CHITINA, AK, USA
N525BB
Hammer AVID FLYER
The pilot was departing in a homebuilt airplane from a remote airstrip. After departure, the airplane climbed to about 250 feet above the ground, and then the engine suddenly lost power. The pilot performed a 180 degree turn back toward the runway, but landed in rough terrain, just short of the runway. The engine was overhauled 5 hours before the accident, and one piston was replaced with an oversize piston. Following the accident, an examination of the engine revealed the oversize piston was seized in the cylinder. The seized piston was found to be the same size as the cylinder bore.
On May 3, 1997, about 1900 Alaska daylight time, a wheel equipped homebuilt, experimental Hammer, Avid Flyer airplane, N525BB, crashed during the initial takeoff climb from the Chitina Airport, Chitina, Alaska. The airplane was being operated as a visual flight rules (VFR) cross-country personal flight to McCarthy, Alaska, when the accident occurred. The airplane, operated by the pilot, sustained substantial damage. The certificated private pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed. On May 4, 1997, at 1222, the pilot reported in a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), that he just departed runway 13 at Chitina and climbed to about 250 feet above the ground. The engine, a Rotax 618, suddenly quit. The pilot made a 180 degree turn to return to the runway. The pilot performed an emergency landing short of the runway into low brush. The airplane received damage to the fuselage and wingtips. On November 20, 1997, the pilot reported the engine was last overhauled 5 hours before the accident at a facility in Birchwood, Alaska. During the overhaul, one of the engine's two pistons was replaced with an oversize piston. The piston cylinder was also bored oversize. The second engine piston was not replaced, and remained standard size. After the accident, the pilot sent the engine to an overhaul facility in San Leandro, California. The examination revealed the oversize engine piston was found seized in the cylinder. Measurement of the oversize piston revealed it was the same size as the cylinder bore, both measuring 2.998 inches.
improper overhaul of the engine, which resulted in a seized piston and resultant loss of engine power. Rough terrain in the emergency landing area was a related factor.
Source: NTSB Aviation Accident Database
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