Accident Details
The aircraft was returning from an evening cross-country flight when it operated in instrument meteorological conditions (IMC). The forecast for the area included rain showers and thunderstorms. Subsequently, the aircraft crashed after experiencing an in-flight breakup.
Investigation Findings
An investigation revealed that the horizontal stabilator failed first, followed by the outboard portion of both wings. The failures occurred in a down and aft direction. The stabilator and portions of the wings were discovered approximately 1,200 feet from the main fuselage wreckage.
Radar data indicated that the aircraft had entered an increasing left descending turn, followed by a rapid descent rate just before ground impact.
The aircraft's gross weight was estimated to be about 3,000 pounds. Its maximum certified gross weight was 2,900 pounds.
Pilot Background
A review of the pilot's logbook showed that he had obtained one hour of instrument flight time and one instrument approach in the previous six months.