What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Pilot's description of sequence of events during landing and touchdown:
Inbound for landing on RY29 at kbed ~1230 EDT after ~1 hour 40 min originating from kbed. On short final, experienced turbulence and wind shear down from 300 feet AGL. 20 deg flaps. Approach speed 65 knots. (From memory), the wind check when I was on short final to RY29 (~1636Z) was 340(magnetic) 6 gusting 18. Weather was very good VMC. Crossed threshold and touched down 100 - 150 feet after the numbers.
Pilot's statement provided post accident investigation:
It felt like I landed heavily on the nose wheel. I believe that the combination of the turbulence just before touch down and not enough flare contributed to the hard landing on the nosewheel.
Note: upon exiting runway the aircraft taxied to west ramp, the pilot upon postflight after mooring aircraft on tiedown spot, did not notice aircraft damage.
Aircraft damage was reported by the rental agency at 15:21 as a prop-strike. Subsequent inspection the following day revealed additional damage to the aircraft which resulted in the continued investigation and the upgrading of the reported prop-strike occurrence to an accident based on the following:
The aircraft propeller showed evidence of contacting the runway surface under power, albeit briefly as damage to the tip of one blade was confined to approximately 2MM of the tip and curling of the opposite blade of approximately 30MM.
The nose landing gear was compressed and appeared to be slightly off-center to the left approximately 2 degrees from center. The firewall at the attachment point for the nose gear support fitting was noted to be forced upward and reward by evidence of buckling on the left, right and upper surfaces adjacent to support fitting. There were several sheared rivets associated with the buckled firewall. The lower surface of the fuselage directly aft of the nose gear attachment showed signs of buckling between the longerons and frames aft approximately 1METER to the junction of the wing lift strut attach points. The aircraft skin showed separation between overlapping surfaces and evidence of cracking on the left side.
As the FAA filed it
PILOT'S DESCRIPTION OF SEQUENCE OF EVENTS DURING LANDING AND TOUCHDOWN:
INBOUND FOR LANDING ON RY29 AT KBED ~1230 EDT AFTER ~1 HOUR 40 MIN ORIGINATING FROM KBED. ON SHORT FINAL, EXPERIENCED TURBULENCE AND WIND SHEAR DOWN FROM 300 FEET AGL. 20 DEG FLAPS. APPROACH SPEED 65 KNOTS. (FROM MEMORY), THE WIND CHECK WHEN I WAS ON SHORT FINAL TO RY29 (~1636Z) WAS 340(MAGNETIC) 6 GUSTING 18. WEATHER WAS VERY GOOD VMC. CROSSED THRESHOLD AND TOUCHED DOWN 100 - 150 FEET AFTER THE NUMBERS.
PILOT'S STATEMENT PROVIDED POST ACCIDENT INVESTIGATION:
IT FELT LIKE I LANDED HEAVILY ON THE NOSE WHEEL. I BELIEVE THAT THE COMBINATION OF THE TURBULENCE JUST BEFORE TOUCH DOWN AND NOT ENOUGH FLARE CONTRIBUTED TO THE HARD LANDING ON THE NOSEWHEEL.
NOTE: UPON EXITING RUNWAY THE AIRCRAFT TAXIED TO WEST RAMP, THE PILOT UPON POSTFLIGHT AFTER MOORING AIRCRAFT ON TIEDOWN SPOT, DID NOT NOTICE AIRCRAFT DAMAGE.
AIRCRAFT DAMAGE WAS REPORTED BY THE RENTAL AGENCY AT 15:21 AS A PROP-STRIKE. SUBSEQUENT INSPECTION THE FOLLOWING DAY REVEALED ADDITIONAL DAMAGE TO THE AIRCRAFT WHICH RESULTED IN THE CONTINUED INVESTIGATION AND THE UPGRADING OF THE REPORTED PROP-STRIKE OCCURRENCE TO AN ACCIDENT BASED ON THE FOLLOWING:
THE AIRCRAFT PROPELLER SHOWED EVIDENCE OF CONTACTING THE RUNWAY SURFACE UNDER POWER, ALBEIT BRIEFLY AS DAMAGE TO THE TIP OF ONE BLADE WAS CONFINED TO APPROXIMATELY 2MM OF THE TIP AND CURLING OF THE OPPOSITE BLADE OF APPROXIMATELY 30MM.
THE NOSE LANDING GEAR WAS COMPRESSED AND APPEARED TO BE SLIGHTLY OFF-CENTER TO THE LEFT APPROXIMATELY 2 DEGREES FROM CENTER. THE FIREWALL AT THE ATTACHMENT POINT FOR THE NOSE GEAR SUPPORT FITTING WAS NOTED TO BE FORCED UPWARD AND REWARD BY EVIDENCE OF BUCKLING ON THE LEFT, RIGHT AND UPPER SURFACES ADJACENT TO SUPPORT FITTING. THERE WERE SEVERAL SHEARED RIVETS ASSOCIATED WITH THE BUCKLED FIREWALL. THE LOWER SURFACE OF THE FUSELAGE DIRECTLY AFT OF THE NOSE GEAR ATTACHMENT SHOWED SIGNS OF BUCKLING BETWEEN THE LONGERONS AND FRAMES AFT APPROXIMATELY 1METER TO THE JUNCTION OF THE WING LIFT STRUT ATTACH POINTS. THE AIRCRAFT SKIN SHOWED SEPARATION BETWEEN OVERLAPPING SURFACES AND EVIDENCE OF CRACKING ON THE LEFT SIDE.
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 N249FS · 1
Matched to the same aircraft by N-number and date.