What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) privacy data omitted aircraft enroute from cmh to ottawa, Canada. At approx 7,500 ft. aircraft experienced loss of power. Pilot stated prop continued to windmill as he switched fuel sources and magneto's, no help. He then attempted to divert and land at 10G. On approach right wing struck tree and departed aircraft. Aircraft impacted ground and cartwheeled approx 50 ft. until coming to rest. Left wing was broken from fuselage and aircraft destroyed. Pilot sustained numerous injuries, but none life threatening. Initial investigation found significant water and debris in fuel selector valve sump drain collection point. Aircraft was fueled on 3/4/05 in cmh, then sat unhangered until it departed on 3/14/05. During this timeframe columbus, OH, experienced significant snowfall. Further investigation found the gaskets for fuel caps on the main and wingtip tanks hard and not pliable. The right main tank fuel cap was loose in secured position. The fuel system from the fuel selector valve, through the lines and into the engine did not contain any significant presence of fuel.
As the FAA filed it
(-23) ^PRIVACY DATA OMITTED^ AIRCRAFT ENROUTE FROM CMH TO OTTAWA, CANADA. AT APPROX 7,500 FT. AIRCRAFT EXPERIENCED LOSS OF POWER. PILOT STATED PROP CONTINUED TO WINDMILL AS HE SWITCHED FUEL SOURCES AND MAGNETO'S, NO HELP. HE THEN ATTEMPTED TO DIVERT AND LAND AT 10G. ON APPROACH RIGHT WING STRUCK TREE AND DEPARTED AIRCRAFT. AIRCRAFT IMPACTED GROUND AND CARTWHEELED APPROX 50 FT. UNTIL COMING TO REST. LEFT WING WAS BROKEN FROM FUSELAGE AND AIRCRAFT DESTROYED. PILOT SUSTAINED NUMEROUS INJURIES, BUT NONE LIFE THREATENING. INITIAL INVESTIGATION FOUND SIGNIFICANT WATER AND DEBRIS IN FUEL SELECTOR VALVE SUMP DRAIN COLLECTION POINT. AIRCRAFT WAS FUELED ON 3/4/05 IN CMH, THEN SAT UNHANGERED UNTIL IT DEPARTED ON 3/14/05. DURING THIS TIMEFRAME COLUMBUS, OH, EXPERIENCED SIGNIFICANT SNOWFALL. FURTHER INVESTIGATION FOUND THE GASKETS FOR FUEL CAPS ON THE MAIN AND WINGTIP TANKS HARD AND NOT PLIABLE. THE RIGHT MAIN TANK FUEL CAP WAS LOOSE IN SECURED POSITION. THE FUEL SYSTEM FROM THE FUEL SELECTOR VALVE, THROUGH THE LINES AND INTO THE ENGINE DID NOT CONTAIN ANY SIGNIFICANT PRESENCE OF FUEL.