# N442UP: 1994 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: 27387
- Year built: 1994
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 13, 1994
- Certificate issued: November 9, 1994
- Expires: November 30, 2028
- Mode S code: A553DB
- 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=442UP
- Page: https://openairdocs.org/aircraft/N442UP

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/N442UP/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 N442UP.

## FAA accident and incident reports

None matched to N442UP.

## Service difficulty reports (145, 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 IPXA2026030931783](https://openairdocs.org/sdr/IPXA2026030931783), Mar 5, 2026: WINDOW. WARNING MESSAGE. RIGHT FWD WINDOW EICAS POSTED DURING TAXI IN, AFTER LANDING. REMOVED AND REPLACED FO'S WINDSHIELD IAW AMM 56-11-01. OPS CHECKED GOOD.
- [SDR IPXA2026030531783](https://openairdocs.org/sdr/IPXA2026030531783), Mar 5, 2026: TERMINAL. OUT OF TOLERANCE. R FWD WINDOW EICAS POSTED ON TAXI IN AFTER LANDING AS PER FIM 30-41 FT 804 NOTE, APU HISTORY REVIEWED IN MTX AND NO START DISCREPANCIES NOTED IN PAST 60 DAYS. T
- [SDR IPXA2025040747037](https://openairdocs.org/sdr/IPXA2025040747037), Apr 5, 2025: CARABINER. MISSING. ONE ESCAPE HARNESS IS MISSING A CARABINER. INSTALLED CARABINER AND STOWED ESCAPE HARNESS IN BAG PER AMM 25-61-02
- [SDR IPXA2025032846557](https://openairdocs.org/sdr/IPXA2025032846557), Mar 4, 2025: SEAL. DAMAGED. FAULT: APG Z200, CREW ENTRY DOOR HAS 1 EA PINCH POINT LWR AFT CORNER.REPAIRED CREW ENTRY DOOR SEAL IAW AMM 52-09-00-358-020.
- [SDR IPXA2025031846582](https://openairdocs.org/sdr/IPXA2025031846582), Mar 4, 2025: DOOR FRAME. CORRODED. FWR CARGO DOOR INTERNAL LWR FWD FRAME HAS CORROSION NOTED. DOT 06677-01. VERIFIED INSTALLATION OF ANGLE AT FWR CARGO DOOR INTERNAL LWR FWD FRAME IAW B757-200 SR
- [SDR IPXA2025031746582](https://openairdocs.org/sdr/IPXA2025031746582), Mar 4, 2025: FRAME. CORRODED. **SDR FILED OPEN** FAULT: STR Z800 FWR CARGO DOOR INTERNAL LWR FWD FRAME HAS CORROSION NOTED. DOT 06677-01 OK TO APPLY LEVELING COMPOUND GIVEN.
- [SDR IPXA2025031364002](https://openairdocs.org/sdr/IPXA2025031364002), Mar 4, 2025: BRACKET. CORRODED. FAULT: WTB PANEL BRACKET AT 196AR HAS HEAVY CORROSION. DOT 95334-5. INSTALLED 1 NEW BRACKET IAW B757-200-SRM 51-40-02-OG FASTENERS INSTALLED QTY 5 BACB30NX6K4X 
- [SDR IPXA2025030446557](https://openairdocs.org/sdr/IPXA2025030446557), Mar 4, 2025: DOOR. OUT OF ADJUST. CREW ENTRY DOOR HAS 1 EA PINCH POINT LWR AFT CORNER.
- [SDR IPXA2025031727544](https://openairdocs.org/sdr/IPXA2025031727544), Mar 2, 2025: ANGLE. CORRODED. APU INLET DOOR UPPER FWD CORNER ANGLE S-3R HAS CORROSION.REMOVE AND REPLACE 1 EACH S-3R CORNER SUPPORT ANGLE (P/N: 148N3141-6) PER PRODUCTION DRAWING REQUIREMEN
- [SDR IPXA2025031827756](https://openairdocs.org/sdr/IPXA2025031827756), Mar 2, 2025: CHANNEL. GOUGED. APU COMPARTMENT RH DOOR (316AR) LOWER AREA FIRE DETECTION LOOP CHANNEL HAS GOUDED.- DOT 43-06. INSTALLED NEW CHANNEL IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2025031727595](https://openairdocs.org/sdr/IPXA2025031727595), Mar 2, 2025: ANGLE. CORRODED. FAULT: Z-300 STR APU INLET DOOR UPPER ANGLE FROM STA 1787.45 TO STA 1825.00 S-3R HAS CORROSION. INSTALLED 01EA ANGLE. IAW B757-200 SRM 51-40-02. REVIEWED.
