# N470UP: 1997 Boeing 757-24APF

- Status: Valid registration
- Airframe: [Boeing 757-24APF](https://openairdocs.org/model/boeing-757-24apf) (registry code 1384969, 178 seats)
- Engine: [Rolls-Royce RB-211 series](https://openairdocs.org/engine/rolls-royce-rb-211-series) (registry code 54555)
- Serial number: 25486
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 23, 1997
- Certificate issued: January 28, 2026
- Expires: January 31, 2033
- Mode S code: A5C2EA
- 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=470UP
- Page: https://openairdocs.org/aircraft/N470UP

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/N470UP/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 N470UP.

## FAA accident and incident reports

None matched to N470UP.

## Service difficulty reports (152, 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 IPXA2026031646305](https://openairdocs.org/sdr/IPXA2026031646305), Mar 12, 2026: DOOR. BLOWN. DURING WALK AROUND FOUND A BLOW OUT PANEL DAMAGED ON THE RIGHT ENGINE PYLON R & R STRUT RELIEF AND ACCESS DOOR PER AMM 54-53-01
- [SDR IPXA2025122402818](https://openairdocs.org/sdr/IPXA2025122402818), Dec 23, 2025: FLEX LINE. LEAKING. EMERGENCY DECLARED, L HYD QTY RAN QRH CHECKLIST STATUS PAGE SHOWS 0.40 RF PRESSURE FLEX LINE REPLACED IAW 20-10-10, RAN HYDRAULIC SYSTEMS USING THE LEFT SYSTEM 
- [SDR IPXA2025090390433](https://openairdocs.org/sdr/IPXA2025090390433), Aug 27, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR, MC FLOOR PANEL DAMAGE INSTALLED FLOOR PANEL AT POS. 7 REF. 25-55-07. STILL REQUIRES SEALANT AND ROLLER INSTALL. REF. ITEM 47 FOR COMPLETION
- [SDR IPXA2025902000433](https://openairdocs.org/sdr/IPXA2025902000433), Aug 27, 2025: FLOOR PANEL. NOT REPORTED. MC FLOOR PANEL P/N 143N5457-26 DAMAGE INSTALLED FLOOR PANEL AT POS. 7 REF. 25-55-07. STILL REQUIRES SEALANT AND ROLLER INSTALL. REF. ITEM 47 FOR COMPLETION
- [SDR IPXA2025082758064](https://openairdocs.org/sdr/IPXA2025082758064), Aug 13, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR. FLOOR PANEL DAMEGED P/N 144N5361-12 FABRICATED NEW FLOOR PANEL P/N 144N5361-12 PER SREO-9692-REQ001.
- [SDR IPXA2025082158064](https://openairdocs.org/sdr/IPXA2025082158064), Aug 13, 2025: FLOOR PANEL. DAMAGED. FLOOR PANEL DAMEGED P/N 144N5361-12 FABRICATED NEW FLOOR PANEL P/N 144N5361-12 PER SREO-9692-REQ001.
- [SDR IPXA2025042390147](https://openairdocs.org/sdr/IPXA2025042390147), Apr 22, 2025: WEB. CORRODED. FAULT STR Z300: REMOVED THE 148N8201-8 FWD WEB ON JOB CARD T3F18E006CLWR. INSTALL FWD WEB (148N8201-8) AFTER SKIN REPAIR IS COMPLETED.148N8201-8 WEB (LONGERON 1
- [SDR IPXA2025050222871](https://openairdocs.org/sdr/IPXA2025050222871), Apr 15, 2025: FLOORBEAM. CORRODED. MDC, STA 1100, BETWEEN RBL 45 AND RBL 60, BEHIND FLOOR PANEL 242XJF, FLOOR BEAM HAS 2EA SPOTS WITH CORROSION. NO DOT. REMOVED RH SIDE RAIL FROM STA 1100-1200 TO
- [SDR IPXA2025041403757](https://openairdocs.org/sdr/IPXA2025041403757), Apr 14, 2025: FLOOR PANEL. DAMAGED. FAULT- MCD FLOOR PANEL 242XCF HAS GOUGES AND EDGE DAMAGE.FABRICATED MCD FLOOR PANEL 242XCF, IAW UPS SREO: B757-9692-REQ 001.VERIFIED FABRICATION OF MCD FLOOR PA
- [SDR IPXA2025041017701](https://openairdocs.org/sdr/IPXA2025041017701), Apr 9, 2025: FLOOR PANEL. DAMAGED. MCD FLOOR PANEL 241XEF DAMAGED AT CORNER. FABRICATED MCD FLOOR PANEL 241XEF, IAW UPS SREO: B757-9692-REQ 001.VERIFIED FABRICATION OF PANEL 241XEF.
