ATL07LA012

According to the pilot, during the takeoff climb at about 100 to 150 feet above ground level the engine shut down. He rolled the airplane level, pushed the nose over, and attempted a landing in a turf field. The airplane struck the ground substantially damaging the airplane. The pilot egressed the airplane with assistance from witnesses. Examination of the airplane by an FAA Inspector found the landing gear, spray equipment, and the right wing separated from the airframe. Fuel was observed in both fuel tanks. Examination of the engine found the propeller separated from the engine crankshaft and the engine was seized due to impact damage. The engine was rotated 90-degrees within the engine mounts. Both magnetos and the fuel manifold were observed impact damaged. Oil was observed on the oil dipstick when it was removed. According to witnesses on the ground the engine was not running smoothly from the time of taxi through the takeoff and subsequent engine shut-down. The FAA Inspector further stated that the aircraft operator did not hold an FAA 14 CFR Part 137 Aerial Application Certificate at the time of the accident, as required by FAA regulation.

On October 21, 2006, at 1605 eastern daylight time, a Cessna A188B, N9176R, registered to a private owner, operating as a aerial application flight, collided with the ground during following loss of engine power shortly after takeoff from a field in New Bern, North Carolina. Visual meteorological conditions prevailed and no flight plan was filed. The airplane sustained substantial damage, and the airline transport-rated pilot received minor injuries. The flight was originating at the time of the accident,

According to the pilot, during the takeoff climb at about 100 to 150 feet above ground level the engine shut down. He rolled the airplane level, pushed the nose over, and attempted a landing in a turf field. The airplane struck the ground substantially damaging the airplane. The pilot egressed the airplane with assistance from witnesses.

Examination of the airplane by an FAA Inspector found the landing gear, spray equipment, and the right wing separated from the airframe. Fuel was observed in both fuel tanks. Examination of the engine found the propeller separated from the engine crankshaft and the engine was seized due to impact damage. The engine was rotated 90-degrees within the engine mounts. Both magnetos and the fuel manifold were observed impact damaged. Oil was observed on the oil dipstick when it was removed. According to witnesses on the ground the engine was not running smoothly from the time of taxi through the takeoff and subsequent engine shut-down. The FAA Inspector further stated that the aircraft operator did not hold an FAA 14 CFR Part 137 Aerial Application Certificate at the time of the accident, as required by FAA regulation.