- [SDR IPXA2025031727556](https://openairdocs.org/sdr/IPXA2025031727556), Mar 2, 2025: ANGLE. CORRODED. APU INLET DOOR LOWER ANGLE BETWEEN STA 1787.45 TO STA 1825.00 HAS CORROSION. INSTALLED 01EA ANGLE. IAW B757-200 SRM 51-40-02. RIVET P/N: MS20470AD6-10, BATCH: 0
- [SDR IPXA2025031827619](https://openairdocs.org/sdr/IPXA2025031827619), Mar 2, 2025: ANGLE. CORRODED. APU INLET DOOR LOWER FWD CORNER ANGLE S-6R HAS CORROSION.REMOVED LOWER FWD ANGLE IAW B757-200PF SRM 51-40-02-0G-0.REMOVE AND REPLACE 1 EACH S-6R CORNER SUPPORT 
- [SDR IPXA2025031726547](https://openairdocs.org/sdr/IPXA2025031726547), Mar 2, 2025: SKIN. GOUGED. MAJOR REPAIR, ACCESS DOOR 119BL REAR CUT OUT FUSELAGE, OUTER SKIN HAS (2EA) GOUGES. DOT 72-024 ACCOMPLISHED PER UPS EO: EO-93125-REQI AND VT MAE EA 757-5330-27-
- [SDR IPXA2025030327533](https://openairdocs.org/sdr/IPXA2025030327533), Mar 2, 2025: STRAP. CORRODED. APU INLET DOOR STA 1825.00 AFT STRAP HAS CORROSION.REMOVED CORROSION IAW B757-200PF SRM 51-10-02-0G-0 AND EVALUATED IAW SRM 53-80-15-1A-1 TABLE 101.REMOVED FAST
- [SDR IPXA2025031482551](https://openairdocs.org/sdr/IPXA2025031482551), Feb 27, 2025: STRAP. CORRODED. FAULT:STR ZONE 300 APU INLET DOOR AT STA 1787.45 FWD STRAP HAS CORROSION. REPLACE 1 EACH APU INLET FORWARD STRAP AT STA 1787.45 (P/N: 148N3138-20) PER PRODUCTIO
- [SDR IPXA2023030791647](https://openairdocs.org/sdr/IPXA2023030791647), Mar 7, 2023: SEAT TRACK. CORRODED. INSPECTION TYPE:SEG3MAIN DECK AT STA 290 RBL 12.5 LONGITUDINAL FITTING HAS CORROSION. OUT OF LIMITS. PART IS BEING REPLACED P/N 141N5131-35, MATERIAL ID, BAC152
- [SDR IPXA2023030891673](https://openairdocs.org/sdr/IPXA2023030891673), Feb 25, 2023: DECK PLATE. CORRODED. INSPECTION TYPE:SEG3STA 290 TO STA 340 BL 0 TO RBL 24.5 MULTIPLE SPOTS OF CORROSIONREMOVED CORROSION AND FOUND WITHIN LIMITS IAW SRM 53-10-51-1A-2
- [SDR IPXA2023030891672](https://openairdocs.org/sdr/IPXA2023030891672), Feb 25, 2023: DECK PLATE. CORRODED. INSPECTION TYPE:SEG3STA 290 TO STA 380 RBL 45.5 TO RBL 24.5 MULTIPLE SPOTS OF CORROSIONREMOVED CORROSION AND FOUND WITHIN LIMITS IAW SRM 53-10-51-1A-2
- [SDR IPXA2023030891669](https://openairdocs.org/sdr/IPXA2023030891669), Feb 25, 2023: DECK PLATE. CORRODED. INSPECTION TYPE:SEG3STA 290 TO STA 340 BL 0 TO LBL 24.5 MULTIPLE SPOTS OF CORROSIONREMOVED CORROSION AND FOUND WITHIN LIMITS IAW SRM 53-10-51-1A-2
