What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Aircraft experienced rough engine operation as stated by pilot just after leaving pne airspace. Engine RPM began decreasing and aircraft began a slow descent. Pilot stated he was unable to maintain altitude. He then contacted pne airport and stated he was inbound with mechanical difficulties. Unable to make airport pilot decided to land in a vacant park. Pilot stated that the engine had made a loud popping noise prior to landing and the prop stopped rotating. The aircraft touched down at approximately 396 ft. prior to impacting a tree with his left wingtip and striking a large wrought iron fence where aircraft came to rest at about a 30 degree incline on fence posts. There was substantial damage to the aircraft. Both wings were separated from the fuselage, left wing sheared spar. Prop spinner and hub were severely damaged, prop blades had minor scoring from fence. Upper and lower cowling had substantial damage. Right upper engine mount was bent and firewall damage. No oil registered on dip stick. Belly of aircraft was streaked in oil to tail.
As the FAA filed it
(-23) AIRCRAFT EXPERIENCED ROUGH ENGINE OPERATION AS STATED BY PILOT JUST AFTER LEAVING PNE AIRSPACE. ENGINE RPM BEGAN DECREASING AND AIRCRAFT BEGAN A SLOW DESCENT. PILOT STATED HE WAS UNABLE TO MAINTAIN ALTITUDE. HE THEN CONTACTED PNE AIRPORT AND STATED HE WAS INBOUND WITH MECHANICAL DIFFICULTIES. UNABLE TO MAKE AIRPORT PILOT DECIDED TO LAND IN A VACANT PARK. PILOT STATED THAT THE ENGINE HAD MADE A LOUD POPPING NOISE PRIOR TO LANDING AND THE PROP STOPPED ROTATING. THE AIRCRAFT TOUCHED DOWN AT APPROXIMATELY 396 FT. PRIOR TO IMPACTING A TREE WITH HIS LEFT WINGTIP AND STRIKING A LARGE WROUGHT IRON FENCE WHERE AIRCRAFT CAME TO REST AT ABOUT A 30 DEGREE INCLINE ON FENCE POSTS. THERE WAS SUBSTANTIAL DAMAGE TO THE AIRCRAFT. BOTH WINGS WERE SEPARATED FROM THE FUSELAGE, LEFT WING SHEARED SPAR. PROP SPINNER AND HUB WERE SEVERELY DAMAGED, PROP BLADES HAD MINOR SCORING FROM FENCE. UPPER AND LOWER COWLING HAD SUBSTANTIAL DAMAGE. RIGHT UPPER ENGINE MOUNT WAS BENT AND FIREWALL DAMAGE. NO OIL REGISTERED ON DIP STICK. BELLY OF AIRCRAFT WAS STREAKED IN OIL TO TAIL.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.