# N57870: 2003 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: 33525
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 23, 2003
- Certificate issued: October 19, 2023
- Expires: October 31, 2030
- Mode S code: A76F87
- 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=57870
- Page: https://openairdocs.org/aircraft/N57870

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/N57870/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 N57870.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20110917023989I](https://openairdocs.org/incident/20110917023989I), Sep 17, 2011: Boeing 757-33N (N57870), Cleveland, OH, No damage. The aircraft was taxiing for takeoff from atlantic aviation for a charter flight. The flight was instructed to taxi via lima two to lima to runway 6 right. The…

## Service difficulty reports (74, 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 CALA2026030414311](https://openairdocs.org/sdr/CALA2026030414311), Mar 4, 2026: STATIC LINE. UNSECURE. L4 DOOR WILL NOT ARM. FOUND STATIC LINE OUT OF POCKET REPACKED STATIC LINE IAW AMM 25-66-10 DOOR ARMS AND DISARMS NORMAL
- [SDR CALA2026022514062](https://openairdocs.org/sdr/CALA2026022514062), Feb 22, 2026: ADIRU. FAULTED. IN CLIMB AT FL290, AUTOPILOT DISENGAGED. NO MODES WOULD RE ENGAGE ACCOMPLISHED MCDP FCC TEST, TEST 30 & TEST 40. ALL TEST PASS. MCDP FLT FAULT WITH ADIRU LT. RE
- [SDR CALA2025110410871](https://openairdocs.org/sdr/CALA2025110410871), Nov 3, 2025: NONE. NONE. INSTALLED EMERGENCY POWER RESERVOIR SAFETY PIN AND DOOR SLIDE SAFETY PIN ON DOOR R4 DUE TO MX. REMOVED EMERGENCY POWER RESEVOIR SAFETY PIN AND DOOR SLIDE SAFETY
- [SDR CALA2025101710211](https://openairdocs.org/sdr/CALA2025101710211), Oct 17, 2025: OVEN. ODOR. FRONT GALLEY OVEN 204 TURND OFF DUE TO SMOKE AND ODOR. REPLACED GALLEY OVEN WITH SERVICEABLE ONE IAW AMM 25-34-00. OPS CHECKED GOOD, NO SMOKE PRESENT.
- [SDR CALA2025082007953](https://openairdocs.org/sdr/CALA2025082007953), Aug 16, 2025: GAUGE. OBSTRUCTED. 2L DOOR RAFT/SLIDE MOVE INSTRUCTIONS FALLING AND BEGINING TO BLOCK SLIDE, PRESSURE GAUGE REMOVED SLIDE COVER ON 2L DOOR REF AMM 25-66-01-014-006. INSTRUCTIONS P
- [SDR CALA2025041503843](https://openairdocs.org/sdr/CALA2025041503843), Apr 12, 2025: COVER. LOOSE. SLIDE COVER HAS COME LOOSE AND IS NOT FLUSH WITH DOOR 02L INSTALLED DOOR 2L ESCAPE SLIDE COVER. REF. AMM 25-66-01-404-044 VERIFIED CORRECT INSTALL REF. AMM 25-6
- [SDR CALA2025032003043](https://openairdocs.org/sdr/CALA2025032003043), Mar 18, 2025: PRESSURE SWITCH. FAULTED. CENTER RIGHT PUMP PRESS LIGHT ILLUMINATED AT FL230 AND SAME EIC AS MESSAGE PERFORMED FIM 28-22 TASK 804. BITE UFI FAULT CODE "A" FLASHING (UNDER FREQUENTCY). RE
- [SDR CALA2025022500438](https://openairdocs.org/sdr/CALA2025022500438), Feb 23, 2025: WARNING LIGHT. INOPERATIVE. (EA-5210-03219-004) R2 DOOR GIRT BAR WARNING LIGHT INOP REMOVED AND REPLACED NO. 2 PASS DOOR GIRT BAR AND LIGHT I.A.W. B757 SSM 25-66-01, WDM 25-66-11 AND PERFO
- [SDR CALA2025022500437](https://openairdocs.org/sdr/CALA2025022500437), Feb 23, 2025: WARNING LIGHT. ILLUMINATED. R4 DOOR GIRT BAR WARNING LIGHT INOP REMOVED AND REPLACED NO#4 PASS DR RIGHT GIRT BAR ANN LIGHT IAW B757 SRM 25-66-01, WDM 25-66-11 AND PERFORMED OP TEST I.AW B7
- [SDR CALA2025021400365](https://openairdocs.org/sdr/CALA2025021400365), Feb 13, 2025: FLOOR SUPPORT. CRACKED. (SUPPORT TASK) AFT CARGO FLOOR STRINGER STA 1180 +100 TO 1180+120 RBL 5 IS CRACKED/PUNCTURE. TRANSCRIBED FROM HAECO GSO N R 9286305 REMOVED CUT OUT DAMAGE AREAS
- [SDR CALA2025021100339](https://openairdocs.org/sdr/CALA2025021100339), Feb 10, 2025: DOOR SILL. CORRODED. (B757-53-3-0526) AFT CARGO DOOR (CUTOUT) LOWER SILL HAS MULTIPLE AREAS OF CORROSION. DOT:T772 TRANSCRIBED FROM HAECO GSO NR 9286332
- [SDR CALA2024112201253](https://openairdocs.org/sdr/CALA2024112201253), Nov 20, 2024: SWITCH. FAULTED. L FWD ENT DOOR CAME ON DURING CRUISE ALL CABIN PRESSURE INDICAT IONS NORMAL CLEANED 1 FWD ENT DOOR SWITCH , OP CK OK .
