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Sabine Pass, TX
WHILE EN ROUTE AT AN ALT OF 500 TO 700 FT, THE #1 ENG SPOOLED DOWN. THE PLT SECURED THE #1 ENG & TURNED BACK TOWARD THE HELIPORT TO MAKE A SINGLE ENG LANDING. HOWEVER, HE COULD NOT MAINTAIN LEVEL FLT & THE ROTOR RPM BEGAN DROPPING. THE PLT NOTED THAT THE #2 ENG HAD HI TEMP (ABOVE 900 DEGS) & LOW TORQUE. SUBSEQUENTLY, HE INFLATED THE POPOUT FLOATS & MADE A PARTIAL POWER LANDING IN A MARSH. DUE TO LOW ROTOR RPM, THE HELICOPTER TOUCHED DOWN HARD & WAS DAMAGED. THE #1 ENG WAS REMOVED & CHECKED IN A TEST CELL & IT OPERATED NORMALLY. THE #2 ENG WAS DAMAGED; HOWEVER, IT'S FUEL MANAGEMENT SYS CHECKED NORMAL. THE ACFT WAS BEING FLOWN IN RAIN SHOWERS WITHOUT USING THE ENG ANTI-ICE. OPERATOR PERSONNEL SUSPECTED THAT INLET ICING CAUSED THE #1 ENG TO FLAME OUT & THE #2 ENG TO LOSE PARTIAL POWER. A WITNESS ESTIMATED THE SURFACE AIR TEMP WAS 33 DEGS.
WHILE EN ROUTE AT AN ALT OF 500 TO 700 FT, THE #1 ENG SPOOLED DOWN. THE PLT SECURED THE #1 ENG & TURNED BACK TOWARD THE HELIPORT TO MAKE A SINGLE ENG LANDING. HOWEVER, HE COULD NOT MAINTAIN LEVEL FLT & THE ROTOR RPM BEGAN DROPPING. THE PLT NOTED THAT THE #2 ENG HAD HI TEMP (ABOVE 900 DEGS) & LOW TORQUE. SUBSEQUENTLY, HE INFLATED THE POPOUT FLOATS & MADE A PARTIAL POWER LANDING IN A MARSH. DUE TO LOW ROTOR RPM, THE HELICOPTER TOUCHED DOWN HARD & WAS DAMAGED. THE #1 ENG WAS REMOVED & CHECKED IN A TEST CELL & IT OPERATED NORMALLY. THE #2 ENG WAS DAMAGED; HOWEVER, IT'S FUEL MANAGEMENT SYS CHECKED NORMAL. THE ACFT WAS BEING FLOWN IN RAIN SHOWERS WITHOUT USING THE ENG ANTI-ICE. OPERATOR PERSONNEL SUSPECTED THAT INLET ICING CAUSED THE #1 ENG TO FLAME OUT & THE #2 ENG TO LOSE PARTIAL POWER. A WITNESS ESTIMATED THE SURFACE AIR TEMP WAS 33 DEGS.