4 fatalities

1996-06-02: Piper PA-46 (Malibu/Meridian/Mirage/Matrix/M-Class) (N9114Q) — Home Oil Stations — Aitkin, United States of America

Aitkin, United States of AmericaFlight

On June 2, 1996, a Piper PA-46 (Malibu/Meridian/Mirage/Matrix/M-Class) (registration N9114Q) operated by Home Oil Stations was involved in an aviation accident near Aitkin, United States of America in flight. 4 people were killed. Investigators recorded the probable cause as: The pilot's continued flight into known adverse weather conditions and the pilot exceeding the design stress limits of the airplane. 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 1781206985Data APIEditorial standards

While cruising at 17,000 feet, the pilot of N9114Q reported ice and rain, requested weather avoidance, then later stated the aircraft was out of control. The aircraft was 548 pounds over maximum takeoff weight.

Flight and Weather Encounter

The aircraft was in cruise flight at 17,000 feet mean sea level (msl) when the pilot contacted Minneapolis Air Route Traffic Control Center (ARTCC) and stated, "We're picking up some ice and rain, and we're going to turn around." ARTCC approved the request. Two minutes later, the pilot reported, "We're looking for some help to get around this weather southbound." ARTCC advised the pilot that he could turn either east or west. The pilot turned west, and four minutes later turned back to the south. The pilot then informed ARTCC that they were still encountering weather. ARTCC directed the pilot to turn north and then east when possible.

Loss of Control

Approximately one minute after the last direction, ARTCC radar showed the aircraft in a rapid descent. The pilot transmitted, "Minneapolis center, N9114Q is out of control." Prior to departure, the pilot had received a Flight Service Station (FSS) briefing and was advised of convective conditions and precipitation building to the south along the intended route.

Contributing Factors

The aircraft was approximately 548 pounds over its maximum takeoff weight. The probable cause, as determined by the investigation, was the pilot's continued flight into known adverse weather conditions and exceeding the design stress limits of the airplane. Factors contributing to the accident included thunderstorms, hail, wind gusts, and the aircraft's over-maximum gross weight condition.