N4604Y

Substantial
None

BELL 206B S/N: 556

Accident Details

Date
Tuesday, August 9, 1994
NTSB Number
ANC94LA103
Location
CHUIT RIVER, AK
Event ID
20001206X01908
Coordinates
61.080570, -151.159805
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
5
Total Aboard
5

Probable Cause and Findings

THE PILOT'S FAILURE TO MAINTAIN TAIL ROTOR EFFECTIVENESS DURING HOVER.

Aircraft Information

Registration
N4604Y
Make
BELL
Serial Number
556
Engine Type
Turbo-shaft
Model / ICAO
206B B06
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
ONEY JOHN DBA
Address
PO BOX 573
Status
Deregistered
City
QUARTZ SITE
State / Zip Code
AZ 85346
Country
United States

Analysis

On August 9, 1994, at 1230 Alaska daylight time, a skid equipped Bell 206B helicopter, registered to and operated by the pilot, crashed into the Chuit River. The business flight, operating under 14 CFR Part 91 for the purpose of fish guiding, departed the Anchorage, Alaska area and the destination was the Chuit River, 1 mile upstream from the mouth. Visual meteorological conditions prevailed and no flight plan was filed. The pilot and the four passengers were not injured and the helicopter rolled over and sank in the river.

According to the pilot, the wind was variable during his approach and landing. The gravel bar on which he landed was not level so he picked the helicopter back up to a hover to move to a more level location. The helicopter immediately made a turn to the right. He applied left pedal and could feel a response but was unable to stop the rotation before the helicopter struck the water. The helicopter came to rest upright in the river. Everyone exited the helicopter and it rolled over and sank in the river.

According to Bell Helicopter and the FAA, when a helicopter is operating at or near its maximum gross weight, tail rotor control may become marginal depending on wind conditions. Hovering with a tailwind may cause temporary loss of tail rotor effectiveness and allow the helicopter to rotate about its vertical axis.

The pilot's flight time was provided by the FAA and came from his Application for Airman Certificate dated 9/24/92.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC94LA103