# N77867: 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: 32592
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 1, 2002
- Certificate issued: September 29, 2023
- Expires: September 30, 2030
- Mode S code: AA8A09
- 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=77867
- Page: https://openairdocs.org/aircraft/N77867

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/N77867/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 N77867.

## 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 20090426010849I](https://openairdocs.org/incident/20090426010849I), Apr 26, 2009: Boeing 75733N (N77867), Newark, NJ, No damage. (-23) On take off from Newark Liberty airport (kewr) at approximately 800' AGL the left engine on N77867 a Continental airlines B757 had a contained engine…

## Service difficulty reports (85, 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 CALA2026062217223](https://openairdocs.org/sdr/CALA2026062217223), Jun 21, 2026: BALLAST. INOPERATIVE. CONTROL CABIN AND PASSENGER CABIN VISUAL INSPECTION. SIDEWALL LIGHT FOR AFT OVERWING EMERGENCY EXIT. INOP RELAMPED NO HELP, REPLACED BALLAST FOR R/H AFT OVERWIN
- [SDR CALA2026041915471](https://openairdocs.org/sdr/CALA2026041915471), Apr 17, 2026: FERRULE. INOPERATIVE. DOOR 4R EXTERIOR EMERGENCY LIGHT (SLIDE LIGHT) INOP REPLACED SLIDE LIGHT BULB REF AMM 33-51-06 NO HELP. UPON FURTHER INSPECTION NOTICED LIGHT ASSY/ LENS HOLDER 
- [SDR CALA2026032414803](https://openairdocs.org/sdr/CALA2026032414803), Mar 21, 2026: OVEN. ODOR. OVEN 205 HAD BAD ODER OF BURNT ELECTRIC. TURNED OFF AND SMELL DISSIPATED. DEBRIEFED FLIGHT CREW AND FLIGHT ATTENDANTS TO CONFIRM SOURCE WAS OVEN 205 IN FWD GALL
- [SDR CALA2026032014713](https://openairdocs.org/sdr/CALA2026032014713), Mar 19, 2026: CONTROLLER. FAULTED. CABIN ALTITUDE DECREASIN G AT FL 210 POSSIBLE LEAK SEE L/P 8233584, 8236201, 8231369 AND 8236285 FOR FINDINGS, INSPECTIONS AND OPERATIONAL CHECKS. UPDATE REF CO
- [SDR CALA2026031814658](https://openairdocs.org/sdr/CALA2026031814658), Mar 16, 2026: CLAMP. MISSING. LEFT PACK UNABLE TO MAINTAIN CABIN ALTITUDE BELOW 10000FT AT FL330 LOCKED DUE TO CREW DECLARED EMERGENCY. DURING PRESSURIZATION CHECKS NOTICED THAT THE CABIN AI
- [SDR CALA2026011412945](https://openairdocs.org/sdr/CALA2026011412945), Jan 12, 2026: TARGET. LOOSE. FLIGHT DECK DOOR LOCK SENSOR IMPEDES DOOR CLOSURE. FOUND TARGET LOOSE. ADJUSTED TARGET ON DOOR AND SECURED IAW AMM 52-52-01-000-801. VERIFIED OPS CHECK OF DOOR 
- [SDR CALA2025100109485](https://openairdocs.org/sdr/CALA2025100109485), Sep 30, 2025: SLIDE. NO DISCREPANCY. SLIDE PRESSURE GAUGE DOOR 4R TOUCHES RED ZONE NEEDLE IS VISIBLE AND WITHIN LIMITS.OK TO CONT.
- [SDR CALA2025081807890](https://openairdocs.org/sdr/CALA2025081807890), Aug 15, 2025: INDICATOR. OBSTRUCTED. DOOR 3L SLIDE WOULD NOT ARM ADJUSTED LOWER LINER DOOR 4L KNUCKLE KNOCKER AS REQUIRED. KNUCKLE KNOCKER WAS HITTING ON LOWER LINER ADJUSTED LINER IN IAW AMM 52-11
- [SDR CALA2025080807478](https://openairdocs.org/sdr/CALA2025080807478), Aug 6, 2025: INDICATOR. INOPERATIVE. TEST FLIGHT DISCREPANCY, DOOR 4R ARMED INDICATOR FLAPPER STICKS AND DOES NOT SHOW ARMED W ITH DOOR ARMED. REPOSITIONED MID LINING TO MAKE CLEARANCE SO THAT INDI
- [SDR CALA2025080507323](https://openairdocs.org/sdr/CALA2025080507323), Aug 1, 2025: KEELBEAM. CORRODED. KEELBEAM CORRODED AT S-29R AT STA 1405-1414. SEE EC/RA 5360-01994 FOR WORK PERFORMED.