- [SDR CALA2024111501153](https://openairdocs.org/sdr/CALA2024111501153), Nov 13, 2024: HANDLE. BROKEN. LEFT OFFWING ESCAPE SLIDE ACTUTOR RELEASE TRIGGER (HANDLE-LOCK) TIP BROKE OFF. (P/N: 416N2424-17) REF. AIPC: 25-65-05-01. REMOVED DAMAGED HANDLE. DRILLED AND IN
- [SDR CALA2024111501152](https://openairdocs.org/sdr/CALA2024111501152), Nov 13, 2024: BEARING. SEIZED. OVERWING SLIDE LIGHT ILLUMINATED FOUND LT OVERWING SLIDE ACCESS DOOR OPEN ON ARRIVAL ,HANDLE HAD LIFTED,ATTEMPTED TO LOCK DOOR FOUND HANDLE JAMMED AND HARD TO O
- [SDR CALA2024111401136](https://openairdocs.org/sdr/CALA2024111401136), Nov 13, 2024: ACTUATOR. DAMAGED. LEFT OFF WING ESCAPE SLIDE ACTUATOR VENT RED HANDLE 90 DEGREE STOP BUSHING(WASHER) BROKE IN HALF. UNABLE TO IDENTIFY PART. REMOVED AND REPLACED LEFT HAND OFF WI
- [SDR CALA2024111401135](https://openairdocs.org/sdr/CALA2024111401135), Nov 11, 2024: PIN. UNKNOWN. PIN AND PIN ASSEMBLY PARTIALLY REMOVED ON LATCH SYSTEM FOR LEFT OVERWING SLIDE. 40 AND 45 FULLY INSTALLED PIN AND PIN ASSEMBLY ON LATCH SYSTEM. REF 757 AMM 25-6
- [SDR CALA2024110701064](https://openairdocs.org/sdr/CALA2024110701064), Nov 5, 2024: NONE. NONE. R OFF WING ESPACE SYSTEM DISARM REF AMM 25-65-00-002-001. REARMED R OFF WING ESPACE SYSTEM REF AMM 25-65-00-402-018. PENDING INSPECTION BUY BACK ACCOMPLISHED RI
- [SDR CALA2024110701058](https://openairdocs.org/sdr/CALA2024110701058), Nov 5, 2024: ESCAPE HATCH. UNKNOWN. REMOVED FWD R OVERWING EMERGENCY EXIT HATCH REF AMM 52-22-01-902-001. REINSTALLED FWD R OVERWING EMERGENCY EXIT HATCH REF AMM 52-22-01-402-074. PENDING INSPECTI
- [SDR CALA2024062601894](https://openairdocs.org/sdr/CALA2024062601894), Jun 17, 2024: LENS. BROKEN. BROKEN EMERGENCY PATHWAY LIGHT AT SEAT 11C. REPLACED EMERGENCY LIGHT LENS COVER AT SEAT 11C. NO WIRES WERE DISCONNECTED.
- [SDR CALA2024062601893](https://openairdocs.org/sdr/CALA2024062601893), Jun 17, 2024: LENS. DETACHED. BROKEN EMERGENCY PATHWAY LIGHT AT SEAT 26C. REPLACED SEAT 26C EMERGENCY PATHWAY LIGHT COVER. NO WIRES WERE DISCONNECTED. SDR REPORTED. LIGHT LENS REPLACED.
