# N102HT: not currently registered

- Registered now: No (not in the FAA registry file). The mark may be reserved or free to assign
- Earlier aircraft: 1
- Last cancelled: August 14, 2013
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=102HT
- Page: https://openairdocs.org/aircraft/N102HT

## Aircraft that carried N102HT

- [Cancelled 2013-08-14](https://openairdocs.org/deregistered/N102HT-2013-08-14): Hiller UH-12E, S/N 5218, built 1983. Registration expired, pending cancellation. Owner: [Palm Kevin](https://openairdocs.org/faa-owner/PALM%20KEVIN), [Hollister, CA](https://openairdocs.org/faa-place/CA/Hollister)

## NTSB investigations on N102HT (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 ATL96LA104](https://openairdocs.org/ntsb/ATL96LA104), Jul 11, 1996: Hiller UH-12E (N102HT), Cottondale, FL, substantial damage. Probable cause: failure of the main rotor drive torsional coupling and inner gimbal ring, which resulted in jamming of the flight controls during an attempted autorotation.

## FAA accident and incident reports on N102HT (2)

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 20000229014759I](https://openairdocs.org/incident/20000229014759I), Feb 29, 2000: Hiller UH12E (N102HT), Amana, IA, Minor damage. (-23) PIC stated that while landing, (about 10 feet from ground) the transmission broke. Once the aircraft was on the ground, it was froken up. The…
- [Accident 19960711044029A](https://openairdocs.org/incident/19960711044029A), Jul 11, 1996: Hiller UH12E (N102HT), Cottondale, FL, Substantial damage. Loud bang vibration on climbout. Lost tail rotor control. Impacted inverted main drive clutch and gimble failed.

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