What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
On the day of the incident, the pilot in command attempted to takeoff the aircraft, which had not been operated for 2 years, on runway 25. After applying full power, the pilot in command stated the tail of the aircraft began to occilate from side to side. He applied forward pressure on the elevator control, which raised the tail off the ground. The aircraft turned sharply to the left and impacted the PAPI light box nearest to the runway, located 500 feet from the entrance to the runway from the taxiway.
The propeller impacted the PAPI box under power and was destroyed. The tail wheel was also damaged. No damage was observed on the engine cowling or firewall.
Inspection of the aircraft found deformed areas of the aluminum wing struts, and holes in the upper fabric of the horizontal stabilizer. The pilot in command stated that the holes were a result of the flight control mechanism rubbing the fabric and were present prior to the incident.
As the FAA filed it
ON THE DAY OF THE INCIDENT, THE PILOT IN COMMAND ATTEMPTED TO TAKEOFF THE AIRCRAFT, WHICH HAD NOT BEEN OPERATED FOR 2 YEARS, ON RUNWAY 25. AFTER APPLYING FULL POWER, THE PILOT IN COMMAND STATED THE TAIL OF THE AIRCRAFT BEGAN TO OCCILATE FROM SIDE TO SIDE. HE APPLIED FORWARD PRESSURE ON THE ELEVATOR CONTROL, WHICH RAISED THE TAIL OFF THE GROUND. THE AIRCRAFT TURNED SHARPLY TO THE LEFT AND IMPACTED THE PAPI LIGHT BOX NEAREST TO THE RUNWAY, LOCATED 500 FEET FROM THE ENTRANCE TO THE RUNWAY FROM THE TAXIWAY.
THE PROPELLER IMPACTED THE PAPI BOX UNDER POWER AND WAS DESTROYED. THE TAIL WHEEL WAS ALSO DAMAGED. NO DAMAGE WAS OBSERVED ON THE ENGINE COWLING OR FIREWALL.
INSPECTION OF THE AIRCRAFT FOUND DEFORMED AREAS OF THE ALUMINUM WING STRUTS, AND HOLES IN THE UPPER FABRIC OF THE HORIZONTAL STABILIZER. THE PILOT IN COMMAND STATED THAT THE HOLES WERE A RESULT OF THE FLIGHT CONTROL MECHANISM RUBBING THE FABRIC AND WERE PRESENT PRIOR TO THE INCIDENT.