# N75861: 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: 32585
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 7, 2001
- Certificate issued: December 22, 2023
- Expires: December 31, 2030
- Mode S code: AA3B05
- 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=75861
- Page: https://openairdocs.org/aircraft/N75861

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/N75861/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 N75861.

## FAA accident and incident reports

None matched to N75861.

## Reports on N75861 not matched to an aircraft (1)

They name N75861, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19800419039959I](https://openairdocs.org/incident/19800419039959I), Apr 19, 1980: Cessna 172N (N75861), Houston, TX, Minor damage. Student pilot on unauthorized crosscountry flight landed fast and long. Ran out of runway.

## 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 CALA2026071617820](https://openairdocs.org/sdr/CALA2026071617820), Jul 16, 2026: LIGHT. INOPERATIVE. EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - DR LL CLOSET FWD EMER FLOOR PROX LIGHT INOP RELAMPED, OPS CHECK GOOD REF CMM 25-22-37
- [SDR CALA2026071617818](https://openairdocs.org/sdr/CALA2026071617818), Jul 16, 2026: LAMP. INOPERATIVE. EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - DR 1L EXTERIOR DOOR SLIDE LIGHT INOP RELAMPED, OPS CHECK GOOD REF AMM 33-51-06-962-001-002
- [SDR CALA2025122412423](https://openairdocs.org/sdr/CALA2025122412423), Dec 23, 2025: BULB. INOPERATIVE. EMERGENCY DOORS OVERHEAD LIGHT, ONE BULB OUT. RELAMPED THE IGHT IAW AMM 33-13-00-962-033. OPS CHECKED OK.
- [SDR CALA2025121212047](https://openairdocs.org/sdr/CALA2025121212047), Dec 10, 2025: COVER. BROKEN. EMERGENCY LIGHTS - OPS TEST WITH THE TEST SWITCH PROCEDURE - ROW 25ABC EMERGENCY PATHWAY LIGHT BROKEN REPLACED PLASTIC COVER ON EMERGENCY PATHWAY LIGHT, OPS CHE
- [SDR CALA2025100909859](https://openairdocs.org/sdr/CALA2025100909859), Oct 8, 2025: TRANSMITTER. FAULTED. INBOUND FLT CREW REPORTED ASSYMETRICAL FLAP POSITION ON APPROACH, CREW UNSURE OF WHICH FLAP SIDE WAS AT 30 DETENT AND WHICH ONE WAS AT 25 DETENT. GO AROUND PERF
- [SDR CALA2025050504438](https://openairdocs.org/sdr/CALA2025050504438), May 2, 2025: CHARGER. FAULTED. EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - AFT EMERGENCY EXIT LOCATOR SIGN (M10255) INOP SWAPPED EMERGENCY BATTERY CHARGER M737 WITH M
- [SDR CALA2025050504437](https://openairdocs.org/sdr/CALA2025050504437), May 2, 2025: HINGE. FAULTED. DOOR 196HR HAS GAP AT UPPER SIDE.LEFT SLIDE SERVICE ACCESS PANEL.ABOVE LEFT WING AFT REMOVED AND REPLACED HINGE ASSEMBLY REF AIPC 53-65-52-01A.PARTS USED: 19-53
- [SDR CALA2025042104053](https://openairdocs.org/sdr/CALA2025042104053), Apr 19, 2025: SKIN. CORRODED. AFT R/LWR FUSELAGE LAV SERVICE ACCESS PNL 166AR SKIN AROUND IT BOWED OUT. ESFR REPORTING FOR MAJOR REPAIR REF ECRA 5360-01946 TO LAV SERVICE PANEL ACCOMPLISHED 
