# N77871: 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: 33526
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 30, 2003
- Certificate issued: December 13, 2023
- Expires: December 31, 2030
- Mode S code: AA8A26
- 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=77871
- Page: https://openairdocs.org/aircraft/N77871

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/N77871/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 N77871.

## FAA accident and incident reports

None matched to N77871.

## Service difficulty reports (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 CALA2026070617557](https://openairdocs.org/sdr/CALA2026070617557), Jul 3, 2026: SWIVEL. DAMAGED. LEFT HYDRAULIC FAILURE ON APPROACH. HYD QTY AT .14 FOUND FLEX HYDRAULIC LINE DAMAGED AND HAS COME OFF FROM TAIL SKID LINEAR ACTUATOR. SEE PIC. FOUND THAT FWD SW
- [SDR CALA2026010812807](https://openairdocs.org/sdr/CALA2026010812807), Jan 6, 2026: GOVERNOR. FAULTED. RIGHT ENGINE WOULD NOT GO TO TAKEOFF THRUST WITH AUTO THROTTLE ENGAGED, REMOVED NR 2 ENGINE (PHASE 2) FUEL FLOW GOVERNOR MFG PART NR 8062-551 IAW AMM 73-21-01-0
- [SDR CALA2026010612699](https://openairdocs.org/sdr/CALA2026010612699), Jan 4, 2026: SMOKE DETECTOR. FALSE ACTIVATION. FWD LAV A FIRE ALARM WENT OFF IN CRUISE FOR 2 -3 MINUTES. NO SMOKE/FIRE INDICATIONS. STOPPED. VERIFIED NO INDICATIONS OF FIRE ON LAV A TRASH WAHL TEMP PLATE REC
- [SDR CALA2025111111106](https://openairdocs.org/sdr/CALA2025111111106), Nov 10, 2025: LAMP. INOPERATIVE. EMERGENCY LIGHTS OPS TEST WITH THE TEST SWITCH PROCEDURE, R4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-06-962-001-002. OPS CHEC
- [SDR CALA2025081507827](https://openairdocs.org/sdr/CALA2025081507827), Aug 15, 2025: LANYARD. UNPACKED. CHRONIC HISTORY OF DOOR 4-L DIFFICULT TO ARM PER CABIN CREW. LOG HISTORY SHOWS ISSUE IS CAUSED BY DOOR SLIDE LANYARD UNSECURE, HINDERING GIRT BAR MECHANISM ENGA
- [SDR CALA2025081807884](https://openairdocs.org/sdr/CALA2025081807884), Aug 14, 2025: WARNING LIGHT. FALSE ACTIVATION. DOOR 4L ARM LIGHT EXTINGUSHED ON TAXI OUT. DOOR 4 LEFT ARM AND DISARME DGIRT BAR SLIDERS INDICATED WHEN LEVER SET TO ARM AND DISARM. DOOR SLIDE LIGHT INCONSITEN
- [SDR CALA2025081407720](https://openairdocs.org/sdr/CALA2025081407720), Aug 12, 2025: GIRT BAR. OBSTRUCTED. L4 DOOR WILL NOT ARM. FOUND SLIDE STRING BLOCKING GIRT BAR MECHANISM. SECURED STRING ON L4 SLIDE IAW AMM 52-11-25. VERIFIED DOOR L4 SLIDE ARMS CORRECTLY.
