORCING ANGLE REPAIR IAW PER 757-200PF SRM REV 117.00 CHAPTER 53-00-07-2R-5, DETAIL I PE
- [SDR IPXA2023083177808](https://openairdocs.org/sdr/IPXA2023083177808), Aug 22, 2023: FRAME. DENTED. AFT CARGO PIT STA 1480 AND STR 26 LH FRAME HAS A DENT VERIFIED FINAL INSTALLATION OF FRAME REPAIR.JOB COMPLETE. IAW B757-200PF REV 117.00 SRM 53-00-07-2R-5, TAB
- [SDR IPXA2023090760281](https://openairdocs.org/sdr/IPXA2023090760281), Aug 20, 2023: STRINGER. CORRODED. MAJOR REPAIR. LOWER FUSELAGE SKIN AT STA.1440, STRINGER 29L HAS A BULDGE BETWEEN STRINGER ATTACH RIVETS. DOT 8-001. APPLIED CIC AT NEW STRINGER I.A.W. AMM 51-00
- [SDR IPXA2023090660307](https://openairdocs.org/sdr/IPXA2023090660307), Aug 20, 2023: SHEAR TIE. CORRODED. FAULT- AFT FUSELAGE SKIN BETWEEN STA. 1680-1700, S-27L HAS BULDGING BETWEEN TWO STRINGER RIVETS. DOT 8-002. VERIFIED JOB COMPLETE.
- [SDR IPXA2022042881548](https://openairdocs.org/sdr/IPXA2022042881548), Apr 28, 2022: BRACKET. BROKEN. L1 DOOR PROXIMITY SENSOR SUPPORT BRACKET BROKEN OFF. (DAMAGED BY LOADING).SECURED PROX SENSOR PER EO B757-5210-83581-A. LINK TO M779933. CREW ENTRY DOOR INDICAT
- [SDR IPXA2021092974395](https://openairdocs.org/sdr/IPXA2021092974395), Sep 29, 2021: SKIN. NONE. INSPECTION TYPE:SEG4#2 ENGINE PYLON. OUTBD INTERNAL STRUCTURE HAS BULDGING CORRISION.SKIN REPLACED IAW SRM 51-40-02-0G.
- [SDR IPXA2021092974396](https://openairdocs.org/sdr/IPXA2021092974396), Sep 29, 2021: FLOORBEAM. CORRODED. INSPECTION TYPE:SEG4MAIN CABIN FLOOR BEAM BETWEEN 24.75 RBL - 45.5 STA 1200 SHOWING SIGNS OF CORROSION.REPAIR PER EA# 757-5360-27-A2671 REV-.
- [SDR IPXA2021092574274](https://openairdocs.org/sdr/IPXA2021092574274), Sep 25, 2021: SKIN. CORRODED. INSPECTION TYPE:SEG4#2 ENGINE PYLON, INBD SKIN, INTERIOR, AT APPROX. NAC STA 169.8 INBD SIDE HAS CORROSIONAFTER REMOVED CORROSION IN THE AREA FOUND TO BE IN LIM
- [SDR IPXA2021092474227](https://openairdocs.org/sdr/IPXA2021092474227), Sep 24, 2021: SKIN. CORRODED. INSPECTION TYPE:SEG4#1 ENGINE INBD PYLON FRAME FOR DOOR PANEL 433GR HAS CORROSION ON INSIDE LOWERREMOVE AND REPLACE SKIN
- [SDR IPXA2021092374183](https://openairdocs.org/sdr/IPXA2021092374183), Sep 23, 2021: FLOORBEAM. CORRODED. INSPECTION TYPE:SEG4MAIN CABIN FLOOR BEAM BETWEEN 24.75 RBL - 24.75 LBL STA 110 SHOWING SIGNS OF CORROSIONREPAIRED PER EA# 757-5340-27-A2673 REV-

All 193: https://openairdocs.org/aircraft/N466UP/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.