20180702009009A

Accident · Substantial damage

FAA accident report · Ronnie Koonce SAFARI 400 · Aguilares, TX · July 2, 2018

Date
July 2, 2018 · 10:00 local
Place
Aguilares, TX
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N326RW
NTSB investigation
NTSBCEN18LA247
Reported as
Ronnie Koonce Safari 400
People aboard
1
Fatal injuries
0
Other injuries
1

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Pilot was attempting to further phase I requirements following certification. During flight the aircraft started to vibrate. The pilot turned and started to descend in an effort to land in an opening when he heard a loud pop sound followed by a loss of the tail rotor authority and aircraft started to counter rotate. Aircraft struck the ground and rolled upon its left side causing substantial damage and serious injury to the pilot. The main rotors were destroyed and there was no damage to the tail rotor blades. Investigation revealed the flight control continuity was intact. The tail rotor quill did not rotate with the main rotor blades upon inspection. Teardown analysis revealed the tail rotor pinion sheared.

As the FAA filed it

PILOT WAS ATTEMPTING TO FURTHER PHASE I REQUIREMENTS FOLLOWING CERTIFICATION. DURING FLIGHT THE AIRCRAFT STARTED TO VIBRATE. THE PILOT TURNED AND STARTED TO DESCEND IN AN EFFORT TO LAND IN AN OPENING WHEN HE HEARD A LOUD POP SOUND FOLLOWED BY A LOSS OF THE TAIL ROTOR AUTHORITY AND AIRCRAFT STARTED TO COUNTER ROTATE. AIRCRAFT STRUCK THE GROUND AND ROLLED UPON ITS LEFT SIDE CAUSING SUBSTANTIAL DAMAGE AND SERIOUS INJURY TO THE PILOT. THE MAIN ROTORS WERE DESTROYED AND THERE WAS NO DAMAGE TO THE TAIL ROTOR BLADES. INVESTIGATION REVEALED THE FLIGHT CONTROL CONTINUITY WAS INTACT. THE TAIL ROTOR QUILL DID NOT ROTATE WITH THE MAIN ROTOR BLADES UPON INSPECTION. TEARDOWN ANALYSIS REVEALED THE TAIL ROTOR PINION SHEARED.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.