- [SDR CALA2025080507322](https://openairdocs.org/sdr/CALA2025080507322), Aug 1, 2025: FRAME. CORRODED. AFT CARGO COMPT FUSELAGE FRAME CORRODED BS 1420 BETWEEN S30 AND S29R. THE FRAME WAS REPLACED,
- [SDR CALA2025080507320](https://openairdocs.org/sdr/CALA2025080507320), Jul 29, 2025: FRAME. CORRODED. AFT CARGO, STRINGER S29R, BS 1424 FRAME IS CORRODED UNDER LEVELING COMPOUND AT RIVET. FRAME WAS REPLACED IAW DRAWINGS 146N3100 AND 146N3300.
- [SDR CALA2025080507319](https://openairdocs.org/sdr/CALA2025080507319), Jul 29, 2025: FRAME. CORRODED. AFT CARGO FRAME BS 1440 HAS CORROSION IN SEVERAL PLACES.
- [SDR CALA2025040403520](https://openairdocs.org/sdr/CALA2025040403520), Apr 3, 2025: BOTTLE. DEFECTIVE. RH ESCAPE SQUIB LIGHT TEST NO.2 WILL NOT ILLUMINATEPICTURE ADDED TS PER TSM 25-65 FAULT TREE 803. REPLACED M32 SQUIB TEST PANEL. NO HELP RE INSTALLED ORIGINAL P
- [SDR CALA2025030302538](https://openairdocs.org/sdr/CALA2025030302538), Feb 28, 2025: LAMP. INOPERATIVE. MED #2 L EMERGENCY LIGHT (EXTERIOR) WAS FOUND INOP ON #2 SVC CHECK. RELAMPED SLIDE LT REF AMM 33-51-06. OPC GOOD. NO FURTHER DEFECTS NOTED.
- [SDR CALA2025011301879](https://openairdocs.org/sdr/CALA2025011301879), Jan 9, 2025: INDICATOR. BROKEN. UNARMED ANNUNCIATOR LIGHT ON EMERGENCY LIGHT PANEL BROKE OFF REMOVED EMERGENCY LIGHTS/PASSENGER OXIGEN CONTROL PANEL REF AMM 33-51-08-404-011. REPLACED UNARMED 
- [SDR CALA2024121001465](https://openairdocs.org/sdr/CALA2024121001465), Dec 8, 2024: BULB. INOPERATIVE. OVERHEAD PANEL EMER LIGHTS UNARMED ONE BULB INOP REPLACED EMER LIGHTS UNARMED BULB.
- [SDR CALA2024112701320](https://openairdocs.org/sdr/CALA2024112701320), Nov 22, 2024: SKIN. DENTED. FOUND REPAIR SKIN DOUBLER DENTED APPROXIMATELY 6 FT FWD OF DOOR #2L. DENTED DOUBLER IS LIFTING AFT UPPER AND LOWER CORNERS OF DOUBLER AND DRAWING SKIN INTO DENT
- [SDR CALA2024112701319](https://openairdocs.org/sdr/CALA2024112701319), Nov 22, 2024: STRINGER. BENT. STRINGER 16LH BENT AT STATION 613-618 REQUIRES REPAIR FOUND WHILE WORKING SKIN DAMAGE ON LOG PAGE 9913805ORIGINAL STRINGER MATERIAL IS. 0.063 7075-T6 PER SRM 53
- [SDR CALA2024112101224](https://openairdocs.org/sdr/CALA2024112101224), Nov 19, 2024: PACKING. TORN. AT CRUISE ALT R ENG OVHT EICAS. QRH EXECUTED EICAS GONE WITH RT THROTTLE IDLE.AT ALTITUDE R ENG OVHT MESSAGE APPEARED. N1 SHOWED SLIGHT SPLIT WITH ENG 1 AT 93 A
- [SDR CALA2024112001206](https://openairdocs.org/sdr/CALA2024112001206), Nov 18, 2024: LIGHT. MALFUNCTIONED. SLIDE RAFT LIGHT ON DOOR 4L WENT OFF AFTER TAKEOFF. DID OPERATION CK OF 4L ESCAPE SLIDE ARMING LIGHT, INDICATION FUNCTIONS NORMALLY AMM25-66-00.
