What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Aircraft crashed on landing due to a strong crosswind. (.4)the private pilot attempted to compensate for crosswind conditions during final approach in the twin-engine airplane with the use of power. He began to drift off the east (left) side of the runway, and he stated that the right engine did not respond to throttle inputs during the landing. He lost directional control of the airplane and impacted rough, grassy terrain off the edge of the runway. The landing gear collapsed and the airplane was substantially damaged. Examination of both propellers revealed damage consistent with applied power on the left engine, and no power on the right engine. An examination of the maintenance records revealed that the engine had recently been rebuilt by the manufacturer and installed on the airplane. Prior to the accident flight, it underwent an annual inspection and was operated for 6.2 hours during six flights with no problems noted. An examination of the right engine throttle controls and a functional test of the right engine did not reveal any evidence of preimpact mechanical discrepancies that would have resulted in a power loss or hesitation.
As the FAA filed it
AIRCRAFT CRASHED ON LANDING DUE TO A STRONG CROSSWIND. (.4)THE PRIVATE PILOT ATTEMPTED TO COMPENSATE FOR CROSSWIND CONDITIONS DURING FINAL APPROACH IN THE TWIN-ENGINE AIRPLANE WITH THE USE OF POWER. HE BEGAN TO DRIFT OFF THE EAST (LEFT) SIDE OF THE RUNWAY, AND HE STATED THAT THE RIGHT ENGINE DID NOT RESPOND TO THROTTLE INPUTS DURING THE LANDING. HE LOST DIRECTIONAL CONTROL OF THE AIRPLANE AND IMPACTED ROUGH, GRASSY TERRAIN OFF THE EDGE OF THE RUNWAY. THE LANDING GEAR COLLAPSED AND THE AIRPLANE WAS SUBSTANTIALLY DAMAGED. EXAMINATION OF BOTH PROPELLERS REVEALED DAMAGE CONSISTENT WITH APPLIED POWER ON THE LEFT ENGINE, AND NO POWER ON THE RIGHT ENGINE. AN EXAMINATION OF THE MAINTENANCE RECORDS REVEALED THAT THE ENGINE HAD RECENTLY BEEN REBUILT BY THE MANUFACTURER AND INSTALLED ON THE AIRPLANE. PRIOR TO THE ACCIDENT FLIGHT, IT UNDERWENT AN ANNUAL INSPECTION AND WAS OPERATED FOR 6.2 HOURS DURING SIX FLIGHTS WITH NO PROBLEMS NOTED. AN EXAMINATION OF THE RIGHT ENGINE THROTTLE CONTROLS AND A FUNCTIONAL TEST OF THE RIGHT ENGINE DID NOT REVEAL ANY EVIDENCE OF PREIMPACT MECHANICAL DISCREPANCIES THAT WOULD HAVE RESULTED IN A POWER LOSS OR HESITATION.
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 N3425Q · 1
Matched to the same aircraft by N-number and date.