MS STATE UNIV, MS, USA
N9944J
SCHWEIZER SGS 1-26C
AN AUTO TOW WAS BEING USED TO LAUNCH THE GLIDER. AS THE GLIDER REACHED AN ALT OF ABOUT 200 TO 250 FT, THE AUTO DRIVER REALIZED HE WAS EXCEEDING THE PLANNED SPEED, SO HE SLOWED THE AUTO BY 5 TO 10 MPH. AT THAT TIME, THE TOW LINE SLACKENED,THEN RELEASED AUTOMATICALLY. THE STUDENT PLT DECIDED TO LAND STRAIGHT AHEAD INTO AN UNCUT HAY FIELD. DRG THE LANDING, THE HAY CAUGHT THE RIGHT WING & THE GLIDER GROUND LOOPED, DAMAGING THE WING & FUSELAGE. THE RECOGNIZED SOARING PUBLICATIONS ADVISED THAT 180 DEG TURNS BACK TO THE RWY FOR DOWNWIND LNDGS WERE SAFE & PERMISSIBLE AT ALTITUDES OF 200 FT OR MORE.
IMPROPER IN-FLIGHT PLANNING/DECISON BY THE PILOT. CONTRIBUTING FACTORS WERE: FAILURE OF THE TOW VEHICLE DRIVER TO USE/MAINTAIN THE PROPER SPEED, THE PILOT'S LACK OF TOTAL FLYING EXPERIENCE, AND HIGH VEGETATION (UNCUT HAY).
Source: NTSB Aviation Accident Database
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