Preflight Inspection
The pilot reported that a normal preflight check was conducted, which included draining fuel from the fuel tank sumps and the strainer. During this procedure, about one inch of water was drained from the left wing fuel sump, as measured in a fuel sampler cup. No water was detected in the right wing sump or the fuel strainer.
Takeoff and Engine Failure
The before-takeoff check was normal, and all engine instruments indicated normal readings when power was added for takeoff. However, at an altitude of approximately 150 to 200 feet above ground level, the engine lost power. The pilot was unable to land on the remaining runway from that position.
Forced Landing
With full flaps extended, the pilot executed a forced landing into the tops of trees in a wooded area.
Post-Accident Examination
During an examination of the wreckage, water was found in the carburetor and the left wing.