# N463UP: 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: 28267
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 17, 1997
- Certificate issued: July 17, 1997
- Expires: November 30, 2027
- Mode S code: A5A690
- 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=463UP
- Page: https://openairdocs.org/aircraft/N463UP

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/N463UP/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 N463UP.

## FAA accident and incident reports

None matched to N463UP.

## Service difficulty reports (217, 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 IPXA2026102228872](https://openairdocs.org/sdr/IPXA2026102228872), Sep 25, 2026: SUPPORT ANGLE. DAMAGED. WHILE REMOVING CREASE BEAM FOUND KICKPLATE SUPPORT ANGLE BETWEEN STA 350 AND STA 358 L/H SIDE WITH ELONGATED HOLE AFTER FASTENER REMOVAL AUDIT C\W
- [SDR IPXA2026102242761](https://openairdocs.org/sdr/IPXA2026102242761), Sep 20, 2026: LANDING. CRACKED. NR 2 INBD THRUST REVERSER UPPER PANEL LANDING HAS A CRACK.
- [SDR IPXA2026101949482](https://openairdocs.org/sdr/IPXA2026101949482), Sep 15, 2026: BUSHING. CRACKED. NR 1-ENG. INBD THRUST REVERSER, UPON THE REMOVAL PHASE, FOUND UPR-CTR-HINGE WITH (HAT) BUSHING CRACKED AT FWD-SIDE.
- [SDR IPXA2026100354024](https://openairdocs.org/sdr/IPXA2026100354024), Sep 15, 2026: GUSSET. CORRODED. WHILE EVALUATING JCW T3F18E009L4M8, FOUND CORROSION AT BS 1885, BULKHEAD FWD SIDE SERVICE DOOR LATCH FITTINGS. INSTALLED 4EA NEW GUSSETS P/N 148N6614U9 B/N 4512
- [SDR IPXA2026102018336](https://openairdocs.org/sdr/IPXA2026102018336), Sep 6, 2026: SUPPORT PLATE. GOUGED. MAIN DECK BTW STA 1660 AND 1681.1 AND S-17 PLATE SUPPORT HAS SEVERAL GOUGES.
- [SDR IPXA2026101918056](https://openairdocs.org/sdr/IPXA2026101918056), Sep 6, 2026: SEAT TRACK. GOUGED. MAIN DECK SEAT TRACK BETWEEN STA 580 - 600, LBL 62.225 HAS GOUGES.
- [SDR IPXA2026101816920](https://openairdocs.org/sdr/IPXA2026101816920), Sep 6, 2026: FRAME. CRACKED. AFT CARGO COMPARTMENT FUSELAGE FRAME HAS A CRACK APPROX AT BS 1500, STGR 26R. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-98861REQ1 AND EA 757-5360-01-B0826, REV 
- [SDR IPXA2026101617312](https://openairdocs.org/sdr/IPXA2026101617312), Sep 6, 2026: WEB. BENT. AFT CARGO COMPARTMENT INTERNAL FUSELAGE STRUCTURE INTERCOSTAL IS DEFORMED APPROX BTW BS 1440 & BS 1460, BTW STGR 25R AND STGR 24R, INSTALLED NEW INTERCOSTAL AT 
- [SDR IPXA2026091716966](https://openairdocs.org/sdr/IPXA2026091716966), Sep 6, 2026: FRAME. DENTED. AFT CARGO COMPARTMENT FUSELAGE FRAME HAS 2 DENTS APPROX AT BS 1460, STGR 26R, VERIFIED REMOVAL OF FITTING ON STEP 27 PER DOCUMENT AND PER GMM RII 04-02
- [SDR IPXA2026091018202](https://openairdocs.org/sdr/IPXA2026091018202), Sep 6, 2026: FLOORBEAM. CORRODED. MAIN DECK, BS 860 BTW BL 0 TO LBL 24.75, FLOORBEAM HAS EXFOLATION.
