What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Pilot lost control of the acft during a crosswind landing, the left wheel left the rwy, the wingtip struck the ground, and the acft nosed over stopping inverted and damaging both wings, the vertical stabilizer, and the fuselage, other circumstances are unknown. (.19)on June 25, 1999, at 1205 central daylight time, a Cessna 150G, N2263J, owned and piloted by a private pilot,, sustained substantial damage after a loss of control and subsequent nose over during a landing rollout on runway 17 (4,400 feet by 74 feet, dry/asphalt) at the Fort Scott Municipal Airport, Fort Scott, Kansas. Visual meteorological conditions prevailed at the time of the accident. The personal flight was operating under the provisions of 14 CFR part 91 and was not on a flight plan. The pilot and one passenger reported no injuries. The flight departed butler memorial airport, butler, Missouri at 1140. (-23) during landing the aircraft veered off of the runway. The left main wheel departed the paved runway then the left wing tip contacted the ground. The aircraft then flipped forward over the propeller and came to rest inverted. The aircraft sustained substantial damage. The pilot and the passenger was n ot injured. The pilot stated that the left brake had locked up during the landing. (.4) on landing rollout the airplane veered to the left side of the runway. The pilot reported that the airplane departed the runway surface, the tires sunk into soft turf on the side of the runway, and the airplane nosed over coming to rest in an inverted position. Inspection of the runway surface revealed a single tire skid mark that initiated approximately 240 feet from the runway threshold, 10 feet left of the runway centerline, and followed a left curved path terminating approximately 465 feet from the runway threshold, 20 feet left of the runway edge. The tire skid mark was approximated 225 feet long. Inspection of the wreckage revealed no mechanical anomalies with the aircraft's control and the brake systems. Both main landing gear wheels were free moving and the brake system was exercised and operated without any anomalous behavior.
As the FAA filed it
PILOT LOST CONTROL OF THE ACFT DURING A CROSSWIND LANDING, THE LEFT WHEEL LEFT THE RWY, THE WINGTIP STRUCK THE GROUND, AND THE ACFT NOSED OVER STOPPING INVERTED AND DAMAGING BOTH WINGS, THE VERTICAL STABILIZER, AND THE FUSELAGE, OTHER CIRCUMSTANCES ARE UNKNOWN. (.19)ON JUNE 25, 1999, AT 1205 CENTRAL DAYLIGHT TIME, A CESSNA 150G, N2263J, OWNED AND PILOTED BY A PRIVATE PILOT,, SUSTAINED SUBSTANTIAL DAMAGE AFTER A LOSS OF CONTROL AND SUBSEQUENT NOSE OVER DURING A LANDING ROLLOUT ON RUNWAY 17 (4,400 FEET BY 74 FEET, DRY/ASPHALT) AT THE FORT SCOTT MUNICIPAL AIRPORT, FORT SCOTT, KANSAS. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME OF THE ACCIDENT. THE PERSONAL FLIGHT WAS OPERATING UNDER THE PROVISIONS OF 14 CFR PART 91 AND WAS NOT ON A FLIGHT PLAN. THE PILOT AND ONE PASSENGER REPORTED NO INJURIES. THE FLIGHT DEPARTED BUTLER MEMORIAL AIRPORT, BUTLER, MISSOURI AT 1140. (-23) DURING LANDING THE AIRCRAFT VEERED OFF OF THE RUNWAY. THE LEFT MAIN WHEEL DEPARTED THE PAVED RUNWAY THEN THE LEFT WING TIP CONTACTED THE GROUND. THE AIRCRAFT THEN FLIPPED FORWARD OVER THE PROPELLER AND CAME TO REST INVERTED. THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE. THE PILOT AND THE PASSENGER WAS N OT INJURED. THE PILOT STATED THAT THE LEFT BRAKE HAD LOCKED UP DURING THE LANDING. (.4) ON LANDING ROLLOUT THE AIRPLANE VEERED TO THE LEFT SIDE OF THE RUNWAY. THE PILOT REPORTED THAT THE AIRPLANE DEPARTED THE RUNWAY SURFACE, THE TIRES SUNK INTO SOFT TURF ON THE SIDE OF THE RUNWAY, AND THE AIRPLANE NOSED OVER COMING TO REST IN AN INVERTED POSITION. INSPECTION OF THE RUNWAY SURFACE REVEALED A SINGLE TIRE SKID MARK THAT INITIATED APPROXIMATELY 240 FEET FROM THE RUNWAY THRESHOLD, 10 FEET LEFT OF THE RUNWAY CENTERLINE, AND FOLLOWED A LEFT CURVED PATH TERMINATING APPROXIMATELY 465 FEET FROM THE RUNWAY THRESHOLD, 20 FEET LEFT OF THE RUNWAY EDGE. THE TIRE SKID MARK WAS APPROXIMATED 225 FEET LONG. INSPECTION OF THE WRECKAGE REVEALED NO MECHANICAL ANOMALIES WITH THE AIRCRAFT'S CONTROL AND THE BRAKE SYSTEMS. BOTH MAIN LANDING GEAR WHEELS WERE FREE MOVING AND THE BRAKE SYSTEM WAS EXERCISED AND OPERATED WITHOUT ANY ANOMALOUS BEHAVIOR.
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 N2263J · 1
Matched to the same aircraft by N-number and date.