# N57862: 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: 32586
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 5, 2001
- Certificate issued: December 8, 2023
- Expires: December 31, 2030
- Mode S code: A76F66
- 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=57862
- Page: https://openairdocs.org/aircraft/N57862

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/N57862/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 N57862.

## FAA accident and incident reports

None matched to N57862.

## Service difficulty reports (70, 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 CALA2026091019359](https://openairdocs.org/sdr/CALA2026091019359), Sep 9, 2026: ACCESS DOOR. MISSING. INSTALLED NEW STRUT ACCESS DOOR ASSEMBLY REF AMM 54-53-01
- [SDR CALA2026070617568](https://openairdocs.org/sdr/CALA2026070617568), Jul 2, 2026: WIRE. PULLED. EMERGENCY LIGHTS OPS TEST WITH THE TEST SWITCH, ROW 22C RED EMER LIGHT INOPERATIVE. WIRING PULLED OUT OF ELECTRICAL CONNECTOR. REPLACED SEAT 22 LIGHT ASSY AND H
- [SDR CALA2026063017478](https://openairdocs.org/sdr/CALA2026063017478), Jun 28, 2026: HUB CAP. MISSING. DURING ETOPS CHECKS THE MECHANICS NOTICED NR 2 WHEEL WAS MISSING THE HUB CAP. FOUND A PIECE OF HUB CAP ATTACHED AT THE 6 O'CLOCK POSITION SUGGESTING THE HUB CAP
- [SDR CALA2026040315062](https://openairdocs.org/sdr/CALA2026040315062), Apr 3, 2026: GIRT BAR. FOD. R1 DOOR WILL NOT ARM, AND NOW WILL NOT DISARM COMPLETELY. FOUND DEBRIS INLINE WITH GIRT BAR ATTACHMENT POINTS. CLEARED THE SAME. OPERATED DOOR THRU ARMED/ DISAR
- [SDR CALA2025110610937](https://openairdocs.org/sdr/CALA2025110610937), Nov 5, 2025: LIGHT. NO DISCREPANCY. OVERHEAD LIGHTING AT L1 DOOR FOUND INOPERATIVE ON ARRIVAL AT GATE, PROBLEM WAS RESOLVED. OPERATED FWD GALLEY LIGHTS WITH SLIDE ARMED & DISARMED, AS WELL AS WITH
- [SDR CALA2025102810673](https://openairdocs.org/sdr/CALA2025102810673), Oct 20, 2025: SKIN. CRACKED. ACCOMPLISH INITIAL INSPECTION OF RT WING UPPER SKIN FASTENER HOLES #1-18 IAW PART 2C OF THE LATEST REVISION OF EC/RA 5720-03571 ON OR BEFORE THE AIRCRAFT REACHE
- [SDR CALA2025102810671](https://openairdocs.org/sdr/CALA2025102810671), Oct 17, 2025: SKIN. CORRODED. REPAIR ON THE FUSELAGE SKIN BETWEEN STA 1540 - 1560 AND STR 27R - 29R AT LAVATORY SERVICE DOOR CUTOUT PER THE LATEST REVISION OF EC/RA 5330-07636
- [SDR CALA2025092209094](https://openairdocs.org/sdr/CALA2025092209094), Sep 18, 2025: OIL SYSTEM. LEAKING. WHILE RUNNING THE APU BLEED THERE IS A STRONG ODOR IN THE CABIN. TS APU FOR SOUCE OF ODOR/OIL LEAKS. ACCOMPLISHED AMM 21-00-01-002-001 REMOVAL OF OIL CONTAMINAT
- [SDR CALA2025091909050](https://openairdocs.org/sdr/CALA2025091909050), Sep 18, 2025: APU. ODOR. ACFT SMELLS OF VAPOR & BURNING OIL WITH APU & ENG BLEED. REPLACED RECIRCULATION FILTERS IAW 21-25-02/401. RAN APU AND BOTH ENGINES ONE AT A TIME. THE ODOR WAS O
