Casualties unknown

2000-04-21: Mooney M20J (N5632H) — Norton, VA

Norton, VA, US

On April 21, 2000, a Mooney M20J (registration N5632H) was involved in an aviation accident near Norton, VA. Investigators recorded the probable cause as: The pilot's improper weather evaluation, which resulted in a loss of aircraft control. Factors in this accident were icing conditions, and aircraft loading which exceed the airplane's weight and balance limitations. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

An aircraft, not approved for known icing, crashed after entering a steep descent. Investigation revealed it was overweight and had an incorrect center of gravity. No mechanical failure was found.

Accident Overview

An aircraft crashed into uneven, wooded terrain at an elevation of about 3,600 feet after a loss of radar contact. The accident occurred during a flight that began with a weather briefing that included advisories for icing along the intended route.

Flight History

During the flight, the pilot reported being "riding in the tops of the clouds" while cruising at 9,000 feet. The pilot requested and was cleared to climb to 11,000 feet. The airplane leveled off at 9,400 feet, then began another climb, reaching a maximum altitude of 9,700 feet. Shortly thereafter, the airplane entered a steep vertical descent, and radar contact was lost. The wreckage came to rest at an elevation of about 3,600 feet.

Examination Findings

Examination of the wreckage did not reveal any evidence of a mechanical failure of the airframe or engine. Satellite data obtained for the flight indicated the potential for icing in the area of the airplane's last radar return. The airplane was not approved for flight into known icing conditions.

Weight and Balance

An airplane weight and balance calculation revealed that the airplane's weight was about 2,945 pounds, and the center of gravity (CG) was about 142.88 inches at the time of the accident. According to the pilot operating handbook, the maximum certificated gross weight for the airplane was 2,740 pounds. Additionally, the CG range at the maximum certificated gross weight was about 128 to 138 inches.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X20892. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.