# N73860: 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: 32584
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 4, 2001
- Certificate issued: November 17, 2023
- Expires: November 30, 2030
- Mode S code: A9EC06
- 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=73860
- Page: https://openairdocs.org/aircraft/N73860

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/N73860/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 N73860.

## FAA accident and incident reports

None matched to N73860.

## Service difficulty reports (60, 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 CALA2026060416824](https://openairdocs.org/sdr/CALA2026060416824), Jun 3, 2026: RIB. DAMAGED. NR 3 SLAT OTBD MAIN TRACK UPPER SUPPORT RIB DAMAGED. REMOVED AND REPLACED RIB IAW SRM 51-40-02 AND DWG 114N2165 REV C.
- [SDR CALA2026060416822](https://openairdocs.org/sdr/CALA2026060416822), Jun 3, 2026: RIB. DAMAGED. NR 3 SLAT OB MAIN TRACK LE ON RIB IS DAMAGED. REMOVED AND REPLACED RIB PER SRM 51-40-02 AND BAC DWG 114N2165, REV C.
- [SDR CALA2026052916648](https://openairdocs.org/sdr/CALA2026052916648), May 27, 2026: BATTERY PACK. INOPERATIVE. R1 DOOR INTERIOR & EXTERIOR EMERGE3NCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M730 IAW B757 AMM 33-51-07. OPS CHECK GOOD.
- [SDR CALA2025112611488](https://openairdocs.org/sdr/CALA2025112611488), Nov 22, 2025: FAN. FAULTED. OVERHEAT LIGHT FLICKERED SEVERA. TIMES WITH FAINT ELEC ODOR ALTN SELECTED. LIGHT EXTINGUISHED SMELL WENT AWAY. CREW REPORTS IN ALT MODE SYSTEM WORKS NORMAL. WIT
- [SDR CALA2025101410049](https://openairdocs.org/sdr/CALA2025101410049), Oct 12, 2025: D-RING. UNSECURE. DOOR 2L SLIDE RAFT D RING CONNECTION POINT NEEDS TO BE RESECUR ED FOUND D RING STRAP TUCKED AND HANGING BEHIND BUSTLE. RESECURED D RING ON VELCRO MOUNTING POINT
- [SDR CALA2025100209555](https://openairdocs.org/sdr/CALA2025100209555), Oct 2, 2025: BOTTLE. NO DISCREPANCY. SAFETY PIN INSTALLED AT R4 DOOR EMERGENCY ASSIT BOTTLE AND SLIDE PACK FOR MX REMOVED SAFETY PIN AT R4 DOOR EMERGENCY ASSIT BOTTLE AND SLIDE PACK. OK FOR SERVICE
- [SDR CALA2025100209544](https://openairdocs.org/sdr/CALA2025100209544), Oct 2, 2025: SLIDE. NO DISCREPANCY. SAFETY PIN INSTALLED AT R2 DOOR EMERGENCY ASSIT BOTTLE AND SLIDE PACK FOR MX REMOVED SAFETY PIN AT R2 DOOR EMERGENCY ASSIT BOTTLE AND SLIDE PACK. OK FOR SERVICE
- [SDR CALA2025100209543](https://openairdocs.org/sdr/CALA2025100209543), Oct 2, 2025: PIN. INSTALLED. SAFETY PIN INSTALLED AT L1 DOOR EMERGENCY ASSIT BOTTLE AND SLIDE PACK FOR MX. REMOVED SAFETY PIN AT L1 DOOR EMERGENCY ASSIT BOTTLE AND SLIDE PACK. OK FOR SERVIC
- [SDR CALA2025100209541](https://openairdocs.org/sdr/CALA2025100209541), Oct 2, 2025: PIN. INSTALLED. SAFETY PIN INSTALLED AT R1 DOOR EMERGENCY ASSIT BOTTLE AND SLI DE PACK FOR MX REMOVED SAFETY PIN AT L1 DOOR EMERGENCY ASSIT BOTTLE AND SLIDE PACK. OK FOR SERVIC
