Accident Sequence
During a dual instructional flight, the engine lost power at approximately 100 feet above ground level (AGL). The certified flight instructor (CFI) executed a forced landing straight ahead. During the landing roll, the nose gear collapsed after striking a rut.
Post-Accident Inspection
Immediately after arriving at the accident site, the fixed-base operator (FBO) inspected the fuel filter and observed no contamination. The Federal Aviation Administration (FAA) later examined the aircraft. The engine was started and operated at full power for 10 minutes without any noted malfunctions.
The pilot reported that the engine exhibited a drop of approximately 300 RPM during the carburetor heat check performed before the flight.
Environmental Conditions
The ambient temperature on the day of the accident was 85 degrees Fahrenheit, with a dew point of 59 degrees Fahrenheit.