# N57863: 2001 Boeing 757-33N

- Status: Valid registration
- Airframe: [Boeing 757-33N](https://openairdocs.org/model/boeing-757-33n) (registry code 1384931, 275 seats)
- Engine: [Rolls-Royce RB-211 series](https://openairdocs.org/engine/rolls-royce-rb-211-series) (registry code 54555)
- Serial number: 32587
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 22, 2001
- Certificate issued: September 8, 2023
- Expires: September 30, 2030
- Mode S code: A76F67
- Registered owner: [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC)
- Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago)
- Owner type: Corporation
- Owner's area on the map: 41.8813° N, 87.6375° W: Placed by OpenAirDocs at the center of ZIP code 60606, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=57863
- Page: https://openairdocs.org/aircraft/N57863

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 757-33N)

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/N57863/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 N57863.

## FAA accident and incident reports

None matched to N57863.

## Service difficulty reports (72, 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 CALA2026080418254](https://openairdocs.org/sdr/CALA2026080418254), Aug 2, 2026: REHEATER. FAULTED. R ENG BLEED OFF CAUTION MESSAGE CAME ON AT 110 KNOTS ON TAKEOFF ROLL. CONTINUED TAKEOFF. RAN QRC AND RESET BLEED SWITCH AND IT ILLUMINATED AFTER 5 SECONDS ALONG
- [SDR CALA2026071617797](https://openairdocs.org/sdr/CALA2026071617797), Jul 15, 2026: GUARD. BROKEN. BROKEN BRACKET ON THE LT MLG OTBD SIDE. NOTED BRACKET IS A GUARD FOR NR 1 BRAKE ASSY HYDRAULIC HOSE. APPROX. 30 SQ. INCHES. LT MLG WHEEL NR 1 OTBD TILT TRUCK ME
- [SDR CALA2026041315314](https://openairdocs.org/sdr/CALA2026041315314), Apr 11, 2026: CIRCUIT BREAKER. TRIPPED. DURING LT ENG START, LT GEN FAILED. RESET SUCCESSFUL. LT RECIRC FAN INOP. FOUND LT RECIRC FAN CB ON P70 PANEL TRIPPED. RESET CB, LT RECIRC FAN FUNCTIONS NORMALL
- [SDR CALA2026030214157](https://openairdocs.org/sdr/CALA2026030214157), Feb 27, 2026: LENS. FAULTED. ARMED LIGHT ABOVE DOOR 4L INOP REF AIPC 33-51-51-28 REPLACED LED LENS ABOVE DOOR 4L. VERIFIED LIGHT OPERATION.
- [SDR CALA2026012613285](https://openairdocs.org/sdr/CALA2026012613285), Jan 26, 2026: NONE. NONE. EMERGENCY POWER RESERVOIR CHECK PROCEDURE, INSTALLED SAFE DOOR PINS FOR DOOR SLIDE. INSTALLED EMARGENCY RESERVOIR SAFETY PINS L2 FOR GIRT BAR LUBE REMOVED SAFE 
- [SDR CALA2026012613281](https://openairdocs.org/sdr/CALA2026012613281), Jan 26, 2026: GIRT BAR. LACK OF LUBE. EMERGENCY POWER RESERVOIR CHECK PROCEDURE - INSTALLED SAFE DOOR PINS FOR DOOR SLIDE. INSTALLED EMARGENCY RESERVOIR SAFETY PINS L1 FOR GIRT BAR LUBE REMOVED SAFE
- [SDR CALA2026012613279](https://openairdocs.org/sdr/CALA2026012613279), Jan 26, 2026: GIRT BAR. LACK OF LUBE. EMERGENCY POWER RESERVOIR CHECK PROCEDURE - INSTALLED SAFE DOOR PINS FOR DOOR SLIDE. INSTALLED EMARGENCY RESERVOIR SAFETY PINS L4 FOR GIRT BAR LUBE REMOVED SAFE
