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Warrenton, VA
AFTER LIFTOFF BOTH THE PIC AND THE PLT GETTING CHECKED OUT IN THE SCHWEIZER SGS 2-33A STATED THAT THEY ENCOUNTERED MODERATE TURBULENCE IN THE AREA. WHEN THE SAILPLANE RECHED APPROXIMATELY 200 FT AGL THE TOM ROPE SEPARATED FROM THE AIRCRAFT AND N65818 WAS FORCED TO MAKE AN EMERGENCY LANDING DURING WHICH THE ACFT WAS SUBSTANTIALLY DAMAGED AND THE PIC SUFFERED SERIOUS INJURIES. EXAMINATION OF THE WRECKAGE REVEALED THAT THE TOW HOOK RELEASE SPRING TENSION WAS SET WITHIN MANUFACTURERS LIMITS AND ALL OTHER AIRCRAFT SYSTEMS APPEARED TO WORK PROPERLY.
AFTER LIFTOFF BOTH THE PIC AND THE PLT GETTING CHECKED OUT IN THE SCHWEIZER SGS 2-33A STATED THAT THEY ENCOUNTERED MODERATE TURBULENCE IN THE AREA. WHEN THE SAILPLANE RECHED APPROXIMATELY 200 FT AGL THE TOM ROPE SEPARATED FROM THE AIRCRAFT AND N65818 WAS FORCED TO MAKE AN EMERGENCY LANDING DURING WHICH THE ACFT WAS SUBSTANTIALLY DAMAGED AND THE PIC SUFFERED SERIOUS INJURIES. EXAMINATION OF THE WRECKAGE REVEALED THAT THE TOW HOOK RELEASE SPRING TENSION WAS SET WITHIN MANUFACTURERS LIMITS AND ALL OTHER AIRCRAFT SYSTEMS APPEARED TO WORK PROPERLY.