- [SDR IPXA2025042701425](https://openairdocs.org/sdr/IPXA2025042701425), Apr 8, 2025: FLOOR SUPPORT. CORRODED. FAULT-STR-100-AFT CARGO COMP ON 3RD RH SIDE FLOOR PANEL SUPORT STR AROUND NUTPLATES, BETWEEN STA 1460 AND 1480 HAS EVIDENCE OF CORROSION. DOT 23-152. INSTALLED 
- [SDR IPXA2025042401310](https://openairdocs.org/sdr/IPXA2025042401310), Apr 8, 2025: FLOOR SUPPORT. CORRODED. FAULT-STR-100-AFT CARGO COMP ON FIRST RH SIDE FLOOR PANEL SUPORT STR AROUND NUTPLATES, BETWEEN STA 1460 AND 1480 HAS EVIDENCE OF CORROSION. DOT 23-150. INSTALLE
- [SDR IPXA2025042401530](https://openairdocs.org/sdr/IPXA2025042401530), Apr 8, 2025: FLOOR SUPPORT. CORRODED. AFT CARGO COMP ON 4TH LH SIDE FLOOR PANEL SUPORT STR AROUND NUTPLATES, BETWEEN STA 1460 AND 1480 HAS EVIDENCE OF CORROSION. LOCATED AND DRILLED NEW FLOOR SUPPOR
- [SDR IPXA2025042501411](https://openairdocs.org/sdr/IPXA2025042501411), Apr 8, 2025: FLOOR SUPPORT. CORRODED. AFT CARGO COMP ON 2ND RH SIDE FLOOR PANEL SUPORT STR AROUND NUTPLATES, BETWEEN STA 1460 AND 1480 HAS EVIDENCE OF CORROSION. DOT 23-151. LOCALED AND DRILLED NEW 
- [SDR IPXA2025042701512](https://openairdocs.org/sdr/IPXA2025042701512), Apr 8, 2025: FLOOR SUPPORT. CORRODED. AFT CARGO COMP ON 2ND LH SIDE FLOOR PANEL SUPORT STR AROUND NUTPLATES, BETWEEN STA 1460 AND 1480 HAS EVIDENCE OF CORROSION. LOCATED AND DRILLED FLOOR STRINGER S
- [SDR IPXA2025042701464](https://openairdocs.org/sdr/IPXA2025042701464), Apr 8, 2025: FLOOR SUPPORT. CORRODED. AFT CARGO COMP ON 4TH RH SIDE FLOOR PANEL SUPORT STR AROUND NUTPLATES, BETWEEN STA 1460 AND 1480 HAS EVIDENCE OF CORROSION. DOT 23-153. INSTALLED 4TH RH SIDE FL
- [SDR IPXA2025042837359](https://openairdocs.org/sdr/IPXA2025042837359), Apr 4, 2025: FRAME. CORRODED. AFT CARGO DOOR: AFT CARGO DOOR INTERNAL LWR FRAME NO.3 (FROM FWD) HAS CORROSION. DOT NO. 17-10. INSTALLED NEW LOWER FRAME ON AFT CARGO DOOR. P/N MS20470AD6-6, B
- [SDR IPXA2025042838583](https://openairdocs.org/sdr/IPXA2025042838583), Apr 4, 2025: SUPPORT BRACKET. CORRODED. AFT CARGO DOOR: AFT CARGO DOOR INTERNAL LIGHT L391 ATTACHMENT PLATE IS CORRODED. INSTALLED NEW LIGHT SUPPORT OF L391 (01EA) ON AFT CARGO DOOR IAW SRM 51-40-02.
