# N57864: 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: 32588
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 11, 2001
- Certificate issued: September 22, 2023
- Expires: September 30, 2030
- Mode S code: A76F68
- 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=57864
- Page: https://openairdocs.org/aircraft/N57864

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/N57864/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 N57864.

## FAA accident and incident reports

None matched to N57864.

## Service difficulty reports (108, 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 CALA2026100920236](https://openairdocs.org/sdr/CALA2026100920236), Oct 7, 2026: SWITCH. FAULTY. RIGHT REVERSER STOW SIG & RT REVERSER ISOLATION VALE STATUS MESSAGES APPEARED AFTER TAKEOFF. PERFORMED PSEU BITE FOUND NO ACTIVE FAULTS, ON LEG 00, FOUND 5 FAUL
- [SDR CALA2026100820212](https://openairdocs.org/sdr/CALA2026100820212), Oct 6, 2026: AUTOBRAKE SYS. FAULTED. NORM ANTISKID EICAS S ANTI SKID SYSTEM FAILURE IN THE NORMAL SYSTEM. PILOTS STATED: TRIED RESET TWO TIMES. MESSAGES CAME BACK BOTH TIMES. AFTER 3RD, RESET MESSA
- [SDR CALA2026100720199](https://openairdocs.org/sdr/CALA2026100720199), Oct 5, 2026: FLIGHT DIR. FAULTED. AUTOPILOT/FLIGHT DIRECTOR INTERCHANGE DATA NO LAND 3 (OR NO AUTO LND) DISPLAYED ON AUTOLAND STATUS ANNUNCIATOR WITH APP MODE NOT SELECTED AND AUTOPILOT OR FLIGH
- [SDR CALA2026082418867](https://openairdocs.org/sdr/CALA2026082418867), Aug 21, 2026: COMPRESSOR. STALLED. REJECTED TAKEOFF SUSPECTED COMPRESSOR STALL ON TAKEOFF RUN ON IN ITIAL POWER UP DEBRIEFED BY FLIGHT CREW AS FOLLOWED SPEED LESS THAN 80 KTS DURING INCIDENT, NO 
- [SDR CALA2026051816346](https://openairdocs.org/sdr/CALA2026051816346), May 14, 2026: LIGHT. INOPERATIVE. RH AFT EMERGENCY LIGHT INOP. DOOR 4 RIGHT EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED AFT RIGHT EMERGENCY LIGHT IN REF TO AMM 33-51-06-962-001-002 OPS C
- [SDR CALA2026043015860](https://openairdocs.org/sdr/CALA2026043015860), Apr 27, 2026: LANYARD. OUT OF POSITION. L4 DOOR WILL NOT ARM, FOUND STATIC LINE FOR SLIDE JAMMED UNDER GIRT BAR. REPOSTIONED THE STATIC IAW AMM 25-66-10 DOOR ARMS AND DISARMS NORMAL.
- [SDR CALA2026042015530](https://openairdocs.org/sdr/CALA2026042015530), Apr 20, 2026: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHT AT DOOR 4 R INOPERATIVE. REPLACED THE LAMPS, NO FIX IAW AMM 33-51-06. REPLACED LAMP L00060 LIGHT AT DOOR R4, OPS CHKD NORMAL IAW AMM33-
- [SDR CALA2026032514827](https://openairdocs.org/sdr/CALA2026032514827), Mar 23, 2026: VALVE. FAULTY. LEFT ENG FUEL VALVE REMAINED ON DURING ENTIRE FLT THIS ISSUE HAS RECENT HISTORY AND MAY NEED PRESSURIZING AND DRAIN VALVE SWITCH OR FFG AASY ALONG WITH NECESSAR
- [SDR CALA2026031714627](https://openairdocs.org/sdr/CALA2026031714627), Mar 11, 2026: PITOT TUBE. FOD. IAS DISAGREE EICAS AT CRUISE. QRH ACCOMPLISHED DETERMINED RIGHT SIDE INCORRECTCREW REPORTS F/O AIRSPEED FLUCTUATES FROM 6-20 KNOTS DIFFERENCE FROM CAPTAIN , STA
- [SDR CALA2026031114507](https://openairdocs.org/sdr/CALA2026031114507), Mar 7, 2026: FITTING. FOD. DOOR R1 WILL NOT ARM. CLEANED GIRT BAR FLOOR ATTACHMENTS REF AMM 52-11-00 OPS CK GOOD.
