Accident Overview
After striking electrical power lines, the aircraft crashed near an open field. The initial impact occurred where the wires crossed a draw between two ridges. Following the collision, the aircraft came to rest inverted in the area between the power lines and the open field.
Aircraft Condition
The aircraft was relatively intact but sustained extensive ground impact damage to the left wing. The rear fuselage exhibited compression and twisting. Heavy scrape marks were present on the left main landing gear. The propeller showed no evidence of rotational marks or damage.
Examination Findings
The left fuel cap was found off, with some fuel remaining in the rear corner of the tank; the right fuel cap was in place. The carburetor heat control was wedged in the on/hot position. The connecting wires to the starter switch were corroded at the attachment screws, partially separated, and the switch case was broken. No preimpact part failure or malfunction was verified.