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Lancaster, CA
DURING AN AERIAL APPLICATION FLIGHT, JUST AFTER TAKEOFF, THE NOSE OF THE HELICOPTER SUDDENLY PITCHED UP. THE PILOT REDUCED POWER TO KEEP FROM CLIMBING. THE FORE/AFT CYCLIC CONTROL HAD NO EFFECT. THE HELICOPTER SETTLED TO THE GROUND RESULTING IN SUBSTANTIAL DAMAGE. INSPECTION OF THE FORE/AFT CONTROL LINKAGE, REVEALED THAT A BOLT WAS MISSING BETWEEN THE SWASH PLATE AND THE PUSH PULL TUBE.
DURING AN AERIAL APPLICATION FLIGHT, JUST AFTER TAKEOFF, THE NOSE OF THE HELICOPTER SUDDENLY PITCHED UP. THE PILOT REDUCED POWER TO KEEP FROM CLIMBING. THE FORE/AFT CYCLIC CONTROL HAD NO EFFECT. THE HELICOPTER SETTLED TO THE GROUND RESULTING IN SUBSTANTIAL DAMAGE. INSPECTION OF THE FORE/AFT CONTROL LINKAGE, REVEALED THAT A BOLT WAS MISSING BETWEEN THE SWASH PLATE AND THE PUSH PULL TUBE.