Incident Overview
A pilot reported that during an initial climb, the engine experienced a loss of power at approximately 300 feet above ground level (AGL). The pilot had previously completed a preflight inspection and performed engine run-up and control checks, with all engine indications appearing normal. The aircraft subsequently landed in a ditch and collided with a concrete bridge abutment/culvert.
Witness Accounts
Witnesses on the ground reported that the engine was "missing, faltering, and sputtering" prior to the forced landing.
Post-Accident Inspection
An inspection of the aircraft's engine and systems revealed that all components had continuity or were capable of operating normally. A fuel sample taken from the aircraft was clear and bright. The engine was removed and run on a test stand, where it operated within manufacturing specifications.
Weight and Balance
The aircraft's weight and balance were within limits at the time of takeoff. The takeoff weight was about 2,856 pounds, and the gross weight limit was 2,900 pounds.
Probable Cause
The investigation did not determine a probable cause for the loss of engine power.