What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Ran out of fuel and attempted to land at alternate airport, landed short of airport on highway. (.4)the pilot experience a total loss of power when beginning a descent. He reported that the fuel analyzer gauge showed that 1.5 hours of fuel was remaining, but the fuel quantity gauges were erratic. The pilot received radar vectors toward an airport, but he was unable to see it and elected to land on a road. Examination of the wreckage disclosed that there was about 1 gallon of fuel in the fuel system. The fuel tanks were not compromised. The upper surface of the left wing disclosed numerous orange/brownish streaks aft of the fuel cap. The right wing did not display any fuel streaking aft of the fuel cap. The left wing fuel tank was pressurized with water and water leaked from the cap. The right wing fuel cap was put on the left wing fuel tank. Water did not leak from the tank with the right wing fuel cap installed. The left wing fuel cap seal was brittle. Examination of the engine logbooks disclosed that the applicable airworthiness directive for the fuel cap was complied with about 33 hours before the accident.
As the FAA filed it
RAN OUT OF FUEL AND ATTEMPTED TO LAND AT ALTERNATE AIRPORT, LANDED SHORT OF AIRPORT ON HIGHWAY. (.4)THE PILOT EXPERIENCE A TOTAL LOSS OF POWER WHEN BEGINNING A DESCENT. HE REPORTED THAT THE FUEL ANALYZER GAUGE SHOWED THAT 1.5 HOURS OF FUEL WAS REMAINING, BUT THE FUEL QUANTITY GAUGES WERE ERRATIC. THE PILOT RECEIVED RADAR VECTORS TOWARD AN AIRPORT, BUT HE WAS UNABLE TO SEE IT AND ELECTED TO LAND ON A ROAD. EXAMINATION OF THE WRECKAGE DISCLOSED THAT THERE WAS ABOUT 1 GALLON OF FUEL IN THE FUEL SYSTEM. THE FUEL TANKS WERE NOT COMPROMISED. THE UPPER SURFACE OF THE LEFT WING DISCLOSED NUMEROUS ORANGE/BROWNISH STREAKS AFT OF THE FUEL CAP. THE RIGHT WING DID NOT DISPLAY ANY FUEL STREAKING AFT OF THE FUEL CAP. THE LEFT WING FUEL TANK WAS PRESSURIZED WITH WATER AND WATER LEAKED FROM THE CAP. THE RIGHT WING FUEL CAP WAS PUT ON THE LEFT WING FUEL TANK. WATER DID NOT LEAK FROM THE TANK WITH THE RIGHT WING FUEL CAP INSTALLED. THE LEFT WING FUEL CAP SEAL WAS BRITTLE. EXAMINATION OF THE ENGINE LOGBOOKS DISCLOSED THAT THE APPLICABLE AIRWORTHINESS DIRECTIVE FOR THE FUEL CAP WAS COMPLIED WITH ABOUT 33 HOURS BEFORE THE ACCIDENT.
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 N4924D · 1
Matched to the same aircraft by N-number and date.