- [SDR CALA2025091909047](https://openairdocs.org/sdr/CALA2025091909047), Sep 15, 2025: COOLING FAN. LEAKING. CREW REPORTS AUTO SHUTDOWN OF APU AFTER CREW NOTICED & WAS INFORMED OF SMOKE & ODOR COMING FROM VENTILATION SYS. CREW SHUTDOWN PACS & APU BLEED FOLLOWED BY APU 
- [SDR CALA2025091508946](https://openairdocs.org/sdr/CALA2025091508946), Sep 15, 2025: UNKNOWN. ODOR. CREW REPORTS HEAVY ELECTRICAL BURNING SMELL IN FLIGHT DECK AND THROUGH OUT THE CABIN WITH VISIBLE GREY SMOKE THROUGHOUT AIRCRAFT. LOCKING UNLOCKED WAS NOT AN EL
- [SDR CALA2025091108793](https://openairdocs.org/sdr/CALA2025091108793), Sep 8, 2025: NONE. NONE. BIRD STRIKE ON RADOM. PERFORMED BIRD STRIKE INSPECTION. AND INSPECTIONS, INCLUDING RADOME, NO DELAMINATION OR DAMAGE FOUND.OK TO CONTINUE.REF AMM TASK 05-51-18-
- [SDR CALA2025090508525](https://openairdocs.org/sdr/CALA2025090508525), Sep 1, 2025: ACCESS PANEL. MISSING. ACCESS PANEL 443JL IS MISSING FROM THE INBD SIDE OF NR 2 PYLON. INSTALLED ACCESS PANEL 443JL IAW MM 54-53-01. SECURED.
- [SDR CALA2025082508097](https://openairdocs.org/sdr/CALA2025082508097), Aug 22, 2025: WARNING MESSAGE. FALSE ACTIVATION. R ENG OVHT AT FL360. WENT AWAY AFTER R EPR REDUCED BY .02. R OVH T DET STATUS ALSO. PER CREW ALSO GOT STRUT OVERHEAT EICAS MOMENTARILY ACP FIM 26-11 TASK 802 EN
- [SDR CALA2025081907936](https://openairdocs.org/sdr/CALA2025081907936), Aug 17, 2025: PCB. FAULTED. R OVHT DET STATUS MSG FOLLOWED BY R ENG OVHT CAUTION. COMPLIED W ITH QRH. WENT AWAY WITH IDLE DEBRIEFED FLIGHT CREW, ADVANCED THROTTLES AT LANDING, MSG DID NOT 
- [SDR CALA2025081507823](https://openairdocs.org/sdr/CALA2025081507823), Aug 15, 2025: COVER. LOOSE. DOOR 2L SLIDE COVER LOOSE ADJUSTED 2L DOOR BUSSLE, INSTALLATION AND RIGGING NOT AFFECTED
- [SDR CALA2025080507292](https://openairdocs.org/sdr/CALA2025080507292), Aug 4, 2025: UNKNOWN. UNKNOWN. POSSIBLE BIRD STRIKE OUT OF 10K, SOMTHING DID MAKE CONTACT WITH ACFT. ODOR DETECTED INSPECTED ACFT FOUND NO EVIDENCE OF A BIRDSTRIKE OR IMPACT OF SPECIFIED AREA
- [SDR CALA2025042804285](https://openairdocs.org/sdr/CALA2025042804285), Apr 26, 2025: 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 SAF
- [SDR CALA2025042304168](https://openairdocs.org/sdr/CALA2025042304168), Apr 20, 2025: PSEU. FAULTED. GEAR DISAGREE EICAS ON TAKEOFF FROM DCA PER CREW GEAR DISAGREE EICAS ONTAKEOFF. RIGHT NOSE GEAR LIGHT ILLUMINATED W/GEAR IN UP/OFF POSITION. CREW DEBRIEF ON ARR
- [SDR CALA2025030302546](https://openairdocs.org/sdr/CALA2025030302546), Feb 28, 2025: WARNING MESSAGE. FALSE ACTIVATION. R FWD ENT DOOR EICAS C THE RIGHT FORWARD ENTRY DOOR IS NOT LATCHED MOMENTARY CAUTION MSG AT FL330. PRESSURIZATION NO RMAL. DOOR HAN DLE MOVING IN TURBULENCE DEB
