# N57869: 2002 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: 32593
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 31, 2002
- Certificate issued: October 13, 2023
- Expires: October 31, 2030
- Mode S code: A76F6D
- 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=57869
- Page: https://openairdocs.org/aircraft/N57869

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/N57869/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 N57869.

## 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 20090311001779I](https://openairdocs.org/incident/20090311001779I), Mar 11, 2009: Boeing 75733N (N57869), Kirksville, MO, No damage. (-23) While cruising at 35000 feet, the cabin filled with smoke. The "left recirculation fan" warning light annunciated and the overboard exhaust valve opened.…

## Service difficulty reports (94, 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 CALA2026092919984](https://openairdocs.org/sdr/CALA2026092919984), Sep 27, 2026: LIGHT. DETACHED. SEAT 11C EMERGENCY EXIT LIGHT HANGING. SECURED LOOSE BRACKET.
- [SDR CALA2026081818720](https://openairdocs.org/sdr/CALA2026081818720), Aug 17, 2026: LIGHT. DETACHED. EMERGENCY PATH LIGHT NEAR SEAT 18ABC NEEDS TO BE REINSTALLED 33-51-11. EMERGENCY ESCAPE PATH LIGHT REPLACED. OPS CHECK GOOD OK FOR SERVICE
- [SDR CALA2026061917199](https://openairdocs.org/sdr/CALA2026061917199), Jun 18, 2026: BATTERY PACK. WEAK. EMERGENCY BATTERY PACK M11488 IS WEAK AFTER EXTENSIVE TROUBLE SHOOTING. REMOVED AND REPLACED EMERGENCY BATTERY PACK M11488 REF: AMM 33-51-07. OPS CHECK NORMAL.
- [SDR CALA2026061717165](https://openairdocs.org/sdr/CALA2026061717165), Jun 16, 2026: LIGHT. BROKEN. EMERGENCY LIGHT ON SEAT 22C FOUND BROKEN. REPLACED EMERGENCY LIGHT. OPS CHECK GOOD. IAW AMM 33-51-00
- [SDR CALA2026033014904](https://openairdocs.org/sdr/CALA2026033014904), Mar 27, 2026: INTERCOSTAL. CRACKED. (SDR) EA 5311-01827 REV G: RG STA 1640 INTERCOSTAL TEE CLIP AREA AT S-14R, CRACK INDICATION NOTED IN ALL LAYERS AT UPPER I/B HOLE. REF NR 136365. ESFR CREATED. 
- [SDR CALA2026032514824](https://openairdocs.org/sdr/CALA2026032514824), Mar 23, 2026: SKIN. CRACKED. DURING ROTO INSP OF LT UPPER WING SKIN. CRACK INDICATION WAS NOTED IN FASTENER HOLE #3 ON THE SKIN LAYER AT 12 O' CLOCK. NR 3 HOLE TAKEN TO SECOND OVER, NO CRAC
- [SDR CALA2026032514823](https://openairdocs.org/sdr/CALA2026032514823), Mar 20, 2026: FRAME. CRACKED. AFT CARGO COMP, BS 1500, S27R, FRAME WITH CRACK BY SCREW. MAJOR REPAIR. WORKED IAW EC/RA:5360-02123 AND EA: 757-5360-13-A4300 R EV-.
- [SDR CALA2026032314737](https://openairdocs.org/sdr/CALA2026032314737), Mar 19, 2026: ANGLE. DENTED. AFT CARGO BAY, BS 1480, S26L, FRAME DENTED. REMOVED DAMAGED AND REPAIRED ACCOMPLISHED WITH EA 757-5360-13-A4 297 REV-.
- [SDR CALA2026032014700](https://openairdocs.org/sdr/CALA2026032014700), Mar 18, 2026: FLOORBEAM. CORRODED. MAIN CABIN, FLOOR AREA, RH SIDE, APPROX STA.330, PANEL 222AF CUTOUT, BEAM FLOOR, UPPER SURFACE HAS CORROSION. NR#136805 FLOORBEAM AT STA330 PANEL 222AF CUTOUT A
- [SDR CALA2026031214518](https://openairdocs.org/sdr/CALA2026031214518), Mar 7, 2026: FRAME. CORRODED. AFT CARGO BAY, BS 1420 FRAME CORRODED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02-0G-0. MAJOR REPAIR.
