Accident Overview
During the takeoff initial climb phase of flight, at an altitude of approximately 100 ft above ground level (AGL), the airplane experienced a total loss of engine power. This occurred while the airplane was climbing after departure. The pilot executed a forced landing, during which the airplane collided with rough terrain and railroad tracks.
Post-Accident Inspection
Subsequent inspection of the airplane's systems revealed that the ignition system was operationally correct. Additionally, there was sufficient fuel on board the airplane for the intended flight. Examination of the fuel distribution system indicated it was operationally correct, with the exception of the carburetor float bowl, which contained no fuel.
Investigation Findings
The absence of fuel in the carburetor float bowl was identified as a notable condition. However, no explicit determination of cause was provided in the source material. All other relevant systems were found to be functioning properly.