# N475UP: 1999 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: 28845
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 12, 1999
- Certificate issued: August 13, 1999
- Expires: February 29, 2028
- Mode S code: A5D57D
- 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=475UP
- Page: https://openairdocs.org/aircraft/N475UP

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/N475UP/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 N475UP.

## FAA accident and incident reports

None matched to N475UP.

## Service difficulty reports (113, 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 IPXA2026013038362](https://openairdocs.org/sdr/IPXA2026013038362), Jan 30, 2026: CHARGER. NO TEST. EMERGENCY EXIT LIGHT WILL NOT TEST REMOVED AND REPLACED EMERGANCY LIGHT BATTERY ASSY AND BATTERY CHARGER REF 757MM 33-51-07-902-001 33-51-07-862-054 TEST OK. OK
- [SDR IPXA2025092531819](https://openairdocs.org/sdr/IPXA2025092531819), Sep 25, 2025: ADC. MALFUNCTIONED. ATB, LOSS L AIR DATA DURING CLIMB-OUT AROUND 400FT. REMOVED AND REPLACED LEFT ADC PER AMM 34-12-01. OPS CHECK NORMAL.
- [SDR IPXA2025082160238](https://openairdocs.org/sdr/IPXA2025082160238), Aug 20, 2025: ENGINE. FAULTED. DIVERSION, EMERGENCY DECLARED, DURING CLIMB PASSING APPROXIMATELY 20,000 FT WITH EPR'S MATCHED AT CLIMB POWER WE NOTICED RIGHT HAND ENGINE EGT AMBER AT 800 DEGR
- [SDR IPXA2025082060238](https://openairdocs.org/sdr/IPXA2025082060238), Aug 20, 2025: ENGINE. OVERTEMP. DIVERSION, EMERGENCY DECLARED, DURING CLIMB PASSING APPROXIMATELY 20,000 FT WITH EPR'S MATCHED AT CLIMB POWER WE NOTICED RIGHT HAND ENGINE EGT AMBER AT 800 DEGR
- [SDR IPXA2025061648182](https://openairdocs.org/sdr/IPXA2025061648182), Jun 10, 2025: SKIN. DENTED. HORIZONTAL STABILIZER LH UPPER SKIN RIB 12 HAS A DENT.REMOVED DAMAGE APPROX. 1.90" X 2.95", WITH CORE REMOVAL. LOCATED FROM CENTER OF CUTOUT, 6.250" AFT OF FWD 
- [SDR IPXA2025061608397](https://openairdocs.org/sdr/IPXA2025061608397), Jun 8, 2025: SKIN. DAMAGED. FAULT-STR-ZONE 200. UPPER FUSELAGE (CROWN), STA 1200-1220 AT S-L3 PREVIOUS BLEND OUT AROUND FASTENER NOT LISTED ON MAPPING.REMOVED PAINT ON PREVIOUS BLEND OUT A
- [SDR IPXA2025061608628](https://openairdocs.org/sdr/IPXA2025061608628), Jun 8, 2025: SKIN. DAMAGED. UPPER FUSELAGE (CROWN), STA 1300-1320 BETWEEN S-4L AND S-3L PREVIOUS BLEND OUT AROUND FASTENER NOT LISTED ON MAPPING.REMOVED PAINT ON PREVIOUS BLEND OUT IAW 757
- [SDR IPXA2025062712469](https://openairdocs.org/sdr/IPXA2025062712469), Jun 8, 2025: STRUCTURE. DAMAGED. FAULT Z100 STR: REFERANCE EO-92743-REQ2 #2 ENGINE PYLON OB NACELLE STRUT INTERNAL UPPER STRUCTURE AT PPS 162.76 HAS HEAT DAMAGE.VERIFIED ACCOMPLISHMENT OF STEP 
- [SDR IPXA2025062112617](https://openairdocs.org/sdr/IPXA2025062112617), Jun 8, 2025: STOP FITTING. CORRODED. ACCESS PANEL 313AL RIGHT DOOR STOP BRACKETS (2EA) CORRODED.REMOVED 02EA BRACKETS FROM ACCESS DOOR 313AL LATCH STOPS FOR EVALUATION IAW 757-200PF SRM 51-40-02.FA
- [SDR IPXA2025062512268](https://openairdocs.org/sdr/IPXA2025062512268), Jun 8, 2025: ANGLE. CRACKED. FWD CARGO COMPT, STA 560 ANGLE HAS A CRACK AT PANEL 122AZ SUPPORT STRUCTURE. INSTALLED NEW PART AT THE FWD CARGO COMP STA 560 ANGLE. I.A.W SRM 51-40-02-0G.
