What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Narrative: N401SX struck deer on runway during landing. The right wheel assembly and lower strut broke off. During final on runway 22, just before touch down, a small herd of deer ran in front of aircraft. The pilot pulled up in an attempt to "balloon," over the deer. One or two deer hit the right gear. The pilot continued with landing. The aircraft left gear touched down, and the right wing continued to settle, till the strut hit the runway. The pilot maintained directional control by differential braking with rudder inputs until aircraft came to a stop; 5 feet off center line approximately 1100 feet from end of runway. Damage: airframe. Right main landing gear strut, outer cylinder, bottom portion broke off. Piston, wheel and tire assembly separated from a main strut. Hydraulic brake line separated from both ends and lodged in the gap, between the right outboard elevator and horizontal stabilizer. Right landing light is scraped on bottom of extended light. Engine and propeller: engine continued to rotate after propeller impacted the runway. Propeller - all three blade tips have 180 to 270 degree reverse bends (approximately 8-10 inches). This investigation is closed.
As the FAA filed it
NARRATIVE: N401SX STRUCK DEER ON RUNWAY DURING LANDING. THE RIGHT WHEEL ASSEMBLY AND LOWER STRUT BROKE OFF. DURING FINAL ON RUNWAY 22, JUST BEFORE TOUCH DOWN, A SMALL HERD OF DEER RAN IN FRONT OF AIRCRAFT. THE PILOT PULLED UP IN AN ATTEMPT TO "BALLOON," OVER THE DEER. ONE OR TWO DEER HIT THE RIGHT GEAR. THE PILOT CONTINUED WITH LANDING. THE AIRCRAFT LEFT GEAR TOUCHED DOWN, AND THE RIGHT WING CONTINUED TO SETTLE, TILL THE STRUT HIT THE RUNWAY. THE PILOT MAINTAINED DIRECTIONAL CONTROL BY DIFFERENTIAL BRAKING WITH RUDDER INPUTS UNTIL AIRCRAFT CAME TO A STOP; 5 FEET OFF CENTER LINE APPROXIMATELY 1100 FEET FROM END OF RUNWAY. DAMAGE: AIRFRAME. RIGHT MAIN LANDING GEAR STRUT, OUTER CYLINDER, BOTTOM PORTION BROKE OFF. PISTON, WHEEL AND TIRE ASSEMBLY SEPARATED FROM A MAIN STRUT. HYDRAULIC BRAKE LINE SEPARATED FROM BOTH ENDS AND LODGED IN THE GAP, BETWEEN THE RIGHT OUTBOARD ELEVATOR AND HORIZONTAL STABILIZER. RIGHT LANDING LIGHT IS SCRAPED ON BOTTOM OF EXTENDED LIGHT. ENGINE AND PROPELLER: ENGINE CONTINUED TO ROTATE AFTER PROPELLER IMPACTED THE RUNWAY. PROPELLER - ALL THREE BLADE TIPS HAVE 180 TO 270 DEGREE REVERSE BENDS (APPROXIMATELY 8-10 INCHES). THIS INVESTIGATION IS CLOSED.