What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Beechcraft A45, N34MR while on personal flight, over ran runway while landing at Merritt Island Airport, Florida. VMC conditions existed and no flight plan was filed. The airplanes nose gear collapsed after leaving the runway and encountering a drainage ditch, where aircraft came to rest. Inspection revealed no extensive airframe damage. The commercial rated pilot and commercial rated passenger were not injured. Lower nose cowling and nose gear wheel well will need sheetmetal replaced. Propeller missing two blades from hub. The pilot stated that during the descent phase of the approach to Merritt Island Airport at around 2000 feet, oil and grease covered the windscreen and the engine lost power due to the propeller blades departing the hub (Beech 2 bladed prop). He performed emergency procedures, and at about 1 mile from runway 29, he had to slip the aircraft in order to reduce airspeed and to attain a visual on the runway off the nose of the aircraft. The aircraft touched down at around mid point of the runway and speed was excess for braking ability and runway remaining. Post examination of the aircraft revealed both propeller blades missing and the propeller hub still attached to the engine.
As the FAA filed it
(-23) BEECHCRAFT A45, N34MR WHILE ON PERSONAL FLIGHT, OVER RAN RUNWAY WHILE LANDING AT MERRITT ISLAND AIRPORT, FLORIDA. VMC CONDITIONS EXISTED AND NO FLIGHT PLAN WAS FILED. THE AIRPLANES NOSE GEAR COLLAPSED AFTER LEAVING THE RUNWAY AND ENCOUNTERING A DRAINAGE DITCH, WHERE AIRCRAFT CAME TO REST. INSPECTION REVEALED NO EXTENSIVE AIRFRAME DAMAGE. THE COMMERCIAL RATED PILOT AND COMMERCIAL RATED PASSENGER WERE NOT INJURED. LOWER NOSE COWLING AND NOSE GEAR WHEEL WELL WILL NEED SHEETMETAL REPLACED. PROPELLER MISSING TWO BLADES FROM HUB. THE PILOT STATED THAT DURING THE DESCENT PHASE OF THE APPROACH TO MERRITT ISLAND AIRPORT AT AROUND 2000 FEET, OIL AND GREASE COVERED THE WINDSCREEN AND THE ENGINE LOST POWER DUE TO THE PROPELLER BLADES DEPARTING THE HUB (BEECH 2 BLADED PROP). HE PERFORMED EMERGENCY PROCEDURES, AND AT ABOUT 1 MILE FROM RUNWAY 29, HE HAD TO SLIP THE AIRCRAFT IN ORDER TO REDUCE AIRSPEED AND TO ATTAIN A VISUAL ON THE RUNWAY OFF THE NOSE OF THE AIRCRAFT. THE AIRCRAFT TOUCHED DOWN AT AROUND MID POINT OF THE RUNWAY AND SPEED WAS EXCESS FOR BRAKING ABILITY AND RUNWAY REMAINING. POST EXAMINATION OF THE AIRCRAFT REVEALED BOTH PROPELLER BLADES MISSING AND THE PROPELLER HUB STILL ATTACHED TO THE ENGINE.
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 N34MR · 2
Matched to the same aircraft by N-number and date.