- [SDR CALA2025100209539](https://openairdocs.org/sdr/CALA2025100209539), Oct 2, 2025: PIN. INSTALLED. SAFETY PIN INSTALLED AT L4 DOOR EMERGENCY ASSIT BOTTLE AND SLI DE PACK FOR MX REMOVED SAFETY PIN AT L4 DOOR EMERGENCY ASSIT BOTTLE AND SLIDE PACK. OK FOR SERVIC
- [SDR CALA2025100209538](https://openairdocs.org/sdr/CALA2025100209538), Oct 2, 2025: PIN. INSTALLED. SAFETY PIN INSTALLED AT L2 DOOR EMERGENCY ASSIT BOTTLE AND SLIDE PACK FOR MX REMOVED SAFETY PIN AT L2 DOOR EMERGENCY ASSIT BOTTLE AND SLIDE PACK. OK FOR SERVICE
- [SDR CALA2025072506914](https://openairdocs.org/sdr/CALA2025072506914), Jul 21, 2025: BULB. INOPERATIVE. EMER LIGHTS UNARMED LIGH T NEED RELAMPED ONE BULB OUT ON EMERGENCY LIGHT UNNARMED ON OVERHEAD PANEL IN FLIGHTDECK. REJECTED RELAMPED EMERGENCY LIGHT UNARMED LIG
- [SDR CALA2025062605904](https://openairdocs.org/sdr/CALA2025062605904), Jun 23, 2025: SEAT. WORN. ON TAKEOFF ROLL CA SEAT SLID FULLY AFT. REPLACED CAPTAIAN SEAT PER AMM25-11-01-000-801.
- [SDR CALA2025040703564](https://openairdocs.org/sdr/CALA2025040703564), Mar 30, 2025: LAMP. INOPERATIVE. EMERGENCY EXIT SIGN BY ROW 21+22 NOT FLUSH AND BURNED-OUT BULB 21&22 A SIDEWALL LIGHT INOP PLACED ON MEL 3321B. OK TO PLACE THE ADJACENT TWO SIDEWALL LIGHTS ON 
- [SDR CALA2025021702345](https://openairdocs.org/sdr/CALA2025021702345), Feb 14, 2025: UNKNOWN. ODOR. BURNING SMELL AROUND ROW 30. UNABLE TO LOCATE SOURCE. PERFOMED INSPECTION TASK 05-51-58-910-C1. FOUND NO SMOKE OR SMOKE ODER.
- [SDR CALA2025021102283](https://openairdocs.org/sdr/CALA2025021102283), Feb 10, 2025: LAMP. FAULTY. EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - TWO INCANDESCENT SIDEWALL EMERGENCY LIGHTS INOP ABOVE RH AFT OVERWING EMERGENCY EXIT RELAMP
- [SDR CALA2024100100737](https://openairdocs.org/sdr/CALA2024100100737), Sep 29, 2024: CIRCUIT BREAKER. FAULTY. 115 VAC BUS L SECT 1 BREAKER FOUND POPPED ON P31 PANEL. REF WDM 24-51-11-06. DID NOT ATTEMPT RESET REPLACED C901 GCB REF AMM 24-22-03-424-006. INSPECTED #1 FIRE
- [SDR CALA2024093002522](https://openairdocs.org/sdr/CALA2024093002522), Sep 28, 2024: CIRCUIT BREAKER. FAILED. 115 VAC BUS L SECT 1 BREAKER FOUND POPPED ON P31 PANEL. AND WDM INFO. SEE WDM 24-51-11-06. DID NOT ATTEMPT RESET REPLACED C901 GCB REF AMM 24-22-03-424-006. INS
- [SDR CALA2024090902402](https://openairdocs.org/sdr/CALA2024090902402), Aug 31, 2024: FLOORBEAM. CORRODED. GEN ITEM 53-5330-1-2802 CORROSION ON FLOOR BEAM AT STA 1640 ON B LO MARKED 13065 REF NR 173733-0100-0175 INSTALLED FRAME REPAIR AT STA 1640 UPPER CABIN BLO IAW 
- [SDR CALA2024083002332](https://openairdocs.org/sdr/CALA2024083002332), Aug 29, 2024: WEB. CORRODED. REF AMES NR 173733-0100-0204 ALC STA1520-1540 JUST FWD OF LAV TANK DRAIN PAN. WEB IS CORRODED.
