Preflight and Takeoff
The pilot reported draining the fuel sumps during the preflight inspection and finding no water. On takeoff, the airplane became airborne at a speed just under 70 knots and remained in ground effect at an altitude of about 3 to 5 feet while accelerating to almost 80 knots.
Engine Power Loss and Aircraft Behavior
During the takeoff roll, the left engine experienced a reduction in power. The airplane began to settle but did not touch the runway. Subsequently, the left engine increased in power, then decreased again, and the airplane drifted to the left.
Off-Airport Landing
The pilot maneuvered the airplane over a fence, ditch, and trees before landing in a field. Upon landing, the main landing gear collapsed, and the airplane collided with trees.
Post-Accident Examination
An examination of the airplane by the Federal Aviation Administration (FAA) revealed no evidence of a mechanical failure of either engine. Water was present in the left engine gascolator sump bowl and internal baffle assembly. Congealed contaminants were found on the fuel screen. Additionally, the No. 2, 3, and 6 cylinder sparkplugs and piston domes appeared white in color.