- [SDR CALA2025081307676](https://openairdocs.org/sdr/CALA2025081307676), Aug 11, 2025: LANYARD. UNSECURE. DOOR 4L SLIDE LIGHT NOT ARMING REF AMM TASK 25-66-01-206-041. FOUND DOOR 4L LANYARD UNTUCKED FROM PACK ASSY. RETURNED LANYARD TO CORRECT POSITION, CLOSED AND AR
- [SDR CALA2025081207623](https://openairdocs.org/sdr/CALA2025081207623), Aug 9, 2025: LANYARD. UNSECURE. SLIDE LIGHT FOR DOOR 4L INOPERATIVE. FOUND LANYARD HANGING DOWN AND INTERFERING WITH GIRT BAR. RESTOWED LANYARD AND ARMED SLIDE. OPS CHECK GOOD. REF AMM 25-66-0
- [SDR CALA2025081207618](https://openairdocs.org/sdr/CALA2025081207618), Aug 9, 2025: LIGHT. NOT SEATED. SLIDE LIGHT FOR 4L DOOR INOPERATIVE. COMPLIED WITH MEL 2566N, PLACED INOP STICKER. VERIFIED DOOR 4L IN ARMED POSITION. RESEATED 4L DOOR LIGHT, OPS CHECK GOOD
- [SDR CALA2025080507306](https://openairdocs.org/sdr/CALA2025080507306), Aug 1, 2025: SENSOR. FAULTED. LEVEL 2 CHRONIC HISTORY OF DOOR 4L ARMING ISSUE WITH ARM LIGHT NOT ON WHEN DOOR ARMED. PERFORMED FIM 25-66 FAULT TREE 802 BOX 1, ENGAGEMENT LIGHT OK. OK TO CONT
- [SDR CALA2025080107192](https://openairdocs.org/sdr/CALA2025080107192), Jul 30, 2025: LIGHT. NO DISCREPANCY. L4 SLIDE LIGHT NOT TURNING ON WHEN ARMED. REPOSITIONED DOOR L4 BY OPENING AND CLOSING DOOR, SLIDE LIGHT ON, WHEN ARMED, OK FOR SERVICE.
- [SDR CALA2025073107143](https://openairdocs.org/sdr/CALA2025073107143), Jul 30, 2025: SENSOR. DIRTY. DOOR 4L KNUCKLE KNOCKER NOT COMING OUT AND SLIDE ARMED LIGHT NOT ILLUMINATING FOUND DOOR ARMING PROPERLY BUT MICROSWITCH THAT SENSES SIGNAL TO ARM LIGHT WAS CAK
- [SDR CALA2025080107191](https://openairdocs.org/sdr/CALA2025080107191), Jul 29, 2025: WARNING LIGHT. MALFUNCTIONED. DOOR MOUNTED ESCAPE SYSTEM DOOR 4L GIRT BAR ENGAGEMENT LIGHT OFF WITH EVACUATION SLIDE ARMING LEVER IN ARMED, ENGAGE POSITION AT ENTRY /SERVICE DOOR LIGHT EXTIN
- [SDR CALA2025072406871](https://openairdocs.org/sdr/CALA2025072406871), Jul 22, 2025: LIGHT. NO TEST. EMERGENCY LIGHTS OPS TEST WITH THE TEST SWITCH PROCEDURE. EMERGENCY LIGHT OUTSIDE OF DOOR 4R INOPERATIVE. RELAMPED, OPS GOOD IAW AMM 33-51-06-001-002. ONE SPACE
- [SDR CALA2025070706231](https://openairdocs.org/sdr/CALA2025070706231), Jul 2, 2025: LIGHT. DETACHED. SEAT 12C EMER EXIT PATH LIGHT HAS FALLEN OFF REPLACED EXIT PATH LIGHT BRACKET.REF AMM TASK33-51-05-402-030
- [SDR CALA2025070106109](https://openairdocs.org/sdr/CALA2025070106109), Jun 28, 2025: LANYARD. OUT OF POSITION. DOOR 4L SLIDE ARM LIGHT NOT ILLUMINATED WITH DOOR ARMED IN FLI GHT REMOVED L4 SLIDE COVER, PINNED SLIDE AND FOUND GREEN SURVIVAL LANYARD IN THE WAY OF GIRT BAR.
- [SDR CALA2025063006047](https://openairdocs.org/sdr/CALA2025063006047), Jun 26, 2025: SLIDE. NO DISCREPANCY. DOOR 2L WAS OPENED FROM THE OUTSIDE WHILE ARMED. DOOR DISARMED ITSELF. PERFORMED INSPECTION OF 2L DOOR AND SLIDE PACK, NO DEFECTS, CONFIRMED SLIDE WAS DISARMED 
- [SDR CALA2025061605554](https://openairdocs.org/sdr/CALA2025061605554), Jun 12, 2025: GOVERNOR. FAULTED. AT FL 350 EQUAL N1 + FF ENG 2 THROTTLE 2 KNOB W IDTHS AHEAD ENG1 THROTTL E INFORMATION FROM THE CREW IS AS FOLLOWS ; WITH AN ESTIMATED N1 OF 89 ON LEFT ENGINE A
- [SDR CALA2025051204611](https://openairdocs.org/sdr/CALA2025051204611), Apr 29, 2025: SKIN. DAMAGED. DOUBLER PREVENTATIVE MODIFICATION TO THE L1 DOOR SURROUND FWD UP PER CORNER WAS INSTALLED PER EA 5330-04213 REV D WITH DEVIATIONS NOTED IN EC/RA #: 5330-07520. 
