What happened
The aircraft touched down on a private airstrip located atop a ridge characterized by steep terrain. The facility lacked any wind direction or speed indicators for pilots to reference during approach. As the pilot neared the runway threshold, intense sunlight entered his field of vision. Calculations indicate the sun was positioned five degrees above the horizon and approximately twenty-one degrees to the right of his center vision reference point at the time.
Simultaneously, strong lateral winds affected the aircraft's trajectory. Fire department personnel reported that the wind direction was roughly forty-five degrees left of the runway heading. The sustained wind speed was about seventeen knots, with peak gusts reaching thirty knots. These conditions exceeded the factory-tested maximum demonstrated crosswind capability for this specific aircraft model, which is rated at thirteen knots.
The combination of visual obstruction and excessive lateral drift pushed the aircraft off the right side of the paved surface. It struck the ground hard on the right main landing gear. The impact caused the aircraft to veer further right and cartwheel down the thirty-degree slope adjacent to the runway edge. The plane eventually came to rest at the bottom of the hill, where it ignited and was consumed by fire.
Findings
The investigation highlighted several critical factors contributing to the loss of control. The primary mechanical limitation was the crosswind component. The observed winds were significantly stronger than the aircraft's demonstrated capability. The pilot likely underestimated the wind conditions due to the absence of visual aids on the private strip.
Environmental conditions played a major role in the accident sequence. The low angle of the sun created significant glare, reducing the pilot's ability to judge alignment and height accurately. The steep terrain surrounding the airstrip left no margin for error during the final approach or initial rollout. The lack of wind indicators on the facility prevented the pilot from making informed decisions about go-around procedures or landing gear configuration adjustments.