- [SDR IPXA2023030891668](https://openairdocs.org/sdr/IPXA2023030891668), Feb 25, 2023: DECK PLATE. CORRODED. INSPECTION TYPE:SEG3STA 290 TO STA 400 LBL 67.5 TO LBL 45.5 MULTIPLE SPOTS OF CORROSIONREMOVED CORROSION AND FOUND WITHIN LIMITS IAW SRM 53-10-51-1A-2
- [SDR IPXA2023030891667](https://openairdocs.org/sdr/IPXA2023030891667), Feb 25, 2023: DECK PLATE. CORRODED. INSPECTION TYPE:SEG3STA 290 TO STA 400 RBL 67.5 TO RBL 45.5 MULTIPLE SPOTS OF CORROSIONREMOVED CORROSION AND FOUND WITHIN LIMITS IAW SRM 53-10-51-1A-2
- [SDR IPXA2023030891666](https://openairdocs.org/sdr/IPXA2023030891666), Feb 25, 2023: DECK PLATE. CORRODED. INSPECTION TYPE:SEG3STA 290 TO STA 380 LBL 45.5 TO LBL 24.5 MULTIPLE SPOTS OF CORROSIONREMOVED CORROSION AND FOUND WITHIN LIMITS IAW SRM 53-10-51-1A-2
- [SDR IPXA2023022491321](https://openairdocs.org/sdr/IPXA2023022491321), Feb 24, 2023: FRAME. DENTED. INSPECTION TYPE:SEG3STA 1240 RH STA 25R FRAME HAS A DENT ON THE INNER CHORD OUT OF LIMITSACCOMPLISHED REPAIR ON FRAME PER SRM 53-00-07-2R-6 DETAIL 3 AND UPS RCD
- [SDR IPXA2023022391292](https://openairdocs.org/sdr/IPXA2023022391292), Feb 23, 2023: FRAME. DENTED. INSPECTION TYPE:SEG3STA 800 BETWEEN STR 22R AND 23R HAS A DENT ON THE INNER CHORD.ACCOMPLISHED REPAIR ON FRAME PER SRM 53-00-07-2R-5 DETAIL 1 AND UPS RCD 270883
- [SDR IPXA2023022391290](https://openairdocs.org/sdr/IPXA2023022391290), Feb 23, 2023: FRAME. DENTED. INSPECTION TYPE:SEG3STA 1520 AT STR 26R HAS A DENT ON THE INNER CHORD.ACCOMPLISHED REPAIR ON FRAME PER SRM 53-00-07-2R-5 DETAIL 1 AND UPS RCD 270782
- [SDR IPXA2023030891664](https://openairdocs.org/sdr/IPXA2023030891664), Feb 18, 2023: DECK PLATE. CORRODED. INSPECTION TYPE:SEG3STA 1681.8 DECK PLATE BETWEEN RBL 0 TO RBL 26 HAS CORROSIONREMOVED CORROSION AND FOUND WITHIN LIMITS IAW SRM 53-60-51-1A PROCEDURE 1 TABLE 1
- [SDR IPXA2023030391505](https://openairdocs.org/sdr/IPXA2023030391505), Feb 18, 2023: FLOORBEAM. CORRODED. INSPECTION TYPE:SEG3, *MAJOR REPAIR* STA 1681.80 FLOOR BEAM UNDER CHORD FWD FLANGE HAS CORROSION OUT OF LIMITS AT LBL 26-40ACCOMPLISHED REPAIR ON FLOOR BEAM PER
- [SDR IPXA2023030391504](https://openairdocs.org/sdr/IPXA2023030391504), Feb 18, 2023: SEAT TRACK. CORRODED. INSPECTION TYPE:SEG3*MAJOR REPAIR* SEAT TRACK AT STA 1540 LBL 24.75 HAS CORROSION ON THE IB FLANGE OUT OF LIMITSACCOMPLISHED REPAIR ON SEAT TRACK PER SRM 53-00-
- [SDR IPXA2023030391503](https://openairdocs.org/sdr/IPXA2023030391503), Feb 18, 2023: SEAT TRACK. CORRODED. INSPECTION TYPE:SEG3*MAJOR REPAIR* SEAT TRACK AT STA 1540 LBL 45.5 HAS CORROSION ON THE IB FLANGE OUT OF LIMITSACCOMPLISHED REPAIR ON SEAT TRACK PER SRM 53-00-5
