SYRACUSE, KS, USA
N5781C
CESSNA 170A
WHILE THE PLT WAS MAKING HIS SECOND LANDING, THE ACFT BEGAN TO ROCK BACK & FORTH DURING THE ROLL-OUT. HE ADDED POWER TO CORRECT THE OSCILLATION, BUT SAID THE POWER HAD THE OPPOSITE EFFECT. HE LOST DIRECTIONAL CONTROL & THE ACFT SWERVED OFF THE LEFT SIDE OF THE RWY. THE RIGHT MAIN GEAR COLLAPSED & THE RIGHT WING & PROP WERE DAMAGED. THE PLT BELIEVED HE RELEASED CONTROL PRESSURE WHEN THE AIRSPEED WAS TOO HIGH, THEN OVER CONTROLLED WITH THE RUDDER.
Source: NTSB Aviation Accident Database
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