- [SDR IPXA2025062197411](https://openairdocs.org/sdr/IPXA2025062197411), Jun 7, 2025: SUPPORT ANGLE. CRACKED. RIGHT W/W FWD SEAL RETAINER/ DOOR SENSOR, 2ND FROM OUTBD SUPPORT CLIP IS CRACKED IN LOWER CORNER. DOT 8-002.IDENTIFIED, CLIP CRACKED AT W/W FWD SEAL RETAINER/ D
- [SDR IPXA2025062100870](https://openairdocs.org/sdr/IPXA2025062100870), Jun 7, 2025: GUSSET. CRACKED. FAULT-100-STR- LEFT WHEEL WELL FWD SEAL RETAINER/DOOR SENSOR SUPPORT CLIP, SECOND FROM OUTB IS CRACKED. DOT 8-010. IDENTIFIED AND REMOVED CRACKED SUPPORT CLIP (
- [SDR IPXA2024120405940](https://openairdocs.org/sdr/IPXA2024120405940), Dec 3, 2024: A/C PACK. FAULTED. VERY LOUD BUZZING NOISE FROM LEFT A/C PACK WHEN USING ENGINE BLEED AIR SOUND NOT PRESENT WHEN USING APU BLEED AIR. SOUND SEEMS TO COME FROM RIGHT SIDE GLARE SHI
- [SDR IPXA2023090612540](https://openairdocs.org/sdr/IPXA2023090612540), Aug 24, 2023: UNKNOWN. UNKNOWN. *** SUPPLEMENTAL SDR *** LH WING WILL NOT TAKE FUEL. **OII 2** CLEANED CANNON PLUG L/H FUEL SHUTOFF VALVE AND OPS CHECK IAW AMM 28-21-02. OPS CHECK GOOD. PLACAR
- [SDR IPXA2023082412540](https://openairdocs.org/sdr/IPXA2023082412540), Aug 24, 2023: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** LH WING WILL NOT TAKE FUEL. **OII 2** DEFFERED LH WING FUEL SHUTOFF VALVE PER MEL 28-21-1-1. DMP COMPLIED WITH PLACARD INSTALLED.
- [SDR IPXA2023071173358](https://openairdocs.org/sdr/IPXA2023071173358), Jun 8, 2023: DOOR LATCH. GOUGED. **SUPPLEMENTAL SDR**FAULT:CREW DOOR. UPPER LATCH IS GOUGED, DOT. 65-014 REVIEWED.BLENDED OUT NICK AND GOUGED DAMAGED AREA SMOOTH PER 757-200PF SRM 51-10-02 SERO
- [SDR IPXA7202306093358](https://openairdocs.org/sdr/IPXA7202306093358), Jun 8, 2023: UNKNOWN. UNKNOWN. **SDR FILED OPEN**FAULT :CREW DOOR. UPPER LATCH IS GOUGED, DOT. 65-014 APPROVED
- [SDR IPXA2021120876788](https://openairdocs.org/sdr/IPXA2021120876788), Dec 8, 2021: UNKNOWN. ODOR. ON SHORT FINAL & FULLY CONFIGURED A STRONG SMELL OF BURING RUBBER THAT LASTED APPROXIMATELY 1 MINTUE & DISSIPATED AFTER TOUCHDOWN. INSPECTED PACK & ENGINE INLET
- [SDR IPXA2021071271567](https://openairdocs.org/sdr/IPXA2021071271567), Jul 12, 2021: STIFFENER. CORRODED. INSPECTION TYPE:SEG4AFT MAIN CARGO COMPARTMENT DECK PLATE STIFFENER AT LBL 26.7 HAS MULTIPLE HOLES WITH CORROSION STILL INDICATED AFTER SECOND OVER CLEAN (REMOV
- [SDR IPXA2021071271566](https://openairdocs.org/sdr/IPXA2021071271566), Jul 12, 2021: STIFFENER. CORRODED. INSPECTION TYPE:SEG4AFT MAIN CARGO COMPARTMENT DECK PLATE STIFFENER AT LBL 9.20 HAS MULTIPLE HOLES WITH CORROSION STILL INDICATED AFTER SECOND OVER CLEAN (REMOV