- [SDR CALA2026031214517](https://openairdocs.org/sdr/CALA2026031214517), Mar 7, 2026: FRAME. CORRODED. AFT CARGO BAY, BS 1460, FRAME CORRODED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02-0G-0. MAJOR REPAIR.
- [SDR CALA2026031214516](https://openairdocs.org/sdr/CALA2026031214516), Mar 7, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO BAY, BTW BS 1420-1440, RBL 10.45, FLOOR SUPPORT CORROSDED. REMOVED AND REPLACED THE FLOOR SUPPORT BTW BS 1420 -1440, RBL 10.45 IAW SRM 51-40-02-0G-0. 
- [SDR CALA2026031014467](https://openairdocs.org/sdr/CALA2026031014467), Mar 7, 2026: INTERCOSTAL. CORRODED. AFT CARGO COMP, BTW STA 1400-1420, RBL 2.90, INTERCOSTAL AND BRACKET WITH CORROSION. NR: 136683 COMPLETED SFR REPORTING ONLY REMOVED AND REPLACED INTERCOSTAL AN
- [SDR CALA2026030914419](https://openairdocs.org/sdr/CALA2026030914419), Mar 6, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMP, FLOOR STRUCTURE, NUTPLATES (LOWER SKIN) AN D 2 DENTS. NR: 136711 ESFR CREATED. REMOVED AND REPLACED LH TRANSITION PANEL IAW B757-300 SRM 51-40- 
- [SDR CALA2026030914416](https://openairdocs.org/sdr/CALA2026030914416), Mar 5, 2026: TRANSITION PANEL. CORRODED. (SDR) AFT CARGO COMP, BTW STA 1520 AND 1560, R/H TRANSITION PANE L WITH CORROSION IN LOWER AND R/H LATERAL SKIN WC:136732 COMPLETED SFR REPORTING ONLY REMOVED A
- [SDR CALA2026030914411](https://openairdocs.org/sdr/CALA2026030914411), Mar 5, 2026: TRANSITION PANEL. CORRODED. AFT CARGO COMP, BTW BS 1440-1520, RT TRANSITION PANEL WITH CORROSION AT UPPER AND LOWER SKIN (UNDER NUTPLATES) WC:136713. REMOVED AND REPLACED TRANSITION PANEL 
- [SDR CALA2026030414316](https://openairdocs.org/sdr/CALA2026030414316), Mar 4, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMP, FLOOR SUPPORT, BTW BS 1460 - 1480, RBL 14, CORRODED AT UPPER AND LWR SURFACE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR CALA2026030414314](https://openairdocs.org/sdr/CALA2026030414314), Mar 4, 2026: STRINGER. CORRODED. AFT CARGO COMP, BS 1500, RBL 2,90, STRINGER UNION WITH CORROSION AT UPPER SECTION, LOWER SURFACE. REMOVED AND REPLACED STRINGER BS 1500 RBL 2-90 IAW SRM 51-40-0
- [SDR CALA2026030314277](https://openairdocs.org/sdr/CALA2026030314277), Mar 2, 2026: INTERCOSTAL. CORRODED. AFT CARGO BAY, BTW BS 1520 - 1540, RBL 2.9, INTERCOSTAL CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G.
- [SDR CALA2026030314273](https://openairdocs.org/sdr/CALA2026030314273), Mar 2, 2026: FLOOR SUPPORT. CORRODED. FWD CARGO BAY, FLOOR SUPPORT CORRODED AT BS 780+20, RBL 19. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02-0G.
