C-FBTW

Substantial
None

Eurocopter AS350 B-2S/N: 3289

Accident Details

Date
Sunday, August 12, 2001
NTSB Number
DEN01LA145
Location
Cody, WY
Event ID
20010816X01699
Coordinates
44.615276, -109.115554
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the pilot's inadequate in-flight planning for an off site landing, which resulted in failure of the tail rotor drive shaft due to entanglement of his long-line in the drive shaft.

Aircraft Information

Registration
Make
EUROCOPTER
Serial Number
3289
Year Built
2000
Model / ICAO
AS350 B-2
No. of Engines
1
FAA Model
AS 350 B-2

Registered Owner (Current)

Name
TRK Helicopters (B.C.) Ltd.
Address
5225 - 216 St
Hangar 9
City
Langley
State / Zip Code
British Columbia V2Y2N-3
Country
United States

Analysis

On August 12, 2001, at 1430 mountain daylight time, a Eurocopter AS350 B-2 helicopter, Canadian registration C-FBTW, was substantially damaged when its long-line became entangled in its tail rotor during landing near Cody, Wyoming. The commercial pilot, the sole occupant in the aircraft, was not injured. Turbowest Helicopters Ltd. of Calgary, Canada, was operating the helicopter under Title 14 CFR Part 133. Visual meteorological conditions prevailed for the local long-line flight which originated approximately 25 minutes before the accident. The pilot had not filed a flight plan.

The pilot said that he was retrieving geophysical seismic bags, and attempted to land beside a bag of equipment. The area was flat, open, brush-covered terrain. During a "high hover," the long line became entangled in a mesquite bush. As the pilot moved forward and down, the line became taut. Approximately 20 feet above the ground, the line became entangled in the tail rotor drive shaft, breaking the control rods and the tail rotor drive shaft. The aircraft rotated to the left, and the pilot retarded the throttle and executed an engine out landing. Upon touchdown, the equipment on the ground punctured the bottom of the helicopter's fuselage breaking a fuel line, and spilling 40 gallons of fuel. There was no fire. The aircraft's tail boom was bent, the horizontal stabilizer was damaged, and the tail rotor drive shaft was broken.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN01LA145