- [SDR CALA2025121612176](https://openairdocs.org/sdr/CALA2025121612176), Dec 13, 2025: GIRT BAR. OBSTRUCTED. DOOR 1R SLIDE WILL NOT ARM. REMOVED GARBAGE DEBRIS FROM BOTTOM OF DOOR OBSTRUCTING GIRT BAR ENGAGEMENT. NO DEFECT NOTED. OK TO CONTINUE.
- [SDR CALA2025103110788](https://openairdocs.org/sdr/CALA2025103110788), Oct 31, 2025: ELEC CONNECTOR. DISCONNECTED. EMERGENCY LIGHTS OPS TEST WITH THE TEST SWITCH PROCEDURE. ROW 9 FLOOR EMERGENCY LIGHT INOPERATIVE, FOUND CONNECTOR BETWEEN SEAT ROW FLOOR AND SEAT ASSY DISCONNE
- [SDR CALA2025091809032](https://openairdocs.org/sdr/CALA2025091809032), Sep 17, 2025: LIGHT. INOPERATIVE. EMERGENCY PATHWAY LIGHT ASSY'S AT L/H ROW 36 AND 40 DAMAGED INOPERATIVE. REPLACED PATHWAY LIGHT ASSY'S AT ROW 36 AND 40 AMM 33-51-00. OPS CHECKED GOOD.
- [SDR CALA2025091108769](https://openairdocs.org/sdr/CALA2025091108769), Sep 10, 2025: UNKNOWN. ODOR. LAV D AIR VENT MAKING LOUD NOISE AND ODOR, UNABLE TO CONFIRM FAULT ON GROUND, CHECK VENT CONNECTION OPS GOOD. OK TO CONTINUE.
- [SDR CALA2025082908263](https://openairdocs.org/sdr/CALA2025082908263), Aug 28, 2025: BULB. BURNED OUT. EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE. RT FWD OVER WING EMERGENCY LIGHT INOP RELAMPED. OPS CKD OK REF AMM 33-51-06.
- [SDR CALA2025082708185](https://openairdocs.org/sdr/CALA2025082708185), Aug 24, 2025: STRAP. OUT OF POSITION. 4L WILL NOT ARM MULT CYCLES SECURED DOOR ARM LIGHT SOCKET. OPERATION CHECKED OK. SECURED SLIDE STRAP THAT WAS HANGING DOWN AND INTERMITTENTLY MAKING DOOR 4L HAR
- [SDR CALA2025072106744](https://openairdocs.org/sdr/CALA2025072106744), Jul 11, 2025: FRAME. DENTED. FWD CABIN, FRAME AT STA 310.5, AROUND S-4L HAS A DENT.
- [SDR CALA2025070906380](https://openairdocs.org/sdr/CALA2025070906380), Jul 7, 2025: FRAME. DENTED. AFT CARGO COMP, LT SIDE, LOWER FRAME STA 1 400, HAS DENT. ESFR COMPLETED. REPAIRED LOWER FRAME STA 1400 LH SIDE IAW B757-300 EA#757-5360-1 3-A3955 AND EC/RA# 53
- [SDR CALA2025070906377](https://openairdocs.org/sdr/CALA2025070906377), Jul 7, 2025: TEE FITTING. CRACKED. LEFT WING TO BODY FAIRING STRUCTURE FRAME AT BS 1180, BEHIND PANEL, CRACKED. REMOVED AND REPLACED T-FITTING AT LT WING TO BODY FAIRING STRUCTURE FRAME AT BS 118
- [SDR CALA2025070906375](https://openairdocs.org/sdr/CALA2025070906375), Jul 7, 2025: FRAME. DENTED. AFT CARGO COMP, LH SIDE, LOWER FRAME STA 1 520, HAS 2EA DENTS. PERFORMED REPAIR IAW EA#757-5360-13-A3956 AND EC/RA 5360-01983. MAJOR REPAIR.
