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Caldwell, NJ
THE PILOT FAILED TO ACTIVATE THE FUEL TRANSFER PUMP AFTER TAKEOFF AND UPON ARRIVAL AT HIS DESTINATION, HE EXPERIENCED A POWER LOSS DUE TO FUEL STARVATION DURING A GO-AROUND. THE AIRPLANE USES A 5 GALLON HEADER TANK TO GRAVITY FEED THE ENGINE. ACCORDING TO THE PILOT THE AIRPLANE USES 5 GALLONS OF FUEL BETWEEN MT. HOLLY, NEW JERSEY, AND CALDWELL, NEW JERSEY. ON SCENE EXAMINATION BY THE FAA FOUND THE MAIN AND AUXILIARY FUEL TANKS RUPTURED, AND THE HEADER FUEL TANK EMPTY AND NOT RUPTURED.
THE FAILURE OF THE PILOT TO MONITOR HIS FUEL SUPPLY WHICH RESULTED IN THE POWER LOSS. A FACTOR IN THE ACCIDENT WAS UNSUITABLE TERRAIN.
THE PILOT FAILED TO ACTIVATE THE FUEL TRANSFER PUMP AFTER TAKEOFF AND UPON ARRIVAL AT HIS DESTINATION, HE EXPERIENCED A POWER LOSS DUE TO FUEL STARVATION DURING A GO-AROUND. THE AIRPLANE USES A 5 GALLON HEADER TANK TO GRAVITY FEED THE ENGINE. ACCORDING TO THE PILOT THE AIRPLANE USES 5 GALLONS OF FUEL BETWEEN MT. HOLLY, NEW JERSEY, AND CALDWELL, NEW JERSEY. ON SCENE EXAMINATION BY THE FAA FOUND THE MAIN AND AUXILIARY FUEL TANKS RUPTURED, AND THE HEADER FUEL TANK EMPTY AND NOT RUPTURED.