What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
While practicing autorotations on the grass runway 35 at Chambers County (T00), during the third landing, the pilot experienced a sudden loss of lift during the flare due to a possible strong wind shear, resulting in a vertical drop of about four feet. Pilot immediately attempted recovery with full power, but was unable to prevent a hard landing during the go-round which caused the propeller to strike the bottom keel. The aircraft bounced to the left initially, bending the left main landing gear, the raters impacted the ground, and the detachable mast sheared at the junction and twisted off, still being held in place with the control rods. The aircraft came to rest on the mast junction on its right side.
Major damage caused was to the three propeller blades which sheared at the hub, mast sheared/bent at the detachable junction, and both rotor blades gouged and bent.
Minor damage to horizontal stabilizer on left sheared, pre-rotator vertical shaft detached/bent and upper control rods bent/broken.
Pilot was uninjured.
As the FAA filed it
WHILE PRACTICING AUTOROTATIONS ON THE GRASS RUNWAY 35 AT CHAMBERS COUNTY (T00), DURING THE THIRD LANDING, THE PILOT EXPERIENCED A SUDDEN LOSS OF LIFT DURING THE FLARE DUE TO A POSSIBLE STRONG WIND SHEAR, RESULTING IN A VERTICAL DROP OF ABOUT FOUR FEET. PILOT IMMEDIATELY ATTEMPTED RECOVERY WITH FULL POWER, BUT WAS UNABLE TO PREVENT A HARD LANDING DURING THE GO-ROUND WHICH CAUSED THE PROPELLER TO STRIKE THE BOTTOM KEEL. THE AIRCRAFT BOUNCED TO THE LEFT INITIALLY, BENDING THE LEFT MAIN LANDING GEAR, THE RATERS IMPACTED THE GROUND, AND THE DETACHABLE MAST SHEARED AT THE JUNCTION AND TWISTED OFF, STILL BEING HELD IN PLACE WITH THE CONTROL RODS. THE AIRCRAFT CAME TO REST ON THE MAST JUNCTION ON ITS RIGHT SIDE.
MAJOR DAMAGE CAUSED WAS TO THE THREE PROPELLER BLADES WHICH SHEARED AT THE HUB, MAST SHEARED/BENT AT THE DETACHABLE JUNCTION, AND BOTH ROTOR BLADES GOUGED AND BENT.
MINOR DAMAGE TO HORIZONTAL STABILIZER ON LEFT SHEARED, PRE-ROTATOR VERTICAL SHAFT DETACHED/BENT AND UPPER CONTROL RODS BENT/BROKEN.
PILOT WAS UNINJURED.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.