- [SDR CALA2026030314248](https://openairdocs.org/sdr/CALA2026030314248), Mar 1, 2026: CHANNEL. CORRODED. AFT CARGO COMPT, BS 1620, RBL 2.90, LOWER BRACKET CORRODED. R & R THE SPLICE CHANNEL IAW SRM 51-40-02, TREATED AND PRIMED IAW SRM 51-20-01. RESTORED SURFACE IAW
- [SDR CALA2026030314246](https://openairdocs.org/sdr/CALA2026030314246), Mar 1, 2026: TRANSITION PANEL. CORRODED. AFT CARGO FLOOR SUPPORT, RT TRANSITION PANEL FROM BS 1310 - 1380 CORRODED IN UPPER SURFACE & UNDER NUT PLATES. REMOVED AND REPLACED THE TRANSITION PANEL IAW SRM
- [SDR CALA2026030314240](https://openairdocs.org/sdr/CALA2026030314240), Feb 28, 2026: TRANSITION PANEL. CORRODED. AFT CARGO BAY, BTW BS 1380 - 1440 , RT TRANSITION PANEL CORRODED AT UPPER & LOWER SURFACE UNDER NUTPLATES. R & R THE TRANSITION PANEL IAW SRM 51-40-02.
- [SDR CALA2026022614090](https://openairdocs.org/sdr/CALA2026022614090), Feb 24, 2026: INTERCOSTAL. CORRODED. AFT CARGO COMP, BTW STA 1360-1380, S27R, INTERCOSTAL ANGLE WITH CORROSION.REF NR 1336679. PARTS FABRICATED PER DWG 146N4512-4, 146N5213-1, 146N5213-1, AND 654N0
- [SDR CALA2026022614088](https://openairdocs.org/sdr/CALA2026022614088), Feb 24, 2026: FLOORBEAM. CORRODED. FLOORBEAM BTW BL 0 - RBL 24.75, BS 333.45, CORRODED. REPAIR FABRICATED IAW DWG 141N5160, REV D. REMOVED AND REPLACED, REMOVED 100%, EXFOLIATED BS 333.45 BTW BL 
- [SDR CALA2026021613818](https://openairdocs.org/sdr/CALA2026021613818), Feb 14, 2026: SILL DRAIN. CORRODED. R4 DOOR LOWER SILL, UNDER DRAIN GUTTER BTWN BS 1640 - 1681, HAS CORROSION. REMOVED CORROSION IN R4 DOOR LOWER SILL, FOUND OUT OF LIMITS IAW SRM 51-10-02-0G, REM
- [SDR CALA2026021613802](https://openairdocs.org/sdr/CALA2026021613802), Feb 13, 2026: FLOORBEAM. CORRODED. EXT LOWER MID FUSELAGE STA 900 BL0-RBL5 T- CHORD CORRODED. REF NR: 136283. ESFR REPAIRED AREA AT EXT LOWER MID FUSELAGE STA 900 BTW RBL 25 TO LB L 25 T-CHORD IA
- [SDR CALA2026021613800](https://openairdocs.org/sdr/CALA2026021613800), Feb 13, 2026: DOOR SILL. CORRODED. (SDR) (EA 5210-03219 REV D OP 002) L2 DOOR LWR SILL FLOOR SUPPORT HAS CORROSION. AFTER FINDING CORROSION AT L2 DOOR LWR SILL OUT OF LIMITS IAW SRM 53-30-13-1A-1
- [SDR CALA2026021613798](https://openairdocs.org/sdr/CALA2026021613798), Feb 13, 2026: FLOOR SUPPORT. CORRODED. (SDR) (B757-MP-2100-53-216-00) FLOOR STR, FLOOR BEAM ON BL0, BTW STA 1640-1681 HAS CORROSION. REF NR: 136782. PART WAS REPLACED. REMOVED AND REPLACED CHANNEL AT
- [SDR CALA2026021113693](https://openairdocs.org/sdr/CALA2026021113693), Feb 10, 2026: FLOOR SUPPORT. CORRODED. MAIN DECK FLOOR AREA ADJACENT TO R1 DOOR SILL BET. STA 324 - 377 INTERCOSTAL UPPER SKIN CORRODED. 16-23. REF NRC 136578. COMPLETED SFR REPORTING ONLY REMOVED AN
