Casualties unknown

2002-05-30: Cessna A185F (N1577B) — Robert E. Fulton — Pleasant Mount, PA

Pleasant Mount, PA, US

On May 30, 2002, a Cessna A185F (registration N1577B) operated by Robert E. Fulton was involved in an aviation accident near Pleasant Mount, PA. Investigators recorded the probable cause as: The pilot's inadequate in-flight planning/decision resulting in flight into adverse weather, and his failure to maintain aircraft control, resulting in overstress of the aircraft. A factor was the thunderstorm activity. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

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

An aircraft with a private pilot and passenger broke up in flight while attempting to deviate around thunderstorms. Witnesses observed a descent of 30-45 degrees nose-down and heard the engine operating before breakup.

Flight Details

The aircraft was in cruise flight at an altitude of 11,000 feet. Onboard were an instrument-rated private pilot and a passenger.

Weather and Pilot Actions

Thunderstorms and convective activity were present in the area. The pilot chose to continue flying toward the weather and requested permission to deviate around it, but did not specify a direction. After receiving clearance for the deviation, the airplane first turned left while maintaining altitude, then turned right more than 90 degrees and began to descend. The last radar contact was recorded at 9,300 feet, after which both radio and radar contact were lost.

Witness Observations

Witnesses on the ground observed the airplane in a descent estimated to be between 30 and 45 degrees nose-down, below the base of the clouds. They could hear the engine operating. The witnesses saw the airplane come apart while it was operating clear of clouds. One witness reported that the descent started to shallow just prior to the breakup.

Wreckage Examination

The debris trail extended 1,033 feet to the impact crater, with an additional 486 feet of debris beyond the crater. Examination of the wreckage revealed downward bending on the spars of the horizontal stabilizer and wings. One propeller blade was found separated from its hub in the main impact crater, exhibiting "S" bending on both the leading and trailing edges.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020611X00846. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.