What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
A Robinson R-44 helicopter operating under CFR part 91 sustained substantial damage during a hard landing at the North Las Vegas airport. The helicopter was on a flight instruction flight with a student pilot and flight instructor.
The student pilot, who was maniplulating the controls at the time of the event, was working on a private certificate. He was being instructed on power recovery auto rotations at the time of the event.
The pilot stated that he became nervous during the maneuver and froze on the controls which prevented the instructor from applying throttle and collective corrections.
It appeared that the aircraft struck a taxiway, in a relatively level attitude, a high rate of descent causing the forward and aft landing gear cross tubes and side struts to bend.
The pilot and the instructor were both uninjured.
Subsequent examination of the aircraft revealed the tailboom was dented and angled downward due to the force of impact. It also revealed that the lower engine support frame assembly was bent.
Inspection of the aircraft revealed that the aircraft damage appeared to be consistent with the facts provided by the pilot and instructor.
Flight control continuity and engine control was established.
Report to be amended.
As the FAA filed it
A ROBINSON R-44 HELICOPTER OPERATING UNDER CFR PART 91 SUSTAINED SUBSTANTIAL DAMAGE DURING A HARD LANDING AT THE NORTH LAS VEGAS AIRPORT. THE HELICOPTER WAS ON A FLIGHT INSTRUCTION FLIGHT WITH A STUDENT PILOT AND FLIGHT INSTRUCTOR.
THE STUDENT PILOT, WHO WAS MANIPLULATING THE CONTROLS AT THE TIME OF THE EVENT, WAS WORKING ON A PRIVATE CERTIFICATE. HE WAS BEING INSTRUCTED ON POWER RECOVERY AUTO ROTATIONS AT THE TIME OF THE EVENT.
THE PILOT STATED THAT HE BECAME NERVOUS DURING THE MANEUVER AND FROZE ON THE CONTROLS WHICH PREVENTED THE INSTRUCTOR FROM APPLYING THROTTLE AND COLLECTIVE CORRECTIONS.
IT APPEARED THAT THE AIRCRAFT STRUCK A TAXIWAY, IN A RELATIVELY LEVEL ATTITUDE, A HIGH RATE OF DESCENT CAUSING THE FORWARD AND AFT LANDING GEAR CROSS TUBES AND SIDE STRUTS TO BEND.
THE PILOT AND THE INSTRUCTOR WERE BOTH UNINJURED.
SUBSEQUENT EXAMINATION OF THE AIRCRAFT REVEALED THE TAILBOOM WAS DENTED AND ANGLED DOWNWARD DUE TO THE FORCE OF IMPACT. IT ALSO REVEALED THAT THE LOWER ENGINE SUPPORT FRAME ASSEMBLY WAS BENT.
INSPECTION OF THE AIRCRAFT REVEALED THAT THE AIRCRAFT DAMAGE APPEARED TO BE CONSISTENT WITH THE FACTS PROVIDED BY THE PILOT AND INSTRUCTOR.
FLIGHT CONTROL CONTINUITY AND ENGINE CONTROL WAS ESTABLISHED.
REPORT TO BE AMENDED.