Introduction
A pilot reported an incident involving an engine power reduction during initial climb. The flight departed from Runway 30 and, at about 900 feet, the engine power level smoothly reduced to approximately 2,000 RPM. The pilot noted that there was no roughness associated with the power loss. Concerned about the terrain ahead, the pilot elected to perform a 180-degree turn and land downwind on Runway 12.
Landing and Go-Around
During the landing attempt, the aircraft touched down about two-thirds of the way down the runway. The pilot believed the aircraft could not be stopped before colliding with a fence at the runway end. In response, she added all available power, and the aircraft lifted off and cleared the fence. However, the aircraft then settled back to the ground and collided with two coral fences approximately one-quarter of a mile beyond the end of the runway.
Wind Conditions
The pilot reported that the winds at the time were from about 310 degrees at about 10 knots.
Post-Accident Examination
FAA airworthiness inspectors examined the engine and airframe but did not find evidence to explain the reported loss of power.