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Akron, AL
WITNESSES RPRTD THAT BEFORE THE ACDNT, THE ACFT WAS BETWEEN 400 & 1000 FT AGL IN STRAIGHT & LEVEL FLIGHT. IT WAS OBSERVED TO ENTER A ROLL TO THE RIGHT. AFTER ROLLING INVERTED, THE ACFT ENTERED A SPIN. THE ENG WAS HEARD TO REV UP AS THE ACFT CONTINUED INTO A FLAT SPIN. SUBSEQUENTLY, IT COLLIDED WITH TERRAIN & WAS DESTROYED. THE FLT MANUAL STATED THAT AEROBATIC FLT WAS NOT TO BE PERFORMED BELOW 1500 FT AGL; A MIN ALT OF 3000 FT TO 5000 FT AGL WAS RECOMMENDED FOR AEROBATIC FLT. THE PLT HAD ONLY ABOUT 14 HRS IN THIS MAKE/MODEL OF ACFT. THE BAGGAGE COMPARTMENT CONTAINED A PARACHUTE CANOPY, THOUGH IT WAS TO BE EMPTY FOR AEROBATIC FLT.
FAILURE OF THE PILOT TO MAINTAIN CONTROL OF THE AIRCRAFT AND TO RECOVER FROM (OR AVOID) A SUBSEQUENT (FLAT) SPIN. FACTORS RELATED TO THE ACCIDENT WERE: THE PILOT'S FAILURE TO FOLLOW ESTABLISHED PROCEDURES, HIS LACK OF FAMILIARITY WITH THE AIRCRAFT, AND THE LACK OF SUFFICIENT ALTITUDE TO RECOVER FROM THE SPIN.
WITNESSES RPRTD THAT BEFORE THE ACDNT, THE ACFT WAS BETWEEN 400 & 1000 FT AGL IN STRAIGHT & LEVEL FLIGHT. IT WAS OBSERVED TO ENTER A ROLL TO THE RIGHT. AFTER ROLLING INVERTED, THE ACFT ENTERED A SPIN. THE ENG WAS HEARD TO REV UP AS THE ACFT CONTINUED INTO A FLAT SPIN. SUBSEQUENTLY, IT COLLIDED WITH TERRAIN & WAS DESTROYED. THE FLT MANUAL STATED THAT AEROBATIC FLT WAS NOT TO BE PERFORMED BELOW 1500 FT AGL; A MIN ALT OF 3000 FT TO 5000 FT AGL WAS RECOMMENDED FOR AEROBATIC FLT. THE PLT HAD ONLY ABOUT 14 HRS IN THIS MAKE/MODEL OF ACFT. THE BAGGAGE COMPARTMENT CONTAINED A PARACHUTE CANOPY, THOUGH IT WAS TO BE EMPTY FOR AEROBATIC FLT.