- [SDR IPXA2026090912765](https://openairdocs.org/sdr/IPXA2026090912765), Sep 6, 2026: FLOORBEAM. CORRODED. MAIN DECK STA 1500 BTW LBL 45.50 TO 54.9 FLOORBEAM HAS CORROSION AROUND SCREW HOLE. VERIFIED STEP 9 REF GMM RII 04-02. EVALUATED REWORKED AREA ON MAIN DECK STA 
- [SDR IPXA2026101507031](https://openairdocs.org/sdr/IPXA2026101507031), Sep 5, 2026: NUT PLATE. DAMAGED. MAIN DECK STA 1681.1 AND BTW LBL 45.50 AND 54.9 RETAINER NUT HAS CORROSION BOTTOM SURFACE OF THE TOP FLANGE, INSTALLED NEW NUT PLATE RETAINER STRIP ON MAIN DECK
- [SDR IPXA2026101498292](https://openairdocs.org/sdr/IPXA2026101498292), Sep 5, 2026: PLATE. CORRODED. RIGHT HORIZONTAL STAB FAIRING 342AR LOWER SIDE EXTENDING AFT TRANSITION END PLATE HAS CORROSION.
- [SDR IPXA2026100298223](https://openairdocs.org/sdr/IPXA2026100298223), Sep 5, 2026: FAIRING. GOUGED. MAJOR REPAIR, GOUGE IN FUSELAGE SKIN EXTENDING UNDER R/H HORZ STAB LOWER SLIDING FAIRING. RL108 (NOTE: CHECK LOWER SLIDING FAIRING SCREW LENGTH TO PREVENT REOCC
- [SDR IPXA2026091406679](https://openairdocs.org/sdr/IPXA2026091406679), Sep 5, 2026: DECK PLATE. CORRODED. MAIN DECK FROM BS 1681.1 - 1720, LBL 54.9 - RBL 54.9 DECK PLATE HAS MULTIPLE AREAS WITH CORROSION, REQUEST NDT UT THICKNESS. AT REWORKED AREAS IAW SRM 53-60-51-
- [SDR IPXA2026090997871](https://openairdocs.org/sdr/IPXA2026090997871), Sep 5, 2026: FAIRING. CORRODED. LEFT HORZ STAB FAIRING 332AL LOWER SIDE EXTENDING AFT TRANSITION END PLATE HAS CORROSION. VERIFIED STEPS 5 AND 6 C/W
- [SDR IPXA2026102080618](https://openairdocs.org/sdr/IPXA2026102080618), Sep 4, 2026: SKIN PANEL. DELAMINATED. APU COMPARTMENT R/H SIDE COMPOSITE SKIN PANEL SECTION BETWEEN STA 1941 AND 1963 DELAMINATED. REPAIR FILLER AND DOUBLER MADE FROM 0.012-INCH-THICK 2024-T3 BARE A
- [SDR IPXA2026102380237](https://openairdocs.org/sdr/IPXA2026102380237), Sep 4, 2026: SUPPORT BRACKET. DAMAGED. ALL APU COMPARTMENT R/H SIDE CEILING ELECTRICAL WIRE HARNESS SUPPORT BRACKETS HAVE CORROSION AND MISSING PROTECTIVE FININSH. RL037.INSTALLED 3EA SUPPOR BRACKETS
- [SDR IPXA2026101780235](https://openairdocs.org/sdr/IPXA2026101780235), Sep 4, 2026: BRACKET. CORRODED. ALL APU COMPARTMENT L/H SIDE CEILING ELECTRICAL WIRE HARNESS SUPPORT BRACKETS HAVE CORROSION AND MISSING PROTECTIVE FINISH. INSTALLED 4EA NEW SUPPORT BRACKETS A
- [SDR IPXA2026101680268](https://openairdocs.org/sdr/IPXA2026101680268), Sep 4, 2026: SUPPORT BRACKET. DAMAGED. ALL ELECTRICAL WIRE BUNDLES, POWER FEED CABLES AND FLUID LINE SUPPORT BRACKETS ATTACHED TO APU COMPARTMENT FWD BULKHEAD STA 1885 HAVE CORROSION AND MISSING PROT
