Accident Overview
An aircraft experienced a loss of power shortly after takeoff, leading to a forced landing. During the landing, the aircraft contacted terrain and sustained substantial damage.
Inspection Findings
A post-accident inspection of the engine revealed that the carburetor valve assembly had separated from the lever assembly. This separation allowed the valve to seat flat against the carburetor, blocking airflow into the engine. The three screws that secure the valve assembly, part number 77671-09, to the lever, part number 77671-10, were missing. Additionally, the spot-welded safety bar, which serves to lock the screws in place, was found broken.