20120716014899A

Accident · Substantial damage

FAA accident report · Robinson Helicopter R22 · Bountiful, UT · July 16, 2012

Date
July 16, 2012 · 12:00 local
Place
Bountiful, UT
Airport
Skypark
Phase of flight
Other, Specify
Operating rules
Pilot school (Part 141)
Operator
UZRS
Damage
Substantial damage
Aircraft
N47WH
NTSB investigation
NTSBWPR12CA307
Reported as
Robinson Helicopter R22
Reported engine
Lycoming O-360 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
1,100 total781 in this make and model180 in the last 90 days

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.

During a simulated power-off autorotation with a power recovery, the instructor and the pilot receiving refresher proficiency training both noted the airspeed was exceeding optimum for main rotor RPM and the main rotor RPM was decaying. At about 200-150 feet, the instructor pilot took the controls, and executed a good flare at about 50 feet. He determined the aircraft was going to fall through and it was not possible to abort the maneuver so close to the runway. He leveled the aircraft and the aircraft hit hard enough to spread the skid gear. The aircraft slid approximately 75 feet down runway 16. It then skid to the left and when the skids struck the dirt on the east side of the runway it caused the aircraft to roll several times before coming to rest on its left side.

As the FAA filed it

DURING A SIMULATED POWER-OFF AUTOROTATION WITH A POWER RECOVERY, THE INSTRUCTOR AND THE PILOT RECEIVING REFRESHER PROFICIENCY TRAINING BOTH NOTED THE AIRSPEED WAS EXCEEDING OPTIMUM FOR MAIN ROTOR RPM AND THE MAIN ROTOR RPM WAS DECAYING. AT ABOUT 200-150 FEET, THE INSTRUCTOR PILOT TOOK THE CONTROLS, AND EXECUTED A GOOD FLARE AT ABOUT 50 FEET. HE DETERMINED THE AIRCRAFT WAS GOING TO FALL THROUGH AND IT WAS NOT POSSIBLE TO ABORT THE MANEUVER SO CLOSE TO THE RUNWAY. HE LEVELED THE AIRCRAFT AND THE AIRCRAFT HIT HARD ENOUGH TO SPREAD THE SKID GEAR. THE AIRCRAFT SLID APPROXIMATELY 75 FEET DOWN RUNWAY 16. IT THEN SKID TO THE LEFT AND WHEN THE SKIDS STRUCK THE DIRT ON THE EAST SIDE OF THE RUNWAY IT CAUSED THE AIRCRAFT TO ROLL SEVERAL TIMES BEFORE COMING TO REST ON ITS 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.