Probable cause: The flight instructor’s inadequate in-flight fuel management, which resulted in fuel starvation and a total loss of engine power.
Detached rudder cable brings down Piper
Probable cause: The loss of yaw control due to an inadequately compressed rudder swage, which resulted from inadequate maintenance and led to the separation of the forward right rudder cable.
Loss of engine power leads to student’s forced landing
Probable cause: A total loss of engine power for reasons that could not be determined based on the available evidence.
Post-maintenance flight fatal for pilot
Probable cause: The pilot’s failure to identify the alternate runway, to perform a timely precautionary landing, and to maintain airplane control. Contributing to the accident was the failure of the left engine due to oil starvation for reasons that could not be determined based on the postaccident examination.
Attempted go-around in gusting crosswind conditions fatal for pilot
Probable cause: The pilot’s failure to maintain airplane control during an attempted go-around in gusting crosswind conditions, which resulted in an exceedance of the airplane’s critical angle of attack and a subsequent aerodynamic stall.
VFR into IMC fatal for two
Probable cause: The pilot’s decision to continue visual flight rules flight into instrument meteorological conditions, which resulted in controlled flight into mountainous terrain.
Drugs combined with vision problems fatal for two
Probable cause: The pilot’s impairment, due to his use of a combination of psychoactive drugs and a vision deficiency in his left eye, which resulted in a failure to maintain adequate altitude during final approach to landing and subsequent collision with power lines.
Loss of control proves fatal
Probable cause: The pilot’s loss of control after exceeding the airplane’s critical angle of attack during takeoff, which resulted in an aerodynamic stall.
Two die in Luscombe crash
Probable cause: The flying pilot’s excessive maneuvering of the airplane at a slow airspeed, which resulted in exceedance of the critical angle of attack and an aerodynamic stall. Contributing to the accident was the pilots’ operation of the airplane over its maximum allowable gross weight.