- [SDR CALA2024083002331](https://openairdocs.org/sdr/CALA2024083002331), Aug 28, 2024: THRESHOLD. CORRODED. REF AMES NR 173733-0200-0185 GEN ITEM AGING AC INSP AGING A/C INSP: CORROSION UNDER R4 DOOR THRESHOLD SCUPPER / DRAI N
- [SDR CALA2024083002329](https://openairdocs.org/sdr/CALA2024083002329), Aug 28, 2024: FLOORBEAM. CRACKED. REF AMES NR 173733-0100-0065 GEN ITEM 53-0630-1-2202 GENERATING ITEM B757-06-3-0228: COCKPIT FLOOR BEAM BOTTOM SUPPOR T STRAP IS CRACKED, LOCATED BETWEEN FRAME 
- [SDR CALA2024083002327](https://openairdocs.org/sdr/CALA2024083002327), Aug 28, 2024: FLOORBEAM. CORRODED. REF AMES NR 173733-0200-0216 CORROSION FOUND ON UPPER CABIN FLOOR BEAM AT STA 365.25 RBL 60. BLENDED CORROSION AND RESTORED FINISH ON UPPER CABIN FLOOR BEAM STA
- [SDR CALA2024082902312](https://openairdocs.org/sdr/CALA2024082902312), Aug 27, 2024: FLOORBEAM. CORRODED. CORROSION ON FLOOR BEAM AT STA 395 ON BL10 REMOVED AND REPLACED FLOOR BEAM @ STA395 BL10 IAW B757 SRM 51-40 -02 PARA 7.
- [SDR CALA2024090302343](https://openairdocs.org/sdr/CALA2024090302343), Aug 25, 2024: SKIN. CORRODED. CORROSION UNDER AND AROUND WITH FASTENER HEADS PULLING THROUGH AFT LAX SERVICE PAN / FUSELAGE SKIN LOWER SIDE AT STA 1560 10110 REPIRED PER AMES DOCUMENT 47627R
- [SDR CALA2024083002326](https://openairdocs.org/sdr/CALA2024083002326), Aug 25, 2024: STRAP. BROKEN. GEN ITEM ZONE 120 / CLOSE UPPER CABIN FLOOR SUPPORT STRAP IS BROKE IN FLC AT STA 560 CEILING REPAIRED UPPER CABIN FLOOR SUPPORT STRAP IN FLC AT STA 560 IAW B 75
- [SDR CALA2024080902185](https://openairdocs.org/sdr/CALA2024080902185), Aug 7, 2024: FLOORBEAM. CRACKED. REF AMES NR 173733-0100-0112 GEN ITEM 53-5310-1-2616 UPPER CABIN FLOOR SUPPORT TOP ANGLE IS CRACKED AROUND FIVE NUTPL ATES, LOCATED BETWEEN B.S. 1180+80 AND B.S
- [SDR CALA2024080902183](https://openairdocs.org/sdr/CALA2024080902183), Aug 7, 2024: FLOOR SUPPORT. CORRODED. REF AMES NR 173733-0100-0133 GEN ITEM 53-5310-1-2612 AFT LOWER CARGO FLOOR SUPPORT BEAM AT STATIONS 1516 TO 1520 BETW EEN STRINGERS S-30/S-29R HAS CORROSION REM
- [SDR CALA2024080902184](https://openairdocs.org/sdr/CALA2024080902184), Aug 7, 2024: FLOOR SUPPORT. CRACKED. REF AMES NR 173733-0100-0111 GEN ITEM 53-5310-1-2616 UPPER CABIN FLOOR SUPPORT TOP ANGLE IS CRACKED A NUTPLATE, LOCAT ED BETWEEN B.S. 1180+20 AND B.S. 1180+40, 
- [SDR CALA2024073002139](https://openairdocs.org/sdr/CALA2024073002139), Jul 25, 2024: PLATE. CRACKED. REF AMES NR 173733-0500-0036 GEN ITEM 53-5700-1-2107 L/W TE WIGGLE PLAT AT WS330.50 CRACKED/BROKEN REMOVED AND REPLACED 2 EA L/W T/E WIGGLE PLATES AT WS330.5 IA
- [SDR CALA2021082001376](https://openairdocs.org/sdr/CALA2021082001376), Aug 18, 2021: TRANSMITTER. FAULTED. AT FL340 LEVEL FLIGHT L HYD QTY EICAS QTY AS LOW AS .36 WITH RF. RAN CHECK LIST REPLCD LEFT HYD TRANSMITTER REF LP 6880844