- [SDR CALA2024092700701](https://openairdocs.org/sdr/CALA2024092700701), Sep 25, 2024: ADI. MALFUNCTIONED. CAP AND FO ADI AND NAV DISPLAYS FLICKER WITH WX AND TERR INTERMI TTANT FAILURES ITEM LOCKED DUE TO HISTORY. FROM TECH SUPPORT ADVICE, R&R LOW FLOW SENSOR REF AM
- [SDR CALA2024012300182](https://openairdocs.org/sdr/CALA2024012300182), Jan 22, 2024: BATTERY PACK. INOPERATIVE. STA 351 WL 289 RBL 1 , MOUNTED ON CEILING PANEL JUST TO RIGHT OF THE FWD ENTRY LIGHT PANEL, EMERGENCY LIGHT EXIT INOP. REMOVED AND REPLACED BATTERY PACK M730 IA
- [SDR CALA2024012200164](https://openairdocs.org/sdr/CALA2024012200164), Jan 19, 2024: FRAME. CRACKED. EA5311-01827 REV E OP 002 FRAME 1640 R/H SIDE, HAS A SMALL CRACK ON THE FRAME INNER CHORD FLANGE BY THE INNER CHORD STRAP AREA LOCATED JUST BELOW S-14R. ELB REP
- [SDR CALA2024012200163](https://openairdocs.org/sdr/CALA2024012200163), Jan 18, 2024: SKIN. CRACKED. R/H OUTBOARD MAIN FLAP OUTBOARD LOWER SKIN CRACK REPAIR ON ST ENGINEERING NON ROUTINE 86900 AS PER SRM 57-53-01-2R-4 REPAIR 4 REQUIRES DIP TO REINSPECT BLIND FA
- [SDR 2023FA0000544](https://openairdocs.org/sdr/2023FA0000544), Sep 15, 2023: CASE. CRACKED. DURING INDUCTION AT STANDARDAERO, SAN ANTONIO FOR A SHOP VISIT. A CRACK OF APPROXIMATELY 4.5" WAS FOUND IN THE REAR FAN CASE AT THE 12 O'CLOCK POSITION AFT OF T
- [SDR CALA2023030300619](https://openairdocs.org/sdr/CALA2023030300619), Mar 3, 2023: WIRE. NONE. TO CONFIG SPEED BRK ON TO ROLL. WORKED ON TO CONFIG CHK ON WAY OUT...NOT AFTER LOCKING L/P UNLOCKED FOR UPDATE. PERFORMED CHECK FOR A GROUND ON PIN 12 OF D117, 
- [SDR CALA2022082402169](https://openairdocs.org/sdr/CALA2022082402169), Aug 22, 2022: SKIN. DENTED. SUPPORT TASK LEFT WING OB FWD FLAP UPPER SKIN HAS DENTS AS MARK TRANSCRIBED FROM HAECO GSO NR 9286084 EVALUATED, REMOVED DAMAGE AND REPAIRED AND RESTORED FINSIH
- [SDR CALA2022080501956](https://openairdocs.org/sdr/CALA2022080501956), Aug 4, 2022: ENGINE. NONE. *THIS IS A SUPPLEMENTAL REPORT TO THE ORIGINAL REPORT, WITH THE SAME CONTROL NUMBER, CIRCULATED ON 08/08/2022*. R ENG OVHT EICAS AND LIGHT. CHECKLIST COMPLETE E
- [SDR CALA2022080101929](https://openairdocs.org/sdr/CALA2022080101929), Jul 31, 2022: NONE. NONE. THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 8/01/22. AFTER LANDING DURING TAXI IN SMOKE IN FLIGHT DECK AND IN CABIN SMELLED OF OIL.PE
- [SDR CALA2022080101924](https://openairdocs.org/sdr/CALA2022080101924), Jul 31, 2022: ENGINE. UNKNOWN. SMOKE SEEN AROUND RIGHT ENGINE WE THEN SHUT THE ENGINE DOWN SMOKE STOPPED
- [SDR CALA2022070801674](https://openairdocs.org/sdr/CALA2022070801674), Jul 8, 2022: ENGINE. WARNING MESSAGE. FL380 R ENG OVHT EICAS. REDUCED PWR HALF AND SHUT ENG BLD VALVE W NO EFF ECT. WENT IDLE W RT TH. T/S IN PROGRESS.
