20070313002769A

Accident · Substantial damage

FAA accident report · Robsin R22 BETA · Denver, CO · March 13, 2007

Date
March 13, 2007 · 17:15 local
Place
Denver, CO
Airport
Jeffco Airport
Phase of flight
Sfl Autorotation
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N7681H
NTSB investigation
NTSBDEN07CA072
Reported as
Robsin R22BETA
People aboard
2
Fatal injuries
0
Pilot’s flight hours
363 total222 in this make and model118 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.

(-23) On March 13, 2007 at 1615 MST a robertson R22 registration number N7681H was operating FAR part 91 flight instruction when during autorotation training the helicopter landed hard. Instructor reported that on a full down autorotation demonstration he had a 20 knot head wind when at less than 20 feet AGL the wind dropped to 0 and rotor RPM dropped 15%. The instructor reacted by leveling the helicopter where he contacted the pavement at approximately 1000 feet per minute and 40 knots forward. The helicopter bounced several times coming to rest upright. No injuries were reported. The helicopter sustained an under/over speed on the main rotor and substantial damage to the tail boom from a main rotor blade strike.

As the FAA filed it

(-23) ON MARCH 13, 2007 AT 1615 MST A ROBERTSON R22 REGISTRATION NUMBER N7681H WAS OPERATING FAR PART 91 FLIGHT INSTRUCTION WHEN DURING AUTOROTATION TRAINING THE HELICOPTER LANDED HARD. INSTRUCTOR REPORTED THAT ON A FULL DOWN AUTOROTATION DEMONSTRATION HE HAD A 20 KNOT HEAD WIND WHEN AT LESS THAN 20 FEET AGL THE WIND DROPPED TO 0 AND ROTOR RPM DROPPED 15%. THE INSTRUCTOR REACTED BY LEVELING THE HELICOPTER WHERE HE CONTACTED THE PAVEMENT AT APPROXIMATELY 1000 FEET PER MINUTE AND 40 KNOTS FORWARD. THE HELICOPTER BOUNCED SEVERAL TIMES COMING TO REST UPRIGHT. NO INJURIES WERE REPORTED. THE HELICOPTER SUSTAINED AN UNDER/OVER SPEED ON THE MAIN ROTOR AND SUBSTANTIAL DAMAGE TO THE TAIL BOOM FROM A MAIN ROTOR BLADE STRIKE.

NTSB investigation

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