Flight Details
The cross-country flight was conducted under an instrument flight rules (IFR) flight plan. Approximately 42 nautical miles from the tower-controlled destination airport, the pilot was cleared for the visual approach. Dark night visual meteorological conditions prevailed, with an overcast layer of clouds at 11,000 feet.
Accident Sequence
After en route radar service was terminated, the pilot contacted the local control tower and made a garbled and partially unintelligible transmission. Shortly after that transmission, local law enforcement personnel received reports of a downed aircraft. The wreckage was located later that evening approximately 80 feet below the peak of a ridge that rose to an elevation of about 5,700 feet. From the initial point of contact with terrain, the debris path scattered over the crest of the ridge and continued down the opposing side in a south-southeast direction toward the airport. The ridge was the highest obstruction between the accident location and the destination airport.
Terrain and Lighting Conditions
The airport is located in a large valley and is surrounded by rising mountainous terrain. At night, clouds and terrain are difficult for pilots to see, and a gradual loss of visual cues can occur as flight is continued toward darker terrain. Additionally, the horizon is less visible and less distinct at night than during the day. The pilot was descending the airplane over rural, mountainous terrain that provided few visual ground reference cues. The overcast cloud layer would have prevented moonlight from illuminating the terrain, making it likely that the pilot did not see the rising terrain as the airplane continued toward it.
Aircraft Examination
The airplane was equipped with an Enhanced Ground Proximity Warning System (EGPWS); however, impact damage to the unit precluded post-accident testing. It is not known how the unit was configured during the flight or what type of alerts the pilot received prior to impact. Post-accident examination of the wreckage, including both engines, did not disclose evidence of a mechanical malfunction prior to impact. Additionally, no evidence was found to suggest an in-flight structural failure.