- [SDR CALA2021082001375](https://openairdocs.org/sdr/CALA2021082001375), Aug 18, 2021: TRANSMITTER. READS LOW. AT FL340 LEVEL FLIGHT L HYD QTY EICAS QTY AS LOW AS .36 WITH RF. RAN CHECK LIST REPLCD LEFT HYD TRANSMITTER REF LP 6880844
- [SDR CALA2021080901299](https://openairdocs.org/sdr/CALA2021080901299), Aug 8, 2021: SKIN. DAMAGED. SUPPORT TASK: RUDDER DAMAGED AT TRAILING EDGE BETWEEN STA 190 AN D STA 140 DUE TO CONTACT WITH LIFT. TRANSCRIBED FROM HAECO GSO NRC# 9282712 REPAIRED RUDDER DAM
- [SDR CALA2021071901130](https://openairdocs.org/sdr/CALA2021071901130), Jul 16, 2021: FITTING. GOUGED. SUPPORT TASK L2 DOOR TOP FWD DOOR STOP BRACKET ON FUSELAGE SIDE OF DOOR CUTOUT HAS GOUGE TRANSCRIBED FROM HAECO GSO NR 9282409 M ECH V900838 REMOVED AND INSTALL
- [SDR CALA2021071201079](https://openairdocs.org/sdr/CALA2021071201079), Jul 11, 2021: FITTING. GOUGED. B757-53-3-0482 L1 DOOR CUTOUT UPPER FWD STOP FITTING GOUGED TRAN SCRIBED FROM HAECO GSO NR 9282105 REMOVED DAMAGED STOP FITTING IAW B757-300 SRM 51-40-02, LOCAT
- [SDR CALA2020021600438](https://openairdocs.org/sdr/CALA2020021600438), Feb 14, 2020: SEAL. MISSING. PDA 2 FOUND SEAL MISSING FROM INBD EGDE OF OTBD LH FLAP. RPL''D SEAL REF IPC 57-53-10-51 ITEM 100
- [SDR CALA2019061000912](https://openairdocs.org/sdr/CALA2019061000912), Jun 7, 2019: FRAME. CORRODED. CORROSION ON AFT CARGO FRAME FWD SIDE AROUND SHEAR TIES, BRACKETS AND STR CLIPS AT STA 1440 BETWEEN STR 28L-29R. R EF ST-ENG N/R 0063844 LIMITS (L=7.0" W=4.0" D
- [SDR CALA2019060430874](https://openairdocs.org/sdr/CALA2019060430874), May 29, 2019: HOUSING. GOUGED. R2 DOOR EXTERNAL HANDLE PAN GOUGE AS MARKED 034-052 OFF A/C PART. REF ST-SAA NR 0064108. GOUGE ON R2 DOOR EXT HANDLE PAN (DEPTH WAS .020, MAX ALLOWABLE I SRM 52
- [SDR CALA2019053100870](https://openairdocs.org/sdr/CALA2019053100870), May 28, 2019: FRAME. DENTED. B757-06-3-0243 DENT ON AFT CARGO FRAME UPPER FLANGE AT STA 1440 ABOVE STR 26L RG7 REF. ST.ENGINEERING N/R 0063855 AFT CARGO FRAME UPPER FLANGE DENT AT STA 1440 
- [SDR CALA2019053100869](https://openairdocs.org/sdr/CALA2019053100869), May 28, 2019: ANGLE. CORRODED. B757-49-3-8083 APU AIR INLET DOOR HOUSING CUTOUT SURROUNDING EDG E HAS CORROSION PUSHING UP SEALANT. REF ST-ENG N/R 0063617 REMOVED CORROSION FROM APU AIR INLET
- [SDR CALA2019060700886](https://openairdocs.org/sdr/CALA2019060700886), May 26, 2019: SKIN. DENTED. B757-06-3-0222 LOWER FUSELAGE EXTERIOR SKIN DENT AT APPROX. STA 650, BETWEEN 27L AND 26L, 16-8. REF ST-ENG CARD NO 0063664. SKIN DENT AT STA 650 BETWEEN STR 26L
- [SDR CALA2019052700845](https://openairdocs.org/sdr/CALA2019052700845), May 26, 2019: STRINGER. CRACKED. B757-53-3-0556 CRACK ON STR 16L AT STA 780+35 FROM EDGE OF STR TO FIRST FASTENER HOLE. REF ST-ENG N/R 0064014 REPAIRED CRACK ON EDGE OF STRINGER TO FIRST FASTEN