- [SDR CALA2025070306194](https://openairdocs.org/sdr/CALA2025070306194), Jul 2, 2025: SEAL DEPRESSOR. CRACKED. (SDR) B757-MP-20FW-52-802-00, FWD CARGO DOOR FWD LWR CORNER EDGE SEAL DEPRESSOR DEFORMED/CRACKED. ESFR REPORTING ONLY REMOVED AND REPLACED FWD CARGO DOOR FWD SE
- [SDR CALA2025070906373](https://openairdocs.org/sdr/CALA2025070906373), Jun 26, 2025: FRAME. DENTED. AFT CARGO COMP, LH SIDE, LOWER FRAME STA 1 440, HAS A DENT. REPAIRED AFT CARGO COMP. LH SIDE LOWER FRAME STA 1440 BETWEEN S- 25L AND S-26L PER EA 757-5360-13-A3
- [SDR CALA2025063006061](https://openairdocs.org/sdr/CALA2025063006061), Jun 26, 2025: INTERCOSTAL. CORRODED. AFT CARGO FLOOR L/H FRAME WEB HAS CORROSI ON STA 1500-1520, STR 29L-30. REMOVED AND REPLACED INTERCOSTAL WEB AT AFT CARGO COMP STA 1500- 1520 STR 29L-30 I.A.W. 
- [SDR CALA2025062705993](https://openairdocs.org/sdr/CALA2025062705993), Jun 25, 2025: FRAME. DENTED. AFT CARGO COMP, LH SIDE, LOWER FRAME STA 1 500, HAS A DENT. SDR REPORTING ONLY PERFORMED REPAIR I.A.W. EA#757-5360-13-A3954. RII VERIFIED REPAIR PERFORMED.
- [SDR CALA2025062605915](https://openairdocs.org/sdr/CALA2025062605915), Jun 24, 2025: FLOORBEAM. CORRODED. CABIN FLOORBEAM HAS BARE METAL STA 1661 LBL-57" TO RBL-57". REPAIRED CABIN FLOORBEAM BS 1661 LBL-57 TO RBL 57 IAW EC/RA 5360-01972 THIS IS A CATEGORY A REPAIR N
- [SDR CALA2025071406492](https://openairdocs.org/sdr/CALA2025071406492), Jun 20, 2025: FRAME. DENTED. FWD CABIN, FRAME AT STA 310.5, AROUND S-6 L HAS A DENT ESRF REPORTING PERFORMED REPAIR AT FRAME STA 310.5 AROUND S-4L I.A.W B757-300 U AL EC/RA#:5310-08635 PART
- [SDR CALA2025070906372](https://openairdocs.org/sdr/CALA2025070906372), Jun 20, 2025: FRAME. DENTED. AFT CARGO COMP, RH SIDE, LOWER FRAME STA 1300, HAS A DENT. PERFORMED REPAIR ON RH WIDE FRAME 1300 IAW EA 757-5360-13-A3953 AND EC/RA 5360-01982. MAJOR REPAIR.
- [SDR CALA2025062305815](https://openairdocs.org/sdr/CALA2025062305815), Jun 20, 2025: SUPPORT ANGLE. CORRODED. RIGHT WING, UPPER SURFACE, WTB, UNDER FAIRINGS 192CR AND 192DR, BRACKETS SUPPORTS (8EA) AT AFT/FRON T FACES HAVE CORROSION ESFR REPORTING REMOVED AND REPLACED 5
- [SDR CALA2025062005734](https://openairdocs.org/sdr/CALA2025062005734), Jun 18, 2025: FLOOR SUPPORT. CRACKED. CABIN L/H FLOOR SUPPORT HAS EDGES BROKEN THRU - CRACKS WITH PNEU - DUCT IN CARGO CEILING STA 1630, LBL 4 7". SREPAIRED ON FLOOR BEAM STABILIZATION STRAP AT STA 
- [SDR CALA2025061805679](https://openairdocs.org/sdr/CALA2025061805679), Jun 17, 2025: PANEL. CRACKED. FWD CARGO, RH SIDE, BETWEEN STA. 860 TO 879, AIR FILTER STRUCTURE HAS CRACKS (2 PLACES). ESFR COMPLETED. REPAIRED AIR FILTER STRUCTURE IAW B757-300 SRM 51-70-11
- [SDR CALA2025061805678](https://openairdocs.org/sdr/CALA2025061805678), Jun 17, 2025: FLOORBEAM. CORRODED. AFT CARGO FLOOR R/H FRAME CLIP HAS CORR OSION STA 1520, STR 28R - 29R. ESFR ENTRY FOR THIS REPAIR REMOVED CORROSION AT SHEAR TIE AND FOUND OUT OF LIMITS, CORROS
