Accident Description
Upon touchdown, the left landing gear leg began to fail as the aircraft's weight transferred to the wheels. The left gear folded outward, causing the airplane to veer left. The left wing tip then struck an embankment, bringing the airplane to a stop.
Examination Findings
An FAA inspector examined the airplane and discovered structural damage to the left gear box, left wing strut, left wing tip, left aileron, the rear spar of the left wing, and the propeller. The investigation revealed that the 7/16-inch AN bolt securing the left gear leg to the fuselage had failed in shear loading. This failure allowed the gear to pivot on the landing gear box, which subsequently led to failure of the lower landing gear box web.
Damage
The following components sustained damage: left gear box, left wing strut, left wing tip, left aileron, rear spar of the left wing, and the propeller.