- [SDR IPXA2026092678940](https://openairdocs.org/sdr/IPXA2026092678940), Sep 4, 2026: SKIN. DEBONDED. MAJOR REPAIR, LOWER BILGE COMPOSITE SKIN PANEL BETWEEN STA 1963 TO 1992 FWD AND AFT EDGES DISBONDED WITH AREAS OF CORROSION INCLUDING FWD EDGE LEVELING COMPOUND
- [SDR IPXA2026100280598](https://openairdocs.org/sdr/IPXA2026100280598), Sep 4, 2026: SKIN. DELAMINATED. MAJOR REPAIR, APU COMPARTMENT R/H SIDE COMPOSITE SKIN PANEL SECTION BETWEEN STA 1918 AND 1941 DELAMINATED. RL038 QCI(RII) VERIFIED FABRICATION OF DOUBLER PER ST
- [SDR IPXA2026100280618](https://openairdocs.org/sdr/IPXA2026100280618), Sep 4, 2026: SKIN. DELAMINATED. MAJOR REPAIR, APU COMPARTMENT R/H SIDE COMPOSITE SKIN PANEL SECTION BETWEEN STA 1941 AND 1963 DELAMINATED. RL039 QCI(RII) VERIFIED STEP 13 IS C/W AND VERIFIED T
- [SDR IPXA2026091580268](https://openairdocs.org/sdr/IPXA2026091580268), Sep 4, 2026: BRACKET. CORRODED. ALL ELECTRICAL WIRE BUNDLES, POWER FEED CABLES AND FLUID LINE SUPPORT BRACKETS ATTACHED TO APU COMPARTMENT FWD BULKHEAD STA 1885 HAVE CORROSION AND MISSING PROT
- [SDR IPXA2026091580804](https://openairdocs.org/sdr/IPXA2026091580804), Sep 4, 2026: FRAME. CORRODED. FRAME STA 1992 FWD AND AFT SIDES HAS AREAS OF CORROSION AND MISSING PROTECTIVE FINISH WITH HEAVY DEBRIS ON BACK SIDE PLUGGING DRAIN HOLE.
- [SDR IPXA2026091478857](https://openairdocs.org/sdr/IPXA2026091478857), Sep 4, 2026: FRAME. CORRODED. AFT FUSLAGE FRAME STA 1963 FWD AND AFT SIDES AND ALL ATTACHING STRUCTURE CIRCUMFERENTIALLY HAVE AREAS OF CORROSION AND LARGE AREAS OF MISSING PROTECTIVE FINISH 
- [SDR IPXA2026090881106](https://openairdocs.org/sdr/IPXA2026090881106), Sep 4, 2026: SKIN. CORRODED. EXTERNAL FUSELAGE SKIN BS 1862 HAS AREAS OF CORROSION AREA JUST FWD OF ACCESS DOOR 313AL. RL050 ACCOMPLISHED VISUAL INSP WITH 10X MAGNIFYING GLASS AT CORROSION 
- [SDR IPXA2026090880235](https://openairdocs.org/sdr/IPXA2026090880235), Sep 4, 2026: SUPPORT BRACKET. CORRODED. ALL APU COMPARTMENT L/H SIDE CEILING ELECTRICAL WIRE HARNESS SUPPORT BRACKETS HAVE CORROSION AND MISSING PROTECTIVE FININSH. RL036 VERIFIED STEPS 1,2 AND 3
- [SDR IPXA2026090880237](https://openairdocs.org/sdr/IPXA2026090880237), Sep 4, 2026: SUPPORT BRACKET. CORRODED. ALL APU COMPARTMENT R/H SIDE CEILING ELECTRICAL WIRE HARNESS SUPPORT BRACKETS HAVE CORROSION AND MISSING PROTECTIVE FINISH. RL037 VERIFIED STEPS 1,2 AND 3