- [SDR CALA2022030700607](https://openairdocs.org/sdr/CALA2022030700607), Mar 7, 2022: PITOT HEAD. FOD. *EMERGENCY DECLARED* HAD AIRSPEED DISAGREE ON TAKEOFF. APPEARED TO BE CAPT SIDE THAT WAS IN ERROR. SWITCHED SOURCE BACK TO ''L'', THEN CAPT SD AIRSPEED IND WAS 
- [SDR CALA2021042800551](https://openairdocs.org/sdr/CALA2021042800551), Apr 27, 2021: PSU. NO TEST. REFERENCING THE FOLLOWING L/P #''S FOR PASSENGER SERVICE UNITS FAILING TO OPEN CORRECTLY DURING TEST, CORRECTIVER ACTION AND REPAIR CONFIMRATION. 6202091 620209
- [SDR CALA2021041400450](https://openairdocs.org/sdr/CALA2021041400450), Apr 12, 2021: SIGN. INOPERATIVE. SUPPORT TASK: EMERGENCY LIGHTING AT L2 DOOR INOP ON TEST TROUBLESHOT EMERGENCY LIGHT AT L2 DOOR IAW B757-300 AMM 33-51-00 AND B757-300 WDM 33-51-21 PG 104 AND F
- [SDR CALA2021040500427](https://openairdocs.org/sdr/CALA2021040500427), Apr 3, 2021: CONNECTOR. DETERIORATED. B757-20-3-0039 CONNECTOR D835 AND D3975 AT ELEVATOR FEEL COMPUTE R BOTH FAIL LOOP RESISTANCE TESTER PER AMM 20-55-44. FOUND BOTH CONNECTORS DETERIORATED. REPLAC
- [SDR CALA2021040100410](https://openairdocs.org/sdr/CALA2021040100410), Mar 31, 2021: FRAME. CORRODED. SUPPORT TASK: AFT PIT UNDERFLOOR FRAME AT STA 1460 CORRODED ON F WD AND AFT SIDES. REF HAECO GSO NR 9281011 ACCOMPLISHED REPAIR OF AFT CARGO UNDERFLOOR FRAME AT
- [SDR CALA2021040100409](https://openairdocs.org/sdr/CALA2021040100409), Mar 31, 2021: FLOOR SUPPORT. CORRODED. B757-53-3-0553; MAIN CABIN FLOOR LONGITUDINAL FLOOR SUPPORT CORR ODED AT BS 365 RBL 24 REF HAECO GSO NR 9281476 REMOVED CORROSION ON FLOOR SUPPORT IAW B757-300 
- [SDR CALA2021040100408](https://openairdocs.org/sdr/CALA2021040100408), Mar 31, 2021: FRAME. CORRODED. AFT CARGO UNDERFLOOR FRAME AT STA. 1540 CORRODED. REF. HAECO GS O NR 9281018 ACCOMPLISHED REPAIR OF AFT CARGO UNDERFLOOR FRAME AT STA 1540 ST R S28R-S30 IAW ECR
- [SDR CALA2021040100407](https://openairdocs.org/sdr/CALA2021040100407), Mar 31, 2021: FLOORBEAM. CORRODED. B757-53-3-0553 FLOOR BEAM BS 365.25 BL 0 - RBL 60 HAS CORROSION REF HAECO GSO NR 9281269 REPAIRED FLOOR BEAM AT BS 365.25 LBL 10 - RBL 70 PR B757 SRM 53- 00-51 
- [SDR CALA2021032200359](https://openairdocs.org/sdr/CALA2021032200359), Mar 21, 2021: FLOOR SUPPORT. CORRODED. B757-53-3-0553 FLOOR SUPPORT BETWEEN BS365 AND BS377 RBL 61 HAS CORROSION REF HAECO GSO NR 9281272 REMOVED CORROSION FROM FITTING IAW B757-300 SRM 51-10-02. ORI
- [SDR CALA2021032200358](https://openairdocs.org/sdr/CALA2021032200358), Mar 21, 2021: FLOORBEAM. CORRODED. B757-53-3-0551 FLOOR BEAM 377.7 BL0-LBL24 HAS CORROSION. REPAIRED FLOORBEAM AT BS 377.7 BL0-LBL59 PER B757 SRM 53-00-51 R EPAIR 10 DWG 141N5161 REV AG. REF HAEC