- [SDR IPXA2021071271565](https://openairdocs.org/sdr/IPXA2021071271565), Jul 12, 2021: STIFFENER. CORRODED. INSPECTION TYPE:SEG4AFT MAIN CARGO COMPARTMENT DECK PLATE STIFFENER AT RBL 9.20 HAS MULTIPLE HOLES WITH CORROSION STILL INDICATED AFTER SECOND OVER CLEAN (REMOV
- [SDR IPXA2021071271564](https://openairdocs.org/sdr/IPXA2021071271564), Jul 12, 2021: STIFFENER. CORRODED. INSPECTION TYPE:SEG4AFT MAIN CARGO COMPARTMENT DECK PLATE STIFFENER AT LBL 26.7 HAS MULTIPLE HOLES WITH CORROSION STILL INDICATED AFTER SECOND OVER CLEAN (REMOV
- [SDR IPXA2021071271563](https://openairdocs.org/sdr/IPXA2021071271563), Jul 12, 2021: STIFFENER. CORRODED. INSPECTION TYPE:SEG4AFT MAIN CARGO COMPARTMENT DECK PLATE STIFFENER AT LBL 20.8 HAS MULTIPLE HOLES WITH CORROSION STILL INDICATED AFTER SECOND OVER CLEAN (REMOV
- [SDR IPXA2021071271562](https://openairdocs.org/sdr/IPXA2021071271562), Jul 12, 2021: STIFFENER. CORRODED. INSPECTION TYPE:SEG4AFT MAIN CARGO COMPARTMENT DECK PLATE STIFFENER AT LBL 15.0 HAS MULTIPLE HOLES WITH CORROSION STILL INDICATED AFTER SECOND OVER CLEAN (REMOV
- [SDR IPXA2021071271561](https://openairdocs.org/sdr/IPXA2021071271561), Jul 12, 2021: STIFFENER. CORRODED. INSPECTION TYPE:SEG4AFT MAIN CARGO COMPARTMENT DECK PLATE STIFFENER AT LBL 39.5 HAS MULTIPLE HOLES WITH CORROSION STILL INDICATED AFTER SECOND OVER CLEAN (REMOV
- [SDR IPXA2021071271560](https://openairdocs.org/sdr/IPXA2021071271560), Jul 12, 2021: STIFFENER. CORRODED. INSPECTION TYPE:SEG4AFT MAIN CARGO COMPARTMENT DECK PLATE STIFFENER AT LBL 33.1 HAS MULTIPLE HOLES WITH CORROSION STILL INDICATED AFTER SECOND OVER CLEAN (REMOV
- [SDR IPXA2021071271559](https://openairdocs.org/sdr/IPXA2021071271559), Jul 12, 2021: STIFFENER. CORRODED. INSPECTION TYPE:SEG4AFT MAIN CARGO COMPARTMENT DECK PLATE AT BL 0 HAS MULTIPLE HOLES WITH CORROSION STILL INDICATED AFTER SECOND OVER CLEAN (REMOVE AND REPLACE)
- [SDR IPXA2021071271558](https://openairdocs.org/sdr/IPXA2021071271558), Jul 12, 2021: STIFFENER. CORRODED. INSPECTION TYPE:SEG4AFT MAIN CARGO COMPARTMENT DECK PLATE STIFFENER AT RBL 39.5 HAS MULTIPLE HOLES WITH CORROSION STILL INDICATED AFTER SECOND OVER CLEAN (REMOV
- [SDR IPXA2021071271557](https://openairdocs.org/sdr/IPXA2021071271557), Jul 12, 2021: STIFFENER. CORRODED. INSPECTION TYPE:SEG4AFT MAIN CARGO COMPARTMENT DECK PLATE AT RBL 33.10 HAS MULTIPLE HOLES WITH CORROSION STILL INDICATED AFTER SECOND OVER CLEAN (REMOVE AND REP
- [SDR IPXA2021071271556](https://openairdocs.org/sdr/IPXA2021071271556), Jul 12, 2021: STIFFENER. DAMAGED. INSPECTION TYPE:SEG4AFT MAIN CARGO COMPARTMENT DECK PLATE STIFFENER AT RBL 20.8 HAS MULTIPLE HOLES WITH CORROSION STILL INDICATED AFTER SECOND OVER CLEAN (REMOV
