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Fullerton, CA
THE PILOT OF THE PIPER PA-32-260, THAT HAD BEEN MODIFIED TO A MODEL PA-32-300 BY EXCHANGING THE ENGINE, TAXIED TO THE END OF A 3121 FOOT RUNWAY FOR TAKEOFF WITH CALM WIND CONDITIONS. THE AIRCRAFT LOAD CONSISTED OF FULL FUEL TANKS, PILOT AND PASSENGER, AND 30 POUNDS OF LUGGAGE. A GROUND WITNESS OBSERVED THE AIRCRAFT TO ROLL APPROXIMATELY 2850 FEET BEFORE BECOMING AIRBORNE. IMMEDIATELY AFTER TAKEOFF THE AIRCRAFT TOUCHED DOWN ON A FLAT ROOF OF A COMMERICAL BUILDING, COLLIDED WITH THE PARAPET AND CRASHED INTO THE STREET BELOW. THE POST CRASH ENGINE EXAM REVEALED RUST PARTICLES AND WATER THROUGHOUT THE FUEL SYSTEM.
FAILURE OF THE PILOT TO PROPERLY PREFLIGHT THE ACFT FOLLOWED BY LOSS OF POWER DURING TAKEOFF. THE PLT ALSO FAILED TO ABOUT THE TAKEOFF.
THE PILOT OF THE PIPER PA-32-260, THAT HAD BEEN MODIFIED TO A MODEL PA-32-300 BY EXCHANGING THE ENGINE, TAXIED TO THE END OF A 3121 FOOT RUNWAY FOR TAKEOFF WITH CALM WIND CONDITIONS. THE AIRCRAFT LOAD CONSISTED OF FULL FUEL TANKS, PILOT AND PASSENGER, AND 30 POUNDS OF LUGGAGE. A GROUND WITNESS OBSERVED THE AIRCRAFT TO ROLL APPROXIMATELY 2850 FEET BEFORE BECOMING AIRBORNE. IMMEDIATELY AFTER TAKEOFF THE AIRCRAFT TOUCHED DOWN ON A FLAT ROOF OF A COMMERICAL BUILDING, COLLIDED WITH THE PARAPET AND CRASHED INTO THE STREET BELOW. THE POST CRASH ENGINE EXAM REVEALED RUST PARTICLES AND WATER THROUGHOUT THE FUEL SYSTEM.