What happened
The accident occurred while the aircraft was established on final approach. During this phase of flight, the pilot encountered an excessive sink rate that necessitated immediate corrective action. To arrest the descent and ensure a safe landing, the pilot elected to execute a go-around maneuver.
When power was applied to initiate the climb, the aircraft's pitch attitude changed abruptly. The nose and right wing pitched up significantly, causing the aircraft to turn approximately 90 degrees. This sudden change in configuration and attitude led to an aerodynamic stall. Following the loss of lift, the aircraft descended rapidly and contacted a set of power lines. After striking the wires, the aircraft continued its descent until it impacted the ground.
The investigation
Post-accident examination revealed that the aircraft sustained substantial damage as a result of the collision with the power lines and subsequent impact with the terrain. The sequence of events was driven by the pilot's decision to initiate a go-around while managing an excessive sink rate, which resulted in a stall during the initial climb phase.