- [SDR IPXA2021071271555](https://openairdocs.org/sdr/IPXA2021071271555), Jul 12, 2021: STIFFENER. CORRODED. INSPECTION TYPE:SEG4AFT MAIN CARGO COMPARTMENT DECK PLATE STIFFENER AT RBL 15 HAS MULTIPLE HOLES WITH CORROSION STILL INDICATED AFTER SECOND OVER CLEAN (REMOVE 
- [SDR IPXA2021071271591](https://openairdocs.org/sdr/IPXA2021071271591), Jun 4, 2021: DECK PLATE. CORRODED. INSPECTION TYPE:3MAIN CARGO COMPATMENT FLOOR BEAM STA 1681 FROM LBL 29.00 TO LBL 33.0 HAS CORROSION.REPAIRED DECK PLATE IAW UPS EO B757-5300-80618.
- [SDR IPXA2021071271589](https://openairdocs.org/sdr/IPXA2021071271589), Jun 4, 2021: FLOORBEAM. CORRODED. INSPECTION TYPE:3MAIN CARGO COMPARTMENT. FLOOR BEAM STA 1681.5 FROM LBL 29.00 TO LBL 33.00 HAS CORROSION.REPAIRED FLOOR BEAM IAW EO B757-5300-80618
- [SDR IPXA2021060470168](https://openairdocs.org/sdr/IPXA2021060470168), Jun 4, 2021: PANEL. DELAMINATED. INSPECTION TYPE:SEGR/H LWR FWD TORQUE BOX PANEL HAS A SMALL DELAMINATION MARKED IN RED BELOW FSS 195.390REPAIRED PANEL IAW B757 SRM 51-70-07-OG 250 DEG F CURE P
- [SDR IPXA2020082649438](https://openairdocs.org/sdr/IPXA2020082649438), Aug 23, 2020: SWITCH. FAILED. INSPECTION TYPE:NAFO SELECTED AIR DATA SWITCH AND SMOKE COME OUT OF BEHIND FO'S PANELGVI WIRE BNDL BEHIND F/O'S DISPLAY & BELOW FLOORBRD, NO DMGD WIRES. RT AIR 
- [SDR IPXA2019062843834](https://openairdocs.org/sdr/IPXA2019062843834), Jun 28, 2019: DUCT. DISCONNECTED. INSPECTION TYPE:N/A AT FLT LVL 320 LTN PACK OFF GOT EICAS MSG CAB ALT WARN. RAN CHECKLIST, LT PACK TO ON, MESSAGE GO AWAY. DEFERRED AS PER MEL 21-51-1. **SUPPLE
- [SDR IPXA2019061082992](https://openairdocs.org/sdr/IPXA2019061082992), Jun 8, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG3MAIN CARGO COMPARTMENT, FLOOR PANEL 231XFF IS DAMAGEFABBED PANEL 231XFF FROM 502N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K
- [SDR IPXA2019061082991](https://openairdocs.org/sdr/IPXA2019061082991), Jun 8, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE: SEG3, MAIN CARGO COMPARTMENT, FLOOR PANEL 231XJF IS DAMAGE FABBED PANEL 231XJF FROM 502N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K
- [SDR IPXA2015052789476](https://openairdocs.org/sdr/IPXA2015052789476), May 27, 2015: SKIN. DENTED. INSPECTION TYPE:C-8, LT HORIZONTAL STABILIZER UPPER SKIN WAS DENTED BETWEEN FT AND AUX SPAR, 67" FROM INBD END AND 19" FROM FT SPAR. REPAIRED DAMAGE IAW 51-70-1
- [SDR IPXA2015052889504](https://openairdocs.org/sdr/IPXA2015052889504), May 23, 2015: FLOORBOARD. PUNCTURED. INSPECTION TYPE: C-8, MAIN CABIN FLOORBOARD 252XFF IS PUNCTURED ON THE UPPER SURFACE. FABRICATED A NEW FLOORBOARD IAW REO B757-5320-9692-H.