- [SDR CALA2026012613252](https://openairdocs.org/sdr/CALA2026012613252), Jan 26, 2026: OIL SYSTEM. OVERSERVICED. APU PANDA LIST HAS IDENTIFIED A PERSISTENT EXHAUST ODOR IN CABIN AND RECOMMENDS TROUBLESHOOTING IAW FIM 49-11 FT 895. UPDATE LOG WITH FINGINGS. CARRIED BY ELB P
- [SDR CALA2026012013114](https://openairdocs.org/sdr/CALA2026012013114), Jan 19, 2026: UNKNOWN. ODOR. PERSISTANT EXHAUST ODOR FROM TAXI TO CRUISE ONLY IN COCKPIT, GONE AFTER 25 MINUTES IN FLT. RAN APU, NR 1 ENGINE AND NR 2 ENGINE, ALL SEPARATELY FOR 15 MINUTES. 
- [SDR CALA2026010212582](https://openairdocs.org/sdr/CALA2026010212582), Dec 29, 2025: STRAP. UNSECURE. L2 ENTRY DOOR HAS STRAP HANGING DOWN FROM BOTTOM . RESECURED L2 DOOR EMERGENCY ESCAPE SLIDE STATIC LINE IN THE SLIDE STATIC LINE STORAGE POCKET IAW AMM 25-66-0.
- [SDR CALA2025102010303](https://openairdocs.org/sdr/CALA2025102010303), Oct 20, 2025: LANYARD. OUT OF POSITION. DOOR 2L HAS A PIECE OF THE SLIDE RAFT HANGING OUT AT BOTTOM OF DOOR DOOR 2L HAS LANYARD DROOPING FROM BOTTOM , RE TUCK LANYARD .
- [SDR CALA2025102110337](https://openairdocs.org/sdr/CALA2025102110337), Oct 17, 2025: HOUSING. BROKEN. EXIT PATH LIGHT HANGING IN AISLE AT 33C RESECURED LIGHT AT 33C TO SEAT. COMPLIED WITH DEFERRAL PROCEDURES AND INSTALLED PLACARD MEL 3351G APPROVED. MX REPORT SI
- [SDR CALA2025092409202](https://openairdocs.org/sdr/CALA2025092409202), Sep 21, 2025: GIRT BAR. FOD. FA REPORT THAT DOOR 4L IS DIFFICULT TO ARM AND REQURES GREATER THAN NOR MAL PRESSURE CLEANED DEBRIS AND LUBED GIRT BAR AREAS. OPS CHECKED GOOD.
- [SDR CALA2025082808225](https://openairdocs.org/sdr/CALA2025082808225), Aug 27, 2025: BEZEL. BROKEN. SEAT 27C EMERGENCY LIGHT BEXEL BROKEN OFF REMOVED AND REPLACED BEZEL WITH NEW. FUNCTION CHECK GOOD AT THIS TIME.
- [SDR CALA2025081807879](https://openairdocs.org/sdr/CALA2025081807879), Aug 11, 2025: MAGNET. OUT OF ADJUST. AFTER ARMING DOORS FOR DEPARTURE, FA WORK AND 1L ENTRY LIGHTS WOULD NO LONGER WORK. DR 1L ENTRY LIGHT AND WORK LIGHT EXTINGUISHES WHEN DR 1L IN ARMED POSITION. 
- [SDR CALA2025062605929](https://openairdocs.org/sdr/CALA2025062605929), May 11, 2025: FRAME. CRACKED. FRAME CRACKED AT STA 620 RIGHT HAND SIDE PSU RAIL BRACKET I/B FASTENER HOLE REPAIRED FRAME AT STA 620 RIGHT HAND SIDE PSU BRACKET PER SRM 53-00-07-2R-8. WORK PE
- [SDR CALA2025040303488](https://openairdocs.org/sdr/CALA2025040303488), Apr 2, 2025: INDICATOR. FAULTED. TE FLAP DISAGREE FLAPS AT 20 UPON ENTERING THE COCKPIT THE ALT FLAP SWITCH WAS ON AND CREW ADVISED FLAPS WERE LOCKED OUT. TURNED OFF ALT FLAP SWITCH AND RESET F
- [SDR CALA2024121201481](https://openairdocs.org/sdr/CALA2024121201481), Dec 9, 2024: LIGHT. DISLODGED. EMERGENCY PATH LIGHT AT SEAT 15 C IS DISLODGED PER FLIGHT ATTENDANT. REPLACED EMERGENCY PATH LIGHT AT SEAT 15C REF AMM 33-51-11. OPS CHECK GOOD AT THIS TIME.
- [SDR CALA2024110601038](https://openairdocs.org/sdr/CALA2024110601038), Nov 6, 2024: LAMP. INOPERATIVE. EMERGENCY LIGHTS (USING CONTROL SWITCHES) OPERATIONAL CHECK {MULT-33-3-0001} - 2EA AISLE ILLUMINATION EMERGENCY LIGHTS INOP RELAMPED AISLE LIGHTS AT SEAT ROWS 2
