N997GM

Destroyed
None

Bell 206B-IIIS/N: 2366

Accident Details

Date
Thursday, April 4, 2002
NTSB Number
DEN02LA036
Location
Leadville, CO
Event ID
20020422X00566
Coordinates
39.213333, -106.190002
Aircraft Damage
Destroyed
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

the pilot's inadvertent flight into adverse weather, which resulted in a collision with terrain. A contributing factor was the downdraft.

Aircraft Information

Registration
N997GM
Make
BELL
Serial Number
2366
Engine Type
Turbo-shaft
Year Built
1978
Model / ICAO
206B-IIIB06
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
COPTER LEASE LLC TRUSTEE
Address
4701 HAWKINS ST NE
Status
Deregistered
City
ALBUQUERQUE
State / Zip Code
NM 87109-4333
Country
United States

Analysis

On April 4, 2002, approximately 1400 mountain standard time, N997GM, a Bell 206B-III helicopter, operated by AeroWest Helicopters, Inc., of Corrales, New Mexico, was destroyed when it struck terrain during an uncontrolled descent 5 miles north of Leadville, Colorado. Both the commercial pilot and a passenger received minor injuries. Visual meteorological conditions prevailed, and no flight plan had been filed for the aerial observation flight being conducted under Title 14 CFR (Code of Federal Regulations) Part 91. The flight originated in Eagle, Colorado, approximately 1330.

According to a written statement given to the Lake County Sheriff's Office, the pilot said he was patrolling a power line between Leadville and Breckenridge. He was about 100 feet to the right of the power line, flying east into a 10 to 18 knot headwind. Airspeed was between 70 and 80 knots, altitude was 400 feet above the ground, and power was between 70 to 80 percent torque. The power line turned north towards Mosquito Pass. As the pilot started the turn, a "strong downdraft pushed the helicopter" towards the ground. The LOW ROTOR RPM horn sounded and the pilot lowered the collective control to regain rotor rpm, and simultaneously moved the cyclic control forward and to the right to avoid the power lines. After rotor rpm was regained, the pilot increased torque to 100 to 103 percent "to keep the helicopter flying." He said the downdraft continued to push the helicopter towards the ground and the LOW ROTOR RPM horn continued sounding. The pilot said he "decreased collective with forward airspeed with the cyclic" in an attempt to fly out of the downdraft, but to no avail. The helicopter's aft skids struck snow-covered terrain and "dug in." The helicopter rolled "once or twice" and came to rest on the underside of the fuselage.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN02LA036