- [SDR CALA2025012301983](https://openairdocs.org/sdr/CALA2025012301983), Jan 22, 2025: UNKNOWN. ODOR. UNNATURAL SMELL IN FLIGH T DECK DURING ALL PHASES OF FLIGHT. FAS ADVISE NO ODOR IN CABIN SUBMITTED FORM TO TOMC FOR SMELL IN FD. REF FIM TASK 21-00-01/301 FOUND
- [SDR CALA2024121701545](https://openairdocs.org/sdr/CALA2024121701545), Dec 16, 2024: IDG. FAULTED. R GEN OFF EICASTALKED WITH CREW UPON ARRIVAL. THEY SAID THEY LOST AFT GALLEY POWER AND AFT LAV STOPPED WORKING. THEY THEN GOT THE R GEN CONT OFF LIGHT, THEN THE
- [SDR CALA2024062100058](https://openairdocs.org/sdr/CALA2024062100058), Jun 21, 2024: SEAL. DAMAGED. DOOR 1R EXCESSIVELY LOUD SQUEELATTACHED PHOTO'S TAKEN ON RIGHT SIDE OF AIRPLANE ABOVE DOOR 1 RIGHT. CREW DEBRIEF: F/O THOUGHT HE HEARD NOISE COMING FROM FWD LOW
- [SDR CALA2024052301569](https://openairdocs.org/sdr/CALA2024052301569), May 23, 2024: DOOR. CORRODED. APU DOOR INLET SURROUND STRUCTURE HAS CORROSION AT I/B FWD CORNE R, O/B FWD EXTENDING 10" I/B AND AFT O/B,
- [SDR CALA2024052301568](https://openairdocs.org/sdr/CALA2024052301568), May 22, 2024: STRAP. CRACKED. FRAME STRAP ON BOTTOM OF COCKPIT FLOOR BEAMS BETWEEN F.S. 365.2 5 AND 377.7 AT LBL 25 (LEFT TUNNEL OF MEC) IS CRACKED
- [SDR CALA2024052001531](https://openairdocs.org/sdr/CALA2024052001531), May 20, 2024: CHANNEL. CRACKED. REF AMES NR 170224-0200-0211 GEN ITEM 53-5310-1-2626 CRACK FOUND THROUGH FASTENER ON FRAME IN UPPER CABIN R/H SIDE ST A 1580 FOR OVER HEAD BIN ATTACH BRACKET AB
- [SDR CALA2024051301462](https://openairdocs.org/sdr/CALA2024051301462), May 11, 2024: FLOOR SUPPORT. CRACKED. CABIN FLOOR SUPPORT CRACKED IN MULTIPLE SPOTS FROM BS1420-1440. REMOVED AND REPLACED FLOOR SUPPORT AT BS 1420-1440 BL0 IAW BOEIN G 757 SRM 51-40-02 PAR 4, SEE B
- [SDR CALA2024051301461](https://openairdocs.org/sdr/CALA2024051301461), May 11, 2024: FLOOR SUPPORT. CRACKED. CABIN FLOOR SUPPORT CRACKED IN MULTIPLE SPOTS FROM BS1320-1340 AT BL0 IN CEILING AREA OF ALC MARKED IN RED. REMOVED AND REPLACED CABIN FLOOR SUPPORT AT BS 1320-
- [SDR CALA2024051301460](https://openairdocs.org/sdr/CALA2024051301460), May 11, 2024: FLOOR SUPPORT. CRACKED. CABIN FLOOR SUPPORT CRACKED IN MULTIPLE SPOTS FROM BS1260-1300 AT BL0 IN CEILING AREA OF ALC MARKED IN RED. REMOVED AND REPLACED CABIN FLOOR SUPPORT AT BS 1260-
- [SDR CALA2024051301459](https://openairdocs.org/sdr/CALA2024051301459), May 11, 2024: FLOOR SUPPORT. CRACKED. CABIN FLOOR SUPPORT CRACKED IN MULTIPLE SPOTS FROM BS1500-1520 AT BL0 IN CEILING AREA OF ALC MARKED IN RED. REMOVED AND REPLACED FLOOR SUPPORT IAW BOEING 757 SR
- [SDR CALA2024051001423](https://openairdocs.org/sdr/CALA2024051001423), May 9, 2024: BRACKET. CRACKED. REF AMES NR 170224-0100-00175 GEN ITEM EA 5100-02129 REV H OP 00 1 DURING AGING INSPECTION, FOUND L-BRACKET CRACKED FOR FUSELAGE FA IRING SUPPORT CRACKED, JUST 
