What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Glenn harris, co-owner of aircraft, was in the right seat. Mark davis, in the left seat was performing a demonstration flight. As they were taking-off from runway 23, Mr. Davis asked Mr. Harris what they would do if they lost an engine. Mr. Harris pulled back the left throttle and they continued to climb. The left engine was at idle for downwind, base and final to runway 23. They flared for landing, lowered then retracted the gear, but did not land. Both throttles were advanced to perform a go-around. The right engine responded, but the left engine did not. They experienced a sudden roll and yaw to the left. The left wing first contacted the ground 25' from the left side of runway 23. The aircraft then cartwheeled and came to rest at a heading of 265 degrees approximately 884' from the displaced threshold and 97' from the left side of runway 23. Both men suffered minor injuries. Preliminary investigation shows the right propeller blades damaged consistent with high engine power at time of ground contact. The left propeller blades damage was consistent with no engine power at time of ground contact. There was no post accident fire.
As the FAA filed it
(-23) GLENN HARRIS, CO-OWNER OF AIRCRAFT, WAS IN THE RIGHT SEAT. MARK DAVIS, IN THE LEFT SEAT WAS PERFORMING A DEMONSTRATION FLIGHT. AS THEY WERE TAKING-OFF FROM RUNWAY 23, MR. DAVIS ASKED MR. HARRIS WHAT THEY WOULD DO IF THEY LOST AN ENGINE. MR. HARRIS PULLED BACK THE LEFT THROTTLE AND THEY CONTINUED TO CLIMB. THE LEFT ENGINE WAS AT IDLE FOR DOWNWIND, BASE AND FINAL TO RUNWAY 23. THEY FLARED FOR LANDING, LOWERED THEN RETRACTED THE GEAR, BUT DID NOT LAND. BOTH THROTTLES WERE ADVANCED TO PERFORM A GO-AROUND. THE RIGHT ENGINE RESPONDED, BUT THE LEFT ENGINE DID NOT. THEY EXPERIENCED A SUDDEN ROLL AND YAW TO THE LEFT. THE LEFT WING FIRST CONTACTED THE GROUND 25' FROM THE LEFT SIDE OF RUNWAY 23. THE AIRCRAFT THEN CARTWHEELED AND CAME TO REST AT A HEADING OF 265 DEGREES APPROXIMATELY 884' FROM THE DISPLACED THRESHOLD AND 97' FROM THE LEFT SIDE OF RUNWAY 23. BOTH MEN SUFFERED MINOR INJURIES. PRELIMINARY INVESTIGATION SHOWS THE RIGHT PROPELLER BLADES DAMAGED CONSISTENT WITH HIGH ENGINE POWER AT TIME OF GROUND CONTACT. THE LEFT PROPELLER BLADES DAMAGE WAS CONSISTENT WITH NO ENGINE POWER AT TIME OF GROUND CONTACT. THERE WAS NO POST ACCIDENT FIRE.
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 N8402Y · 1
Matched to the same aircraft by N-number and date.