We’re still collecting data for this aircraft. Routes appear once we’ve seen it fly enough times.
a loss of engine power due to the fatigue failure of the no.1 exhaust push rod. Factors contributing to the accident were: insufficient information on pushrod inspection and overhaul from the manufacturer, unsuitable terrain available for landing, and the pilot's failure to maintain airspeed during the approach which led to an inadvertent stall.
DE Havilland DHC-2 · 4 fatalities