C-GLHQ

Substantial
None

Hughes 369DS/N: 1150D

Accident Details

Date
Sunday, July 11, 2004
NTSB Number
ANC04LA077
Location
Nome, AK
Event ID
20040804X01146
Coordinates
65.541114, -167.391937
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

The pilot's inadequate compensation for wind conditions while the helicopter was standing, which resulted in the coasting main rotor blade contacting the tail boom. A factor associated with the accident was the gusty wind condition.

Aircraft Information

Registration
Make
HUGHES
Serial Number
1150D
Year Built
1980
Model / ICAO
369D
No. of Engines
1
FAA Model
369D

Registered Owner (Current)

Name
9348-8260 Québec inc.
Address
804, avenue du Lac
City
Preissac
State / Zip Code
Quebec J0Y2E-0
Country
United States

Analysis

On July 11, 2004, about 1415 Alaska daylight time, a Canadian registered Hughes 369D helicopter, C-GLHQ, sustained substantial damage when a gust of wind resulted in the coasting main rotor blades striking the tail boom after landing at a remote site, about 80 miles northwest of Nome, Alaska. The helicopter was being operated by Prism Helicopter LTD, Wasilla, Alaska, as a visual flight rules (VFR) contract survey flight under Title 14, CFR Part 135 when the accident occurred. The commercial pilot and two passengers were not injured. Visual meteorological conditions prevailed, and company flight following procedures were in effect.

During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC) on July 13, the pilot said he landed on a ridge where he had landed several times that day. He said he shut down the engine, and was applying the main rotor brake when a gust of wind lifted the forward blades, which allowed the aft moving blades to strike the tail boom. The pilot said there had been a steady 20 knot wind blowing at the site all day, but there were no problems with wind gusts on the previous landings. He said there were no known mechanical anomalies with the helicopter prior to the accident, and that the main rotor blades and tail boom were damaged during the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC04LA077