- [SDR CALA2023083002667](https://openairdocs.org/sdr/CALA2023083002667), Aug 19, 2023: UNKNOWN. INOPERATIVE. AUTOPILOT EICAS MSG WITH L AP ENGAGED. NO CONTROL ISSUES. ENGAGE D R AP AND NO MSG. FL235 M.75 MCDP FLIGHT FAULTS SHOWS "A/P CTN STAB L/FCC L". MCDP TEST 65 T/S
- [SDR CALA2023061901942](https://openairdocs.org/sdr/CALA2023061901942), Jun 15, 2023: UNKNOWN. UNKNOWN. AIRSPEED DISAGREE AND UNRELIABLE CAPT SIDE. L R EEC ALSO POPULAT ED. EEC OFF IAW QRC. VERBALLY DEBRIEFED CREW. CREW ENCOUNTERED ICING CONDITIONS WHICH 34-26 TAS
- [SDR CALA2022021400367](https://openairdocs.org/sdr/CALA2022021400367), Feb 11, 2022: FRAME. CRACKED. (SUPPORT TASK) CRACK FOUND ON LOWER INBD HOLE FWD LAYER AT STA 1 640 L/H FRAME ON THE INTERCOSTAL TEE CLIP. TRANSCRIBED FROM HAEC O GSO TASK CARD 9281318 RESULT
- [SDR CALA2022020800342](https://openairdocs.org/sdr/CALA2022020800342), Feb 7, 2022: INTERCOSTAL. CRACKED. SUPPORT TASK MAIN CABIN FLOOR STA 345 TO STA 365 INTERCOSTAL WEB CRACKED ON INSTALL, TRANSCRIBED FROM HAECO GSO NON ROUTINE 9281 700. REMOVED DAMAGED INTERCOSTA
- [SDR CALA2022020700332](https://openairdocs.org/sdr/CALA2022020700332), Feb 6, 2022: INTERCOSTAL. CRACKED. SUPPORT TASK STA 1640 STR 10L WEB CRACKED AT AFT CTR HOLE ON INS TALL. WEB PN 146N8738-15, TRANSCRIBED FROM HAECO GSO NON ROUTINE 9281722 FABRICATED INTERCOSTAL
- [SDR CALA2022020700328](https://openairdocs.org/sdr/CALA2022020700328), Feb 5, 2022: BEAM. CORRODED. B757-53-3-0479 FLOOR BEAM 365.25 UPPER T-CAP BETWEEN RBL 24.75 T O RBL 45.5 SURFACE CORROSION, TRANSCRIBED FROM HAECO GSO NON ROU TINE 9281118 ACCOMPLISHE T-CAP
- [SDR CALA2022013100276](https://openairdocs.org/sdr/CALA2022013100276), Jan 31, 2022: FLOORBEAM. CORRODED. (SUPPORT TASK) FLOOR BEAM STA 345 UPPER T CAP BETWEEN LBL G-24 H AS SURFACE CORROSION
- [SDR CALA2022013100265](https://openairdocs.org/sdr/CALA2022013100265), Jan 29, 2022: SEAT TRACK. CORRODED. SUPPORT TASK SEAT TRACK SUPPORT AT STA 365, RBL 45.25 HAS CORROS ION, TRANSCRIBED FROM HAECO GSO NR 9281388 BLENDED AND REMOVED DAMAGE FROM SEAT TRACK SUPPORT A
- [SDR CALA2022013100256](https://openairdocs.org/sdr/CALA2022013100256), Jan 28, 2022: FLOOR SUPPORT. CORRODED. (B757-53-3-0479) INTERCOSTAL FLOOR BOARD SUPPORT BL 0 AT STA 345 SURFACE CORROSION, TRANSCRIBED FROM HAECO GSO NON ROUTINE 92811 16 REMOVED DAMAGE PER B757-300 
- [SDR CALA2022012700252](https://openairdocs.org/sdr/CALA2022012700252), Jan 27, 2022: FLOORBEAM. CORRODED. (B757-53-3-0479) R1 DOOR THRESHOLD UPPER CORD FORWARD OF FLOOR B EAM 365.25 - SURFACE CORROSION, TRANSCRIBED FROM HAECO GSO NR LP 9281117 ACCOMPLISHED REPLACEME
- [SDR CALA2022012400209](https://openairdocs.org/sdr/CALA2022012400209), Jan 23, 2022: SKIN. WORN. SUPPORT TASK RIGHT WING OB FWD FLAP IB END LE AREA SKIN WORN AS MARK, TRANSCRIBED FROM HAECO GSO NR LP 9280465 REPAIRED TRAILING EDGE FLAP NOSE SKIN IAW 57-53-0