- [SDR IPXA2023030591548](https://openairdocs.org/sdr/IPXA2023030591548), Feb 18, 2023: FLOORBEAM. CORRODED. INSPECTION TYPE:SEG3, *MAJOR REPAIR* MAIN CARGO FLOOR BEAM AT STA 1681.8 RBL 12.5-26 HAS CORROSION OUT OF LIMITSACCOMPLISHED REPAIR ON FLOOR BEAM PER SRM 53-60-
- [SDR IPXA2023030591549](https://openairdocs.org/sdr/IPXA2023030591549), Feb 16, 2023: SKIN. CORRODED. INSPECTION TYPE:SEG3*MAJOR REPAIR* #2 ENG PYLON O/B SKIN HAS CORROSION INSIDE FWD OF VENT OPENINGACCOMPLISHED REPAIR ON SKIN PER UPS EO B757-5430-86081-A VT MAE
- [SDR IPXA2023030391507](https://openairdocs.org/sdr/IPXA2023030391507), Feb 14, 2023: SKIN. DENTED. INSPECTION TYPE:SEG3*MAJOR REPAIR* PROTRUSION DENT FROM APPROX BSTA 239, STR 20L - 23LWORKED ACCOMPLISHED PER UPS EO# B757-5330-86067-A AND VT MAE EA# 757-5310-
- [SDR IPXA2023030391501](https://openairdocs.org/sdr/IPXA2023030391501), Feb 14, 2023: FRAME. NONE. INSPECTION TYPE:SEG3*MAJOR REPAIR* DURING INSPECTION FROM EO (B757-5310-73926-A) FOUND AN EXISTING REPAIR AT STA 1320 RH STR 23-27RACCOMPLISHED REPAIR ON FRAME 
- [SDR IPXA2022110187729](https://openairdocs.org/sdr/IPXA2022110187729), Nov 1, 2022: ATTACH BRACKET. DAMAGED. ON LDG ROLL CREW ENTRY DOOR EICAS BRIEFLY ILLUMINATED TRIGGERED BLOCK IN ON ACARS FLIGTH DATA COUPON COMPLIED. INSP ACCOMPLISHED PER DMP 52-71-1REMOVED AND REPL
- [SDR IPXA2022081885377](https://openairdocs.org/sdr/IPXA2022081885377), Aug 17, 2022: NONE. INOPERATIVE. INSPECTION TYPE:N/A**SUPPLEMENTAL SDR**UPON LANDING L FWD ENT DOOR LIGHT ILLUMIONATED ON EICAS WITH ENTRY DOORS LIGHT ON OVHD PANEL.DEFERRED PER MEL 53-71-1 CON
- [SDR IPXA2021032067030](https://openairdocs.org/sdr/IPXA2021032067030), Mar 20, 2021: SKIN. CORRODED. INSPECTION TYPE:SEG2AFTER REMOVED 2EA PULLING RIVETS AT STA 1380 BETWEEN S-28R AND 2-29R AND S-29R CORROSION OUT OF LIMITS AREA WAS FOUNDACCOMPLISHED EA# 757-53
- [SDR IPXA2021010864229](https://openairdocs.org/sdr/IPXA2021010864229), Jan 8, 2021: WARNING MESSAGE. FALSE ACTIVATION. INSPECTION TYPE: NA LEFT FWD ENTRY DOOR EICAS CAME ON IN FLIGHT PERIODICALY AND WENT OFF. DOOR CONFIRMED CLOSED AND LOCKED. OPENED & CLOSED LEFT FWD ENTRY DOOR 
- [SDR IPXA2019032140362](https://openairdocs.org/sdr/IPXA2019032140362), Mar 11, 2019: SKIN. DENTED. INSPECTION TYPE:SEG 13EA DENTS ON UPPER RT SIDE OF TAIL (APU EXHAUST) 1 ON AND TWO JUST FWD OF FS1963.8 NO DOT. DENT ON FS 1963.8 FOUND TO BE ALLOWABLE-BLENDED.