- [SDR IPXA2025041029360](https://openairdocs.org/sdr/IPXA2025041029360), Apr 4, 2025: FLOOR PANEL. DAMAGED. MDC, ABOVE CENTER BOX, FLOOR PANEL 242XGF EXTERNAL/INNER SURFACE AND EDGE IS DAMAGED. DOT 103-46.FABRICATED MCD FLOOR PANEL 242XGF, IAW UPS SREO: B757-9692-REQ 
- [SDR IPXA2025041029238](https://openairdocs.org/sdr/IPXA2025041029238), Apr 4, 2025: FLOOR PANEL. DENTED. MDC, ABOVE CENTER BOX, FLOOR PANEL 242XHF, EXERNAL AND INNER SURFACE HAS DENTS AND EDGE DAMAGED. FABRICATED MCD FLOOR PANEL 242XHF, IAW UPS SREO: B757-9692-REQ 
- [SDR IPXA2025041029564](https://openairdocs.org/sdr/IPXA2025041029564), Apr 4, 2025: FLOOR PANEL. DENTED. FAULT - Z200, COMP, MDC, ABOVE CENTER BOX, FLOOR PANEL 242XEF INNER SURFACE AND EDGE IS DAMAGED. DOT 103-51. FABRICATED MCD FLOOR PANEL 242XEF, IAW UPS SREO: B7
- [SDR IPXA2025040929634](https://openairdocs.org/sdr/IPXA2025040929634), Apr 4, 2025: FLOOR PANEL. DAMAGED. MDC, ABOVE CENTER BOX, FLOOR PANEL 242XDF HAS INNER SURFACE AND EDGE DAMAGED. FABRICATED MCD FLOOR PANEL 242XDF, IAW UPS SREO: B757-9692-REQ 001.VERIFIED FABRIC
- [SDR IPXA2025041029490](https://openairdocs.org/sdr/IPXA2025041029490), Apr 4, 2025: FLOOR PANEL. PUNCTURED. MDC, ABOVE CENTER BOX, FLOOR PANEL 242XBF INNER SURFACE HAS PUCTURES AND DENTS. FABRICATED MCD FLOOR PANEL 242XBF, IAW UPS SREO: B757-9692-REQ 001.VERIFIED FABR
- [SDR IPXA2025041029722](https://openairdocs.org/sdr/IPXA2025041029722), Apr 4, 2025: FLOOR PANEL. DAMAGED. MDC, ABOVE CENTER BOX, FLOOR PANEL 242XAF HAS EDGE DAMAGED. FABRICATED MCD FLOOR PANEL 242XAF, IAW UPS SREO: B757-9692-REQ 001.VERIFIED FABRICATION OF MCD FLOOR
- [SDR IPXA2025040322399](https://openairdocs.org/sdr/IPXA2025040322399), Apr 3, 2025: TRANSITION PANEL. CORRODED. AFT CARGO TRANSITION PANEL R/H SIDE BETWEEN STA 1440-1460 HAS CORROSION UNDER NUTPLATE DOT#21-5. INSTALLED FLOOR PANEL SUPPORT IAW B757 SRM 51-40-02.
- [SDR IPXA2025040323286](https://openairdocs.org/sdr/IPXA2025040323286), Apr 3, 2025: TEE ANGLE. CORRODED. FAULT, STR, ZONE 100,T-CHORD AT FS 1220 RBL 15 UNDER WING TO BODY PANEL 198 MR HAS CORROSION DOT#21-10. REMOVED FRAME AT 1220 RBL 15 UNDER WTB PANEL 198MR IAW B
- [SDR IPXA2025042122221](https://openairdocs.org/sdr/IPXA2025042122221), Apr 3, 2025: FRAME. DENTED. FAULT: STR, ZONE 100, AFT CARGO FRAME AT STA 1460 HAS A DENT BETWEEN SR26 AND SR27 DOT#21-4.STRIPPED PROTECTIVE FINISHES ON TRANSITION PANEL ANCHOR-PLATE AT RHS
- [SDR IPXA2025041011799](https://openairdocs.org/sdr/IPXA2025041011799), Apr 3, 2025: INSERT. MISSING. MAIN DECK FLOORBOARD PANEL 241XFF MISSING INSERT FWD EDGE. DOT 140-010. REPLACED MISSING FLOORBOARD PANEL 241XFF IAW SREO B757-5320-9692-K
- [SDR IPXA2025042807149](https://openairdocs.org/sdr/IPXA2025042807149), Apr 2, 2025: TEE ANGLE. CORRODED. CORROSION ON T CHORD STA 1150-1200 BL 70. INSTALLED (14EA NUT PLATES AND 3EA FASTENERS) AT AREA I.A.W B757-200 RM 51-40-02-OG.
