皇冠体育app

Hal-26 Push Pak, G-AVPO

Summary:

During the landing roll, the aircraft 鈥榞round looped鈥� after it had curved to the left of the grass runway and struck a hedge, despite the application of full right rudder by the pilot. 皇冠体育app pilot assessed the cause of the loss of directional control as being due to the tailwheel sinking into a patch of soft ground, and that the springs which connected it to the rudder circuit were insufficiently strong to counteract the wheel castoring forces.

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