# N460UP: 1996 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: 25481
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 14, 1996
- Certificate issued: November 15, 1996
- Expires: November 30, 2028
- Mode S code: A59B6B
- Registered owner: [C C & E I LLC](https://openairdocs.org/faa-owner/C%20C%20%26%20E%20I%20LLC)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: LLC
- 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=460UP
- Page: https://openairdocs.org/aircraft/N460UP

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/N460UP/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 N460UP.

## FAA accident and incident reports

None matched to N460UP.

## Service difficulty reports (205, 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 IPXA2026050849719](https://openairdocs.org/sdr/IPXA2026050849719), May 6, 2026: PUMP. FAULTED. EMERGENCY DECLARED. L HYD SYS PRESS. BOTH L ENG DRIVEN & L ELECTRIC DRIVEN HYD PUMPS DEACTIVATED WITHIN 90 SECS OF EICAS MSGS R&R L ENG HYD SUPPLY HOSE TO EDP I
- [SDR IPXA2026050749719](https://openairdocs.org/sdr/IPXA2026050749719), May 6, 2026: FILTER. FAULTED. EMERGENCY DECLARED, LT HYD SYS PRESS. BOTH L ENG DRIVEN & L ELECTRIC DRIVEN HYD PUMPS DEACTIVATED WITHIN 90 SECS OF EICAS MSGS R&R L ENG EDP CASE DRAIN FILTER A
- [SDR IPXA2026033023913](https://openairdocs.org/sdr/IPXA2026033023913), Mar 28, 2026: SKIN. DENTED. REMOVED PREVIOUS REPAIR ON THE RT, INBD MAIN FLAP PANEL. 3.5" DIA CUTOUT, 12.5" OTBD OF INBD EOP, 96" INBD OF OTBD EOP, 19. 3/4" FWD OF T/E. IAW SRM 51-70-10-2R
- [SDR IPXA2026031739174](https://openairdocs.org/sdr/IPXA2026031739174), Feb 10, 2026: CREASE BEAM. CORRODED. DURING MAIN CABIN BS 1200 FLOORBEAM REPAIR, AFTER REMOVAL OF RT OTBD WEB, BS 1180-1210, RBL 65. CREASE BEAM WAS FOUND WITH CORROSSION. REMOVED ONE CRACKED ANGLE
- [SDR IPXA2026030239174](https://openairdocs.org/sdr/IPXA2026030239174), Feb 10, 2026: CREASE BEAM. CORRODED. MAJOR REPAIR. DURING MAIN CABIN FLOOR BS 1200, FLOORBEAM REPAIR, AFTER REMOVAL OF RT OTBD WEB, BS 1180 - 1210, RBL 65 CREASE BEAM WAS FOUND WITH CORROSSION. WOR
- [SDR IPXA2026030318640](https://openairdocs.org/sdr/IPXA2026030318640), Feb 9, 2026: SKIN. DENTED. MAJOR REPAIR. SEVERAL SMALL DENTS ON TOP SKIN OF RT INBD FLAP. OUTER SKIN OF RT WING INBD MAIN FLAP ASSY WAS FOUND WITH ONE DENT OUT OF SRM 57-53-01-1A-1 ALLOWA
- [SDR IPXA2026030291662](https://openairdocs.org/sdr/IPXA2026030291662), Feb 7, 2026: STRAP. CORRODED. STR ACCESS DOOR313AL LOWER STRAP HAS CORROSION BETWEEN RBL 9 AND LBL 12. REMOVED COVER STRAP FOR ACCESS AND STRAP CORRODED IAW SRM 51-40-02-0G-0 INSTALLED AND P
- [SDR IPXA2026030282338](https://openairdocs.org/sdr/IPXA2026030282338), Feb 6, 2026: FRAME. DENTED. MAJOR REPAIR. FWD CARGO BS 800 RT SIDE FRAME DENTED. WORK ACCOMPLISHED IAW EO-96553-REQ 1 & EA 757-5330-27-A4327, REV-.
- [SDR IPXA2026022079132](https://openairdocs.org/sdr/IPXA2026022079132), Feb 6, 2026: SKIN. DENTED. SLAT NR 5 WITH SEVERAL DENTS IN THE UPPER SURFACE. REMOVED DAMAGE AND PREPARED AREA AT SLAT NR 5 2EA DENTS IAW B757-200 SRM 51-70-10-2R-0.
