2 fatalities

1990-03-10: Piper PA-61 Aerostar (Ted Smith 601) (N410HC) — BHP Inc. — Bartonville, United States of America

Bartonville, United States of AmericaFlight

On March 10, 1990, a Piper PA-61 Aerostar (Ted Smith 601) (registration N410HC) operated by BHP Inc. was involved in an aviation accident near Bartonville, United States of America in flight. 2 people were killed. Investigators recorded the probable cause as: The pilot allowed the aircraft to exceed its design stress limits after encountering adverse weather. Factors related to the accident were: the pilot's improper evaluation of the weather and the adverse weather conditions. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781213114Data APIEditorial standards

An aircraft broke up in flight after the pilot deviated to avoid clouds, with a witness seeing a funnel cloud. The left wing separated due to overload; both occupants were killed.

Accident Sequence

Before departure, the pilot received a weather briefing that included thunderstorms, heavy rain, a severe thunderstorm watch with hail and wind gusts up to 65 knots, and a SIGMET (31c). The pilot filed an IFR flight plan and took off at 1148 CST. While en route at 15,000 feet MSL, the pilot requested and received clearance to divert 10° left to avoid "some clouds." Shortly after, air traffic control observed the aircraft about 500 feet high and reminded the pilot to maintain 15,000 feet. The pilot acknowledged, but no further communication was received.

An in-flight breakup occurred, and the aircraft crashed. The left outboard wing panel separated due to a positive overload failure and was found about one mile from the main wreckage. No preimpact fatigue was detected. A witness reported seeing the aircraft descending out of the clouds and also observed a funnel cloud in the area before the accident. Both occupants were killed.

Investigation Findings

The investigation determined that the pilot allowed the aircraft to exceed its design stress limits after encountering adverse weather. Factors identified were the pilot's improper evaluation of the weather and the adverse weather conditions themselves.

Probable cause

The pilot allowed the aircraft to exceed its design stress limits after encountering adverse weather. Factors related to the accident were: the pilot's improper evaluation of the weather and the adverse weather conditions.