20060512008459A

Accident · Substantial damage

FAA accident report · Hughes 269C · Lees Summit, MO · May 12, 2006

Date
May 12, 2006 · 15:25 local
Place
Lees Summit, MO
Phase of flight
Pwr On Vertical Ldng/Rtrcrft
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N7506L
NTSB investigation
NTSBCHI06CA131
Reported as
Hughes 269C
People aboard
2
Fatal injuries
0
Pilot’s flight hours
1,750 total550 in this make and model60 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) According to the CFI, his instructor student entered autorotation with intention of touching down on cfi's private property. It became apparent that they would not clear a tree line and reach the landing area due to strong winds, so the CFI attempted to recover with power. However, he was unable to overcome his student's grip on the throttle. The CFI applied some collective to extend the glide and clear the tree line; however, there was little energy remaining in the main rotor system, and the helicopter firmly contacted the ground, bounced forward, the main rotors drooped and struck the tail boom, and the aircraft rolled onto its side.

As the FAA filed it

(-23) ACCORDING TO THE CFI, HIS INSTRUCTOR STUDENT ENTERED AUTOROTATION WITH INTENTION OF TOUCHING DOWN ON CFI'S PRIVATE PROPERTY. IT BECAME APPARENT THAT THEY WOULD NOT CLEAR A TREE LINE AND REACH THE LANDING AREA DUE TO STRONG WINDS, SO THE CFI ATTEMPTED TO RECOVER WITH POWER. HOWEVER, HE WAS UNABLE TO OVERCOME HIS STUDENT'S GRIP ON THE THROTTLE. THE CFI APPLIED SOME COLLECTIVE TO EXTEND THE GLIDE AND CLEAR THE TREE LINE; HOWEVER, THERE WAS LITTLE ENERGY REMAINING IN THE MAIN ROTOR SYSTEM, AND THE HELICOPTER FIRMLY CONTACTED THE GROUND, BOUNCED FORWARD, THE MAIN ROTORS DROOPED AND STRUCK THE TAIL BOOM, AND THE AIRCRAFT ROLLED ONTO ITS 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.