- [SDR IPXA2026021949700](https://openairdocs.org/sdr/IPXA2026021949700), Feb 5, 2026: ANGLE. PUNCTURED. CREW ENTRY DOOR, INNER SIDE, LOWER SILL, CLOSE TO LT STA 297, ANGLE SUPPORT HAS A HOLE. REMOVED FROM CREW ENTRY DOOR, INNER SIDE, LOWER SILL, BETWEEN LH STA 297
- [SDR IPXA2026021950684](https://openairdocs.org/sdr/IPXA2026021950684), Feb 5, 2026: CHANNEL. CRACKED. LH WW MLG, BULKHEAD 1180, UNDER PANEL 143XAL, VERTICAL BRACKET SUPPORT AT JOGGLE AREA HAS A CRACK. REMOVED LH WW MLG, BULKHEAD 1180, UNDER PANEL 143XAL, VERTICA
- [SDR IPXA2026022350890](https://openairdocs.org/sdr/IPXA2026022350890), Feb 5, 2026: CHANNEL. CRACKED. RH WW MLG, BULKHEAD 1180, UNDER PANEL 144XAR, VERTICAL BRACKET SUPPORT AT JOGGLE AREA HAS A CRACK. REMOVED RH W/W MLG BULKHEAD 1180 UNDER PANEL 144XAR ANGLE SUP
- [SDR IPXA2026030244157](https://openairdocs.org/sdr/IPXA2026030244157), Feb 4, 2026: FLOORBEAM. CORRODED. MAJOR REPAIR. MAIN CABIN FLOORBEAM, STA 1200 RBL 45-65 CORRODED. WORK ACCOMPLISHED IAW EO-96554-REQ 1, & EA 757-5360-27-A4326, REV-.
- [SDR IPXA2026021744310](https://openairdocs.org/sdr/IPXA2026021744310), Feb 4, 2026: SEAT TRACK. CORRODED. MAJOR REPAIR. MAIN CABIN FLOOR STRUCTURE, STA 1160-1200 BL 0 SEAT TRACK CORRODED. DOT 28-28 REMOVED CORROSION IN SEAT TRACK I.A.W. B757-200 SRM 51-10-02 INSTALL
- [SDR IPXA2026022243116](https://openairdocs.org/sdr/IPXA2026022243116), Feb 4, 2026: SKIN. CORRODED. MAJOR REPAIR, L/H PYLON INBD INNER SKIN BETWEEN BETWEEN PANELS 433JR ANS 433HR HAS EVIDENCE OF CORROSION AT LOWER AREA. MARKED IN RED PERFORMED BLENDOUT OF DAMA
- [SDR IPXA2026021734376](https://openairdocs.org/sdr/IPXA2026021734376), Feb 4, 2026: FLOORBEAM. CORRODED. MAIN CABIN FLOOR STRUCTURE, FLOOR BEAM STA 1680 RBL 25-65 HAS (3EA) AREAS WITH EXFOLIATION. REMOVED DAMAGE IAW SRM 51-10-02. REQUEST NDT TO VERIFY DAMAGE FREE. 
