Accident Sequence
The pilot was operating the aircraft at an altitude of 150 to 200 feet above ground level (AGL) with an indicated airspeed of 80 to 85 miles per hour. When power was applied to return to a higher altitude, the pilot reported that the carburetor heat control had not been returned to the 'off' position. The aircraft did not respond to the power input and failed to climb. The pilot then removed power and attempted to fly beneath surrounding trees. During this maneuver, the left wing contacted tree branches, and the aircraft subsequently struck the ground.
Pre-Flight and Post-Accident Findings
The pilot reported that during the pre-flight run-up, the left magneto was rough. However, a post-accident investigation of the magnetos revealed no abnormalities. The lower spark plugs were found to be carbon fouled.
Aircraft and Pilot Information
No further details about the aircraft type, registration, operator, or pilot qualifications were provided in the source. The date, time, location, and weather conditions at the time of the accident are not specified. There is no information regarding occupants, injuries, or the extent of damage to the aircraft.