20151015020769A

Accident · Substantial damage

FAA accident report · Bell 206L-3 · Dickinson, AL · October 15, 2015

Date
October 15, 2015 · 16:00 local
Place
Dickinson, AL
Phase of flight
Other, Specify
Operating rules
Agricultural (Part 137)
Operator
2CSG
Damage
Substantial damage
Aircraft
N206CJ
NTSB investigation
NTSBERA16LA015
Reported as
Bell 206L-3
Reported engine
Allison 250-C20 series
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificates
Airline transport, flight instructor
Pilot’s flight hours
21,000 total6,500 in this make and model50 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.

Pilot had been conducting agricultural helicopter operations all day. On second to last pass, just as he was going to initiate left turn to reposition for the next pass and while at 75 -100 feet AGL , the pilot heard a loud pop sound. Pilot then experienced a complete loss of tail rotor control. The helicopter spun to the right. Pilot maintained main rotor power and used collective to cushion descent into the pine trees adjacent to the field he had been spraying. Helicopter hit the ground in a left side nose down position and came to rest on its left side. Investigation found that the tail rotor drive shaft had broken in two places and that a bolt was missing from the most forward coupling of the tail rotor drive shaft. Drive shaft was sheared in the middle of the short shaft and in the mid section of the shaft.

As the FAA filed it

PILOT HAD BEEN CONDUCTING AGRICULTURAL HELICOPTER OPERATIONS ALL DAY. ON SECOND TO LAST PASS, JUST AS HE WAS GOING TO INITIATE LEFT TURN TO REPOSITION FOR THE NEXT PASS AND WHILE AT 75 -100 FEET AGL , THE PILOT HEARD A LOUD POP SOUND. PILOT THEN EXPERIENCED A COMPLETE LOSS OF TAIL ROTOR CONTROL. THE HELICOPTER SPUN TO THE RIGHT. PILOT MAINTAINED MAIN ROTOR POWER AND USED COLLECTIVE TO CUSHION DESCENT INTO THE PINE TREES ADJACENT TO THE FIELD HE HAD BEEN SPRAYING. HELICOPTER HIT THE GROUND IN A LEFT SIDE NOSE DOWN POSITION AND CAME TO REST ON ITS LEFT SIDE. INVESTIGATION FOUND THAT THE TAIL ROTOR DRIVE SHAFT HAD BROKEN IN TWO PLACES AND THAT A BOLT WAS MISSING FROM THE MOST FORWARD COUPLING OF THE TAIL ROTOR DRIVE SHAFT. DRIVE SHAFT WAS SHEARED IN THE MIDDLE OF THE SHORT SHAFT AND IN THE MID SECTION OF THE SHAFT.

NTSB investigation

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