- [SDR CALA2022012400208](https://openairdocs.org/sdr/CALA2022012400208), Jan 23, 2022: SKIN. CORRODED. (B757-53-3-0479) AFT GALLEY WET AREA - STA 1680 FLOOR BEAM PRESS URE DECK - FROM LBL 51.50 TO RBL 51.50 - SPLICE PLATE AT BL 0 - STA 1720 AT BL 0 - UPPER SKIN H
- [SDR CALA2022012400202](https://openairdocs.org/sdr/CALA2022012400202), Jan 22, 2022: DECK PLATE. DAMAGED. SUPPORT TASK AFT DECK PLATE REPAIR REQUIRED AT STA 1681 RBL 36 - RBL 49 WHICH INCORPORATES AREA 10 AREA 11 AND AREA 12 INTO ONE REPAIR (NRC GENERATED FROM LP 92
- [SDR CALA2022012400201](https://openairdocs.org/sdr/CALA2022012400201), Jan 22, 2022: DECK PLATE. DAMAGED. SUPPORT TASK AFT DECK PLATE REPAIR REQUIRED AT STA 1681 FROM RBL 10 - RBL 18 WHICH INCORPORATES AREA 7 AREA 8 AND 9 INTO ONE REP AIR (NRC GENERATED FROM LP 9281
- [SDR CALA2022011400130](https://openairdocs.org/sdr/CALA2022011400130), Jan 13, 2022: SKIN. DAMAGED. SUPPORT TASK R4 DOOR INNER SKIN AT FWD LOWER LIGHTENING HOLE DAM AGE EDGE, TRANSCRIBED FROM HAECO GSO NR LP 9280846 R4 DOOR INNER SKIN LOWER FWD LIGHTENING HOLE
- [SDR CALA2022011400129](https://openairdocs.org/sdr/CALA2022011400129), Jan 13, 2022: SKIN. CRACKED. SUPPORT TASK L4 DOOR INNER SKIN LIGHTENING HOLE ADJACENT TO UPPE R SURFACE HINGE ARM CRACKED, TRANSCRIBED FROM HAECO GSO NR LP 92 80926 REPAIRED INNER SKIN REF 
- [SDR CALA2022010300003](https://openairdocs.org/sdr/CALA2022010300003), Dec 31, 2021: INTERCOSTAL. GOUGED. TRANSCRIBED FROM HAECO GSO NR LP 9280965 SUPPORT TASK R2 DOOR IN NER SKIN INTERCOSTAL AT UPPER HINGE ARM HAS DEEP GOUGES REMOVED DAMAGED INTERCOSTAL, CLIP AND 2
- [SDR CALA2021030500257](https://openairdocs.org/sdr/CALA2021030500257), Mar 3, 2021: MOTOR. BURNED. AC DIVERTED TO DEN WITH SMOKE IN THE COCKPIT. DEBRIEFED CREW AND FROM FILLED OUT. OBVIOUS ELECTRICAL SMELL AND FOUND THE FWD WQU IP COOLING SUPPLY FAN CB POPPED
- [SDR CALA2020062501017](https://openairdocs.org/sdr/CALA2020062501017), Jun 13, 2020: SLIDE. PARTIAL DEPLOY. DOOR 2L DOOR WAS DISARMED. AS DOOR OPENED THE SLIDE PACK DEPLOYED BUT DID NOT INFLATE OCED FR FERRY UNLOCK FOR UPDATE AFTER SLIDE FELL OUT OF BUSTLE. REMOVED GI
- [SDR CALA2019011200065](https://openairdocs.org/sdr/CALA2019011200065), Jan 10, 2019: FIREWALL. CHAFED. (B757-53-3-0587) APU COMPT. FWD FIREWALL SKIN CHAFED AT STA 1885 . 090-18. REF: ST-SAA NR 0033528. REMOVED DAMAGED AREA OF APU FIREWALL AND REMOVED 5EA FASTENER
- [SDR CALA2018122872650](https://openairdocs.org/sdr/CALA2018122872650), Dec 24, 2018: SLIDE. NO TEST. (SUPPORT TASK 53-2560-1-7804) RH OFF WING ESCAPE SLIDE DID NOT D EPLOY DURING OPERATIONAL TEST. REF ST SAA N/R 0033834 PERFORMED R/H OFF WING ESCAPE SLIDE ELECT
- [SDR CALA2018122002616](https://openairdocs.org/sdr/CALA2018122002616), Dec 18, 2018: WEB. CRACKED. (SUPPORT TASK EA 5210-01364 REV G) R4 DOOR INNER WEB IS CRACKED, AT LOWER AREA, EDGE OF A LIGHTING HOLE. REF VTSAA N/R 0033768. ACCOMPLISHED PERMANENT REPAIR AT
