What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Pilot landed at coastal airport, Pensacola, FL (83J) a grass airstrip. He stated, upon brake application the aircraft failed to stop and rolled into fence at runway end causing the aircraft to flip inverted. The propeller contacted the barbed fence and struck the ground as aircraft inverted. The aircraft sustained substantial damage to the upper and lower wings, vertical tail section, and rudder. The elevator damage was minor, the upper wing center and outboard leading edges were damaged. Inboard forward wing brace assemblies bowed. Lower right wing tip leading edge and spar damaged, suspect hidden damae this area. Unable to assess upper wing damage. Vertical tail section and rudder assembly forward bend approx. 25 degrees. Upon inspection brake reservoir was empty. Suspect brake failure due to loss of fluid from reservoir. (.4) during landing rollout the brakes did not work. The aircraft overran the runway, collided with a fence, and nosed over. Postcrash examination of the brake system showed the hydraulic fluid reservoir was empty and there was no evidence of postcrash leakage of fluid from the reservoir.
As the FAA filed it
(-23) PILOT LANDED AT COASTAL AIRPORT, PENSACOLA, FL (83J) A GRASS AIRSTRIP. HE STATED, UPON BRAKE APPLICATION THE AIRCRAFT FAILED TO STOP AND ROLLED INTO FENCE AT RUNWAY END CAUSING THE AIRCRAFT TO FLIP INVERTED. THE PROPELLER CONTACTED THE BARBED FENCE AND STRUCK THE GROUND AS AIRCRAFT INVERTED. THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE TO THE UPPER AND LOWER WINGS, VERTICAL TAIL SECTION, AND RUDDER. THE ELEVATOR DAMAGE WAS MINOR, THE UPPER WING CENTER AND OUTBOARD LEADING EDGES WERE DAMAGED. INBOARD FORWARD WING BRACE ASSEMBLIES BOWED. LOWER RIGHT WING TIP LEADING EDGE AND SPAR DAMAGED, SUSPECT HIDDEN DAMAE THIS AREA. UNABLE TO ASSESS UPPER WING DAMAGE. VERTICAL TAIL SECTION AND RUDDER ASSEMBLY FORWARD BEND APPROX. 25 DEGREES. UPON INSPECTION BRAKE RESERVOIR WAS EMPTY. SUSPECT BRAKE FAILURE DUE TO LOSS OF FLUID FROM RESERVOIR. (.4) DURING LANDING ROLLOUT THE BRAKES DID NOT WORK. THE AIRCRAFT OVERRAN THE RUNWAY, COLLIDED WITH A FENCE, AND NOSED OVER. POSTCRASH EXAMINATION OF THE BRAKE SYSTEM SHOWED THE HYDRAULIC FLUID RESERVOIR WAS EMPTY AND THERE WAS NO EVIDENCE OF POSTCRASH LEAKAGE OF FLUID FROM THE RESERVOIR.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.