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E. Cameron
DURING AN APPROACH TO AN OIL DRILLING RIG PLATFORM, THE ENGINE DECELERATED AS THE PILOT STARTED TO ALL POWER. WITH THE ACFT BELOW THE LANDING AREA, HE MANEUVERED TO MISS THE PLATFORM & INITIATED AN AUTOROTATIVE LANDING. HE MADE A MAYDAY CALL & TRIED TO ELECTRICALLY DEPLOY THE EMERGENCY FLOATS; HOWEVER, THE RIGHT FLOAT FAILED TO INFLATE & THERE WAS INSUFFICIENT TIME FOR MANUAL DEPLOYMENT. IMMEDIATELY ON TOUCHDOWN, THE HELICOPTER ROLLED OVER & BEGAN TO FILL WITH WATER. REPORTEDLY, THERE WAS ONLY MINOR DAMAGE FROM WATER IMMERSION. NO PREIMPACT DISCREPANCIES WERE FOUND THAT WOULD HAVE CAUSED THE POWER LOSS. THE WIRES TO THE RIGHT FLOAT (FOR ELECTRICAL DEPLOYMENT) WERE WORN IN TWO AT A CENTER HEX HEAD SCREW. A FLEET INSPECTION OF 37 ACFT REVEALED THAT 60% WERE WORN THRU IN THE SAME AREA.
DURING AN APPROACH TO AN OIL DRILLING RIG PLATFORM, THE ENGINE DECELERATED AS THE PILOT STARTED TO ALL POWER. WITH THE ACFT BELOW THE LANDING AREA, HE MANEUVERED TO MISS THE PLATFORM & INITIATED AN AUTOROTATIVE LANDING. HE MADE A MAYDAY CALL & TRIED TO ELECTRICALLY DEPLOY THE EMERGENCY FLOATS; HOWEVER, THE RIGHT FLOAT FAILED TO INFLATE & THERE WAS INSUFFICIENT TIME FOR MANUAL DEPLOYMENT. IMMEDIATELY ON TOUCHDOWN, THE HELICOPTER ROLLED OVER & BEGAN TO FILL WITH WATER. REPORTEDLY, THERE WAS ONLY MINOR DAMAGE FROM WATER IMMERSION. NO PREIMPACT DISCREPANCIES WERE FOUND THAT WOULD HAVE CAUSED THE POWER LOSS. THE WIRES TO THE RIGHT FLOAT (FOR ELECTRICAL DEPLOYMENT) WERE WORN IN TWO AT A CENTER HEX HEAD SCREW. A FLEET INSPECTION OF 37 ACFT REVEALED THAT 60% WERE WORN THRU IN THE SAME AREA.