- [SDR CALA2025032403119](https://openairdocs.org/sdr/CALA2025032403119), Mar 21, 2025: SLIDE. NOT REPORTED. SCHEDULED REMOVAL, RESTORE L3 DOOR ESCAPE SLIDES PER MFR CMM AND ANY UNITED SUPPLEMENTS. REMOVED AND REPLACED L3 DOOR ESCAPE SLIDE AND SECURED REF AMM 25-66-03.
- [SDR CALA2025012702061](https://openairdocs.org/sdr/CALA2025012702061), Jan 27, 2025: BULB. BURNED OUT. LEFT BULBS OF UNARMED LIGHT IS BURNED OUT. EMERGENCY LIGHTS RELAMPED.
- [SDR CALA2024121901574](https://openairdocs.org/sdr/CALA2024121901574), Dec 17, 2024: OVEN. FAULTY. OVEN 411 VERY DIRTY, HAS PLASTIC BURNING SMELL. REQUEST NEF FOR OVEN 411 IN AFT GALLEY. NOC DESK: 757 NAME: DATE: 17-DEC-24- APPROVED PLACED ON NEF. FOUND EXCES
- [SDR CALA2023071002199](https://openairdocs.org/sdr/CALA2023071002199), Jul 7, 2023: SKIN. DENTED. AIRCRAFT MOVE TEAM FOUND DENTS FWD OF THE L2 DOOR, DENT FOUND IS AROUND 84 INCHES FWD OF THE L2 DOOR ABOVE THE WATER LINE INBETWEEN STRINGER 15 AND 14. FURTHER 
- [SDR CALA2023052601671](https://openairdocs.org/sdr/CALA2023052601671), May 24, 2023: ACTUATOR. INOPERATIVE. RUDDER TRIM INOP IN FLIGHT STILL NO RESPONSE. CAPT ELECTED NOT TO OPERATE RUDDER TRIM REST M&E 99-2721-9-0005 AVAIL SFO. OF FLIGHT FROM CRUISE TO LANDING. A
- [SDR CALA2023011800146](https://openairdocs.org/sdr/CALA2023011800146), Jan 17, 2023: TRANSCEIVER. INOPERATIVE. HF 1 UNABL 2 TRNSMT 15 MIN AFTER TAKOFF HF2 UNABL TO TRNSMT 28MI N AFTER TAKOFF 3) REPLACE BOTH COUPLERS AS PRECAUTIONARY. DUE TO HISTORY OF HF ISSUES, PLS PERF
- [SDR CALA2022080101930](https://openairdocs.org/sdr/CALA2022080101930), Aug 1, 2022: BATTERY PACK. INOPERATIVE. DOOR 3 EMER EXIT LGTS INOP REPLACED BATTERY PACKS OVER DOORS 4LEFT & 4RIGHT.