- [SDR CALA2026021013654](https://openairdocs.org/sdr/CALA2026021013654), Feb 7, 2026: DOOR SILL. CORRODED. R1 DOOR LOWER SILL UPPER SKIN ATTACH ANGLE BTWN BS 324 - 365 CORRODED. REMOVED AND REPLACED THE ANGLE ON TRAVELER#T26/1849387 AND HEAT TREATED TO T42 IAW SRM 51
- [SDR CALA2026020313520](https://openairdocs.org/sdr/CALA2026020313520), Jan 31, 2026: SEAT TRACK. CORRODED. SEAT TRACK AND FLOORBEAM ON LBL 24.75, BTWN BS 1300 - 1320 CORRODED. IAW NR 136787, COMPLETED SFR REPORTING ONLY. FOUND CORROSION AT LBL 24.75 BTWN BS 1300 - 13
- [SDR CALA2026020213476](https://openairdocs.org/sdr/CALA2026020213476), Jan 30, 2026: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK AT BS .377.7 LBL 45 UPPER SKIN HAS SURFACE CORROSION. R & R THE SEAT TRACK BS 377.7 - 420, LBL 45 IAW SRM 53-10-52-01-1 51-40-05-0G AND 51-
- [SDR CALA2026011412948](https://openairdocs.org/sdr/CALA2026011412948), Jan 10, 2026: WEDGE. DELAMINATED. SLAT NR 5 HAS MULTIPLE DEBONDS - DELAMINATIONS (2EA) ON THE UPPER SURFACE OF THE T/E WEDGE. ALL DAMAGE MARKED. REPAIRED THE AREAS ON THE NR 5 SLAT T/E WEDGE IAW
- [SDR CALA2025102110359](https://openairdocs.org/sdr/CALA2025102110359), Oct 18, 2025: UNKNOWN. ODOR. FAS SMELLED INT SMELL OF SMOKE FIRST NEAR ROW 25/26 THEN THE FWD GALLEY PERFORMED VISUAL INSP OF AREA AROUND ROW 25/26 AND FWD GALLEY NO OBVIOUS DEFECTS NOTED ,
- [SDR CALA2025091508891](https://openairdocs.org/sdr/CALA2025091508891), Sep 9, 2025: TRANSMISSION. TRIPPED. TE FLAP DISAGREE ON APPROACH. FLAPS STUCK BETWEEN 15/20. RAN QRH. WHEN FLAPS WERE SET TO 20, FLAPS STOPPED MOVING HYDRAULICALLY BETWEEN 15 & 20 DEGREES & HAD A 
- [SDR CALA2025090408459](https://openairdocs.org/sdr/CALA2025090408459), Sep 3, 2025: SLIDE. NO DISCREPANCY. INSTALLED 1EA SAFETY PINS AT DOOR L1 IN EACH DOOR ASSIT BOTTLE AND DOOR SLIDE ASSY. FOR REPLACEMENT OF SLIDE ASSY REMOVED AND STOWED 1EA SAFETY PINS AT DOOR L1 
- [SDR CALA2025070906385](https://openairdocs.org/sdr/CALA2025070906385), Jul 8, 2025: FSEU. FAULTED. EMERGENCY DECLARED DUE TO FLAPS STUCK AT 25. REPLACED FSEU #1 IAW AMM 27-51-01-422-011. OP CHECK GOOD IAW AMM 27-51-01-422-005.
- [SDR CALA2025052004856](https://openairdocs.org/sdr/CALA2025052004856), May 17, 2025: MODULATING VALVE. FAULTED. COCKPIT TEMP TOO HOT AND TEMPO UNCOTROLLED AFTER QRH TEMP EVENTU ALY BEGAN TO COME DOWN PER PILOTS-ON THE TAKEOFF ROLL COCKIT VENT OUTLETS POURED OUT AIR THAT W
- [SDR CALA2025022602472](https://openairdocs.org/sdr/CALA2025022602472), Feb 24, 2025: BOTTLE. FAULTED. EMER ESCAPE SQUIB TEST 2 L DOES NOT ILLUMINATE REF FIM 25-65 FAULT TREE 803REF FIM 25-65 FAULT TREE 803 BLOCK 13 REMOVED CONNECTOR D5530 FROM PRESSURE SWITCH S1
- [SDR CALA2025021302309](https://openairdocs.org/sdr/CALA2025021302309), Feb 9, 2025: TACHOMETER. FAULTED. N1 OVERSPEED INDICATION NUMBER 2 ENGINE N1 OVERSPEED BEGAN DURING CLIMB AT 15,000FT . DURING APPROACH BACK EPR WENT BLANK. PILOTS REDUCED THROTTLE TO MATCH N1. 
