# N532H: Enstrom F-28C, registration cancelled 1982-08-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 10, 1982
- Status when cancelled: Valid registration
- Airframe: [Enstrom F-28C](https://openairdocs.org/model/enstrom-f-28c) (registry code 3300407)
- Data sheets: [TCDS H1CE](https://openairdocs.org/tcds/H1CE) (OpenAirDocs)
- Serial number: 331
- Type of aircraft: Rotorcraft
- Certificate issued: October 23, 1978
- Mode S code: A6B88A
- Owner when cancelled: [Alyeska Air Service Nc](https://openairdocs.org/faa-owner/ALYESKA%20AIR%20SERVICE%20NC)
- Location: [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage)
- Owner type: Corporation
- The mark today: https://openairdocs.org/aircraft/N532H
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=532H
- Page: https://openairdocs.org/deregistered/N532H-1982-08-10

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 Enstrom F-28C: https://openairdocs.org/model/enstrom-f-28c.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 ANC79FA065](https://openairdocs.org/ntsb/ANC79FA065), Jul 2, 1979: Enstrom F-28C (N532H), Portage, AK, 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 19790702041809A](https://openairdocs.org/incident/19790702041809A), Jul 2, 1979: Enstrm F28C (N532H), Portage, AK, Substantial damage. Engine quit. Autorotated to landing on soft tundra. Main rotors severed tail boom. Connecting rod cap failure.

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