- [SDR CALA2025061805677](https://openairdocs.org/sdr/CALA2025061805677), Jun 17, 2025: FLOOR SUPPORT. CRACKED. E/E FLOOR BEAM RBL 2 AND STA 480 TO 500 SUPPORT BRACKET WITH CRACK IN THE HOLE OF BOLTS ESFR COMPLETED. REMOVED INTERCOSTAL IAW SRM 51-40-02-0G-0 AND FABRICATE 
- [SDR CALA2025061705624](https://openairdocs.org/sdr/CALA2025061705624), Jun 15, 2025: INTERCOSTAL. CORRODED. AFT CARGO FLOOR R/H FRAME WEB HAS CORROSION FROM STA 1300-1320, STR 27R TO 28R, ON THE O/B SIDE. EVALUATED CORROSION ON FRAME WEB IN AFT CARGO FLOOR BTW STA 130
- [SDR CALA2025061705618](https://openairdocs.org/sdr/CALA2025061705618), Jun 14, 2025: FLOOR SUPPORT. CORRODED. CABIN FLOOR SUPPORT BETWEEN FR365.25 - FR 377.7 / LBL50.0 CORRODED. REMOVED AND REPLACED CABIN FLOOR SUPPORT, FABRICA TED ON TRAVELLER #T25/1818996 IAW SRM 51-4
- [SDR CALA2025061705617](https://openairdocs.org/sdr/CALA2025061705617), Jun 14, 2025: SUPPORT FRAME. CRACKED. R/H W/W CUT OUT FWD SEAL RETAINER SUPPORT FRAME IS CRACKED, ABOUT 6 IN FROM O/B END. REMOVED AND REPLACED R/H W/W CUTOUT SEAT RETAINER SUPPORT FRAME IAW SRM 51-
- [SDR CALA2025061705616](https://openairdocs.org/sdr/CALA2025061705616), Jun 14, 2025: WEB. CORRODED. AFT CARGO FLOOR WEB HAS CORROSION STA 140 0-1420, STR-29R TO 30. REMOVED AND REPLACED INTERCOSTAL/WEB AT AFT CARGO COMP. STA 1400 -1420 STR 29R-30 IAW B757-300 
- [SDR CALA2025061705615](https://openairdocs.org/sdr/CALA2025061705615), Jun 13, 2025: SKIN. CRACKED. LT WING FIXED L/E SKIN UPPER SURFACE HAS 3EA CRACKS UNDER SLAT #3 TO 4. REMOVED, REPAIRED AND REINSTALLED L/H WING FIXED L/E SKIN UNDER S LAT #3 AND 4 IAW SRM 5
- [SDR CALA2025061705614](https://openairdocs.org/sdr/CALA2025061705614), Jun 13, 2025: SCUFF PLATE. CRACKED. L4 DOOR SILL MIDDLE SCUFF PLATE HAS CRAC KS. (WELD CRACKS) ESFR CW W SHAW RECIEVED CAP CNTR LH S. (SCUFF PLATE) LOCATED AND DRILLED IAW B757-300 SRM 51-40-02-0G
- [SDR CALA2025061705613](https://openairdocs.org/sdr/CALA2025061705613), Jun 13, 2025: SKIN. CRACKED. LT WING FIXED L/E SKIN HAS A CRACK, 6'IN LENGTH UNDER SLAT #4. REMOVED REPAIRED AND REINSTALLED L/H WING FIXED L/E SKIN UNDER S LAT #4 IAW B757-300 SRM 51-40-02
- [SDR CALA2025061705612](https://openairdocs.org/sdr/CALA2025061705612), Jun 13, 2025: ANGLE. CORRODED. (SDR) HORIZONTAL STABILIZER REAR SPAR SUPPORT BRACKET THAT ATTAC H JUMPER WIRE HAVE CORROSION. ESFR CW W SHAW REMOVED AND REPLACED BRACKET 183N1341-1 BRACKET ON
- [SDR CALA2025061305544](https://openairdocs.org/sdr/CALA2025061305544), Jun 12, 2025: ATTACH FITTING. CORRODED. AFT CARGO COMPARTMENT LWR DOOR SILL SAFET Y NET ATTACHMENT FITTINGS CORROSION NOTED. REMOVED AND REPLACED AFT CARGO FRAME NET FITTINGS (04E/A) I.A.W. B757-300 S
