N16673

Substantial
Serious

BELL 206BS/N: 2088

Accident Details

Date
Monday, October 28, 2013
NTSB Number
WPR14CA052
Location
Milo, OR
Event ID
20131113X11809
Coordinates
42.953609, -123.149444
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
3
Minor Injuries
0
Uninjured
0
Total Aboard
3

Probable Cause and Findings

The pilot's failure to see and avoid wires while maneuvering at a low-altitude, which resulted in the main rotor blades striking the wires.

Aircraft Information

Registration
N16673
Make
BELL
Serial Number
2088
Engine Type
Turbo-shaft
Year Built
1976
Model / ICAO
206BB06
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
FERREIRA ROBERT A
Address
PO BOX 370
Status
Deregistered
City
ASHLAND
State / Zip Code
OR 97520-0013
Country
United States

Analysis

The pilot stated that the purpose of the flight was for the two passengers, who were both biologists, to conduct a low-level river/land survey. Prior to departure, the pilot discussed the route of flight with the passengers and they all reviewed the maps and sectionals for possible hazards with an emphasis on wire crossings. After departure, the pilot attempted to facilitate the biologists' view out the windows by maneuvering the helicopter in a crab angle with the flight path tracking down the riverbank and the nose pointing left. The pilot maintained an altitude just above tree-top level and about an hour into the flight the pilot observed the first high power line crossing. Approximately 20 minutes thereafter, one of the passengers called attention to another line crossing, which was equipped with marker balls.

The pilot stated that as they continued, the river divided into numerous channels and one of the passengers advised him which path to follow. After surveying one of the channels, he maneuvered the helicopter in a 90-degree turn to circle back and then it was decided they did not need to return to the channel's origin. The pilot then made a left turn to adjoin the river and immediately observed blue sparks and a wire contact on the upper windscreen bubble. The helicopter was substantially damaged after it descended and came to rest in 4.5 feet of water about 50 feet from the power line.

The pilot reported no preimpact mechanical malfunctions or failures with the helicopter that would have precluded normal operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR14CA052