- [SDR CALA2024110601034](https://openairdocs.org/sdr/CALA2024110601034), Nov 4, 2024: LIGHT. UNSECURE. 42C AISLE EMERGENCY EXIT LIGHT LOOSE SECURED EMERGENCY EXIT LIGHT AT 42C REF AMM 33-51-11. LIGHT CHKS OK.
- [SDR CALA2024052801596](https://openairdocs.org/sdr/CALA2024052801596), May 22, 2024: CONTROLLER. FAULTY. N2 OVERSPD ON DEPT MAX N2 103 ON RT ENG PIC UPDATE. #2 ENG AT TAKEOFF. N2 RED 103.2 :05, EGT AMBER 795. :07.9. MAX 796 WITH EPR .05 HIGHER ON RIGHT ENGINE. NO L
- [SDR CALA2024020800363](https://openairdocs.org/sdr/CALA2024020800363), Feb 5, 2024: ANTI-ICE VALVE. INOPERATIVE. LEFT ENG ANTI ICE EICAS L ENG ANTI ICE YELLOW VALVE LIGHT WITH SWIT CH SELECTED ON UPDATE. MARKED AS SDR REPLACED LEFT ENG TAI VALVE (WITHOUT VALVE POSITION IND
- [SDR CALA2024020100273](https://openairdocs.org/sdr/CALA2024020100273), Jan 28, 2024: BLEED VALVE. FAULTY. DISTRIBUTION EICAS MESSAGE L (R) ENG BLEED OFF DISPLAYED. BLEED AIR (01=L ENG, 02=R ENG) OFF LIGHT ON WITH ENGINE RUNNING AND SW ITCH ON. DUCT PRESSURE WAS ZERO
- [SDR CALA2023120803585](https://openairdocs.org/sdr/CALA2023120803585), Dec 5, 2023: BLEED VALVE. LEAKING. R ENG HI STAGE CAUTION UPON APPLIYING TAKEOFF POWER STATUS AND ECS/MSG SHOW NO FAULTS, UPPER EICAS ADVISORY MSG DISPLAYED "R ENG HI STAGE". AUTO EVENT SHOWS - R
- [SDR CALA202306070368](https://openairdocs.org/sdr/CALA202306070368), Jun 7, 2023: HOSE. DAMAGED. ***EMERGENCY DECLARED*** L HYD SYS PRESS CAUTION ILLUMINATED ON FINAL APP. EMERG DECLARE D. FOUND HOLE ON HYDRAULIC HOSE TO DOWN LOCK ACTUATOR. REMOVED AND REPL
- [SDR CALA2023031300727](https://openairdocs.org/sdr/CALA2023031300727), Mar 13, 2023: DRIVE UNIT. FAILED. WX RADAD FAIL INFLT. RESET SYS AND CB...NO HELP. ACP FIM 34-43 FT 809. FOUND WXR ANTTENA FAIL. IN ADDITION FAULT ON WXR RT ELEV AND DRIVE. REPLACED WXR DRIVE UN
- [SDR CALA2022090202242](https://openairdocs.org/sdr/CALA2022090202242), Aug 31, 2022: SKIN. CORRODED. AFT DRAIN MAST AND FUSELAGE AT ATTACH POINT IS CORRODED. MARKED. REPAIRED AFT FUSELAGE SKIN F.S. 1661-1681 S25R-26R IAW AMES REA 47518REA01 REV A AND UAL ECRA 5
- [SDR CALA2022032300761](https://openairdocs.org/sdr/CALA2022032300761), Mar 23, 2022: IDG. FAILED. L GEN OFF IECAS. RAN QRH ONE TIME RESET GEN CAME ONLINE. LATER A LL INST FLASHED CONTINUSELY MEGGERED FEEDERS FROM FIREWALL TO IDG AND THEY CHECKED GOOD. DISCON
- [SDR CALA2022032100743](https://openairdocs.org/sdr/CALA2022032100743), Mar 21, 2022: GENERATOR. FLUCTUATES. LEFT GEN OFF IN FLIGHT AFTER POWER FLUCTUATIONS STEP AV.(E) GOOD @ 1.6 OHMS, 60DEG F. LOCKED FOR FINDINGS. SFOMM WORKING ITEM BPCU SHOWS LEFT GEN FAULTS: "OVER 
- [SDR CALA2022021400374](https://openairdocs.org/sdr/CALA2022021400374), Feb 14, 2022: UNKNOWN. ODOR. FUMES ENTIRE FLIGHT. WENT AWAY AS SOON AS ENGINES SHUTDOWN REPORT FILED BY CAPTAIN FLIGHT CREW AND FLIGHT ATTENDANTS REPORTED UPON ENGINE SHUT DOWN, OIL SMELL I