- [SDR CALA2018121402573](https://openairdocs.org/sdr/CALA2018121402573), Dec 12, 2018: GIRT BAR. WORN. (SUPPORT TASK)(EA 2560-02123 REV D) L-4 PASSENGER DOOR GIRT BAR FAILED LEAF SPRING ENGAGEMENT TEST, AND REQUIRES REPLACEMENT. RE F: ST-SAA NR 0033691. / PROCURE
- [SDR CALA2018120702523](https://openairdocs.org/sdr/CALA2018120702523), Dec 6, 2018: BEARING. BROKEN. (SUPPORT TASK EA 5210-01363 REV F) L2 DOOR LOWER GATE GIRT BAR L OWERING/LIFTING MECHANISM AFT ROD IS BROKEN. THIS IS TRANSCRIBED INFORMATION ACCOMPLISHED AND R
- [SDR CALA2018120702506](https://openairdocs.org/sdr/CALA2018120702506), Dec 3, 2018: SHEAR TIE. DAMAGED. (SUPPORT TASK NO: 120.53-9953-8-0844) SHEAR TIE STA 580 BETWEEN STRG 15L-16L HAS OVERSIZES HOLES. REF VTSAA N/R 0033790. REMOVED DAMAGED SHEAR T/E FROM STA 580 
- [SDR CALA2018120702504](https://openairdocs.org/sdr/CALA2018120702504), Dec 3, 2018: SHEAR TIE. DAMAGED. (SUPPORT TASK NO 120 53-9953-8-0844) SHEAR TIE STA 580 BETWEEN S TRG OVERSIZES HOLE. REF VTSAA N/R 0033791. REMOVED DAMAGED SHEAR T/E FROM STA 580BETWEEN S-17L 
- [SDR CALA2017092203257](https://openairdocs.org/sdr/CALA2017092203257), Sep 22, 2017: LENS. CRACKED. EMERGENCY EXIT LIGHT LENS CRACKED ON SIDE OF LAV BY THE L2 DOOR. REPLACED THE EMERGENCY LIGHT ASSY, CHECKED OK.
- [SDR CALA2017091803214](https://openairdocs.org/sdr/CALA2017091803214), Sep 18, 2017: GOVERNOR. FAULTY. DURING TAKEOFF, THE RT ENGINE DID NOT ACHIEVE TAKEOFF POWER. LEFT ENGINE 1.67 EPR. RT ENGINE 1. 4 EPR. MAX FWD THRUST. REPLACED THE NR 2 FUEL FLOW GOVERNOR IAW 
- [SDR CALA2017090102996](https://openairdocs.org/sdr/CALA2017090102996), Sep 1, 2017: BELLCRANK. FAULTY. LEFT AFT ENTRY DOOR SLIDE ARMED LIGHT NOT ILLUMINATED. REPLACED LATCH BELL CRANK ASSY. PER MM 52-11-25. LIGHT OPERATIONAL. OPERATION CHECK GOOD. OK TO CONTINUE 
- [SDR CALA2017090102997](https://openairdocs.org/sdr/CALA2017090102997), Sep 1, 2017: LAMP. INOPERATIVE. L3 DOOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP IAW AMM 33-51-06.

All 74: https://openairdocs.org/aircraft/N57870/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 N57870

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N57870 before.

- [Cancelled 1991-04-08](https://openairdocs.org/deregistered/N57870-1991-04-08): Piper PA-36-300, S/N 367760035. Exported to Ecuador. Owner: [Neal Aircraft Inc](https://openairdocs.org/faa-owner/NEAL%20AIRCRAFT%20INC), [Lubbock, TX](https://openairdocs.org/faa-place/TX/Lubbock)
- [Cancelled 1959-12-22](https://openairdocs.org/deregistered/N57870-1959-12-22): Cessna T-50, S/N 4289. Owner: [Terry E E](https://openairdocs.org/faa-owner/TERRY%20E%20E), [Helena, AR](https://openairdocs.org/faa-place/AR/Helena)

## 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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