1 fatality

2009-12-04: Piper PA-31 Cheyenne (N85EM) — Cheyenne Sales & Leasing — Harrison, United States of America

Harrison, United States of AmericaFlight

On December 4, 2009, a Piper PA-31 Cheyenne (registration N85EM) operated by Cheyenne Sales & Leasing was involved in an aviation accident near Harrison, United States of America in flight. One person was killed. Investigators recorded the probable cause as: A loss of aircraft control for undetermined reasons. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781196401Data APIEditorial standards

A pilot of a pressurized twin-engine airplane lost control during flight after altitude and course deviations; post-crash investigation could not determine the cause due to fire damage.

Accident Sequence

Shortly after takeoff in a pressurized twin-engine airplane, the pilot was cleared to climb and maintain 16,000 feet. The pilot reported passing through instrument conditions with heavy snow and that he cleared the tops of the clouds at 7,000 feet. The pilot was then cleared to climb and maintain flight level (FL) 230. Radar data showed the airplane's altitude and course varied throughout the flight after reaching FL 230. Several times during the flight, the air traffic controller questioned the pilot regarding his altitude and/or course. Each time the pilot responded that he was at the correct altitude and/or course. The radar data indicated that after each of these conversations, the airplane would return to the assigned altitude and/or course.

The controller then informed the pilot that, because radar showed the airplane’s altitude fluctuating between FL 224 and FL 237, he was going to have to descend out of positive controller airspace. The pilot acknowledged this transmission. The controller instructed the pilot to descend to 17,000 feet. The last transmission from the pilot was his acknowledgment of the descent. Radar data showed that one minute later, the airplane was at FL 234. During the last minute and 12 seconds of radar data, the airplane reversed its course and descended from FL 233 to FL 214, at which time radar data was lost. Witnesses reported hearing loud engine sounds and seeing the airplane in a spiraling descent until ground impact.

Investigation

Post-accident inspection of the engines did not identify any anomalies that would have precluded normal operation. Most of the fuselage was consumed by fire; however, flight control continuity was established. Given the pilot’s experience and the flight’s altitude and course variations, the investigation considered that the pilot may have suffered from hypoxia. However, due to the post-impact fire, the functionality of the airplane’s pressurization system could not be observed, and no conclusive determination could be made that the pilot was impaired.

Probable Cause

The official probable cause was a loss of aircraft control for undetermined reasons.