- [SDR OZIA2021082300369](https://openairdocs.org/sdr/OZIA2021082300369), Mar 24, 2021: HOSE. DAMAGED. ***EMERGENCY DECLARED*** L HYD SYS PRESS CAUTION ILLUMINATED ON FINAL APP. EMERG DECLARE D. FOUND HOLE ON HYDRAULIC HOSE TO DOWN LOCK ACTUATOR. REMOVED AND REPL
- [SDR CALA2021032400468](https://openairdocs.org/sdr/CALA2021032400468), Mar 24, 2021: HOSE. DAMAGED. ***EMERGENCY DECLARED*** L HYD SYS PRESS CAUTION ILLUMINATED ON FINAL APP. EMERG DECLARE D. FOUND HOLE ON HYDRAULIC HOSE TO DOWN LOCK ACTUATOR. REMOVED AND REPL
- [SDR CALA2021032400368](https://openairdocs.org/sdr/CALA2021032400368), Mar 24, 2021: LINE. DAMAGED. EMERGENCY DECLARED, L HYD SYS PRESS CAUTION ILLUMINATED ON FINAL APP. EMERG DECLARE D. FOUND HOLE ON HYDRAULIC HOSE TO DOWN LOCK ACTUATOR. REMOVED AND REPLACED 
- [SDR CALA2021012700096](https://openairdocs.org/sdr/CALA2021012700096), Jan 27, 2021: CONNECTOR. DAMAGED. DURING CLIMB ABOUT 60NM SOUTH OF KORD AT FL260 RT GEN/AC BUS OFFLINE FOLLOWED BY BOTH UTILITY, DID NOT SEE SMOKE OR A ELECTRICAL SMELL. THE CAPT ALSO STATED THA
- [SDR CALA2021012000061](https://openairdocs.org/sdr/CALA2021012000061), Jan 20, 2021: CONTROL SWITCH. INOPERATIVE. DURING FLAP RETRACTION RT AC BUS EICAS FOLLOWED QRC RT GEN RESET BUT RT AC BUS REMAINED ISOLATED CREW COMMENTS, RT AC BUS OFF EICAS ON CLIMB AT 5,000 FT. FIRST 
- [SDR CALA2020033000756](https://openairdocs.org/sdr/CALA2020033000756), Mar 29, 2020: SOLENOID. SHORTED. EICAS MSG. L ENG ANTI-IC E. 5 MIN AFTER SWITCH ACTIVATION REF FIM TASK 30-21-00-815-803 FOUND A/ICE VLV SOLONOID SHORTED. RECCOMEND REPLACING ENGINE A/ICE VLV. 
- [SDR CALA2019092301608](https://openairdocs.org/sdr/CALA2019092301608), Sep 18, 2019: SKIN. PUNCTURED. (SUPPORT EA 5210-01364 REV G SEQ NO.1493) DURING DOOR ADJUSTMENT FOUND INTERNAL WEB PUNCTURED BETWEEN RETRACTABLE DOOR AND ASSIS T HANDLE ON R4 DOOR. REF N/R 00
- [SDR CALA2019092301594](https://openairdocs.org/sdr/CALA2019092301594), Sep 13, 2019: STRINGER. CRACKED. B757-53-3-0559 STRINGER 16R IN MAIN CABIN IS CRACKED AT STA 780+ 24 (96-23) REF ENGINEERING N/R 0073007. REPAIRED CRACK AT MAIN CABIN STA 780+24, S-16R; L=2.0" 
- [SDR CALA2019092301593](https://openairdocs.org/sdr/CALA2019092301593), Sep 13, 2019: DECK PLATE. CORRODED. B757-53-3-0579 LIGHT CORROSION IN MAIN DECK AFT DECK PLATE UPPER SURFACE AT STA 1681 FROM LBL 45 INCH BETWEEN RBL 54 INCH. REF S T-ENG N/R 0073073. REMOVED CORR
- [SDR CALA2019091401536](https://openairdocs.org/sdr/CALA2019091401536), Sep 11, 2019: STRINGER. CRACKED. 5757-53-3-0556 STRINGER 16L IN MAIN CABIN IS CRACKED AT STA 780+ 36 (96-22) REF ST ENGINEERING N/R 0073006 REPAIRED 1.5" CRACK AT STRINGER 16L IN MAIN CABIN STA
- [SDR CALA2019091401535](https://openairdocs.org/sdr/CALA2019091401535), Sep 11, 2019: STRINGER. CRACKED. B757-53-3-0559 STRINGER 16R IN MAIN CABIN IS CRACKED AT STA 780+ 36.(96-24) REF ST ENGINEERING N/R 0073008 REPAIRED 2.0" CRACK AT STRINGER 16R IN MAIN CABIN STA
