N47122

Substantial
None

Bell 206B S/N: 971

Accident Details

Date
Thursday, July 8, 1999
NTSB Number
ANC99TA090
Location
DEADHORSE, AK
Event ID
20001212X19148
Coordinates
70.429885, -149.289657
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

A failure of the pilot-in-command to perform an adequate preflight inspection, and remove a rotor blade tie-down strap.

Aircraft Information

Registration
N47122
Make
BELL
Serial Number
971
Engine Type
Turbo-shaft
Year Built
1973
Model / ICAO
206B B06
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
STALOKT INC
Address
PO BOX 699
Status
Deregistered
City
MEDFORD
State / Zip Code
OR 97501
Country
United States

Analysis

On July 8, 1999, about 1230 Alaska daylight time, a Bell 206B helicopter, N47122, sustained substantial damage during engine start-up, about 75 miles southwest of Deadhorse, Alaska. The helicopter was being operated as a visual flight rules (VFR) U.S. Government flight by the U.S Department of Interior, Bureau of Land Management, Fairbanks, Alaska, when the accident occurred. The helicopter, provided by Tundra Copters Inc., Fairbanks, Alaska, was utilized on an on-demand 14 CFR Part 135 flight. The certificated commercial pilot, and the three passengers, were not injured. Visual meteorological conditions prevailed. VFR company flight following procedures were in effect.

During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on July 8, 1999, the director of operations for Tundra Copters Inc., reported the pilot loaded his passengers into the helicopter at a remote biological survey site. The pilot then began an engine start, but a main rotor blade tie-down strap was still attached to one of the rotor blades. As the rotor blades began to turn, the strap struck the upper end of the vertical stabilizer, crushing the leading edge in an aft direction. The helicopter's tail boom was deformed and wrinkled, just forward of the tail rotor gear box.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC99TA090