# N471UP: 1998 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: 28842
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 22, 1998
- Certificate issued: July 27, 1998
- Expires: November 30, 2027
- Mode S code: A5C6A1
- 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=471UP
- Page: https://openairdocs.org/aircraft/N471UP

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/N471UP/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 N471UP.

## FAA accident and incident reports

None matched to N471UP.

## Service difficulty reports (168, 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 IPXA2026073130927](https://openairdocs.org/sdr/IPXA2026073130927), Jul 30, 2026: WINDOW. FAILED. FO FWD WINDOW STARTED ARCING WE SHUT OF FWD WINDOW HEAT OUTER WINDOW SHATTERED RAN QRH PROCEDURE AND CONTINUED FLIGHT NO SIGNS OF LEAK OR WINDOW BEING DEFORMED.
- [SDR IPXA2026073030927](https://openairdocs.org/sdr/IPXA2026073030927), Jul 30, 2026: WINDOW. ARCED. FO FWD WINDOW STARTED ARCING WE SHUT OF FWD WINDOW HEAT OUTER WINDOW SHATTERED RAN QRH PROCEDURE AND CONTINUED FLIGHT NO SIGNS OF LEAK OR WINDOW BEING DEFORMED.
- [SDR IPXA2025072576091](https://openairdocs.org/sdr/IPXA2025072576091), Jul 11, 2025: STRAP. CORRODED. MAJOR REPAIR, CORROSION FOUND ON STRAP AT AUXILARY POWER UNIT AIR INLET DOOR SURROUND STRUCTURE STA Y=1825 AND BETWEEN S-3R AND S-6R INSTALLED REPAIR PARTS, STR
- [SDR IPXA2025072442329](https://openairdocs.org/sdr/IPXA2025072442329), Jul 9, 2025: STRAP. CORRODED. MAJOR REPAIR, CORROSION ON APU INLET FWD NUT PLATE STRAP INSTALLED STRAP P/N: 148N3138-20, BTCH NO. 0004410942 AT APU INLET DOOR SURROUNDING STRUCTURE IAW B757-
- [SDR IPXA2024012959843](https://openairdocs.org/sdr/IPXA2024012959843), Jan 27, 2024: UNKNOWN. SMOKE. AFTER ENG START , OVERWHELMING FUEL/ OIL SMELL ON FLIGHT DECK. SMOKE/FUMES MEMORY ITEMS COMPLETE. O2 CHECK COMPLETE. SHUT DOWN THE ENGINES TOWED BACK IN ON O2. 
- [SDR IPXA2023111357959](https://openairdocs.org/sdr/IPXA2023111357959), Oct 6, 2023: DOOR. CHAFED. *** SUPPLEMENTAL SDR *** FAULT:CREW ENTRY DOOR CHAFING AT OUTTER SKIN LOWER AREA (4 E/A) DOT119-006 CLEANED SKIN LOWER AREA IAW SOPM 20-30-03 NO CHAFING, NO DAM
- [SDR IPXA2023100957959](https://openairdocs.org/sdr/IPXA2023100957959), Oct 6, 2023: UNKNOWN. UNKNOWN. FAULT:CREW ENTRY DOOR CHAFING AT OUTTER SKIN LOWER AREA (4 E/A) DOT119-006 CLEANED SKIN LOWER AREA IAW SOPM 20-30-03 NO CHAFING, NO DAMAGE WAS FOUND. AUDIT COMP
- [SDR IPXA2023061198722](https://openairdocs.org/sdr/IPXA2023061198722), Jun 9, 2023: SLAT. UNKNOWN. REF T3F18E001Y1WS ANDT3F18E001Y5M1 - ACCOMPLISH AN HFEC ON THE NO. 3 SLAT REPAIR ACCOMPLISHED PER EO-86906-REQ2 AS DIRECTED BY QC COMPLIED WITH EO-86906-REQ3, R
- [SDR IPXA2023012490217](https://openairdocs.org/sdr/IPXA2023012490217), Jan 24, 2023: WARNING MESSAGE. FALSE ACTIVATION. TE EDGE FLAP DISAGREE EICAS AND LIGHT WHEN SELECTING FLAPS FROM 20 TO 25. DECLARED EMERGENCY AND MADE NORMAL LANDING. OPERATED FLAPS/SLATS IN NORMAL AND ALTERNA
