20080427833159A

Accident · Substantial damage

FAA accident report · Hughes 269A · Raymond, NE · April 27, 2008

Date
April 27, 2008 · 14:00 local
Place
Raymond, NE
Phase of flight
Final Approach
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N1020Q
NTSB investigation
NTSBDFW08CA120
Reported as
Hughes 269A
Reported engine
Lycoming HIO360B1A
Fatal injuries
0
Pilot’s flight hours
1,672 total22 in this make and model29 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) Pilot was practicing steep approaches and when she flared, the tail rotor struck the ground. The impact caused torsional failure of the tail rotor driveshaft resulting in loss of the anti-torque system. The helicopter continued down the runway with power applied causing an uncontrollable yaw to the right. Approximately 90 feet from initial impact the right rear skid contacted the ground causing separation of skid, both hockey struts and oleo struts. The helicopter then rolled to the left causing all three main rotor blades to contact the ground. The helicopter came to rest on the right side approximately 150 degrees from the runway heading.

As the FAA filed it

(-23) PILOT WAS PRACTICING STEEP APPROACHES AND WHEN SHE FLARED, THE TAIL ROTOR STRUCK THE GROUND. THE IMPACT CAUSED TORSIONAL FAILURE OF THE TAIL ROTOR DRIVESHAFT RESULTING IN LOSS OF THE ANTI-TORQUE SYSTEM. THE HELICOPTER CONTINUED DOWN THE RUNWAY WITH POWER APPLIED CAUSING AN UNCONTROLLABLE YAW TO THE RIGHT. APPROXIMATELY 90 FEET FROM INITIAL IMPACT THE RIGHT REAR SKID CONTACTED THE GROUND CAUSING SEPARATION OF SKID, BOTH HOCKEY STRUTS AND OLEO STRUTS. THE HELICOPTER THEN ROLLED TO THE LEFT CAUSING ALL THREE MAIN ROTOR BLADES TO CONTACT THE GROUND. THE HELICOPTER CAME TO REST ON THE RIGHT SIDE APPROXIMATELY 150 DEGREES FROM THE RUNWAY HEADING.

NTSB investigation

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

Other reports on N1020Q · 1

Matched to the same aircraft by N-number and date.