NTSB Narrative Summary Released at Completion of Accident
On August 30, 2013, about 1340 eastern daylight time, a Cessna 172, N8063B, was substantially damaged during a takeoff attempt at Limington-Harmon Airport (63B), Limington, Maine. The student pilot was fatally injured. Visual meteorological conditions prevailed, and no flight plan was filed for the local solo instructional flight, which was conducted under the provisions of 14 Code of Federal Regulations Part 91.
According to several witnesses, the pilot completed an engine run-up prior to the takeoff from runway 29. Only one witness saw the accident, and he stated that after liftoff, the airplane was “swerving all over the place before it crashed.” All witnesses heard the engine operating throughout the event, with one stating that the engine “was running smooth, normal sounding.”
On-scene documentation revealed that the airplane impacted the ground to the left of, and about 2,000 feet from the beginning of the 2,973-foot runway. A wreckage trail began an estimated 50 feet left of the runway with green lens material and the remnants of the right wingtip position light. About 20 feet beyond that, heading about 220 degrees magnetic, was a 4-foot impact crater in the sandy soil. About 250 degrees, 60 feet beyond the crater, the airplane came to rest upright, facing opposite the direction of takeoff.
All flight control surfaces were located at the accident scene, and flight control continuity was confirmed to all flight control surfaces, except that the aileron interconnect cable was separated in a broomstraw manner consistent with overload. The flaps were up. The airplane’s engine compartment was bent to the right, and the underside exhibited upward and rearward crushing. The nose landing gear was fractured. The outer 2 feet of the right wing exhibited aft crush, and the right wingtip was deformed upward. The two control yokes were bent downward and to the right. There were no shoulder harnesses installed in the airplane.
The propeller exhibited chordwise scratching and streaking on both blades, with burnishing on the leading edge of one blade. Engine crankshaft continuity, compression, and spark were all confirmed. The fuel selector was in the “Both On” position, and a fuel sample taken was absent of water and debris.
A witness described the wind as “light” and from the right of the runway, while the nearest weather reporting airport, about 17 nautical miles the southeast, recorded winds as variable at 3 knots at 1351, and from 170 degrees true at 8 knots at 1451.