2 fatalities

1999-06-25: Beechcraft 90 King Air (N3019W) — AeroCenter — Munson, United States of America

Munson, United States of AmericaFlight

On June 25, 1999, a Beechcraft 90 King Air (registration N3019W) operated by AeroCenter was involved in an aviation accident near Munson, United States of America in flight. 2 people were killed. Investigators recorded the probable cause as: Poor in-flight weather evaluation by the pilot-in-command and operation of the airplane at an indicated airspeed greater than the design maneuvering speed (Va) in a thunderstorm contrary to the pilot's operating handbook, resulting in an in-flight breakup. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781204292Data APIEditorial standards

A pilot operating an airplane encountered a level 5 thunderstorm echo while descending at an airspeed exceeding the design maneuvering speed, leading to structural failure and in-flight breakup of the wings and horizontal stabilizers.

Flight History

The pilot received a preflight weather briefing warning of thunderstorms with tops reaching 45,000 feet along the intended route. En route, air traffic control advised of significant areas of heavy precipitation. The pilot responded, "uh roger one nine whiskey it looks like on our radar here that uh we go straight ahead we'll be all right there." The flight was cleared to descend to 11,000 feet, and the pilot requested a deviation to the right for weather avoidance.

Weather Conditions

The pilot conducted several routine radio communications while descending at an average rate of approximately 2,571 feet per minute. During this descent, the calculated calibrated airspeed increased from about 190 knots to approximately 265 knots—the design dive speed (Vd). The flight subsequently encountered a level 5 weather echo, after which it began a high rate of descent.

Accident Sequence

Post-accident examination revealed that both horizontal stabilizers with elevators and both outer portions of both wings failed in a downward direction. Investigators found no evidence of preimpact failure or malfunction in the flight control cables, fracture surfaces, engines, or propellers. The pilot did not request any pilot reports during the flight. The airplane's design maneuvering speed (Va) was 169 knots indicated; the Pilot's Operating Handbook (POH) directs pilots to reduce speed to Va for turbulence penetration.

Probable Cause

The official probable cause was the poor in-flight weather evaluation by the pilot-in-command and his operation of the airplane at an indicated airspeed greater than the design maneuvering speed (Va) in a thunderstorm, contrary to the POH, resulting in an in-flight breakup. A contributing factor was the pilot's failure to obtain in-flight weather advisories from air traffic control before encountering the adverse weather.