What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
A Remos light sport aircraft, primarily used for instruction out of the Orlando Executive Airport was conducting pattern work locally. After completing takeoffs and landings, the subject aircraft departed the area returning to the Orlando. After landing without incident on runway 13 and during roll-out the crew felt a binding in the undercarriage. They perceived it to be a punctured tire or binding of the wheel pant. Making the turn off the centerline, the pilot heard a crunching noise and aircraft's attitude rotated nose high causing the left wing to droop. All forward progress was halted. The initial inspection revealed that the left main gear leg (strut) lost structural integrity collapsing with damage to the composite gear leg assembly and subsequently damaging the underside of the horizontal stabilator. No further damage was identified.
As the FAA filed it
A REMOS LIGHT SPORT AIRCRAFT, PRIMARILY USED FOR INSTRUCTION OUT OF THE ORLANDO EXECUTIVE AIRPORT WAS CONDUCTING PATTERN WORK LOCALLY. AFTER COMPLETING TAKEOFFS AND LANDINGS, THE SUBJECT AIRCRAFT DEPARTED THE AREA RETURNING TO THE ORLANDO. AFTER LANDING WITHOUT INCIDENT ON RUNWAY 13 AND DURING ROLL-OUT THE CREW FELT A BINDING IN THE UNDERCARRIAGE. THEY PERCEIVED IT TO BE A PUNCTURED TIRE OR BINDING OF THE WHEEL PANT. MAKING THE TURN OFF THE CENTERLINE, THE PILOT HEARD A CRUNCHING NOISE AND AIRCRAFT'S ATTITUDE ROTATED NOSE HIGH CAUSING THE LEFT WING TO DROOP. ALL FORWARD PROGRESS WAS HALTED. THE INITIAL INSPECTION REVEALED THAT THE LEFT MAIN GEAR LEG (STRUT) LOST STRUCTURAL INTEGRITY COLLAPSING WITH DAMAGE TO THE COMPOSITE GEAR LEG ASSEMBLY AND SUBSEQUENTLY DAMAGING THE UNDERSIDE OF THE HORIZONTAL STABILATOR. NO FURTHER DAMAGE WAS IDENTIFIED.