- [SDR CALA2019091701547](https://openairdocs.org/sdr/CALA2019091701547), Sep 10, 2019: STRUCTURE. DENTED. LT ELEVATOR TRAILING EDGE HAS A NICK. REF ST-ENG N/R 0073310 ACCOMPLISHED A PERMENANT REPAIR ON LT ELEV T/E IAW SRM 51-40-02, 51-60-01, 51-70-04, 55-20-01 AMM 5
- [SDR CALA2019090901506](https://openairdocs.org/sdr/CALA2019090901506), Sep 4, 2019: FLOORBEAM. CORRODED. B757-53-3-0551 (SECONDARY FINDING)MAIN CABIN FWD FLOORBEAM AT A PPROX STA 345 RBL 2-LBL 40 HAS CORROSION,16-126 REF ENGINEERING N/R 0073053 REMOVED CORROSION FR
- [SDR CALA2019083001444](https://openairdocs.org/sdr/CALA2019083001444), Aug 25, 2019: STRINGER. CRACKED. B757-53-3-0556 STRINGER 16L IN MAIN CABIN IS CRACKED AT STA 780+ 24. REF ST-ENG N/R 0073005 REMOVED, FABRICATED AND INSTALLED REPLACEMENT STRINGER AT MAIN C ABI
- [SDR CALA2019083001442](https://openairdocs.org/sdr/CALA2019083001442), Aug 21, 2019: GATE. CORRODED. B757-06-3-036 L2 DOOR LOWER GATE HAS CORROSION.ID NO 30-031 REF. ST. ENGINEERING N/R 0072779 REMOVED CORROSION AT L2 DOOR LWR GATE IAW B757-300 SRM 52-10-02 FIG
- [SDR CALA2019082601433](https://openairdocs.org/sdr/CALA2019082601433), Aug 21, 2019: GATE. CORRODED. B757-06-3-0358 L1 DOOR LOWER GATE HAS CORROSION ID NO 30-017 REF REMOVED CORROSION AT L-1 DOOR LWR GATE IAW SRM 52-10-02 FIG 101 PG 103. FOUND AREA TO BE OUT OF
- [SDR CALA2018041801177](https://openairdocs.org/sdr/CALA2018041801177), Apr 18, 2018: D-RING. OUT OF POSITION. CREW REPORTED THE R1 DOOR IS HARD TO ENGAGE AND DISENGAGE SLIDE ARMING HANDLE. REPOSTIONED D-RING CORD.
- [SDR CALA2018020200441](https://openairdocs.org/sdr/CALA2018020200441), Feb 2, 2018: INDICATOR. LACK OF LUBE. L4 DOOR MOUNTED ESCAPE SYSTEM, AN EVACUATION SLIDE PROBLEM WAS ENCOUNTERED WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS, KNUCKLE KNOCKER DOES NOT POP OUT WHE
- [SDR CALA2018010100001](https://openairdocs.org/sdr/CALA2018010100001), Jan 1, 2018: GCU. FAULTY. L GEN + L BUS TIE FAILURE. ACCOMPLISHED + GEN FAILED SECOND TIME. EMERGENCY DECLARED. REPLACED L GCU PER 24-22-02. RAN BOTH ENGINES OPS OK PER RUN CREW.
- [SDR CALA2017111704111](https://openairdocs.org/sdr/CALA2017111704111), Nov 17, 2017: LIGHT. BROKEN. L2 DOOR SLIDE ARM LIGHT BROKEN. WHOLE MODULE IS MISSING FOR SLIDE INDICATION. REPLACED THE BULBS, OPS CHECKED GOOD

All 72: https://openairdocs.org/aircraft/N57863/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

## Earlier aircraft with N57863

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N57863 before.

- [Cancelled 1978-12-04](https://openairdocs.org/deregistered/N57863-1978-12-04): Piper PA-36-300, S/N 36-7760030. Exported to Libya. Owner: [Food Development Corp](https://openairdocs.org/faa-owner/FOOD%20DEVELOPMENT%20CORP), [Pasco, WA](https://openairdocs.org/faa-place/WA/Pasco)
- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N57863-undated): Hughes 500D, S/N 1113D. N-number assigned, not yet registered

## Related

- Other Boeing 757-33N aircraft: https://openairdocs.org/model/boeing-757-33n/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.