- [SDR CALA2025041103713](https://openairdocs.org/sdr/CALA2025041103713), Apr 10, 2025: ANGLE. CORRODED. (SUPPORT TASK) LEFT SIDE FUSELAGE BETWEEN STA 879 TO STA 984 AT WBL95.00 UPPER WING HAS FAIRING PANEL SUPPORT STRUCTURE 191DL WI TH LIGHT CORROSION. SDR REPORTI
- [SDR CALA2025041103712](https://openairdocs.org/sdr/CALA2025041103712), Apr 10, 2025: STRINGER. CORRODED. (B757-06-3-0243) AFT CARGO PT FLOOR BLIGE AREA STA 1620 AREA BEL OW THE RH TRANSITION PANEL THE STRINGER AND FRAME ATTACH FITTING S HAS SEVERE CORROSION. SDR RE
- [SDR CALA2025040803641](https://openairdocs.org/sdr/CALA2025040803641), Apr 7, 2025: ANGLE. DAMAGED. (SUPPORT TASK) LEFT SIDE FUSELAGE BETWEEN STA 879 TO STA 984 UPP ER WING WBL95.00 HAS 01 SUPPORT WING TO BODY FAIRING PANEL 191DL WITH HOLE MISSDRILL.-(DOT 6-73
- [SDR CALA2025040403522](https://openairdocs.org/sdr/CALA2025040403522), Apr 3, 2025: SEAT TRACK. CORRODED. MID CABIN PAX FLOOR STRUCTURE FR680-FR740/RBL 45.5 FLOOR BEAM HA S CORROSION AT SEVERAL SPOTS AS MARKED. SDR REPORTING ONLY SDR REPORTING REMOVED AND REPLACED S
- [SDR CALA2025032503180](https://openairdocs.org/sdr/CALA2025032503180), Mar 21, 2025: BEAR STRAP. CRACKED. EA5330-04213 REV D OP004: THE L1 DOOR SURROUND STRUCTURE HAS 1EA FASTENER HOLE WITH A CRACK INDICATION AT THE BOTTOM OF BEAR STR AP LAYER ONLY. DISCREPENT FASTE
- [SDR CALA2025031702847](https://openairdocs.org/sdr/CALA2025031702847), Mar 15, 2025: SEAT TRACK. CORRODED. (B757-53-3-0551) FUSELAGE CABIN PASSENGER BETWEEN STA 377.7 TO S TA 395/LBL 50 TO LBL 36.20 / LONGITUDINAL BEAM (SEAT TRACK) HAS CORROSION. ESFR COMPLETED REMOV
- [SDR CALA2025031102707](https://openairdocs.org/sdr/CALA2025031102707), Mar 9, 2025: SEAT TRACK. SCRATCHED. (B757-53-3-0575) PAX CABIN FR1180 - FR1320 RBL 24.75 SEAT TRACK HAS SCRATCHES AND BARE METAL AT SEVERAL SPOTS. ESFR INFORMATION INPUT. REMOVED DAMAGE IAW B757-3
- [SDR CALA2025031102706](https://openairdocs.org/sdr/CALA2025031102706), Mar 9, 2025: SEAT TRACK. SCRATCHED. (B757-53-3-0575) PAX CABIN FR1320 - FR1540 LBL 45.5 SEAT TRACK H AS SCRATCHES AND BARE METAL AT SEVERAL SPOTS. NONE REMOVED DAMAGE IAW B757-300 SRM 51-10-02-0G-
- [SDR CALA2024111701170](https://openairdocs.org/sdr/CALA2024111701170), Nov 13, 2024: GOVERNOR. FAULTY. ON TAXI OIL PRESS RAPIDY DROPPED ON LT ENG EGT CLIMBED AT MOD PACE SHUTDOWN LT ENG MANUALLY REF L/P 9861166 FOR INSPECTION OF MCD THAT WERE FOUND CLEAN. PERFORM
- [SDR CALA2024041601096](https://openairdocs.org/sdr/CALA2024041601096), Apr 13, 2024: DRAG LINK. DAMAGED. #1 ENGINE OUTER C DUCT DAMAGED AT 7 O''CLOCK POSITION. REF LOG PAGE 7639869. PHOTOS ATTACHED ADDTIONAL PHOTOS MORE PHOTOS INTERNAL HEAT BLANKET ADDITIONAL PHOTO
- [SDR CALA2024011700135](https://openairdocs.org/sdr/CALA2024011700135), Jan 15, 2024: IDG. FAULTED. ON ROTATION...R GEN DRIVE DISC ACCOMPLISHED IDG SERVICING. RAN ENGINE TO ACCOMPLISH FUNCTIONAL CHECK. DRIVE LIGHT REMAINS ILLUMINATED. M&E PART NUMBER 19-24
