STANTON, MN, USA
N544J
SCHREDER HP12A
THE PILOT PERFORMED HIS PREFLIGHT CHECKS INCLUDING A FLIGHT CONTROL CHECK. AFTER LIFT OFF THE PILOT COULD NOT CONTROL THE PITCH OF THE GLIDER. AS THE PITCH INCREASED TO ABOUT 30 DEGREES HE ELECTED TO RELEASE THE TOW CABLE FROM THE TOW AIRCRAFT. THE GLIDER STALLED AND 'FELL OVER ON RIGHT WING' AT ABOUT 50 TO 100 FEET AND CONTACTED THE GROUND AT ABOUT A 40 DEGREE NOSE LOW ATTITUDE. EXAMINATION REVEALED THAT THE RUDDERVATOR WAS NOT PROPERLY INSTALLED.
Source: NTSB Aviation Accident Database
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