- [SDR IPXA2026022344163](https://openairdocs.org/sdr/IPXA2026022344163), Feb 4, 2026: SEAT TRACK. CORRODED. F MAIN CABIN FLOOR STRUCTURE, STA 1160-1200 LBL 45 SEAT TRACK CORRODED. REMOVED CORROSION IN SEAT TRACK I.A.W. B757-200 SRM 51-10-02 AND EVALUATED I.A.W. B757-2
- [SDR IPXA2026021927248](https://openairdocs.org/sdr/IPXA2026021927248), Feb 4, 2026: BRACKET. CRACKED. FAULT-STR-ZONE 200: AIR COND. DUCT AT CABIN CEILING STA 1680 SUPPORT BRACKET IS CRACKED. REMOVED MAIN CABIN SUPPORT BRACKET IAW B757-200PF SRM 51-40-02 INSTALLE
- [SDR IPXA2026023834460](https://openairdocs.org/sdr/IPXA2026023834460), Feb 4, 2026: SEAT TRACK. DENTED. MAIN CARGO COMPARTMENT FLOOR STRUCTURE, BL 0 SEAT TRACK HAS (1EA) DENT. REMOVED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-00-52-2R-7 STEP 2 AND SRM 51-40-02-0G-0
- [SDR IPXA2026021939888](https://openairdocs.org/sdr/IPXA2026021939888), Feb 4, 2026: SUPPORT ANGLE. CORRODED. MAIN CABIN FLOOR STRUCTURE, STA 1720 LBL 20 LOWER NUTPLATE ANGLE SUPPORT CORRODED. REMOVED LOWER NUTPLATE ANGLE SUPPORT CORRODED I.A.W. B757-200 SRM 51-40-02-0G
- [SDR IPXA2026021939793](https://openairdocs.org/sdr/IPXA2026021939793), Feb 4, 2026: SUPPORT ANGLE. CORRODED. MAIN CABIN FLOOR STRUCTURE, STA 1720 LBL 45 LOWER NUTPLATE ANGLE SUPPORT CORRODED. DOT 28-05 .REMOVED LOWER NUTPLATE ANGLE SUPPORT CORRODED I.A.W. B757-200 SRM 
- [SDR IPXA2026021940348](https://openairdocs.org/sdr/IPXA2026021940348), Feb 4, 2026: SUPPORT ANGLE. CORRODED. MAIN CABIN FLOOR STRUCTURE, STA 1720 RBL 10 LOWER NUTPLATE ANGLE SUPPORT CORRODED. REMOVED LOWER NUTPLATE ANGLE SUPPORT CORRODED IAW SRM 51-40-02-0G-0 INSTALLED
- [SDR IPXA2026021241625](https://openairdocs.org/sdr/IPXA2026021241625), Feb 4, 2026: DECK PLATE. CORRODED. MAIN CABIN FLOOR STRUCTURE, DECK PLATE STA 1700-1720 BL0 -RBL 50 HAS 15EA AREAS WITH CORROSION. REMOVED CORROSION IN 15 AREAS. MAIN CABIN FLOOR STRUCTURE, DECK 
- [SDR IPXA2026021874039](https://openairdocs.org/sdr/IPXA2026021874039), Feb 1, 2026: BRACKET. CORRODED. ACCESS DOOR 313AL LH AND RH LATCH STOPS AT THE CUT-OUT, 4EA BRACKETS ARE CORRODED. REMOVED 4EA BRACKETS WITH CORROSION I.A.W. SRM 51-40-02-0G-0. INSTALLED 4EA B
- [SDR IPXA2026021188165](https://openairdocs.org/sdr/IPXA2026021188165), Feb 1, 2026: SKIN. CRACKED. AFT CARGO DOOR EXTERNAL SKIN HAS A 2" CRACK APPROX. AT THE LOWER AFT SECTION. DOT 21-01 THIS REQUIRES SUPPLIMENTAL INSPECTION AT THRESHOLD OF 37,500 FC REPEAT I
- [SDR IPXA2026022369212](https://openairdocs.org/sdr/IPXA2026022369212), Jan 31, 2026: SKIN. CRACKED. LT WING FIXED L/E UPPER COMPOSITE SKIN HAS CRACKS UNDER SLAT NR 4. EVALUATED LT WING FIXED L/E UPPER COMPOSITE SKIN UNDER SLAT NR 4. FOUND OUT OF LIMITS, IAW SR
- [SDR IPXA2026021699522](https://openairdocs.org/sdr/IPXA2026021699522), Jan 27, 2026: SEAT TRACK. DAMAGED. WHEN TRYING TO REMOVE THE UPPER BUSHING OF THE BROKEN LINK P/N 143N5096-2 WHICH FOUND SEIZED ON ASSY. 143N5405-920, TRACK ASSY AFT HOLE FOUND ELONGATED. SEE ATT
