What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
An experimental aircraft owner on a pleasure flight departing valkaria airport (X59) decided to land at the Okeechobee (obe) airport for reasons undisclosed and not aircraft related. After landing and taxing on runway 5 approached the intersection for the ramp near the FBO. While taxing his right gear leg collapsed, rolling it up under the fuselage causing the aircraft to make 180 degree turn. The propeller also struck the ground and was destroyed in impact. Finally the aircraft came to rest on the lower right side fuselage. Other damage included fabric tears, antenna damage but most noteworthy is the right wing broke at the spar approximately 5 feet inboard from the tip. Further investigation after the aircraft was transported back to valkaria, shows the gear leg failure came from the main fuselage attachment bolt broke at the shaft leaving the securing nut & cotter pin intact and the saddle bracket could not restrain the gear in the stationary position. The probable cause may be metal fatigue encompassed with age and the possibility of hard landings over a period of time.
As the FAA filed it
AN EXPERIMENTAL AIRCRAFT OWNER ON A PLEASURE FLIGHT DEPARTING VALKARIA AIRPORT (X59) DECIDED TO LAND AT THE OKEECHOBEE (OBE) AIRPORT FOR REASONS UNDISCLOSED AND NOT AIRCRAFT RELATED. AFTER LANDING AND TAXING ON RUNWAY 5 APPROACHED THE INTERSECTION FOR THE RAMP NEAR THE FBO. WHILE TAXING HIS RIGHT GEAR LEG COLLAPSED, ROLLING IT UP UNDER THE FUSELAGE CAUSING THE AIRCRAFT TO MAKE 180 DEGREE TURN. THE PROPELLER ALSO STRUCK THE GROUND AND WAS DESTROYED IN IMPACT. FINALLY THE AIRCRAFT CAME TO REST ON THE LOWER RIGHT SIDE FUSELAGE. OTHER DAMAGE INCLUDED FABRIC TEARS, ANTENNA DAMAGE BUT MOST NOTEWORTHY IS THE RIGHT WING BROKE AT THE SPAR APPROXIMATELY 5 FEET INBOARD FROM THE TIP. FURTHER INVESTIGATION AFTER THE AIRCRAFT WAS TRANSPORTED BACK TO VALKARIA, SHOWS THE GEAR LEG FAILURE CAME FROM THE MAIN FUSELAGE ATTACHMENT BOLT BROKE AT THE SHAFT LEAVING THE SECURING NUT & COTTER PIN INTACT AND THE SADDLE BRACKET COULD NOT RESTRAIN THE GEAR IN THE STATIONARY POSITION. THE PROBABLE CAUSE MAY BE METAL FATIGUE ENCOMPASSED WITH AGE AND THE POSSIBILITY OF HARD LANDINGS OVER A PERIOD OF TIME.
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 N79GH · 1
Matched to the same aircraft by N-number and date.