- [SDR CALA2022062001541](https://openairdocs.org/sdr/CALA2022062001541), Jun 20, 2022: HYDRAULIC SYSTEM. INOPERATIVE. HYD SYSTEM REMAINED AT .25 AND HELD THERE UNTIL GEAR EXTENSION A ND DROP THEN TO .10 AND THAT AND RPR OF HYD LOSS. FOUND LH HYD QTY AT 2 GALS - SERVICED WITH 3 
- [SDR CALA2022050601156](https://openairdocs.org/sdr/CALA2022050601156), May 5, 2022: HARNESS. DAMAGED. LEFT BUSS OFF LIGHT ILLUMINATED ACCOMPANIED BY ISLN LIGHT ON LEFT BUSS TIE SWITCH AND LEFT GEN OFF LIGHT ALSO ILLUMINATED. CREW STATES THE LEFT GEN RESET ONCE S
- [SDR CALA2021063001004](https://openairdocs.org/sdr/CALA2021063001004), Jun 30, 2021: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS (USING CONTROL SWITCHES) OPERATIONAL CHECK - LEFT HAND INTERIOR OVERWING EMERGENCY EXIT SIGN LIGHT IS INOP., AS WELL AS THREE EMERGENCY LIGHTS 
- [SDR CALA2018101502120](https://openairdocs.org/sdr/CALA2018101502120), Oct 15, 2018: GCU. INOPERATIVE. EICAS WENT BLANK AFTER T/O THEN R HYD ELEC PUMP AUTOTHROTTLE DISC FOUND C/B OPEN/POPPED, P31 L GEN PWR PNL. CB 115 VAC BUS L, SECT 1. C/B RESET, BUT NO TIME TO 
- [SDR CALA2018100802066](https://openairdocs.org/sdr/CALA2018100802066), Oct 7, 2018: LIGHT. INOPERATIVE. SUPPORT TASK - EMERGENCY LIGHTS INOP ON BULLNOSE AT ROWS 3, 25, 31, 34 RT AND 17, 33 LT. REF NR 99824640. ITEM WAS ACCOMPLISHED ON 44.0008 SEE ATTACHED COPY. RE
- [SDR CALA2018022300766](https://openairdocs.org/sdr/CALA2018022300766), Feb 23, 2018: LIGHT. UNKNOWN. L1 DOOR SLIDE ARMED LIGHT NOT ON, WITH DOOR ARMED. RESET THE DOOR ARMING HANDLE, INSPECTED DOOR GIRT BAR FOR DEBRIS, AND MECHANICAL CONNECTION OF GIRT BAR. DOOR
- [SDR CALA2018021600619](https://openairdocs.org/sdr/CALA2018021600619), Feb 16, 2018: AIR DATA MODULE. FAULTY. UNRELIABLE AIRSPEED AT FL260.EICAS IAS UNRELIABLE WITH L MACH .79 RMACH IAS L/R 327/347. EMERGENCY DECLARED. REMOVED AND REPLACED THE ADM IAW AMM 34-26-03-004-0
- [SDR CALA2018010500058](https://openairdocs.org/sdr/CALA2018010500058), Jan 5, 2018: BATTERY. INOPERATIVE. FLASHLIGHT AT THE L4 DOOR NOT BLINKING. REPLACED THE FLASHLIGHT BATTERY.
- [SDR CALA2017112704229](https://openairdocs.org/sdr/CALA2017112704229), Nov 27, 2017: GIRT BAR. BENT. L4 DOOR GIRT BAR LEAF SPRING INSPECTION FOUND THE SLIDE GIRT BAR FWD LEAF SPRING BENT NOT ALLOWING SLIDER FULL ENGAGMENT AND CAM TO CENTER. REMOVED THE GIRT BAR
- [SDR CALA2017091103144](https://openairdocs.org/sdr/CALA2017091103144), Sep 11, 2017: CONTACT. DIRTY. L1 DOOR SLIDE ARMED LIGHT GOES ON AND OFF INTERMITTENTLY. CLEANED THE SLIDE LIGHT CONTACTS. CHECKED OK.
- [SDR CALA2017090803087](https://openairdocs.org/sdr/CALA2017090803087), Sep 8, 2017: SWITCH. NO TEST. EMERGENCY LIGHTS WILL NOT TEST WITH PUSH BUTTON AT THE L1 DOOR. REMOVED AND REPLACED THE SWITCH S10292 IAW WDM 33-51-01. OPS CHECKED GOOD.
- [SDR CALA2017082102828](https://openairdocs.org/sdr/CALA2017082102828), Aug 21, 2017: GIRT BAR. DIRTY. F/A REPORTED THE L2 DOOR SLIDE ARMED LIGHT WAS ARMED AND NOW ARMING LIGHT IS NOT ILLUMINATED WHILE AIRBORNE. CLEANED AND LUBRICATED THE GIRT BAR FITTINGS, OPS T
- [SDR CALA2017081102616](https://openairdocs.org/sdr/CALA2017081102616), Aug 11, 2017: LATCH. OUT OF ADJUST. L2 DOOR SLIDE ARMING LEVER CATCHES, HAD TO TRY TO ARM A FEW TIMES FOR THE ARM LIGHT TO ILLUMINATE. ADJUSTED AND SYS TESTED GIRT BAR MECHANISM IAW AMM 52-11-25-7
- [SDR CALA2017072802416](https://openairdocs.org/sdr/CALA2017072802416), Jul 28, 2017: LIGHT. LOOSE. RT AFT OVER WING EMERGENCY LIGHT INOP. FOUND LAMP LOOSE. RELAMPED WITH NEW BULB OPS CHK OKAY.
