TORRANCE, CA, USA
N8557Z
ROBINSON R22A
ACCORDING TO STATEMENTS FROM BOTH THE INSTRUCTOR AND THE STUDENT, FOUR PRACTICE AUTOROTATIONS HAD ALREADY BEEN PERFORMED WITH POWER RECOVERIES PRIOR TO TOUCH DOWN. THE PILOTS NOTED THAT THE FIFTH AUTOROTATION PROCEEDED NORMALLY UNTIL ABOUT 40 FEET AGL WHEN THROTTLE AND COLLECTIVE WAS ADDED TO BEGIN THE POWER RECOVERY. ACCORDING TO BOTH PILOTS STATEMENTS, THE ENGINE DID NOT RESPOND WHEN THE THROTTLE WAS INCREASED. THE HELICOPTER TOUCHED DOWN HARD, SLID ALONG THE GROUND AND ROLLED OVER ON ITS RIGHT SIDE AFTER THE RIGHT SKID ENCOUNTERED SOFT SOIL. THE ENGINE AND HELICOPTER WERE EXAMINED WITH NO EVIDENCE OF A SYSTEM FAILURE OR MALFUNCTION. THE ENGINE WAS STARTED IN THE HELICOPTER AND RUN FOR 10 MINUTES. DURING THE TEST RUN, THE ENGINE WAS CYCLED THROUGHOUT ITS NORMAL OPERATING RANGE.
THIS ACCIDENT WAS A DYNAMIC ROLL OVER DUE TO THE RIGHT SKID ENCOUNTERING SOFT SOIL DURING THE FORCED LANDING.
Source: NTSB Aviation Accident Database
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