- [SDR IPXA2026072066283](https://openairdocs.org/sdr/IPXA2026072066283), Jan 24, 2026: FLOOR PANEL. DAMAGED. MAJOR REPAIR, MCD FLOOR PANEL 242XEF DAMAGED INSTALLED FLOOR PANEL 242XEF REF AMM 53-01-01
- [SDR IPXA2026012666283](https://openairdocs.org/sdr/IPXA2026012666283), Jan 24, 2026: FLOOR PANEL. DAMAGED. MAJOR REPAIR. MCD FLOOR PANEL 242XEF DAMAGED REF ATTACHED IMAGES. CRACK IS ON AFT SIDE TOP FACE OF PANEL. APPROX 15.5€? IN LENGTH. 1€?-1.5€? FROM AFT SIDE OF
- [SDR IPXA2024112643725](https://openairdocs.org/sdr/IPXA2024112643725), Nov 22, 2024: FLAP SYSTEM. MALFUNCTIONED. *SUPPLEMENTAL SDR* * EMERGENCY DECLARED* TE FLAPS DISAGREE RAN QRH PROCEDURE AND LOWERED FLAPS TO 20 FOR LANDING NO HISTORY OF FLIGHT CONTROL ISSUE, PERFORMED O
- [SDR IPXA2024112243725](https://openairdocs.org/sdr/IPXA2024112243725), Nov 22, 2024: WARNING LIGHT. FALSE ACTIVATION. TE FLAPS DISAGREE RAN QRH PROCEDURE AND LOWERED FLAPS TO 20 FOR LANDING NO HISTORY OF FLIGHT CONTROL ISSUE, PERFORMED OP TEST OF TE FLAPS PER 757 AMM 27-51-00-7
- [SDR IPXA2024111471839](https://openairdocs.org/sdr/IPXA2024111471839), Nov 13, 2024: WINDOW. FAILED. ATB, EMERGENCY DECLARED, FAINT FUMES IN COCKPIT PRECEDING UNRELIABLE AIRSPEED L/H L 1 WINDSCREEN STARTED ARCING JUST PRIOR TO FUMES SMELL AND CONTINUED FOR APPR
- [SDR IPXA2024032260994](https://openairdocs.org/sdr/IPXA2024032260994), Mar 2, 2024: SKIN PANEL. CORRODED. *SUPPLEMENTAL SDR* *MAJOR REPAIR* FAULT: EVIDENCE OF CORRISON ON INSIDE SURFACE OF #2 PYLON FWD OF PANEL 443CR. DOT 142-17. ACCOMPLISH EO-89829-REQ1 AND EA 757-
- [SDR IPXA2024032659729](https://openairdocs.org/sdr/IPXA2024032659729), Mar 2, 2024: LATCH. GOUGED. *SUPPLEMENTAL SDR* FAULT - CREW ENTRY DOOR LATCHES UPPER AND LOWER APPEAR TO HAVE GOUGES . 89-237 BLENDED OUT CREW DOOR LATCHES UPPER AND LOWER IAW SREO-14721-R
- [SDR IPXA2024030459729](https://openairdocs.org/sdr/IPXA2024030459729), Mar 2, 2024: LATCH. GOUGED. CREW ENTRY DOOR LATCHES UPPER AND LOWER APPEAR TO HAVE GOUGES . 89-237 APPROVED OPEN
- [SDR IPXA2023122865964](https://openairdocs.org/sdr/IPXA2023122865964), Dec 13, 2023: PANEL. DENTED. **SUPPLEMENTAL SDR**LEFT WING LOWER INBD LE ACCESS PANEL #511HB HAS DENT APX 6 INCHES FROM FWD EDGE AND 10 INCHES FROM INBD EDGE.***SM26/LMX4*** INSTALLED NEW P
- [SDR IPXA2023121365964](https://openairdocs.org/sdr/IPXA2023121365964), Dec 13, 2023: ACCESS PANEL. UNKNOWN. *SDR FILED OPEN* LEFT WING LOWER INBD LE ACCESS PANEL #511HB HAS DENT APX 6 INCHES FROM FWD EDGE AND 10 INCHES FROM INBD EDGE.***SM26/LMX4*** C/W EO. ITEM REQUI
- [SDR IPXA2023050293086](https://openairdocs.org/sdr/IPXA2023050293086), May 2, 2023: BATTERY. UNKNOWN. INSPECTION TYPE:NAINTERIOR AND EXTERIOR EMER. LIGHTS WILL NOT ILLUMINATE WITH SWITCH IN "ON" POSITION.R&R EMERGENCY LIGHT BATTERY IAW AMM 33-51-07. OPS CHECK GO
