What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Aircraft appeared to run out of fuel. Pilot made statement that he had been advised this was a normal fuel leak for this type of aircraft. Statements show aircraft had a fuel leak history. (.4)following loss of engine power, an emergency off-airport landing was made on a city street. Examination of the aircraft revealed an abraded solid aluminum fuel line between the fuel selector valve and the engine. When the fuel selector valve was turned on, a knife-shaped stream of fuel emanated from the line. When viewed with an inspection mirror, the abraded area appeared v-shaped (grooved) and there was a hole approximately 1/16-inch diameter though the wall of the tube at the deepest part of the groove. Dried, crusty fuel stains were present on the fuel line over a distance of approximately 2 inches. Adjacent to the area of the leak there was a bnc-type antenna connector on an unused marker beacon antenna mounted on the lower fuselage. An annual and pre-buy inspection was performed on the aircraft 2.6 months prior to the accident. The hangar proprietor reported that the aircraft had leaked fuel onto the hangar floor since some time before the insp ection, and the aircraft's previous owner had turned off the fuel selector to stop the leaking. The aricraft had flown approximately 10 hours since the inspection.
As the FAA filed it
(-23) AIRCRAFT APPEARED TO RUN OUT OF FUEL. PILOT MADE STATEMENT THAT HE HAD BEEN ADVISED THIS WAS A NORMAL FUEL LEAK FOR THIS TYPE OF AIRCRAFT. STATEMENTS SHOW AIRCRAFT HAD A FUEL LEAK HISTORY. (.4)FOLLOWING LOSS OF ENGINE POWER, AN EMERGENCY OFF-AIRPORT LANDING WAS MADE ON A CITY STREET. EXAMINATION OF THE AIRCRAFT REVEALED AN ABRADED SOLID ALUMINUM FUEL LINE BETWEEN THE FUEL SELECTOR VALVE AND THE ENGINE. WHEN THE FUEL SELECTOR VALVE WAS TURNED ON, A KNIFE-SHAPED STREAM OF FUEL EMANATED FROM THE LINE. WHEN VIEWED WITH AN INSPECTION MIRROR, THE ABRADED AREA APPEARED V-SHAPED (GROOVED) AND THERE WAS A HOLE APPROXIMATELY 1/16-INCH DIAMETER THOUGH THE WALL OF THE TUBE AT THE DEEPEST PART OF THE GROOVE. DRIED, CRUSTY FUEL STAINS WERE PRESENT ON THE FUEL LINE OVER A DISTANCE OF APPROXIMATELY 2 INCHES. ADJACENT TO THE AREA OF THE LEAK THERE WAS A BNC-TYPE ANTENNA CONNECTOR ON AN UNUSED MARKER BEACON ANTENNA MOUNTED ON THE LOWER FUSELAGE. AN ANNUAL AND PRE-BUY INSPECTION WAS PERFORMED ON THE AIRCRAFT 2.6 MONTHS PRIOR TO THE ACCIDENT. THE HANGAR PROPRIETOR REPORTED THAT THE AIRCRAFT HAD LEAKED FUEL ONTO THE HANGAR FLOOR SINCE SOME TIME BEFORE THE INSP ECTION, AND THE AIRCRAFT'S PREVIOUS OWNER HAD TURNED OFF THE FUEL SELECTOR TO STOP THE LEAKING. THE ARICRAFT HAD FLOWN APPROXIMATELY 10 HOURS SINCE THE INSPECTION.
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 N9406X · 1
Matched to the same aircraft by N-number and date.