# N670H: 1981 Rockwell International NA-265-65, registration cancelled 2019-08-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 8, 2019
- Status when cancelled: First renewal notice
- Airframe: [Rockwell International NA-265-65](https://openairdocs.org/model/rockwell-international-na-265-65) (registry code 7630107)
- Engine: [Garrett TFE731 series](https://openairdocs.org/engine/garrett-tfe731-series) (registry code 29001)
- Data sheets: [TCDS A2WE](https://openairdocs.org/tcds/A2WE), [TCDS E6WE](https://openairdocs.org/tcds/E6WE) (OpenAirDocs)
- Serial number: 465-58
- Year built: 1981
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 22, 2019
- Certificate issued: March 2, 2004
- Last registry action: November 15, 2016
- Mode S code: A8DC67
- Owner when cancelled: [Honeywell International Inc](https://openairdocs.org/faa-owner/HONEYWELL%20INTERNATIONAL%20INC)
- Location: [Phoenix, AZ](https://openairdocs.org/faa-place/AZ/Phoenix)
- Owner type: Corporation
- Owner's area on the map: 33.4484° N, 112.0740° W: Placed by OpenAirDocs: center of Phoenix, AZ, within about 13 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N670H
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=670H
- Page: https://openairdocs.org/deregistered/N670H-2019-08-08

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Rockwell International NA-265-65: https://openairdocs.org/model/rockwell-international-na-265-65.md

## Service difficulty reports (2)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR UVVR2016031500043](https://openairdocs.org/sdr/UVVR2016031500043), Jul 15, 2016: FLEX LINE. LEAKING. DURING OPS CHECK OF CREW OXYGEN MASK, FOUND OXYGEN SYSTEM LEAKS BEYOND ALLOWABLE LIMIT WITH A 1 HOUR PERIOD. UPON INVESTIGATION FOUND O2 FLEX TO PILOT SYS OUTLE
- [SDR 1HYR20141103001](https://openairdocs.org/sdr/1HYR20141103001), Nov 3, 2014: SKIN. CRACKED. A SKIN CRACK WAS IDENTIFIED IN THE AFT UNPRESSURIZED AREA OF THE FUSELAGE, RT ABOVE, LT PYLON. THE CRACK IS ABOUT 1.375" LONG LOCATED AT APPROXIMATELY FS 390.5 

## 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 20130805014409I](https://openairdocs.org/incident/20130805014409I), Aug 5, 2013: Rockwell International Corp NA-265-65 (N670H), Spokane, WA, No damage. Pilot observed #2 engine oil pressure was at the low end of the yellow arc. Pilot reduced power and elected to make a precautionary landing at geg. Engine was…

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
