# N8607F: Hughes Helicopters HUGHES 369D, registration cancelled 2013-03-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 21, 2013
- Status when cancelled: Sale reported, pending cancellation
- Airframe: [Hughes Helicopters HUGHES 369D](https://openairdocs.org/model/hughes-helicopters-hughes-369d) (registry code 4470706)
- Data sheets: [TCDS H3WE](https://openairdocs.org/tcds/H3WE) (OpenAirDocs)
- Serial number: 980336D
- Type of aircraft: Rotorcraft
- Airworthiness: Standard, normal
- Airworthiness date: September 21, 1978
- Last registry action: April 7, 2000
- Mode S code: ABD22A
- Location: Langley, Canada
- Owner type: Individual
- The mark today: https://openairdocs.org/aircraft/N8607F
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8607F
- Page: https://openairdocs.org/deregistered/N8607F-2013-03-21

From the FAA registry file of November 3, 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 Hughes Helicopters HUGHES 369D: https://openairdocs.org/model/hughes-helicopters-hughes-369d.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB SEA81DYK02](https://openairdocs.org/ntsb/SEA81DYK02), Dec 15, 1980: Hughes 369 (N8607F), Powers, OR, substantial damage

## 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.

- [Accident 19801215076659A](https://openairdocs.org/incident/19801215076659A), Dec 15, 1980: Hughes 369D (N8607F), Powers, OR, Substantial damage. Clutch gave out during hover for sling load hookup. Crash landed, rolled over after impact.

---
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.