- [SDR IPXA2017041016016](https://openairdocs.org/sdr/IPXA2017041016016), Apr 10, 2017: UNKNOWN. ODOR. DURING DECENT BRIEF ACRID SMELL OCCURRED. IT WAS NOT OVERWHELMING, BUT STRONG & LINGERED. RUN NR 1 & NR 2 ENG, OPERATED BOTH PACKS, NO STRONG SMELL NOTED AT THI
- [SDR IPXA2017041016001](https://openairdocs.org/sdr/IPXA2017041016001), Apr 8, 2017: UNKNOWN. ODOR. DURING DECENT, A BRIEF ACRID ODOR OCCURRED . IT WAS NOT OVERWHELMING, BUT STRONG & LINGERED. RAN NR 1 AND 2 ENGINES. OPERATED BOTH PACKS. NO STRONG ODOR NOTED I
- [SDR IPXA2017032315435](https://openairdocs.org/sdr/IPXA2017032315435), Mar 13, 2017: FLOOR PANEL. DELAMINATED. INSPECTION TYPE: SEG4, MAIN DECK FLOOR PANEL 241XGF IS DELAMINATED. FABRICATED A NEW FLOOE PANEL IAW SREO B757-5320-9692.
- [SDR IPXA2017032315448](https://openairdocs.org/sdr/IPXA2017032315448), Mar 13, 2017: FLOOR PANEL. DELAMINATED. INSPECTION TYPE: SEG4, MAIN DECK FLOOR PANEL 231XFF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-J.
- [SDR IPXA2017032315447](https://openairdocs.org/sdr/IPXA2017032315447), Mar 13, 2017: FLOOR PANEL. DELAMINATED. INSPECTION TYPE: SEG4, MAIN DECK FLOOR PANEL 231XJF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-J.
- [SDR IPXA2017032215419](https://openairdocs.org/sdr/IPXA2017032215419), Mar 13, 2017: FLOOR PANEL. DAMAGED. INSPECTION TYPE: SEG4,MAIN DECK FLOOR PANEL 242XDF, HAS A BROKEN CORNER.FABRICATED A NEW FLOOR PANELIAW SREP B757-532096-2.
- [SDR IPXA2017032315434](https://openairdocs.org/sdr/IPXA2017032315434), Mar 11, 2017: FLOOR PANEL. BROKEN. INSPECTION TYPE: SEG4, MAIN DECK FLOOR PANEL 242XKF IS BROKEN. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692.
- [SDR IPXA2017013113563](https://openairdocs.org/sdr/IPXA2017013113563), Jan 31, 2017: CONTROL PANEL. DEFECTIVE. EMERG EXIT LIGHT"UNARMED" ON OVERHEAD INOP. TRIED TO RELAMP, DISINTEGRATED. R&R EMERGENCY EXIT LIGHT CONTROL PANEL REF AMM33-51-00-501.
- [SDR IPXA2016071505927](https://openairdocs.org/sdr/IPXA2016071505927), Jul 15, 2016: LAMP. INOPERATIVE. EMERGENCY LIGHT ASSY LAMPS FOUND INOPERATIVE. REPLACED THE LAMP IAW AMM 33 51 01 2.
- [SDR IPXA2015101394772](https://openairdocs.org/sdr/IPXA2015101394772), Oct 13, 2015: LAMP. INOPERATIVE. INSPECTION TYPE: PDC 1 OF 2 LAMPS INOPERATIVE ON ENTRY DOOR ANNUNCIATOR. R & R ANNUNCIATOR IAW AMM 33-16-02-002-013. SYSTEM CHECKED OK.
- [SDR IPXA2015092994115](https://openairdocs.org/sdr/IPXA2015092994115), Sep 29, 2015: EVAS UNIT. DISLODGED. CAPTAIN'S EVAS COVER DISLODGED, EVAS PARTIALLY OUT OF CONTAINER. NO AVAILABLE BLOWER MOTOR SOUND. INSTALLED CAPTAIN'S EVAS IAW MM 25-69-00-400-801C1. OPS CHECKE

All 145: https://openairdocs.org/aircraft/N442UP/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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