Beech 35 N5093C accident near Port Hadlock, Washington

Probable cause

A total loss of engine power due to fuel starvation and the pilot’s mismanagement of the available fuel.

NTSB analysis

Shortly after takeoff and during the initial climb, the cabin door opened, and the pilot elected to return to the airport. Upon entering the downwind leg of the traffic pattern, the pilot noticed that the left fuel gauge indicated full; and the right fuel gauge indicated empty. Shortly thereafter, the engine lost total power and the pilot performed a forced landing, during which the airplane impacted trees, resulting in substantial damage.

Examination of the wreckage revealed that the right main fuel tank and right tip tank had been breached during the accident sequence, while the left main wing tank and left tip tank were minimally damaged. Recovery personnel reported that about 12 gallons of aviation fuel was drained from the left main fuel tank and the left tip tank. The fuel selector handle was in the right tank position. When operated by hand, the handle moved freely through 360° rotation by hand, with each detent identified by feel. Examination revealed no mechanical anomalies with the engine or airframe that would have precluded normal operation. It is likely that the loss of engine power was the result of fuel starvation when the pilot failed to switch from the empty right main tank to the left main tank.

Text from the NTSB. Open the NTSB docket for WPR19LA064 for the full record.