20090429004569A

Accident · Substantial damage

FAA accident report · Bell OH58A · Arvin, CA · April 29, 2009

Date
April 29, 2009 · 18:45 local
Place
Arvin, CA
Phase of flight
Maneuver
Operating rules
Agricultural (Part 137)
Operator
CUFA
Damage
Substantial damage
Aircraft
N175SJ
NTSB investigation
NTSBWPR09CA220
Reported as
Bell OH58A
Reported engine
Allison T63*
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s flight hours
2,670 total1,050 in this make and model80 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) While conducting an aerial application, the aircraft struck a power line with its tail rotor. The pilot stated that he conducted a prior inspection of the field revealing there were 2 sets of wires crossing his path. The helicopter was operating at approx 5 ft AGL. The pilot stated that he saw the first set of wires and started a climb to clear the first set of wires (25 ft height). The helicopter tail rotor and lower vertical stabilized made contact with the wire causing the tail rotor and tail rotor gearbox to separate from the aircraft. The pilot tried to maintain directional control and set down the helicopter but due to the uncontrollable yaw the helicopter struck a second set of power lines with its main rotor. The aircraft's main rotor separated and the aircraft came to a standstill in the upright position.

As the FAA filed it

(-23) WHILE CONDUCTING AN AERIAL APPLICATION, THE AIRCRAFT STRUCK A POWER LINE WITH ITS TAIL ROTOR. THE PILOT STATED THAT HE CONDUCTED A PRIOR INSPECTION OF THE FIELD REVEALING THERE WERE 2 SETS OF WIRES CROSSING HIS PATH. THE HELICOPTER WAS OPERATING AT APPROX 5 FT AGL. THE PILOT STATED THAT HE SAW THE FIRST SET OF WIRES AND STARTED A CLIMB TO CLEAR THE FIRST SET OF WIRES (25 FT HEIGHT). THE HELICOPTER TAIL ROTOR AND LOWER VERTICAL STABILIZED MADE CONTACT WITH THE WIRE CAUSING THE TAIL ROTOR AND TAIL ROTOR GEARBOX TO SEPARATE FROM THE AIRCRAFT. THE PILOT TRIED TO MAINTAIN DIRECTIONAL CONTROL AND SET DOWN THE HELICOPTER BUT DUE TO THE UNCONTROLLABLE YAW THE HELICOPTER STRUCK A SECOND SET OF POWER LINES WITH ITS MAIN ROTOR. THE AIRCRAFT'S MAIN ROTOR SEPARATED AND THE AIRCRAFT CAME TO A STANDSTILL IN THE UPRIGHT POSITION.

NTSB investigation

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