20110203000739A

Accident · Substantial damage

FAA accident report · Robinson He R44 · Ogden, UT · February 3, 2011

Date
February 3, 2011 · 18:00 local
Place
Ogden, UT
Airport
Ogden
Phase of flight
Other, Specify
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N441TB
NTSB investigation
NTSBWPR11CA121
Reported as
Robinson He R44
Reported engine
Lycoming 0-540 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
864 total661 in this make and model165 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 demonstration practice engine out autorotation, the pilot mismanaged the controls resulting in low rotor RPM and slower than normal airspeedpilot used an incorrect procedure to attempt to regain rotor RPM without success, at about 200 feet above the ground an attempted a power recovery was tried wit insufficient power to overcome the slow rotor speed. The aircraft hit hard tail low resulting in striking the tail stinger onthe ground and the rotor blades chopping off the tail boom. The aircraft started a left turn on the skids, resulting in the right skid collapsing, the fuselage nose scraping the ground. The aircraft then tuned right about 90 degrees onto its right side with the main rotor blades striking the gound about one time each before coming to rest.

As the FAA filed it

DURING A DEMONSTRATION PRACTICE ENGINE OUT AUTOROTATION, THE PILOT MISMANAGED THE CONTROLS RESULTING IN LOW ROTOR RPM AND SLOWER THAN NORMAL AIRSPEEDPILOT USED AN INCORRECT PROCEDURE TO ATTEMPT TO REGAIN ROTOR RPM WITHOUT SUCCESS, AT ABOUT 200 FEET ABOVE THE GROUND AN ATTEMPTED A POWER RECOVERY WAS TRIED WIT INSUFFICIENT POWER TO OVERCOME THE SLOW ROTOR SPEED.THE AIRCRAFT HIT HARD TAIL LOW RESULTING IN STRIKING THE TAIL STINGER ONTHE GROUND AND THE ROTOR BLADES CHOPPING OFF THE TAIL BOOM.THE AIRCRAFT STARTED A LEFT TURN ON THE SKIDS, RESULTING IN THE RIGHT SKID COLLAPSING, THE FUSELAGE NOSE SCRAPING THE GROUND. THE AIRCRAFT THEN TUNED RIGHT ABOUT 90 DEGREES ONTO ITS RIGHT SIDE WITH THE MAIN ROTOR BLADES STRIKING THE GOUND ABOUT ONE TIME EACH BEFORE COMING TO REST.

NTSB investigation

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