- [SDR IPXA2021101574986](https://openairdocs.org/sdr/IPXA2021101574986), Oct 11, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEGPNL 241XCF DAMAGEDFABBED PNL PER SREO B757-5320-9692-K
- [SDR IPXA2021101474954](https://openairdocs.org/sdr/IPXA2021101474954), Oct 11, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEGPNL 242XAF DAMAGEDFABBED PER SREO B757-5320-9692-K
- [SDR IPXA2021101474953](https://openairdocs.org/sdr/IPXA2021101474953), Oct 11, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEGPNL 242XBF DAMAGEDFABBED PER SREO B757-5320-9692-K
- [SDR IPXA2021101474952](https://openairdocs.org/sdr/IPXA2021101474952), Oct 11, 2021: FLOOR PANEL. NONE. INSPECTION TYPE:SEGPNL 241XEF DAMAGEDÏ¿½FABBED PER SREO B757-5320-9692-K
- [SDR IPXA2021101474951](https://openairdocs.org/sdr/IPXA2021101474951), Oct 11, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEGPNL 242XDF DAMAGEDFABBED PER SREO B757-5320-9692-K
- [SDR IPXA2021101474950](https://openairdocs.org/sdr/IPXA2021101474950), Oct 11, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEGPNL 242XEF DAMAGEDFABBED PER SREO B757-5320-9692-K
- [SDR IPXA2021102675350](https://openairdocs.org/sdr/IPXA2021102675350), Oct 9, 2021: NONE. CRACKED. INSPECTION TYPE:SEGPANEL 119AF IS PEELINGFABRICATED REPLACEMENT PANEL PER DWG 284N1033 USING 4417-41110133-9 BATCH# J5678456 PER GMM 09-10-03-01
- [SDR IPXA2021102575317](https://openairdocs.org/sdr/IPXA2021102575317), Oct 8, 2021: NONE. CRACKED. INSPECTION TYPE:SEG#1 ENGINE AFT OF AFT MOUNT IB BRACKET SUPPORT IS CRACKEDREMOVED CRACKED BRACKET AND INSTALLED REPLACEMENT BRAQCKET SUPPORT PER SRM 51-40-02-0
- [SDR IPXA2021102475271](https://openairdocs.org/sdr/IPXA2021102475271), Oct 8, 2021: NONE. CRACKED. INSPECTION TYPE:SEGMDCC AT STA 1056 & LBL40 FLOOR PANEL SUPPORT STRUCTURE IS CRACKEDREMOVED AND INSTALLED REPLACEMENT 144N5005-3 FLOOR SUPPORT PER SRM 51-40-02-
- [SDR IPXA2021102375234](https://openairdocs.org/sdr/IPXA2021102375234), Oct 6, 2021: NONE. CRACKED. INSPECTION TYPE:CRH WING SLAT #9 OB TRACK PANEL COVER IS CRACKEDREMOVED AND INSTALLED REPLACEMENT COVER PER SRM 51-40-02-0G
- [SDR IPXA2021102375233](https://openairdocs.org/sdr/IPXA2021102375233), Oct 6, 2021: NONE. CRACKED. INSPECTION TYPE:CRH WING SLAT #9 I/B TRACK PANEL COVER IS CRACKEDREMOVED AND INSTALLED REPLACEMENT COVER PER SRM 51-40-02-0G
- [SDR IPXA2020062967028](https://openairdocs.org/sdr/IPXA2020062967028), Jun 26, 2020: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS. OPS NORMAL AW MM 33-51-06
- [SDR IPXA2020022652511](https://openairdocs.org/sdr/IPXA2020022652511), Feb 25, 2020: CONNECTOR. NOT SEATED. INSPECTION TYPE:N/ADIVERSION - GEAR DESAGREE EICAS MSG UPON RAISING GEARC/W PSEU BITE PER FIM 32-09-03-815-804 FIG 103 FOUND SEVERAL FAULTY SENSORS. INSPECTED N
- [SDR IPXA2020022152340](https://openairdocs.org/sdr/IPXA2020022152340), Feb 20, 2020: WARNING LIGHT. ILLUMINATED. EMERGENCY DECLARED DUE TO GEAR DISAGREE EICAS & GEAR LIGHT, IN ADDITION DOOR LIGHT & EICAS AND NOSE GREEN LIGHT ILUMINATED WITH GEAR HANDLE. UNUSUAL AIRCRAFT VI
