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Buford, GA
THE HELICOPTER WAS OBSERVED TO SLOW DOWN OVER THE PARKING LOT THEN CONTINUED OUT OVER THE LAKE. A PUFF OF SMOKE WAS OBSERVED AROUND THE REAR OF THE ENGINE AREA AND THE HELICOPTER FISHTAILED AS IT ALMOST CAME TO A STOP THEN DROPPED INTO THE WATER NOSE FIRST. IT SANK ALMOST IMMEDIATELY. EXAMINATION OF THE AIRCRAFT REVEALED A HOLE IN THE CRANKCASE. THE FRACTURE SURFACES INDICATED AN INTERNAL TO EXTERNAL PUCTURE. FURTHER EXAMINATION REVEALED A FATIGUE FAILURE OF A ROD CAP BOLT AND SUBSEQUENT SEPARATION OF THE ROD FROM THE CRANKSHAFT. EXTENSIVE DAMAGE TO THE INTERNAL COMPONENTS OF THE ENGINE WAS OBSERVED. THE PILOT WAS A LOW TIME HELICOPTER PILOT WHO COULD NOT SWIM AND WAS AFRAID OF THE WATER.
THE HELICOPTER WAS OBSERVED TO SLOW DOWN OVER THE PARKING LOT THEN CONTINUED OUT OVER THE LAKE. A PUFF OF SMOKE WAS OBSERVED AROUND THE REAR OF THE ENGINE AREA AND THE HELICOPTER FISHTAILED AS IT ALMOST CAME TO A STOP THEN DROPPED INTO THE WATER NOSE FIRST. IT SANK ALMOST IMMEDIATELY. EXAMINATION OF THE AIRCRAFT REVEALED A HOLE IN THE CRANKCASE. THE FRACTURE SURFACES INDICATED AN INTERNAL TO EXTERNAL PUCTURE. FURTHER EXAMINATION REVEALED A FATIGUE FAILURE OF A ROD CAP BOLT AND SUBSEQUENT SEPARATION OF THE ROD FROM THE CRANKSHAFT. EXTENSIVE DAMAGE TO THE INTERNAL COMPONENTS OF THE ENGINE WAS OBSERVED. THE PILOT WAS A LOW TIME HELICOPTER PILOT WHO COULD NOT SWIM AND WAS AFRAID OF THE WATER.