- [SDR IPXA2015053089568](https://openairdocs.org/sdr/IPXA2015053089568), May 22, 2015: FLOORBOARD. CRUSHED. INSPECTION TYPE: C8, FLOORBOARD 221XBF CRUSHED. FABRICATED A NEW FLOORBOARD IAW EO B757-5320-9692H.
- [SDR IPXA2015053089571](https://openairdocs.org/sdr/IPXA2015053089571), May 22, 2015: FLOORBOARD. DELAMINATED. INSPECTION TYPE: C8, CABIN FLOORBOARD 252XTF DELAMINATED. FABRICATED A NEW FLOORBOARD IAW EO B757-5320-9692-H.
- [SDR IPXA2015052889503](https://openairdocs.org/sdr/IPXA2015052889503), May 22, 2015: FLOORBOARD. GOUGED. INSPECTION TYPE: C-8, MAIN CABIN FLOORBOARD 221XCF EDGE IS GOUGED. FABRICATED A NEW FLOORBOARD IAW UPS REO B757-5320-9692-H.
- [SDR IPXA2015052889502](https://openairdocs.org/sdr/IPXA2015052889502), May 22, 2015: FLOORBOARD. CRUSHED. INSPECTION TYPE:C-8, MAIN CABIN FLOORBOARD 252XBF EDGE IS CRUSHED. FABRICATED A NEW FLOORBOARD IAW REO B757-5320-9692-H
- [SDR IPXA2015052489393](https://openairdocs.org/sdr/IPXA2015052489393), May 22, 2015: FLOORBOARD. DENTED. INSPECTION TYPE:C-8, MAIN CABIN FLOORBOARD 241XLF HAS MULTIPLE SURFACE DENTS. FABRICATED A NEW FLOORBOARD IAW SREO B757-5320-9692-H.
- [SDR IPXA2015052489392](https://openairdocs.org/sdr/IPXA2015052489392), May 22, 2015: FLOORBOARD. CRACKED. INSPECTION TYPE:C-8, MAIN CABIN FLOORBOARD 231XHF IS CRACKED, FABRICATED NEW FLOORBOARD IAW SREO B757-5320-9692-H.
- [SDR IPXA2015052489391](https://openairdocs.org/sdr/IPXA2015052489391), May 22, 2015: FLOORBOARD. GOUGED. INSPECTION TYPE:C-8, MAIN CABIN FLOORBOARD CORNER IS GOUGED. FABRICATED NEW FLOORBOARD IAW SREO B757-5320-9692-H.
- [SDR IPXA2015052689421](https://openairdocs.org/sdr/IPXA2015052689421), May 22, 2015: FLOORBOARD. BROKEN. INSPECTION TYPE:C-8, MAIN CABIN FLOORBOARD 251XCF CORNER IS BROKEN. FABRICATED NEW PANEL IAW B757-5320-9692-H SREO.
- [SDR IPXA2015052689420](https://openairdocs.org/sdr/IPXA2015052689420), May 22, 2015: FLOORBOARD. DAMAGED. INSPECTION TYPE: C-8, MAIN CABIN FLOORBOARD, 241XJF IS DENTED AND HAS A BROKEN CORNER. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
- [SDR IPXA2015052689419](https://openairdocs.org/sdr/IPXA2015052689419), May 22, 2015: FLOORBOARD. GOUGED. INSPECTION TYPE: C-8, MAIN CABIN FLOORBOARD 231XDF IS GOUGED ON THE UPPER SURFACE. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-96-92-H.

All 113: https://openairdocs.org/aircraft/N475UP/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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