- [SDR IPXA2020010250581](https://openairdocs.org/sdr/IPXA2020010250581), Dec 31, 2019: PROBE. FAILED. INSPECTION TYPE:N/A*** ATB *** TAT PROBE FAILURE AT *31,000 FT, LOW AP AUTOTHROTTLES COMMAND SPEED, MAU CONTROL. PERFORMED FIM TASK 22-02-00-810-801-001 & FIM T
- [SDR IPXA2019111328922](https://openairdocs.org/sdr/IPXA2019111328922), Nov 8, 2019: PANEL. DAMAGED. INSPECTION TYPE:SVWING DRY BAY PANEL #632DZ HAS COMPOSITE DAMAGE.REPAIRED WING DRY BAY PANEL # 632DZ IAW VT-SAA EA 757-5720-01-A7948 REV. I/R. (MAJOR)
- [SDR IPXA2019110878746](https://openairdocs.org/sdr/IPXA2019110878746), Nov 7, 2019: FLOORBEAM. WORN. INSPECTION TYPE:C14 MAIN CARGO DECK BEAMS AT STA 879 HAVE DEEP WEAR MARKS FROM WRONG HARDWARE INSTALLED IN FLOORBOEARD SUPPORT. DOT # 29-211. REMOVED DISCREPANT
- [SDR IPXA2019030639780](https://openairdocs.org/sdr/IPXA2019030639780), Mar 3, 2019: BLOWER. INOPERATIVE. INSPECTION TYPE:NA CAPTS EVAS BLOWER CHECK TEST BUTTON INOP. REMOVED AND REPLACED CAPT'S EVAS PACK PER AMM 25-69-00-401 IPC 25-60-00-401.
- [SDR IPXA2018062230953](https://openairdocs.org/sdr/IPXA2018062230953), Jun 21, 2018: WINDOW. FAILED. AT 17,000 FEET, DURING DESECNT, THE FIRST OFFICER'S R1 WINDOW SHATTERED. EMERGENCY DECLARED, AND LANDED. R & R THE R1 WINDOW IAW MM 56-11-01-424.
- [SDR IPXA2017062918758](https://openairdocs.org/sdr/IPXA2017062918758), Jun 29, 2017: LINER. CORRODED. LEFT ENGINE LP COMPRESSOR FROM CASE HAS NUMEROUS AREAS OF CORROSION UNDER ROTOR PATH LINING. REMOVED CORROSION AND FOUND A LARGE AREA OUT OF LIMITS IAW AMM 72-3
- [SDR IPXA2017011812888](https://openairdocs.org/sdr/IPXA2017011812888), Jan 17, 2017: SMOKE GOGGLES. CRACKED. SUPERNUMERARY SEAT SMOKE GOGGLE LENS CRACKED. R&R'D SMOKE GOGGLE PER AMM 25-64-00-202-021.
- [SDR IPXA2017010412390](https://openairdocs.org/sdr/IPXA2017010412390), Dec 30, 2016: LAMP. INOPERATIVE. EMERGENCY EXIT UN ARMED ANNUC LT HAS 1 LAMP INOPERATIVE. REPLACED THE LAMP IAW MM 33-16-02-962-001. OPS CHECKED NORMAL..
- [SDR IPXA2016021299303](https://openairdocs.org/sdr/IPXA2016021299303), Feb 12, 2016: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHT INOPERATIVE, EGRESS LIGHT, REPLACED THE LAMP IAW AMM 33-51-06. OPS CHECKED NORMAL.
- [SDR IPXA2014120184964](https://openairdocs.org/sdr/IPXA2014120184964), Nov 26, 2014: LAMP. INOPERATIVE. EXTERIOR EGRESS, EVAC SLIDE, LAMP INOPERATIVE. TROUBLESHOT TO A FAULTY LAMP ASSY. R & R SAME. OPS CKS GOOD REF AMM 33-51-06.
- [SDR IPXA2014091984363](https://openairdocs.org/sdr/IPXA2014091984363), Sep 18, 2014: ELECTRONIC UNIT. INOPERATIVE. T/E FLAP DISAGREE MESSAGE ON APPROACH. EMERGENCY DECLARED. PERFORMED FSEU BITE PROCEDURE REF AMM 27-51-00-815. R & R FSEU AND OPS CHECKED GOOD IAW AMM 27-51-01 
- [SDR IPXA4583716](https://openairdocs.org/sdr/IPXA4583716), Jul 19, 2014: LAMP. INOPERATIVE. LAMP INOPERATIVE OVERHEAD PANEL. EMERGENCY LIGHT UNARMED INDICATOR. REPLACED LENS CAP IAW SWDM 20-84-14. OPS CK GOOD.