- [SDR CALA2023111503359](https://openairdocs.org/sdr/CALA2023111503359), Nov 10, 2023: FSEU. FAULTY. TE FLAP DISAGREE. QRH RUN. HANDLE AT 25. FLAPS AT 20. PERFORMED FIM TASK 27-51 FT814 AND REPLACED FSEU 1 IAW AMM27-51-01-401 GROUND OPS CHK GOOD IAW AMM 27-51-0
- [SDR CALA2023092502877](https://openairdocs.org/sdr/CALA2023092502877), Sep 24, 2023: ACTUATOR. FAULTY. ON CLIMB FO INCREASE AILERON TO 3-6UNITS LEFT. CROSS CONTROL WORSE ON LANDING. VERIFY INSTALLATION OF #11 SPOILER ACTUATOR REF. AMM 27-61-02 AND GMM 09-25-05. O
- [SDR CALA2023050901436](https://openairdocs.org/sdr/CALA2023050901436), May 9, 2023: UNKNOWN. LEAKING. APU OIL QTY VERIFIED HMG OPERATES NORMAL, PLACING APU ON MEL. COMPLIED WITH MEL. DISPATCH DESK: 30 NAME: A.G. DATE: 09-MAY-23- NOC DESK: 757 NAME: DARRIN DATE: 
- [SDR CALA2023050801420](https://openairdocs.org/sdr/CALA2023050801420), May 8, 2023: CONNECTOR. UNKNOWN. CONNECTOR D40488J BACKSHELL NEEDS TO BE SAFETIED TO CONNECTOR AND SECURED INTO BRACKET. CONNECTOR SCREWS ARE IN A BAG SECURED TO CONNECTOR. SECURED D40488 BACKS
- [SDR CALA2023051201484](https://openairdocs.org/sdr/CALA2023051201484), May 1, 2023: FAIRING. MISSING. RIGHT WING NO. 6 FLAP TRACK AFT FAIRING FWD LH ATTACH PLATE IS MISSING. SEE PIC AFT FLAP TRACK FAIRING REMOVED. FLAP TRACK FAIRING REMOVED PER CDL27C 486,DELIVE
- [SDR CALA2023032200840](https://openairdocs.org/sdr/CALA2023032200840), Mar 22, 2023: FLAP. WARNING LIGHT. TE FLAPS DISAGREE ON SHORT FINAL FLAPS AROUND 24 DEGREES RAN FLAPS BACK TO FULL UP IN ALTERNATE MODE. POWERED ALL 3 HYD FLAPS 25, THEN TO FLAPS 30. OPS CHKS GOO
- [SDR CALA2023020800368](https://openairdocs.org/sdr/CALA2023020800368), Feb 8, 2023: NOT REPORTED. NOT REPORTED. PULSATING SOUND COMING FROM AURAL WARNING SPEAKERS. SOUND GONE WITH WARN ELEX A (P5 J33) AND WARN ELEX B (P5 B18) BREAKERS PULLED. REPLACED EGPWS COMPUTER , PUL
- [SDR CALA2023012300188](https://openairdocs.org/sdr/CALA2023012300188), Jan 23, 2023: TRANSMITTER. FAULTED. SPOKE TO FLT CREW IN SFO LT SYS 83 ,CENTER 93 ,RT SYS 98 . ALL NORMAL DURING FLT, MLG DOWN CENTER WENT TO ZERO . ALSO CENTER SYS PRESSURE WENT TO ZERO 88%. SERV
- [SDR CALA2022061001478](https://openairdocs.org/sdr/CALA2022061001478), Jun 9, 2022: SKIN. NONE. NUMEROUS BLEND OUTS LOCATED ON LWR AFT FUSELAGE SKIN, STA 1300-1460, STRINGER 25R TO 26L. INFO ONLY INFO ONLY: SEE NR 5715602 (MCO) FOR PREVIOUS REPAIRS & CORRE
- [SDR CALA2022021800438](https://openairdocs.org/sdr/CALA2022021800438), Feb 17, 2022: LIGHT. INOPERATIVE. EMERGENCY BULL NOSE LIGHTS AT SEATS 22,24 AND 27ABC AND EXTERIOR LEFT WING OVERWING EXIT DOOR FWD AND AFT LIGHTS INOP. SUSPECT PWR SPLY AND/OR BATT AT M11383 RE
- [SDR CALA2021082701442](https://openairdocs.org/sdr/CALA2021082701442), Aug 27, 2021: TRANSMITTER. FAILED. CENTER HYD SYSTEM FLUID SHOWING RF AND DECREASING CURRENT .45 REPLACED CENTER HYD SYS QUANITY TRANSMITTER PER AMM 29-33-01 LEAK AND OPS CHK OK ROTABLE PARTS CHA
