What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) The pilot and his passenger, who is also a pilot, stated that while just nearing towchdown they encountered a thermal that lifted them back up into the air about ten feet. The pilot stated that he added full power to recover, but it was not sufficient enough to avoid touching down just to the side of the runway. There is a sandy soil beside the runway, the main wheels dug in slightly, and the right main gear axle and wheel broke off the fiberglass landing gear leg. Post accident investigaion found that the right landing gear leg had prior overheat damage from a hot brake disc and had been improperly repaired, it had been reheated to straighten it that severly weakened the composite material. (.4) on may 2, 2000, at 1435 hours pacific daylight time, an experimental fox long ez, N7FS, was substantially damaged during a main landing gear collapse on landing at Fallon Municipal Airport, Fallon, Nevada. The private pilot and one passenger were not injured. Visual meteorological conditions prevailed for the personal flight, which was operated by mountain west equities, inc., under 14 CFR part 91. The flight originated from truckee, califor nia, exact time unknown, and no flight plan was filed. The pilot reported to a federal aviation administration (FAA) inspector that his approach to runway 21 (5,703 feet x 75 feet) was normal. The surface wind was approximately from 260 degrees at 15 knots. After touching down near the threshold on the main landing gear, the aircraft lifted off the runway to a height of 20-25 feet AGL and drifted laterally off the runway. The pilot initiated a go-around and attempted to correct the flight path back over the runway; however, the aircraft touched down a second time in soft sand off the runway shoulder and the main gear collapsed. The aircraft then skidded down the runway on its belly. In a later report to the same FAA inspector, the pilot speculated that the accident was, in part, attributable to an earlier, improper repair of the fiberglass main landing gear leg that left the leg in a weakened condition. According to the pilot, shortly after he acquired the aircraft from the previous owner, he noted that the right-hand main gear leg was deformed outward; a discrepancy attributed to brake overheating and weakening of the fiberglass leg. The deformed gear leg had been reheated and realigned by a person who represented to the pilot that he was an expert in fiberglass repairs. After the accident, a different mechanic told him that this reheating weakened the fiberglass to the extent that it failed prematurely during his off-runway touchdown.
As the FAA filed it
(-23) THE PILOT AND HIS PASSENGER, WHO IS ALSO A PILOT, STATED THAT WHILE JUST NEARING TOWCHDOWN THEY ENCOUNTERED A THERMAL THAT LIFTED THEM BACK UP INTO THE AIR ABOUT TEN FEET. THE PILOT STATED THAT HE ADDED FULL POWER TO RECOVER, BUT IT WAS NOT SUFFICIENT ENOUGH TO AVOID TOUCHING DOWN JUST TO THE SIDE OF THE RUNWAY. THERE IS A SANDY SOIL BESIDE THE RUNWAY, THE MAIN WHEELS DUG IN SLIGHTLY, AND THE RIGHT MAIN GEAR AXLE AND WHEEL BROKE OFF THE FIBERGLASS LANDING GEAR LEG. POST ACCIDENT INVESTIGAION FOUND THAT THE RIGHT LANDING GEAR LEG HAD PRIOR OVERHEAT DAMAGE FROM A HOT BRAKE DISC AND HAD BEEN IMPROPERLY REPAIRED, IT HAD BEEN REHEATED TO STRAIGHTEN IT THAT SEVERLY WEAKENED THE COMPOSITE MATERIAL. (.4) ON MAY 2, 2000, AT 1435 HOURS PACIFIC DAYLIGHT TIME, AN EXPERIMENTAL FOX LONG EZ, N7FS, WAS SUBSTANTIALLY DAMAGED DURING A MAIN LANDING GEAR COLLAPSE ON LANDING AT FALLON MUNICIPAL AIRPORT, FALLON, NEVADA. THE PRIVATE PILOT AND ONE PASSENGER WERE NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE PERSONAL FLIGHT, WHICH WAS OPERATED BY MOUNTAIN WEST EQUITIES, INC., UNDER 14 CFR PART 91. THE FLIGHT ORIGINATED FROM TRUCKEE, CALIFOR NIA, EXACT TIME UNKNOWN, AND NO FLIGHT PLAN WAS FILED. THE PILOT REPORTED TO A FEDERAL AVIATION ADMINISTRATION (FAA) INSPECTOR THAT HIS APPROACH TO RUNWAY 21 (5,703 FEET X 75 FEET) WAS NORMAL. THE SURFACE WIND WAS APPROXIMATELY FROM 260 DEGREES AT 15 KNOTS. AFTER TOUCHING DOWN NEAR THE THRESHOLD ON THE MAIN LANDING GEAR, THE AIRCRAFT LIFTED OFF THE RUNWAY TO A HEIGHT OF 20-25 FEET AGL AND DRIFTED LATERALLY OFF THE RUNWAY. THE PILOT INITIATED A GO-AROUND AND ATTEMPTED TO CORRECT THE FLIGHT PATH BACK OVER THE RUNWAY; HOWEVER, THE AIRCRAFT TOUCHED DOWN A SECOND TIME IN SOFT SAND OFF THE RUNWAY SHOULDER AND THE MAIN GEAR COLLAPSED. THE AIRCRAFT THEN SKIDDED DOWN THE RUNWAY ON ITS BELLY. IN A LATER REPORT TO THE SAME FAA INSPECTOR, THE PILOT SPECULATED THAT THE ACCIDENT WAS, IN PART, ATTRIBUTABLE TO AN EARLIER, IMPROPER REPAIR OF THE FIBERGLASS MAIN LANDING GEAR LEG THAT LEFT THE LEG IN A WEAKENED CONDITION. ACCORDING TO THE PILOT, SHORTLY AFTER HE ACQUIRED THE AIRCRAFT FROM THE PREVIOUS OWNER, HE NOTED THAT THE RIGHT-HAND MAIN GEAR LEG WAS DEFORMED OUTWARD; A DISCREPANCY ATTRIBUTED TO BRAKE OVERHEATING AND WEAKENING OF THE FIBERGLASS LEG. THE DEFORMED GEAR LEG HAD BEEN REHEATED AND REALIGNED BY A PERSON WHO REPRESENTED TO THE PILOT THAT HE WAS AN EXPERT IN FIBERGLASS REPAIRS. AFTER THE ACCIDENT, A DIFFERENT MECHANIC TOLD HIM THAT THIS REHEATING WEAKENED THE FIBERGLASS TO THE EXTENT THAT IT FAILED PREMATURELY DURING HIS OFF-RUNWAY TOUCHDOWN.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.