- [SDR CALA2024092600695](https://openairdocs.org/sdr/CALA2024092600695), Sep 23, 2024: GOVERNOR. FAULTY. RT ENG REDUCED PWR EPR LIMITED TO 1.44 CREW REPORTS FUEL FLOW INDICATION LOWER ON RH ENGINE REMOVED AND REPLACED #2 ENGINE FUEL FLOW GOVERNOR IAW AMM 73-21-01. 
- [SDR CALA2024090302368](https://openairdocs.org/sdr/CALA2024090302368), Aug 31, 2024: BATTERY PACK. INOPERATIVE. SEATS (AB) 1-2-3 EMERGENCY LIGHT INOP. REPAIR AS REQUIRE. REMOVE AND REPLACED POS M731 BATTERY PACK IAW B757 AMM 33-51-07- 902-005-002 OPS CHECK GOOD.
- [SDR CALA2024090302341](https://openairdocs.org/sdr/CALA2024090302341), Aug 29, 2024: CHANNEL. CRACKED. B757-06-3-0239 - CRACK ON SEAL RETAINER STRUCTURE FWD FRAME CUT OUT OF RH W/W. REMOVED SEAL AND RETAINER, AND REPLACED RETAINER, BRACET AND SEA L IAW B757 SRM 5
- [SDR CALA2024090302345](https://openairdocs.org/sdr/CALA2024090302345), Aug 29, 2024: CHANNEL. CRACKED. LH WHEEL WELL FWD CUT-OUT SEAL RE TAINER OUTB AREA NEXT TO PROX SENSOR WITH CRACK. REMOVED SEAL SUPPORT CHANNEL AND REPLACED SUPPORT CHANNEL AND SE AL IAW B757 
- [SDR CALA2024090302342](https://openairdocs.org/sdr/CALA2024090302342), Aug 28, 2024: ANGLE. CRACKED. B757-06-3-0239 - CRACK ON ANGLE FWD FRAME O/B SIDE OF CUT OUT OF RH W/W. RENOVED AND REINSTALL WTB PANELS 198BR, 198CR, AND 198DR IAW B75 7-300 AMM 53-36-02, RE
- [SDR CALA2024090302349](https://openairdocs.org/sdr/CALA2024090302349), Aug 28, 2024: FLAP TRACK. CORRODED. B757-06-3-0302 - LH WING INB MAIN FLAP L/E NOSE SKIN INB AREA TR UNNION FAIRING WITH SEVERAL CORROSION SPOTS. REPAIRED THE L/H I/B MAIN FLAP IAW B757 SRM 57-53-
- [SDR CALA2024083002335](https://openairdocs.org/sdr/CALA2024083002335), Aug 28, 2024: ANGLE. CRACKED. B757-06-3-0237 - LH WHEEL WELL AREA PANEL 197BL INTERNAL AFT FRAME INB BRACKET AND OUTB BRACKET (2EA) WITH CRACK.
- [SDR CALA2024083002333](https://openairdocs.org/sdr/CALA2024083002333), Aug 28, 2024: BULKHEAD. DENTED. LOG #8798906 DURING OPENING SIDEWALL ACCESS PANEL LEFT SIDE AFT CARGO PIT, FOUND (01EA) DENT AT FR 1400 STRG 26L.
- [SDR CALA2024083002328](https://openairdocs.org/sdr/CALA2024083002328), Aug 28, 2024: DECK PLATE. DENTED. B757-06-3-0254 - FLT COMPT FLOOR HAS LARGE DENT AFT CENTER AREA.

All 94: https://openairdocs.org/aircraft/N57869/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 N57869

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N57869 before.

- [Cancelled 2000-01-20](https://openairdocs.org/deregistered/N57869-2000-01-20): S N I A S AS350D ASTAR, S/N 1324. Exported to Canada. Owner: [Filtertek Of Puerto Rico Inc](https://openairdocs.org/faa-owner/FILTERTEK%20OF%20PUERTO%20RICO%20INC), [Patillas, PR](https://openairdocs.org/faa-place/PR/Patillas)

## 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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