BISHOP, CA, USA
N97DT
Laister NUGGET
THE PILOT OF THE GLIDER ENCOUNTERED EXTREME TURBULENCE DURING CRUISE FLIGHT. THE TURBULENCE BUCKLED THE WINGS, CRACKED THE FUSELAGE, EXTENDED THE LANDING GEAR AND RENDERED THE FLAPS INOPERATIVE. THE PILOT FAILED TO PROPERLY PLAN THE NO-FLAP LANDING APPROACH AND INADVERTENTLY RETRACTED THE LANDING GEAR. THE GLIDER OVERSHOT THE POINT OF INTENDED LANDING AND SLID INTO A RAVINE OFF THE DEPARTURE END OF THE RUNWAY.
THE PILOT-IN-COMMAND'S IMPROPERLY PLANNED NO-FLAP LANDING APPROACH; FAILURE TO FOLLOW THE CHECKLIST; AND INADVERTENT GEAR RETRACTION. FACTORS CONTRIBUTING TO THE ACCIDENT WERE THE BUCKLING OF THE WING SKIN, CRACKING OF THE FUSELAGE AND THE INOPERATIVE FLAPS.
Source: NTSB Aviation Accident Database
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