- [SDR IPXA2026101672642](https://openairdocs.org/sdr/IPXA2026101672642), Sep 3, 2026: FITTING. DAMAGED. LH TRUNNION CANOE FAIRING I/B BEARING HAS RADIAL PLAY MARKED JK-34 ATA 57.INSTALLED FITTING 2 EACH AT L/H MLG AFT TRUNNION / FLAP FAIRING I.A.W. BOEING 757 SRM 
- [SDR IPXA2026101678146](https://openairdocs.org/sdr/IPXA2026101678146), Sep 3, 2026: SUPPORT BRACKET. DAMAGED. STR, ATA 49: APU AIR INTAKE DUCT EXTERNAL DRAIN TUBE SUPPORT BRACKET HAS CORROSION. RL020. INSTALLED NEW BRACKET SUPPORT P/N: 356N1011-1 BTCH #: 0004514718ON AP
- [SDR IPXA2026101448482](https://openairdocs.org/sdr/IPXA2026101448482), Sep 2, 2026: FRAME. CORRODED. RH ELEVATOR O/B UPPER SURFACE AROUND O/B STATIC DISCHARGER HAS LIGHT CORROSION. INSTALLED NEW UPPER CONDUCTIVE FRAME AND UPPER SPLICE PLATE AT R/H ELEVATOR O/B 
- [SDR IPXA2026101448406](https://openairdocs.org/sdr/IPXA2026101448406), Sep 2, 2026: ADAPTER. CORRODED. RH ELEVATOR STATIC DISCHARGER BASE, 2ND FROM O/B, HAS CORROSION. INSTALLED ADAPTER PLATE RH ELEVATOR STATIC DISCHARGER ON RH ELEVATOR UPPER SURFACE. IAW B757-20
- [SDR IPXA2026091453546](https://openairdocs.org/sdr/IPXA2026091453546), Sep 2, 2026: STRAP. CORRODED. WHILE EVALUATING APU INLET SURROUND STRUCTURE FOUND CORROSION ON EXISTING AFT STRAP REPAIR AT BS 1825 BETWEEN S-3R TO S-6R. VERIFIED STEP 10, C/W SRM 53-80-15-2
- [SDR IPXA2026090848406](https://openairdocs.org/sdr/IPXA2026090848406), Sep 2, 2026: STATIC WICK. CORRODED. RIGHT ELEVATOR STATIC DISCHARGER BASE, 2ND FROM O/B, HAS CORROSION. 83-023. ATA 23-60. QCI: VERIFIED STEP 1 AND 2
- [SDR IPXA2026090848482](https://openairdocs.org/sdr/IPXA2026090848482), Sep 2, 2026: STATIC WICK. CORRODED. RH ELEVATOR O/B UPPER SURFACE AROUND O/B STATIC DISCHARGER HAS LIGHT CORROSION. VERIFIED STEP 5 C/W
- [SDR IPXA2026090848502](https://openairdocs.org/sdr/IPXA2026090848502), Sep 2, 2026: FRAME. BULGED. RH ELEVATOR LOWER SURFACE O/B CONDUCTIVE FRAME SPLICE HAS BULGING, EVIDENCE OF CORROSION UNDERNEATH. 83-025. ATA 55-20. QCI: VERIFIED STEP 6 C/W
- [SDR IPXA2026101437466](https://openairdocs.org/sdr/IPXA2026101437466), Sep 1, 2026: BRACKET. CORRODED. RH HORZ STAB TIP BONDING STRAP HAS CORROSION UNDERNEATH DISBONDED SEALANT. INSTALLED BONDING BRACKET, 1 EA RIB AND 1EA NEW BONDING JUMPER PN: BACJ40E20-20 BATCH
- [SDR IPXA2026101636983](https://openairdocs.org/sdr/IPXA2026101636983), Sep 1, 2026: FRAME. CORRODED. LH ELEVATOR UPPER, O/B CONDUCTIVE FRAME HAS BULGING ACROSS FASTENERS. INSTALLED L/H UPPER CONDUCTIVE FRAME, 1 EA UPPER SPLICE PLATE AND 1 EA STATIC DISCHARGER B
- [SDR IPXA2026102135854](https://openairdocs.org/sdr/IPXA2026102135854), Sep 1, 2026: SUPPORT BRACKET. CRACKED. RH WW SUPPORT BRACKET IS CRACKED MARKED JK-22 ATA 32 INSP AUDIT C/W