- [SDR CALA2024051001419](https://openairdocs.org/sdr/CALA2024051001419), May 9, 2024: FLOOR SUPPORT. CRACKED. REF AMES NR 170224-0100-0149 GEN ITEM 53-5310-1-2606 FLC FS676 LBL24 SLOPE WALL FLOOR SUPPORT CRACKED. REPAIRED SLOPE WALL FLOOR SUPPORT FS676 LBL24 IN FLC IAW 
- [SDR CALA2024050701366](https://openairdocs.org/sdr/CALA2024050701366), May 6, 2024: FLOOR PANEL. CRACKED. REF AMES NR 170224-0100-0069 GEN ITEM EA 5100-02244 REV G OP 003 ALC FLOOR PANEL 153AF CRACKED
- [SDR CALA2024050701365](https://openairdocs.org/sdr/CALA2024050701365), May 6, 2024: PANEL. CRACKED. REF AMES NR 170224-0100-0068 GEN ITEM EA 5100-02244 REV G OP 003 ALC PANEL 151AF HAS A CRACK
- [SDR CALA2024051001418](https://openairdocs.org/sdr/CALA2024051001418), May 3, 2024: FLOOR SUPPORT. CRACKED. GENERATING ITEM B757-20-3-0065: FRAME STRAP ON BOTTOM OF COCKPIT FLOOR BEAMS (LEFT TUNNEL OF MEC) BETWEEN F.S. 365.25 AND 377.7 AT BL 0 IS CRACKED (MARKED WITH 
- [SDR CALA2024050701358](https://openairdocs.org/sdr/CALA2024050701358), May 3, 2024: SUPPORT RIB. CRACKED. FOUND CRACKED SUPPORT RIB AT STATION 365.25, JUST ABOVE WIRING B UNDLE #91177 REF AMES NR 170224-0100-0064
- [SDR CALA2024032800901](https://openairdocs.org/sdr/CALA2024032800901), Mar 26, 2024: FMC. FAILED. RIGHT FMC FAIL LIGHT IS ON LP 7452038 MEL 3461AK WAS CLEARED. MUST REPLACE R FMC REF AMM34-61-01-024-001-002 UNLOCKED TO CLEAR WITH R FMC R&R FMC IN SFO WIT
- [SDR CALA2023012000164](https://openairdocs.org/sdr/CALA2023012000164), Jan 19, 2023: RESERVOIR. LOW. LT HYD QTY EICAS C, LEFT HYDRAULIC RESERVOIR QUANTITY IS LOW, HYD AUTO EVEN T RAN CHKLIST IAW QRH. AFT ER SECURING BOTH L PUMPS RUDDER RATIO DISPLAYED. QTY SLOW
- [SDR CALA2021102901999](https://openairdocs.org/sdr/CALA2021102901999), Oct 28, 2021: FUEL SYS. NONE. ABNORMAL FUEL INDICATION S CREW INFO: FUEL CONFIG LIGHT DISPLAYED. CROSS FEED CLOSED, NO DRIP STICKED FUEL TANKS AND THEY COINSIDE WITH COCKPIT FUEL IN CENTER T
- [SDR CALA2021062500955](https://openairdocs.org/sdr/CALA2021062500955), Jun 24, 2021: SKIN. DENTED. (B757-06-3-0253) EXTERIOR FUSELAGE L/H SIDE, 3EACH DENTS ON THE FUSELAGE SKIN BTWN BS 740 AND BS 760 AND BTWN STRINGERS S-15L AN D S-17L. REF HAECO GSO NRC #928
- [SDR CALA2021062500954](https://openairdocs.org/sdr/CALA2021062500954), Jun 24, 2021: SKIN. DAMAGED. B757-06-3-0222, ZONE 100, LOWER HALF FUSELAGE, STA 1605, AFT OF WASTE DRAIN DOOR, SKIN IS DENTED FROM INSIDE HAECO/GSO LOG 9286586, V899290 2EA DENTS AT STA 160
- [SDR CALA2021042600549](https://openairdocs.org/sdr/CALA2021042600549), Apr 26, 2021: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT BATTERY PACK M11490 INOP REPLACED EMERGNCY LIGHT BATTERY PACK M11490 AS PER AMM 33-51-07-902-005-002. OPS CHECKS GOOD.