- [SDR CALA2019052700840](https://openairdocs.org/sdr/CALA2019052700840), May 25, 2019: STRINGER. CRACKED. B757-53-3-0559 CRACK ON STR 16R AT STA 780+35 FROM EDGE OF STR TO FIRST FASTENER HOLE. REF ST-ENG N/R 0064015 REPAIRED CRACK ON EDGE OF STRINGER TO FIRST FASTEN
- [SDR CALA2019053100868](https://openairdocs.org/sdr/CALA2019053100868), May 22, 2019: STRINGER. CRACKED. B757-53-3-0559 CRACK ON STR 16R AT STA 780+24. FROM EDGE OF STR TO FIRST FASTNER HOLE. REF ON ST-ENG N/R CARD NO 0064016. FOUND STRINGER 16R AT STA 780+24 CRACK
- [SDR CALA2019052700835](https://openairdocs.org/sdr/CALA2019052700835), May 22, 2019: GATE. CORRODED. SUPPORT TASK EA 5210-01361 REV F 2R DOOR LOWER GATE HAS CORROSION AT EDGE AS MARKED 034-011. REF ON ST-ENG N/R CARD NO 0064184. FOUND DOOR 2R LWR GATE OUT OF LI
- [SDR CALA2019052400818](https://openairdocs.org/sdr/CALA2019052400818), May 22, 2019: STRINGER. CRACKED. B757-53-3-0556 CRACK ON STR 16L AT STA 780+24 FROM EDGE OF STR TO FIRST FASTENER HOLE. REF ST-ENG N/R 0064013. ACCOMPLISHED PERMANENT REPAIR ON FUSE STRINGER S-
- [SDR CALA2019012500145](https://openairdocs.org/sdr/CALA2019012500145), Jan 22, 2019: COLLAR. WORN. DOOR 2L DIFFICULT TO OPEN FROM OUTSIDE. REMOVED L2 DOOR HANDLE MECHANISM PER AMM 52-11-13-842-001. FOUND CLUTCH COLLAR WORN.
- [SDR CALA2017111704110](https://openairdocs.org/sdr/CALA2017111704110), Nov 17, 2017: BATTERY. FAULTY. FLASHLIGHT AT THE R3 DOOR INOPERATIVE. REPLACED THE BATTERY, OPS CHECKED GOOD.
- [SDR CALA2017100903539](https://openairdocs.org/sdr/CALA2017100903539), Oct 9, 2017: SENSOR. MALFUNCTIONED. DURNG TAXI OUT, THE NR 2 ENGINE MOMENTARILY SHUTDOWN. EICAS MESSAGE FOR THE RT ENGINE EEC, AND RT ENGINE LIMITER. REPLACED THE NR 2 ENGINE TPU IAW AMM 75-32-15-
- [SDR CALA2017090803086](https://openairdocs.org/sdr/CALA2017090803086), Sep 8, 2017: LENS. BROKEN. EMERGENCY EXIT ARM LIGHT ON COCKPIT OVERHEAD PANEL CAME APART. REPLACED LENS IAW AMM 33-13-00

All 60: https://openairdocs.org/aircraft/N73860/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 N73860

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N73860 before.

- [Cancelled 1979-12-10](https://openairdocs.org/deregistered/N73860-1979-12-10): Cessna 172N, S/N 17267728. Exported to New Zealand. Owner: [Anderson Gary](https://openairdocs.org/faa-owner/ANDERSON%20GARY), [Bismarck, ND](https://openairdocs.org/faa-place/ND/Bismarck)
- [Cancelled 1962-04-17](https://openairdocs.org/deregistered/N73860-1962-04-17): Douglas C-47, S/N 43-48244. Exported to Spain. Owner: [Charlotte Aircraft Corp](https://openairdocs.org/faa-owner/CHARLOTTE%20AIRCRAFT%20CORP), [Charlotte, NC](https://openairdocs.org/faa-place/NC/Charlotte)

## 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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