- [SDR IPXA2026100935479](https://openairdocs.org/sdr/IPXA2026100935479), Sep 1, 2026: ANGLE. CORRODED. LH HORZ STAB TIP T/E BONDING STRAP SUPPORT BRACKET HAS EXFOLIATION CORROSION. 83-003. ATA 55-10. INSTALLED 1 EA RIB 1EA HORZ STAB TIP STRAP ANGLE P/N 183N1341-1
- [SDR IPXA2026101736976](https://openairdocs.org/sdr/IPXA2026101736976), Sep 1, 2026: FRAME. CORRODED. LH ELEVATOR LOWER, O/B END CONDUCTIVE FRAME SPLICE HAS EVIDENCE OF CORROSION UNDER SEALANT. ATA 55-20. 83-004.INSTALLED L/H LOWER CONDUCTIVE FRAME AND LOWER SPL
- [SDR IPXA2026102034414](https://openairdocs.org/sdr/IPXA2026102034414), Sep 1, 2026: BRACKET. CRACKED. RH WW PROX SENSOR BRACKET HAS A GOUGE.
- [SDR IPXA2026101934575](https://openairdocs.org/sdr/IPXA2026101934575), Sep 1, 2026: BRACKET. CRACKED. RH WW GUSSET IS CRACKED. INSTALLED REPLACEMENT BRACKET IN R/H WW REF B757-200 PF SRM 51-40-02-0G-0 REV 126-20.
- [SDR IPXA2026101828804](https://openairdocs.org/sdr/IPXA2026101828804), Sep 1, 2026: STRAP. TEMP REPAIR. ACCOMPLISH PERMANENT REPAIR AT MAIN CARGO DOOR CUTOUT LOWER STRAP AT BS 620 BTWN STR 24L-26L. IAW EO-84558-REQ001 REV 1. ACCOMPLISHED REPAIR PER EO-98915-REQ1 &
- [SDR IPXA2026100836983](https://openairdocs.org/sdr/IPXA2026100836983), Sep 1, 2026: FRAME. DAMAGED. LH ELEVATOR UPPER, O/B CONDUCTIVE FRAME HAS BULGING ACROSS FASTENERS.
- [SDR IPXA2026090837466](https://openairdocs.org/sdr/IPXA2026090837466), Sep 1, 2026: BONDING STRAP. DAMAGED. RH HORZ STAB TIP BONDING STRAP HAS CORROSION UNDERNEATH DISBONDED SEALANT. REMOVED 1 EA DAMAGED BONDING JUMPER AT R/H HORZ STAB REAR SPAR TO ELEVATOR FRONT SPAR
- [SDR IPXA2026101818153](https://openairdocs.org/sdr/IPXA2026101818153), Aug 31, 2026: SKIN. DENTED. LEFT EXTERNAL FUSELAGE SKIN EXISTING REPAIR DOUBLER HAS 2 EA DENTS APPROX BTW BS 201 AND BS 222, STRG 20L THRU STGR 21L, ID STICKER NUM. (085-002). ATA 53-30. A
- [SDR IPXA2026090814643](https://openairdocs.org/sdr/IPXA2026090814643), Aug 31, 2026: STRAP. CORRODED. APU INLET SURROUND STRUCTURE (INTERIOR) HAS CORROSION AT LOWER LONGERON COMMON TO FWD STRAP,
- [SDR IPXA2026082195946](https://openairdocs.org/sdr/IPXA2026082195946), Aug 21, 2026: UNKNOWN. ODOR. AT FL 390-410 ACRID BURNING TYPE SMELL COMMING FROM THE PACKS. UNABLE TO DETERMINE WHICH ONE. BACK TO NORMAL ON DESCENT. ACCOMPLISHED TROUBLSHOOTING IAW FIM REF

All 217: https://openairdocs.org/aircraft/N463UP/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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.