- [SDR CALA2021042600547](https://openairdocs.org/sdr/CALA2021042600547), Apr 26, 2021: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT BATTERY PACK M11489 INOP REPLACED EMERGNCY LIGHT BATTERY PACK M11489 AS PER AMM 33-51-07-902-005-002. OPS CHECKS GOOD.
- [SDR CALA2019100501698](https://openairdocs.org/sdr/CALA2019100501698), Oct 2, 2019: TRANSMITTER. MALFUNCTIONED. FLAP ASYMMETRY EICAS INDICATION AFTER FLAP RETRACTION ON TAKEOFF. RH FLAP NEEDLE STUCK WITH NO FLIGHT CHARACTERISTICS NOTICED. FLAPS INDICATION DID RETURN TO NO
- [SDR CALA2019072401241](https://openairdocs.org/sdr/CALA2019072401241), Jul 22, 2019: WIRE. OPEN. FOUND FOWARD EXIT SIGN AT DOOR 3 RIGHT INOP REMOVED CEILING PANEL ABOVE DOOR 3 RIGHT FOR TROUBLESHOOTING AND REMOVED DADO PANEL JUST AFT OF DOOR 3 RIGHT RANG OU
- [SDR CALA2019051300755](https://openairdocs.org/sdr/CALA2019051300755), May 12, 2019: SKIN. DAMAGED. SUBSTASK:B757-53-3-0569: MAIN CABIN, R4 DOOR, ABOVE THE LOWER GATE HAS CUT MARKED SAA-072/61 OFF AIRCRAFT. REF ON REF N/R 0053913. ACCOMPLISHED REPAIR AT MAIN C
- [SDR CALA2019051300760](https://openairdocs.org/sdr/CALA2019051300760), May 8, 2019: GATE. CORRODED. REMOVED CORROSION AT R2 DOOR LWR GATE FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE R-2 DOOR LWR GATE ASSY P/N 19-5211-3-0 709 IAW SRM 52-10-02 FIG 101 AD
- [SDR CALA2019050700698](https://openairdocs.org/sdr/CALA2019050700698), May 4, 2019: SUPPORT FITTING. CORRODED. SUBTASK ZONE 200 OPEN, LAV A SUPPORT FITTING AT STA 340 B/L 0 IS CORRODED. REF N/R 0053993 REMOVED AND REPLACED NEW FITTING P/N 65N57839U2, BATCH 000347007 6, P
- [SDR CALA2019050700697](https://openairdocs.org/sdr/CALA2019050700697), May 4, 2019: FITTING. CORRODED. SECONDARY FINDING ZONE 200 OPEN, FWD GALLEY FLOOR FITTING AT STA 365 IS CORRODED AND PITTED. REF N/R 0053994 REMOVED AND REPLACED NEW FITTING P/N 415N4007-11, B
- [SDR CALA2019050700696](https://openairdocs.org/sdr/CALA2019050700696), May 4, 2019: CROSSBEAM. CORRODED. SECONDARY FINDING ZONE 200 OPEN, FLOOR CROSSBEAM AT STA 395 HAS SEVERAL AREAS OF CORROSION, 22-87. REF NR 0053995. REMOVED DAMAGED CROSSBEAM IAW SRM 51-40-02, F

All 70: https://openairdocs.org/aircraft/N57862/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 N57862

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N57862 before.

- [Cancelled 1975-07-22](https://openairdocs.org/deregistered/N57862-1975-07-22): Boeing E75N1, S/N 75-098. Owner: [Lazy 8 Flying Service Inc](https://openairdocs.org/faa-owner/LAZY%208%20FLYING%20SERVICE%20INC), [Scottsdale, AZ](https://openairdocs.org/faa-place/AZ/Scottsdale)

## 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

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