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Pensacola, FL
SHORTLY AFTER TAKEOFF ON INITIAL CLIMB THE AIRCRAFT WAS SEEN TO CRASH BACK ON THE RUNWAY. EXAMINATION OF THE WRECKAGE REVEALED THAT THE RIGHT STABILATOR ATTACH/HINGE BOLT WAS NOT INSTALLED, AND THE LEFT STABILATOR ATTACH/HINGE BOLT WAS FOUND PARTIALLY INSTALLED AND WAS MISSING THE SECURRING NUT. THE LEFT LEADING EDGE OF THE STABILATOR WAS FOUND CRUSHED AGAINST THE SIDE OF THE FUSELAGE WITH NO SOOT FROM THE POST IMPACT FIRE PRESENT BETWEEN THE MATING SURFACES.THE AIRCRAFT HAD BEEN INSPECTED 7 DAYS BEFORE THE ACCIDENT IN ACCORDANCE WITH A 100 HOUR INSPECTION.
SHORTLY AFTER TAKEOFF ON INITIAL CLIMB THE AIRCRAFT WAS SEEN TO CRASH BACK ON THE RUNWAY. EXAMINATION OF THE WRECKAGE REVEALED THAT THE RIGHT STABILATOR ATTACH/HINGE BOLT WAS NOT INSTALLED, AND THE LEFT STABILATOR ATTACH/HINGE BOLT WAS FOUND PARTIALLY INSTALLED AND WAS MISSING THE SECURRING NUT. THE LEFT LEADING EDGE OF THE STABILATOR WAS FOUND CRUSHED AGAINST THE SIDE OF THE FUSELAGE WITH NO SOOT FROM THE POST IMPACT FIRE PRESENT BETWEEN THE MATING SURFACES.THE AIRCRAFT HAD BEEN INSPECTED 7 DAYS BEFORE THE ACCIDENT IN ACCORDANCE WITH A 100 HOUR INSPECTION.