What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Aircraft took off from runway, lost power at 50FT AGL, landed straight ahead, swerved off runway into safety area. (.4)the pilot performed a preflight inspection and observed the fuel tanks were half empty. After an uneventful local flight, the pilot departed for another flight. During the initial climb after takeoff, about 75 feet, the engine stopped. The pilot performed a forced landing, and the airplane came to rest left wing low. Examination of the wreckage revealed 7 gallons of uncontaminated automotive gasoline in the left fuel tank, and no fuel in the right tank. The fuel selector valve was found in the 'both' position, and the left fuel cap was found open. The pilot could not recall if he secured it properly during his preflight inspection. Additionally, the engine was test run satisfactorily using fuel that was drained from the airplane. The airplane's total fuel capacity was 39 gallons, of which 36 was usable. It was last refueled 8 months prior to the accident with 28.2 gallons of automotive gasoline. The airplane had been flown for 3/10 of an hour on a ferry flight for an annual inspection, 4 days prior to the accident, and had accumulated 1.38 hours since the annual inspection. According to the owner's manual, fuel consumption in cruise flight at 75% power at 2,500 feet was 8.5 gallons per hour.
As the FAA filed it
AIRCRAFT TOOK OFF FROM RUNWAY, LOST POWER AT 50FT AGL, LANDED STRAIGHT AHEAD, SWERVED OFF RUNWAY INTO SAFETY AREA. (.4)THE PILOT PERFORMED A PREFLIGHT INSPECTION AND OBSERVED THE FUEL TANKS WERE HALF EMPTY. AFTER AN UNEVENTFUL LOCAL FLIGHT, THE PILOT DEPARTED FOR ANOTHER FLIGHT. DURING THE INITIAL CLIMB AFTER TAKEOFF, ABOUT 75 FEET, THE ENGINE STOPPED. THE PILOT PERFORMED A FORCED LANDING, AND THE AIRPLANE CAME TO REST LEFT WING LOW. EXAMINATION OF THE WRECKAGE REVEALED 7 GALLONS OF UNCONTAMINATED AUTOMOTIVE GASOLINE IN THE LEFT FUEL TANK, AND NO FUEL IN THE RIGHT TANK. THE FUEL SELECTOR VALVE WAS FOUND IN THE 'BOTH' POSITION, AND THE LEFT FUEL CAP WAS FOUND OPEN. THE PILOT COULD NOT RECALL IF HE SECURED IT PROPERLY DURING HIS PREFLIGHT INSPECTION. ADDITIONALLY, THE ENGINE WAS TEST RUN SATISFACTORILY USING FUEL THAT WAS DRAINED FROM THE AIRPLANE. THE AIRPLANE'S TOTAL FUEL CAPACITY WAS 39 GALLONS, OF WHICH 36 WAS USABLE. IT WAS LAST REFUELED 8 MONTHS PRIOR TO THE ACCIDENT WITH 28.2 GALLONS OF AUTOMOTIVE GASOLINE. THE AIRPLANE HAD BEEN FLOWN FOR 3/10 OF AN HOUR ON A FERRY FLIGHT FOR AN ANNUAL INSPECTION, 4 DAYS PRIOR TO THE ACCIDENT, AND HAD ACCUMULATED 1.38 HOURS SINCE THE ANNUAL INSPECTION. ACCORDING TO THE OWNER'S MANUAL, FUEL CONSUMPTION IN CRUISE FLIGHT AT 75% POWER AT 2,500 FEET WAS 8.5 GALLONS PER HOUR.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N3553S · 1
Matched to the same aircraft by N-number and date.