- [SDR IPXA2023050293096](https://openairdocs.org/sdr/IPXA2023050293096), May 2, 2023: BATTERY PACK. INOPERATIVE. INSPECTION TYPE:NAREF: THIS LP ITEM 2. EMERGENCY BATTERY NEEDS REPLACED DUE TO EXPIRED SHELF LIFE.REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-5
- [SDR IPXA2023031391801](https://openairdocs.org/sdr/IPXA2023031391801), Mar 11, 2023: PBE. INOPERATIVE. INSPECTION TYPE:NAUNABLE TO REMOVED PBE FROM BRACKET IN LAV.OTDERED PART ON REQ 438809 AND REMOVED BRACKET PER MM 25-64-00-20. JG 0559012, 03\11/23. R/R VELCROW
- [SDR IPXA2022031079962](https://openairdocs.org/sdr/IPXA2022031079962), Mar 10, 2022: SKIN. NONE. INSPECTION TYPE:SEG1#2 ENGINE PYLON I/B, EXFOLIATION CORROSION ON INSIDE LIP INSIDE PNL 443GLREPAIRED PER VT MAE EA 757-5450-27-A2856 REV -
- [SDR IPXA2022031079956](https://openairdocs.org/sdr/IPXA2022031079956), Mar 10, 2022: SKIN. NONE. INSPECTION TYPE:SEG1#2 ENGINE PYLON O/B, EXFOLIATION CORROSION ON INSIDE LIP BEHIND PNL 443ARREPAIRED PER VT MAE EA 757-5450-27-A2856 REV -
- [SDR IPXA2022031079952](https://openairdocs.org/sdr/IPXA2022031079952), Mar 10, 2022: FRAME. NONE. INSPECTION TYPE:SEG1PREVIOUS REPAIR FOUND DURING FRAME INSPECTION AT STA 1480, S26R.WORKED PER VT MAE EA 757-5360-27-A2845 REV -
- [SDR IPXA2022031079955](https://openairdocs.org/sdr/IPXA2022031079955), Mar 10, 2022: SKIN. NONE. INSPECTION TYPE:SEG1#1 INBD PYLON INSIDE PANEL 433GR, STRUCTURE HAS EXFOLIATION CORROSION AT AFT LOWER EDGEREPAIRED PER VT MAE EA 757-5450-27-A2855 REV -
- [SDR IPXA2022031079946](https://openairdocs.org/sdr/IPXA2022031079946), Mar 10, 2022: FRAME. NONE. INSPECTION TYPE:SEG1LOWER FRAME GOUGED AT STA 1380 R/H BY STR 26RREPAIRED PER VT MAE EA 757-5360-27-A2850 REV-
- [SDR IPXA2020032553567](https://openairdocs.org/sdr/IPXA2020032553567), Mar 25, 2020: FLOORBEAM. CORRODED. INSPECTION TYPE:SEGMCD FLOOR BEAM AT 1540 IS CORRODEDREPLACED IAW EO NO:B757- 5310-75846-A
- [SDR IPXA2020032553536](https://openairdocs.org/sdr/IPXA2020032553536), Mar 24, 2020: SLAT. DELAMINATED. INSPECTION TYPE:SEG3RT WING #8 SLAT HAS 4EA DENT DELAMINATIONSREPAIRED IAW SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-2
- [SDR IPXA2020032553548](https://openairdocs.org/sdr/IPXA2020032553548), Mar 24, 2020: SKIN. DENTED. INSPECTION TYPE:SEG3RH FUSELAGE STA 1540-1560 BETWEEN STR 22R-23R AREA ON FUSELAGE HAS OUTWARD DENTREPAIRED IAW SRM 53-00-01-2R-29
- [SDR IPXA2020032553547](https://openairdocs.org/sdr/IPXA2020032553547), Mar 24, 2020: SLAT. DELAMINATED. INSPECTION TYPE:SEG3LT WING #5 SLAT HAS DINGSREPAIRED IAW SRM 57-43-02-2R-1 AND 51-70-10-2R
- [SDR IPXA2020032553545](https://openairdocs.org/sdr/IPXA2020032553545), Mar 24, 2020: SLAT. DELAMINATED. INSPECTION TYPE:SEG3LT WING #3 SLAT HAS DELAMINATIONSREPAIRED IAW SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-2

All 205: https://openairdocs.org/aircraft/N460UP/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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