- [SDR IPXA2025040207006](https://openairdocs.org/sdr/IPXA2025040207006), Apr 2, 2025: TEE ANGLE. CORRODED. CORROSION ON T CHORD AT STA 1180-1220 BL 57.50. INSTALLED NEW T-CHORD FROM STA 1180 TO 1220 LBL 57. NUTPLATES-BACN11P3B6CG, BATCH 0004386857, QTY 17. RIVETS-MS2
- [SDR IPXA2025040206822](https://openairdocs.org/sdr/IPXA2025040206822), Apr 2, 2025: FLOORBEAM. CORRODED. CORROSION ON L/H SIDE T CHORD AT STA 1200.REMOVED T-CHORD ON L/H, STA 1200, IAW SRM 51-40-02. RECIVED THE NEW PART P/N: UP-536071011-3.TRAVELER #: T25/1809242.I
- [SDR IPXA2025040206878](https://openairdocs.org/sdr/IPXA2025040206878), Apr 2, 2025: FLOORBEAM. CORRODED. CORROSION ON L/H SIDE T CHORD AT STA 1220 BL 30.75- BL 57.50 REMOVED T-CHORD ON L/H SIDE AT STA 1220 BL 30.75 BL 57.50 FOR DELAMINATION OUT OF LIMITS IAW 53-00-
- [SDR IPXA2025040207472](https://openairdocs.org/sdr/IPXA2025040207472), Apr 2, 2025: BRACKET. CORRODED. FAULT: STR, Z100, RAT SURROUND STRUCTURE BRACKET HAS CORROSSION STA 1216 RBL 57.5 REMOVED BRACKET CORRODED AT STA 1216 RBL 57.5 OUTBD TEE AT RAT DOOR CUTOUT IAW
- [SDR IPXA2025040207538](https://openairdocs.org/sdr/IPXA2025040207538), Apr 2, 2025: BRACKET. CORRODED. FAULT: STR, Z100 RAT SURROUND STRUCTURE BRACKET HAS CORROSSION STA 1230 RBL 57.5 REMOVED BRACKET CORRODED AT STA 1230 RBL 57.5 OUTBD TEE AT RAT DOOR CUTOUT IAW 
- [SDR IPXA2025040207627](https://openairdocs.org/sdr/IPXA2025040207627), Apr 2, 2025: BRACKET. CORRODED. FAULT: STR, Z100, RAT SURROUND STRUCTURE BRACKET HAS CORROSSION STA 1244 RBL 57.5 REMOVED BRACKET CORRODED AT STA 1244 RBL 57.5 OUTBD TEE AT RAT DOOR CUTOUT IAW
- [SDR IPXA2025040207602](https://openairdocs.org/sdr/IPXA2025040207602), Apr 2, 2025: BRACKET. CORRODED. FAULT: STR, Z100, RAT SURROUND STRUCTURE BRACKET HAS CORROSSION STA 1260 RBL 57.50 REMOVED BRACKET CORRODED AT STA 1260 RBL 57.5 OUTBD TEE AT RAT DOOR CUTOUT IA
- [SDR IPXA2025040207149](https://openairdocs.org/sdr/IPXA2025040207149), Apr 2, 2025: TEE ANGLE. CORRODED. **SDR FILED OPEN** CORROSION ON T CHORD STA 1150-1200 BL 70
- [SDR IPXA2025040184922](https://openairdocs.org/sdr/IPXA2025040184922), Apr 1, 2025: ANGLE. CORRODED. APU DOOR SURROUND FS 1790 - 1820 STR 3R THE 148N3152-2 IS CORRODED. REPLACE 1 EACH S-3R SUPPORT ANGLE (P/N: 148N3152-2) PER PRODUCTION DRAWING REQUIREMENTS AND 
- [SDR IPXA2025040185119](https://openairdocs.org/sdr/IPXA2025040185119), Apr 1, 2025: SUPPORT ANGLE. CORRODED. FAULT STR-Z300: APU DOOR SURROUND 148N3152-1 AT FS 1790 - 1820 STR 6R SI CORRODED. FABRICATED NEW SUPPORT ANGLE FOR STR 6 FROM STA 1790 TO 1820. MATERIAL USED- 
- [SDR IPXA2025042588024](https://openairdocs.org/sdr/IPXA2025042588024), Apr 1, 2025: ACCESS PANEL. GOUGED. FAULT - Z400, STR, #2 ENG STRUT ACCESS THROUGH PNL 443CR LOWER CORD HAS A GOUGE. DOT 95-23.ACCOMPLISHED STEP 1 OF EA # 757-5450-27-A3881 PRELIMINARY 1. REMOVED 
