What happened
The Enstrom F28C was operating in a cruise configuration when it suffered an unexpected loss of engine power. The specific mechanical or operational cause for this failure was not immediately apparent during the flight phase.
Following the power loss, the pilot initiated emergency procedures and selected a large open field as a landing site. Upon touchdown, the helicopter sustained significant structural damage. The main rotor assembly was damaged upon impact with the ground, and the tail rotor completely separated from the tail boom structure.
The investigation
Post-accident examination confirmed the extent of the airframe damage described above. Records regarding the pilot's total flight time were not available from either the pilot or their personal records at the time of the report.
Findings
The sole occupant, identified as the pilot, was not injured in the incident. The aircraft sustained substantial damage. The loss of power occurred during cruise flight, leading to a forced landing in an unprepared area.