- [SDR CALA2021032200351](https://openairdocs.org/sdr/CALA2021032200351), Mar 19, 2021: FLOORBEAM. CORRODED. B757-53-0579 FLOOR BEAM UPPER SURFACE BS1640 RBL48 - RBL54 HAS L IGHT CORROSION AROUND FASTENER HOLES. REF HAECO GSO NR 9281256 REPAIRED FLOORBEAM AT BS 1640 PE
- [SDR CALA2021032200350](https://openairdocs.org/sdr/CALA2021032200350), Mar 19, 2021: SUPPORT. CORRODED. SUPPORT TASK: L2 DOOR DRAIN SUPPORT HAS CORROSION REF HAECO GSO NR 9281720 REMOVED CORROSION FROM L2 DOOR UPPER CHORD, TOTAL MATERIAL LOSS .012 OUT OF LIMITS IA
- [SDR CALA2021031900332](https://openairdocs.org/sdr/CALA2021031900332), Mar 17, 2021: FLOORBEAM. CORRODED. B757-53-3-0551 FLOOR SUPPORT BS 338 LBL24 HAS CORROSION. REF H AECO GSO NR 9281263
- [SDR CALA2021031600323](https://openairdocs.org/sdr/CALA2021031600323), Mar 16, 2021: FLOORBEAM. CORRODED. B757-53-3-0579 RH OTBD FLOORBEAM HAS LIGHT CORROSION AT BS1640 RB 44 - RBL 46 REF HAECO GSO NR 9281257 CLEANED AREA ON FLOORBEAM AT BS1640 RBL 44-46 REMOVED .02
- [SDR CALA2021031200312](https://openairdocs.org/sdr/CALA2021031200312), Mar 11, 2021: FLOOR SUPPORT. CORRODED. B757-53-3-0551 FLOOR SUPPORT BS338 LBL22 HAS CORROSION REF HAE CO GSO NR 9281262 BLENDED AREA ORIGINAL .050" REMOVED .027 REMAINING .023 FOUND TO BE OUT OF LIMI
- [SDR CALA2021031000284](https://openairdocs.org/sdr/CALA2021031000284), Mar 9, 2021: SKIN. DENTED. SUPPORT TASK - LEFT WING #3 SLAT SKIN IS DENTED AT O/B AUX TRACK ACCOMPLISHED DOUBLER REPAIR OF #3 SLAT IAW B757-300 SRM 57-43-01, REPAIR 8, FIG 201. PAGE 206 N
- [SDR CALA2021030300249](https://openairdocs.org/sdr/CALA2021030300249), Mar 1, 2021: SHEAR TIE. CORRODED. SUPPORT TASK: AFT CARGO STA 1440, FWD AND AFT SIDE ATTACH BRACKE TS CORODED S28R-S29R RECEIVED MAT ID FOR -7 AND -8 SHEAR TIES 7075-0 BARE ALUM IAW BA C WG #146
- [SDR CALA2021030100248](https://openairdocs.org/sdr/CALA2021030100248), Feb 28, 2021: FRAME. DENTED. B757-53-3-0496: STA 600 FWD CARGO COMPARTMENT LWR SUPPORT HAS A DENT BETWEEN S25L AND S26L ACCOMPLISHED STA 600 FRAME REPAIR REF EC 5330-06798 PT 1. DIP REQUIRE

All 85: https://openairdocs.org/aircraft/N77867/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 N77867

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N77867 before.

- [Cancelled 1971-03-22](https://openairdocs.org/deregistered/N77867-1971-03-22): Luscombe 8A, S/N 3594, built 1946. Owner: [Burbank Elizabeth B](https://openairdocs.org/faa-owner/BURBANK%20ELIZABETH%20B), [Ely, VT](https://openairdocs.org/faa-place/VT/Ely)

## 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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