- [SDR IPXA2014012201508](https://openairdocs.org/sdr/IPXA2014012201508), Jan 8, 2014: FLOOR PANEL. DAMAGED. INSPECTION C8S4, MAIN DECK FLOOR PANEL 252XTF HAS EDGE DAMAGE. FABRICATED FLOOR PANEL IAW EO B757-5320-9692-H.
- [SDR IPXA2014012201507](https://openairdocs.org/sdr/IPXA2014012201507), Jan 8, 2014: FLOOR PANEL. DELAMINATED. INSPECTION C8S4, MAIN DECK FLOOR PANEL 231XFF IS DELAMINATED. FABRICATED FLOOR PANEL IAW EO B757-5320-9692-H.
- [SDR IPXA2014012201506](https://openairdocs.org/sdr/IPXA2014012201506), Jan 8, 2014: FLOOR PANEL. DAMAGED. INSPECTION C8S4, MAIN DECK FLOOR PANEL 232XJF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.
- [SDR IPXA2014012001498](https://openairdocs.org/sdr/IPXA2014012001498), Jan 8, 2014: FLOOR PANEL. DAMAGED. DURING C8S4 INSPECTION, MAIN DECK FLOOR PANEL 251XBF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.
- [SDR IPXA2014012001497](https://openairdocs.org/sdr/IPXA2014012001497), Jan 8, 2014: FLOOR PANEL. DAMAGED. DURING C8S4 INSPECTION, MAIN DECK FLOOR PANEL 252XSF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.
- [SDR IPXA2014012001496](https://openairdocs.org/sdr/IPXA2014012001496), Jan 8, 2014: FLOOR PANEL. DAMAGED. DURING C8S4 INSPECTION, MAIN DECK FLOOR PANEL 242XLF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.
- [SDR IPXA2014012001480](https://openairdocs.org/sdr/IPXA2014012001480), Jan 8, 2014: FLOOR PANEL. DELAMINATED. DURING C INSPECTION, MAIN DECK FLOOR PANEL 231XJF IS DELAMINATED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.
- [SDR IPXA2014012001479](https://openairdocs.org/sdr/IPXA2014012001479), Jan 8, 2014: FLOOR PANEL. DAMAGED. DURING C INSPECTION, MAIN DECK FLOOR PANEL 251XPF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.
- [SDR IPXA2014012001478](https://openairdocs.org/sdr/IPXA2014012001478), Jan 8, 2014: FLOOR PANEL. PUNCTURED. DURING C INSPECTION, MAIN DECK FLOOR PANEL 232XHF PUNCTURED ON UPPER SURFACE. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.
- [SDR IPXA2014012001477](https://openairdocs.org/sdr/IPXA2014012001477), Jan 8, 2014: FLOOR PANEL. DAMAGED. DURING C INSPECTION, MAIN DECK FLOOR PANEL 251XLF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.
- [SDR IPXA2014012001476](https://openairdocs.org/sdr/IPXA2014012001476), Jan 8, 2014: FLOOR PANEL. DAMAGED. DURING C INSPECTION, MAIN DECK FLOOR PANEL 241XLF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.
- [SDR IPXA2014012001475](https://openairdocs.org/sdr/IPXA2014012001475), Jan 8, 2014: FLOOR PANEL. DAMAGED. DURING C INSPECTION, MAIN DECK FLOOR PANEL 231XCF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.
- [SDR IPXA2014012001474](https://openairdocs.org/sdr/IPXA2014012001474), Jan 8, 2014: FLOOR PANEL. DAMAGED. DURING C INSPECTION, MAIN DECK FLOOR PANEL 231XEF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.
- [SDR IPXA2014012001472](https://openairdocs.org/sdr/IPXA2014012001472), Jan 8, 2014: FLOOR PANEL. DAMAGED. DURING C INSPECTION, MAIN DECK FLOOR PANEL 222XBF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL IAW EO 757-5320-9692-H.
- [SDR IPXA2014012001471](https://openairdocs.org/sdr/IPXA2014012001471), Jan 8, 2014: FLOOR PANEL. DAMAGED. DURING C INSPECTION, MAIN DECK FLOOR PANEL 252XEF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.

All 168: https://openairdocs.org/aircraft/N471UP/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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