Aircraft Description
N8190Y is a 1955 Dehavilland DHC-2 MK. I(L20A), a single-engine reciprocating (piston) aircraft registered to Rapids Camp Lodge INC in King Salmon, AK. This aircraft holds a multiple airworthiness certificate issued by the Federal Aviation Administration on August 27, 1999. The registration certificate was issued on June 27, 2025. The registration is set to expire on June 30, 2032. Powered by a P&w R-985 SERIES engine producing 450 horsepower, N8190Y is. The aircraft's Mode S transponder code is AB2D3A (hex), used for ADS-B identification and flight tracking. The FAA registry record for N8190Y was last updated on June 27, 2025. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
de Havilland Aircraft produced iconic aircraft from the Tiger Moth trainer to the Comet jetliner. de Havilland Canada's DHC-2 Beaver and DHC-6 Twin Otter remain among the most respected utility aircraft ever built. AviatorDB tracks 1,814 Dehavilland aircraft currently registered in the FAA database, including the DHC-2 MK. I(L20A) model.
AviatorDB has found no NTSB accident or incident reports involving N8190Y. AviatorDB cross-references all FAA registration data with NTSB accident and incident reports, providing a comprehensive safety overview for every registered aircraft in the United States.
Registered Owner
Powerplant & Avionics
NTSB Accident History (2)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Apr 15, 2005 | ANC05TA058 | Substantial | Minor | The pilot's selection of unsuitable terrain for taxi after landing, which resulted in the collapse of the main landing gear and structural damage to the right wing and forward fuselage. A factor associated with the accident was the rough and uneven terrain. |
| Aug 12, 1992 | ANC92LA128 | Substantial | Minor | THE PILOT'S MISJUDGING HIS ALTITUDE ON FINAL APPROACH. CONTRIBUTING TO THE ACCIDENT WAS THE GLASSY WATER CONDITION. |
The pilot's selection of unsuitable terrain for taxi after landing, which resulted in the collapse of the main landing gear and structural damage to the right wing and forward fuselage. A factor associated with the accident was the rough and uneven terrain.
THE PILOT'S MISJUDGING HIS ALTITUDE ON FINAL APPROACH. CONTRIBUTING TO THE ACCIDENT WAS THE GLASSY WATER CONDITION.
Additional Details
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC