Accident Overview
Shortly after departure, the aircraft's engine began losing power. The pilot was unable to maintain altitude or return to the airport and chose to land on a road. However, oncoming traffic forced the pilot to maneuver to the left side of the roadway. During this maneuver, the left wing struck a utility pole.
Witness Observations
A witness reported that the aircraft was slow to climb after takeoff but noted no unusual engine sounds. No additional details regarding the witness's position or the takeoff sequence were provided.
Engine Examination
Following the accident, an operational check of the engine was conducted. Due to accident damage, the engine could only be run up to 1650 RPM. The only discrepancy found during the engine run was a loose gascolator. The investigation did not verify whether the gascolator had loosened before the accident or during the impact.
Post-Accident Actions
The aircraft sustained damage to the left wing from the utility pole collision. No further details about the aircraft, pilot, or environmental conditions were included in the source.