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Livermore Falls, ME
THE CITABRIA 7GCBC WAS OBSERVED TO MAKE A LOOP. THE LEFT WING BENT UPWARD AT THE STRUT ATTACH POINT AS THE AIRCRAFT WAS AT THE BOTTOM OF THE LOOP AND RECOVERING TO LEVEL FLIGHT. THE AIRCRAFT WAS THEN OBSERVED TO DESCEND IN A RIGHT SPIRAL AND NOT RECOVER PRIOR TO CONTACT WITH THE GROUND. IMPROPER LEFT FWD WING SPAR MANUFACTURING WAS FOUND. NO PROBLEMS WERE NOTED ON THE LEFT REAR WING SPAR. THE FWD WING SPAR FAILED WITH TENSION ON THE TOP AND COMPRESSION ON THE BOTTOM. THE REAR WING SPAR HAD TENSION ON THE BOTTOM AND COMPRESSION ON THE TOP. THE LEFT WING OUTBOARD OF THE STRUT ATTACH POINT SEPARATED FROM THE AIRCRAFT PRIOR TO IMPACT. THE LEFT AILERON WAS BENT UPWARD 90 DEGREES AT THE MIDDLE HINGE POINT WHICH CORRESPONDS TO THE STRUT ATTACH POINT. INVESTIGATION REVEALED THAT THE SLOPE OF THE GRAIN ON THE FWD WING SPAR EXCEEDED SPECIFICATIONS. ALSO TWO AREAS OF POOR BONDING WERE FOUND. THE AIRCRAFT LOG BOOKS WERE NOT FOUND.
THE CITABRIA 7GCBC WAS OBSERVED TO MAKE A LOOP. THE LEFT WING BENT UPWARD AT THE STRUT ATTACH POINT AS THE AIRCRAFT WAS AT THE BOTTOM OF THE LOOP AND RECOVERING TO LEVEL FLIGHT. THE AIRCRAFT WAS THEN OBSERVED TO DESCEND IN A RIGHT SPIRAL AND NOT RECOVER PRIOR TO CONTACT WITH THE GROUND. IMPROPER LEFT FWD WING SPAR MANUFACTURING WAS FOUND. NO PROBLEMS WERE NOTED ON THE LEFT REAR WING SPAR. THE FWD WING SPAR FAILED WITH TENSION ON THE TOP AND COMPRESSION ON THE BOTTOM. THE REAR WING SPAR HAD TENSION ON THE BOTTOM AND COMPRESSION ON THE TOP. THE LEFT WING OUTBOARD OF THE STRUT ATTACH POINT SEPARATED FROM THE AIRCRAFT PRIOR TO IMPACT. THE LEFT AILERON WAS BENT UPWARD 90 DEGREES AT THE MIDDLE HINGE POINT WHICH CORRESPONDS TO THE STRUT ATTACH POINT. INVESTIGATION REVEALED THAT THE SLOPE OF THE GRAIN ON THE FWD WING SPAR EXCEEDED SPECIFICATIONS. ALSO TWO AREAS OF POOR BONDING WERE FOUND. THE AIRCRAFT LOG BOOKS WERE NOT FOUND.