What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) While flying at approximately 4,000 feet, approximately 9 nautical miles northwest of the sussex airport (fwn) in sussex, NJ, the pilot stated he was unable to attain more than 500 revolutions per minute (RPM) on the aircraft's engine. The pilot stated he attempted to reach the sussex airport but landed in the backyard of a home in a residential area approximately 6 sm southwest of fwn. Witnesses who observed the aircraft stated they heard no engine noise. The aircraft circled the area of privacy data omitted, approached on a 290 degree heading, striking a tree at approximately 40 feet AGL, and a fence with the left wing. The aircraft did one half a cartwheel, and came to rest on a 150 degree heading. Both wings were damaged substantially, the nose wheel was torn off, and the fuselage weas severely buckled aft of the cabin. An on-site investigation revealed no water in the remaining 18 gallons of fuel however, a local a&p/ia determined the carburetor float was found to be stuck. A subsequent run-up showed no abnormalities. The weather at the time was VMC, winds were light and there were only minor injuries to the pilot and passenger.
As the FAA filed it
(-23) WHILE FLYING AT APPROXIMATELY 4,000 FEET, APPROXIMATELY 9 NAUTICAL MILES NORTHWEST OF THE SUSSEX AIRPORT (FWN) IN SUSSEX, NJ, THE PILOT STATED HE WAS UNABLE TO ATTAIN MORE THAN 500 REVOLUTIONS PER MINUTE (RPM) ON THE AIRCRAFT'S ENGINE. THE PILOT STATED HE ATTEMPTED TO REACH THE SUSSEX AIRPORT BUT LANDED IN THE BACKYARD OF A HOME IN A RESIDENTIAL AREA APPROXIMATELY 6 SM SOUTHWEST OF FWN. WITNESSES WHO OBSERVED THE AIRCRAFT STATED THEY HEARD NO ENGINE NOISE. THE AIRCRAFT CIRCLED THE AREA OF ^PRIVACY DATA OMITTED^, APPROACHED ON A 290 DEGREE HEADING, STRIKING A TREE AT APPROXIMATELY 40 FEET AGL, AND A FENCE WITH THE LEFT WING. THE AIRCRAFT DID ONE HALF A CARTWHEEL, AND CAME TO REST ON A 150 DEGREE HEADING. BOTH WINGS WERE DAMAGED SUBSTANTIALLY, THE NOSE WHEEL WAS TORN OFF, AND THE FUSELAGE WEAS SEVERELY BUCKLED AFT OF THE CABIN. AN ON-SITE INVESTIGATION REVEALED NO WATER IN THE REMAINING 18 GALLONS OF FUEL HOWEVER, A LOCAL A&P/IA DETERMINED THE CARBURETOR FLOAT WAS FOUND TO BE STUCK. A SUBSEQUENT RUN-UP SHOWED NO ABNORMALITIES. THE WEATHER AT THE TIME WAS VMC, WINDS WERE LIGHT AND THERE WERE ONLY MINOR INJURIES TO THE PILOT AND PASSENGER.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N63483 · 1
Matched to the same aircraft by N-number and date.