- [SDR CALA2021041200442](https://openairdocs.org/sdr/CALA2021041200442), Apr 12, 2021: BATTERY PACK. FAILED. R3 DOOR LOWER SLIDE LIGHT INOP. EXTERIOR FUSELAGE LIGHT INOP. SUSPECT BAD BATTERY PACK. PN M11489. MEL 3351B THIS MEL, THE ACFT CANNOT FLY AT NIGHT (ANY NIGHT T
- [SDR CALA2020101601197](https://openairdocs.org/sdr/CALA2020101601197), Oct 16, 2020: LAMP. INOPERATIVE. 1L EXIT LIGHT ABOVE DOOR ONLY 1/2 ILLUMINATED RELAMPED PER AMM 33-51-01-962-001-002 PARTS REPLACED BULB GE OL-3071BPEGPL 6 EA. OPS CHK OK ACP''D IDT INSP. VERIF
- [SDR CALA2019071501196](https://openairdocs.org/sdr/CALA2019071501196), Jul 13, 2019: SKIN. DENTED. B757-06-3-0380 EXTERNAL FUSELAGE REPAIR HAS DENT AT APPROX. STA 612,ON STGR 17L,16-6 REF. ST. ENGINEERING N/R 0065099 INITIATE A DTA DIP/LP TO ACCOMPLISH INSPEC
- [SDR CALA2019070801164](https://openairdocs.org/sdr/CALA2019070801164), Jul 7, 2019: STRINGER. CRACKED. B757-53-3-0556 MAIN CABIN SRT 16L AT STA 780+40 IS CRACKED FROM EDGE TO FASTENER. (APP .5 INCH) REF ST-ENG N/R 0065402. ACCOMPLISHED PERMANENT REPAIR ON FUSELAG
- [SDR CALA2019070801163](https://openairdocs.org/sdr/CALA2019070801163), Jul 7, 2019: STRINGER. CRACKED. B757-53-3-0556 MAIN CABIN STA 780+20 STR 16L CRACKED FROM EDGE TO FIRST FASTENER. (APP. 5 INCH) REF ST-ENG N/R 0065401 ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE
- [SDR CALA2019070801158](https://openairdocs.org/sdr/CALA2019070801158), Jul 6, 2019: FRAME. GOUGED. B757-53-3-0261 MAIN CABIN FRAME STA 1280 BETWEEN STR 14R AND 11R HAS THREE GOUGES ON FRAME WEB. REF ST-ENG N/R 0065532. ACCOMPLISHED INTERIM REPAIR AT MAIN CABI
- [SDR CALA2019070801154](https://openairdocs.org/sdr/CALA2019070801154), Jul 5, 2019: LONGERON. CRACKED. B757-53-3-0556 LONERON 16R AT STATION 780+40 IS CRACKED ON ITS END. REF ST-ENG N/R 0065379 ACCOMPLISHED PERMANENT REPAIR BETWEEN FUS. STA 780-36 TO STA 780 +40,
- [SDR CALA2019070301119](https://openairdocs.org/sdr/CALA2019070301119), Jul 1, 2019: LONGERON. CRACKED. B757-53-3-0556 LONGERON 16R AT STATION 780+20 IS CRACKED ON ITS END. REF ST-ENG N/R 0065378. ACCOMPLISHED PERMANENT REPAIR AT STA 780+20, STR 16R IAW EC/RA 5330
- [SDR CALA2019070201114](https://openairdocs.org/sdr/CALA2019070201114), Jul 1, 2019: RING. BROKEN. EA 7830-02252 REV A. DURING THRUST REVERSER INSPECTION FOUND NR 2 ENGINE I/B T/R NR9 CASCADE BROKEN- MISSING AND SUPPORT RING BROKEN WITH PARTS MISSING. REF ST-
- [SDR CALA2019070301116](https://openairdocs.org/sdr/CALA2019070301116), Jun 30, 2019: GATE. CORRODED. SUPPORT TASK EA 5210-01360 REV J L1 DOOR LOWER GATE HAS MULTOPLE AREAS OF CORROSION AS MARKED 034-047. REF. ST. ENGINEERING N/R 0065757 REMOVED & INSTALLED 
- [SDR CALA2019070201109](https://openairdocs.org/sdr/CALA2019070201109), Jun 29, 2019: RING. MISSING. PDA 1 DURING INITIAL INSPECTION DURING 4C CHECK AT SAT FOUND #2 ENG. I/B T/R #9 CASCADE BROKEN/MISSING AND SUPPORT RING BROKEN.