- [SDR CALA2017063002036](https://openairdocs.org/sdr/CALA2017063002036), Jun 30, 2017: LATCH. UNSECURE. R4 DOOR SLIDE COVER NOT SECURE, FOUND THE LT BUSTLE LATCH UNSECURE. LATCH CONDITION OK. SECURED THE LATCH.
- [SDR CALA2017051901502](https://openairdocs.org/sdr/CALA2017051901502), May 19, 2017: LIGHT. OUT OF ADJUST. 1L EMERGENCY SLIDE LIGHT WILL NOT ILLUMINATE WHEN ARMED. ADJUSTED LIGHT, OP CKD NORMAL PER 33-10-00.
- [SDR CALA2017042801178](https://openairdocs.org/sdr/CALA2017042801178), Apr 28, 2017: SWITCH. DIRTY. DOOR 1L SLIDE LIGHT DOES NOT ILLUMINATE WITH DOOR ARMED CLEANED L1 DOOR SLIDE GIRT BAR PROX SWITCH. OPS CKS GOOD REF AMM 25-66-11-822-011. OK TO CONTINUE.
- [SDR CALA2016100700734](https://openairdocs.org/sdr/CALA2016100700734), Oct 7, 2016: SWITCH. INOPERATIVE. L2 DOOR SLIDE LIGHT INOPERATIVE. REPLACED L2 ARMING DOOR LIGHT SWITCH IAWAMM 25-66-11 OPS CHECKED GOOD .
- [SDR CALA2015081400677](https://openairdocs.org/sdr/CALA2015081400677), Aug 14, 2015: UNKNOWN. ODOR. JUST CLIMBING OUT FROM AIRPORT, FLIGHT ATTENDANT CALLED STRONG ELEC SMELL, AFT GALLEY. RETURNED TO AIRPORT & PERFORMED SMOKE & ODOR INSPECTION IAW AMM 05-57-58-
- [SDR CALA2013020100073](https://openairdocs.org/sdr/CALA2013020100073), Jan 28, 2013: SKIN. DENTED. ACFT DAMAGE FOUND ON ARRIVAL 30 INCHES AFT OF DOOR 4L AND 12 INCHES BELOW DOOR SILL INDENTATION AT BS 1710 BELOW STRINGER S15AL EXCEEDS SERVICEABLE LIMITS OF SR
- [SDR CALA2012051100342](https://openairdocs.org/sdr/CALA2012051100342), May 11, 2012: CONTROL UNIT. INOPERATIVE. F/A SMELLED BURNING ELEC ODOR AND NOTICED SMOKE COMING OUT OF CELLING IN FWD GALLEY AREA NEAR CEILING LIGHT, F/A SHUT OFF VIDEO SYS, SMOKE WENT AWAY. SMOKE FROM
- [SDR CALA2011121500811](https://openairdocs.org/sdr/CALA2011121500811), Dec 14, 2011: SKIN. CRACKED. SUPPORT TASK - LEFT WING TOP SKIN AND RISER CRACKED AT WS 211.59 STRINGER U12. LEFT WING TOP SKIN AND RISER CRACKED AT WS 211.5 BW STR U12 REPLACED AS PER SRM 5
- [SDR CALA2011111500742](https://openairdocs.org/sdr/CALA2011111500742), Nov 15, 2011: TRANSDUCER. INOPERATIVE. AUTOTHROTTLE FAILED TO ENGAGE DURING TAKEOFF. CHKD & PLACARD THE AUTOTHROTTLE SERVO INOP PER MEL 22-30-01-1. COMPLIED WITH DDP. AIRCRAFT STATUS CAT III LAND

## 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 N77871

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N77871 before.

- [Cancelled 1949-02-23](https://openairdocs.org/deregistered/N77871-1949-02-23): Luscombe 8A, S/N 3598. Owner: [Paul J Rennard](https://openairdocs.org/faa-owner/PAUL%20J%20RENNARD), [Oil City, PA](https://openairdocs.org/faa-place/PA/Oil%20City)

## 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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