- [SDR CALA2025061305543](https://openairdocs.org/sdr/CALA2025061305543), Jun 12, 2025: SUPPORT FITTING. CORRODED. AFT CARGO LWR DOOR SILL THRESHOLD FWD SUPPORT FITTING NUTPLATE AREA HAS CORROSION AS MARKED. REMOVED AND REPLACED FITTING P/N 69-4557807 AT BS 1380 I.A.W. SR M 
- [SDR CALA2025061305542](https://openairdocs.org/sdr/CALA2025061305542), Jun 12, 2025: SUPPORT FITTING. CORRODED. AFT CARGO LWR DOOR SILL THRESHOLD 3RD SUPPORT FITTING HAS CORROSION AS MARKED AND AROUND THE NUTPLATES. REMOVED AND REPLACED AFT CARGO DOOR FRAME FITTING P/N 69
- [SDR CALA2025061305541](https://openairdocs.org/sdr/CALA2025061305541), Jun 12, 2025: SHEAR TIE. CORRODED. (SDR)(53-5300-1-0011): AFT CARGO FLOOR R/H FRAME CLIP HAS CORROS ION STA 1520, STR 29R-30. REMOVED SHEAR TIE I.A.W. B757-300 SRM 51-40-02-0G-0 AND FABRICAT ED, 
- [SDR CALA2025061305540](https://openairdocs.org/sdr/CALA2025061305540), Jun 12, 2025: SHEAR TIE. CORRODED. (SDR) (53-5300-1-0011): AFT CARGO FLOOR FRAME CLIP HAS CORROSION STA 1460, STR 28R-30. REMOVED SHEAR TIES 02 EA I.A.W. B757-300 SRM 51-40-02-0G-0 AND FABRICATED
- [SDR CALA2025061305539](https://openairdocs.org/sdr/CALA2025061305539), Jun 11, 2025: MOUNT. CORRODED. (SDR) (19-5305-1-2068): CABIN FLOOR GALLEY MOUNT FITTING HAS COR ROSION STA 1685, CENTER LINE - "1". ESFR COMPLETED. EVALUATED CORROSION ON CENTER GALLEY MOUNT 
- [SDR CALA2025061205506](https://openairdocs.org/sdr/CALA2025061205506), Jun 11, 2025: SUPPORT FITTING. CORRODED. AFT CARGO LWR DOOR SILL THRESHOLD 2ND SUP PORT FITTING HAS CORROSION AS MARKED AND AROUND THE NUTPLATES. REMOVED AND REPLACED FITTING P/N 69-45578U7 IAW B757-30
- [SDR CALA2025061205505](https://openairdocs.org/sdr/CALA2025061205505), Jun 11, 2025: TRANSITION PANEL. CORRODED. AFT CARGO FLOOR R/H TRANSITION PANEL HAS CORROSION FROM STA 1310-1380. CORROSION ON TRASITION PANEL STA 1310-1380 RH SIDE AND FOUND TO BE EXFOLIATED OUT OF LIMI
- [SDR CALA2025061205502](https://openairdocs.org/sdr/CALA2025061205502), Jun 11, 2025: CREASE BEAM. CORRODED. (SDR)(19-5303-1-2082): CABIN FLOOR R/H O/B CREASE BEAM HAS CORRO SION FROM STA 1320-1360, RBL - 64". SFR CW WSHAW REMOVED AND REPLACED CREASE BEAM CHORD P/N 146
- [SDR CALA2025061205500](https://openairdocs.org/sdr/CALA2025061205500), Jun 11, 2025: MOUNT BRACKET. CRACKED. LEFT MLG W/W HYD FILTER MODULE MOUNTING BRACKET HAS A CRACK AS MARKED, AREA ABOVE THE ELECTRIC HYDRAULIC PUMP. REMOVED AND REPLACED BRACKET ON L/H MLG W/W HYD F

All 108: https://openairdocs.org/aircraft/N57864/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 N57864

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N57864 before.

- [Cancelled 1985-02-06](https://openairdocs.org/deregistered/N57864-1985-02-06): Piper PA-36-300, S/N 36-7760031. Exported to Mexico. Owner: [Mid-Continent Aircraft Corp](https://openairdocs.org/faa-owner/MID-CONTINENT%20AIRCRAFT%20CORP), [Hayti, MO](https://openairdocs.org/faa-place/MO/Hayti)

## 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.