- [SDR CALA2019062211004](https://openairdocs.org/sdr/CALA2019062211004), Jun 18, 2019: FLOORBEAM. CORRODED. B757-53-3-0480 CORROSION ON MAIN CABIN FLOOR BEAM UPPER SURFACE AT STA 680 RBL-53 REF. ST. ENGINEERING N/R 0065606 FOUND CORROSION OUT OF LIMIT IAW B757-300 SRM
- [SDR CALA2019062210979](https://openairdocs.org/sdr/CALA2019062210979), Jun 15, 2019: ANGLE. CORRODED. B757-49-3-8084 HEAVY CORROSION BETWEEN APU AIR INLET DOOR HOUSIN G ASSY AND FUSELAGE CUTOUT SUPPORT STRUCTURE LANDING RL062 REF. ST.ENGINEERING N/R 0065354 REMO
- [SDR CALA2019062401049](https://openairdocs.org/sdr/CALA2019062401049), Jun 11, 2019: SEAL DEPRESSOR. DENTED. B757-52-3-0001 FWD CARGO DOOR AFT SEAL DEPRESSOR HAS TWO DENTS,1 6-14 REF. ST. ENGINEERING N/R 0065107 REMOVED & REPLACED SEAL DEPRESSOR ON AFT SIDE OF FWD 
- [SDR CALA2019062401048](https://openairdocs.org/sdr/CALA2019062401048), Jun 11, 2019: CREASE BEAM. CORRODED. CORROSION ON MAIN CABIN LH CREASE BEAM INNER CHOR D UPPER SURFACE FROM STA 730-755 LBL-64 RG30 REF. ST. ENGINEERIN G N/R 0065600 REMOVED & REPLACED L/H CREA
- [SDR CALA2019061400926](https://openairdocs.org/sdr/CALA2019061400926), Jun 10, 2019: DECK PLATE. CORRODED. B757-53-3-0480 CORROSION ON AFT CABIN FLOOR DECK PLATE UPPER SUR FACE FROM STA 1680-1720 BLO TO LBL-54 RG2 REF. ST. ENGINEERING N/R 0065562 REMOVED CORROSION AT
- [SDR CALA2017121404449](https://openairdocs.org/sdr/CALA2017121404449), Dec 14, 2017: SLIDE. DEFECTIVE. ARMED LT MISSING ON DOOR 1L. CANT TELL IF DOOR IS ARMED OR NOT. REPLACED ESCAPE SLIDE LIGHT AT DOOR 1L, OK FOR SERVICE.
- [SDR CALA2017080802526](https://openairdocs.org/sdr/CALA2017080802526), Aug 8, 2017: UNKNOWN. ODOR. F/A ADVISE PILOTS OF A SCENT OF SMOKE AT ROW 18. PERFORMED SMOKE ODOR CHECK IAW 05-51-58-910-801 C1. NO ODORS FOUND, COMPLETED THROUGH INSPECTION OF ACFT. OK TO
- [SDR CALA2016121201071](https://openairdocs.org/sdr/CALA2016121201071), Dec 12, 2016: BULB. INOPERATIVE. SEAT 20A EMERGENCY LIGHT HAD A BULB INOPERATIVE. REPLACED THE BULB, NOW OK
- [SDR CALA2016100300718](https://openairdocs.org/sdr/CALA2016100300718), Oct 3, 2016: LIGHT. INOPERATIVE. EMERG LTS UNARMED LIGHT NOT ILLUMINATING LEFT BRIGHT BULB. DIM BULB WORKS. REPLACED LIGHT OPS CHECK NORMAL.

All 70: https://openairdocs.org/aircraft/N75861/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

## 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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