- [SDR IPXA2025040184721](https://openairdocs.org/sdr/IPXA2025040184721), Apr 1, 2025: STRAP. CORRODED. APU DOOR SURROUND FS1825.00 FROM FS 3R TO FS 6R THE 148N3138-8000 IS CORRODED.REMOVED RIVETS AND NUTPLATE FOR ACCESS FROM FS 1825 UPPER FUSELAGE APU DOOR SURROU
- [SDR IPXA2025040184095](https://openairdocs.org/sdr/IPXA2025040184095), Apr 1, 2025: STRAP. CORRODED. APU DOOR SURROUND FS1787.45 FROM STR 3R - STR 6R THE 148N3138-20 STRAP IS EXFOLIATED RED DOT. INSTALLED STRAP ON APU DOOR SURROUND FS1787.45 FROM STR 3R - STR 6
- [SDR IPXA2025012108882](https://openairdocs.org/sdr/IPXA2025012108882), Jan 21, 2025: HINGE FITTING. WORN. APU SHUTDOWN IN FLIGHT, DOWN TO SINGLE GEN DUE TO MEL. ATB PER QRH AND FLIGHT CONTROL. REMOVED AND REPLACED APU INLET DOOR INBOARD HINGE BEARING ASSY AND BOTH D
- [SDR IPXA2025011604140](https://openairdocs.org/sdr/IPXA2025011604140), Jan 15, 2025: WARNING MESSAGE. FALSE ACTIVATION. AIR TURNBACK, APU FAULT CLIMBING THROUGH 15,000€™. DID NOT RESTART PER QRH PROCEDURE. ACCOMPLISHED APU BITE REF 757 FIM 49-11-875. NO FAULTS FOUND ON ECU. INSP
- [SDR IPXA202501154140](https://openairdocs.org/sdr/IPXA202501154140), Jan 15, 2025: APU. FAULTED. **ATB** **SDR FILED OPEN** APU FAULT CLIMBING THROUGH 15,000€™. DID NOT RESTART PER QRH PROCEDURE.
- [SDR IPXA2024082635620](https://openairdocs.org/sdr/IPXA2024082635620), Aug 24, 2024: SKIN. CORRODED. EVIDENCE OF 2 PULLED RIVETS AND CORROSION FORWARD OF VHF ANTENNA AT 6 O CLOCK POSITION UNDER AFT CARGO. RESTORED FINISHES PER AMM 51-21-10.
- [SDR IPXA2023111578845](https://openairdocs.org/sdr/IPXA2023111578845), Nov 14, 2023: DISPLAY. INOPERATIVE. *SUPPLEMENTAL SDR* *DIVERSION* AT CRUISE L PFD BLANKED. PFD TRANSFER SWITCH DID WORK TO REGAIN CAPTAINS DISPLAY, BUT WITH F/O€™S NOW BLANK AS A RESULT. REMOVED
- [SDR IPXA2023111478845](https://openairdocs.org/sdr/IPXA2023111478845), Nov 14, 2023: UNKNOWN. UNKNOWN. AT CRUISE L PFD BLANKED. PFD TRANSFER SWITCH DID WORK TO REGAIN CAPTAINS DISPLAY, BUT WITH F/O€™S NOW BLANK AS A RESULT. REMOVED AND REPLACED LEFT GGU PER MM31
- [SDR IPXA2023072177235](https://openairdocs.org/sdr/IPXA2023072177235), Jun 16, 2023: DOOR. INOPERATIVE. *SUPPLEMENTAL SDR* DURING LANDING HAD A GEAR DOOR AND AUTO SPEED BRAKE LIGHT. DID A GO AROUND, RAN CHECKLIST. NEXT APPROACH NOTICED LEFT HYD RES. AT .24. STABIL
- [SDR IPXA202306160001](https://openairdocs.org/sdr/IPXA202306160001), Jun 16, 2023: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** DURING LANDING HAD A GEAR DOOR AND AUTO SPEED BRAKE LIGHT. DID A GO AROUND, RAN CHECKLIST. NEXT APPROACH NOTICED LEFT HYD RES. AT .24. ST

All 152: https://openairdocs.org/aircraft/N470UP/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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