What happened
The aircraft experienced a loss of engine power during the initial climb phase immediately following takeoff. This failure occurred at an altitude of approximately 75 feet above ground level (AGL). Unable to maintain flight, the pilot executed a forced landing into a wooded area.
The investigation
Following the accident, investigators conducted a thorough examination of the aircraft to determine the cause of the power loss. The inspection focused on the engine and related systems for any signs of mechanical failure or malfunction. However, the examination revealed no evidence of pre-existing failures or malfunctions within the aircraft's systems.
Findings
Environmental conditions played a significant role in the incident. At the time of the accident, the ambient temperature and dew point were within the range conducive to carburetor icing. The pilot reported that the carburetor heat control was left in the cold position for takeoff, which is standard procedure but leaves the engine vulnerable to icing under specific atmospheric conditions.
The combination of weather conditions favorable for ice formation and the lack of applied carburetor heat led to carburetor icing, which restricted fuel/air flow and caused the sudden loss of power. This mechanical restriction, rather than a system failure, was the primary factor in the accident.