What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Aircraft engine quit on takeoff at a low altitude. (.4)the pilot departed with the fuel selector set to the 'both' tanks position. However, during the flight fuel appeared to have been mostly used from the right tank. To equalize the burn off, he repositioned the fuel selector to the left tank only position. Fuel continued to be consumed out of the right tank, and the engine quit when the right fuel tank gauge registered empty and the left tank gauge registered 3/4 full. The pilot made a forced landing on a road. Thereafter, the pilot examined his airplane and noted that the fuel selector handle was 'real loose.' The pilot manually siphoned between 12 and 15 gallons of fuel out of the left tank, poured it into the right tank, and took off. Several seconds into the initial climb, between 100 and 150 feet above ground level, all engine power was lost again. Unable to return to the road, the pilot made a forced landing on rough terrain. The fuel tank selector assembly was examined and its control shaft was found disconnected at its attachment to the fuel valve assembly.
As the FAA filed it
AIRCRAFT ENGINE QUIT ON TAKEOFF AT A LOW ALTITUDE. (.4)THE PILOT DEPARTED WITH THE FUEL SELECTOR SET TO THE 'BOTH' TANKS POSITION. HOWEVER, DURING THE FLIGHT FUEL APPEARED TO HAVE BEEN MOSTLY USED FROM THE RIGHT TANK. TO EQUALIZE THE BURN OFF, HE REPOSITIONED THE FUEL SELECTOR TO THE LEFT TANK ONLY POSITION. FUEL CONTINUED TO BE CONSUMED OUT OF THE RIGHT TANK, AND THE ENGINE QUIT WHEN THE RIGHT FUEL TANK GAUGE REGISTERED EMPTY AND THE LEFT TANK GAUGE REGISTERED 3/4 FULL. THE PILOT MADE A FORCED LANDING ON A ROAD. THEREAFTER, THE PILOT EXAMINED HIS AIRPLANE AND NOTED THAT THE FUEL SELECTOR HANDLE WAS 'REAL LOOSE.' THE PILOT MANUALLY SIPHONED BETWEEN 12 AND 15 GALLONS OF FUEL OUT OF THE LEFT TANK, POURED IT INTO THE RIGHT TANK, AND TOOK OFF. SEVERAL SECONDS INTO THE INITIAL CLIMB, BETWEEN 100 AND 150 FEET ABOVE GROUND LEVEL, ALL ENGINE POWER WAS LOST AGAIN. UNABLE TO RETURN TO THE ROAD, THE PILOT MADE A FORCED LANDING ON ROUGH TERRAIN. THE FUEL TANK SELECTOR ASSEMBLY WAS EXAMINED AND ITS CONTROL SHAFT WAS FOUND DISCONNECTED AT ITS ATTACHMENT TO THE FUEL VALVE ASSEMBLY.
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 N2294D · 1
Matched to the same aircraft by N-number and date.