N216EH

Substantial
None

Eurocopter AS-350B2 S/N: 3184

Accident Details

Date
Saturday, November 11, 2000
NTSB Number
ANC01LA020
Location
GIRDWOOD, AK
Event ID
20001226X45477
Coordinates
60.899974, -148.909591
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's failure to maintain adequate altitude/clearance from terrain. A factor in the accident was flat light conditions.

Aircraft Information

Registration
Make
EUROCOPTER
Serial Number
3184
Engine Type
Turbo-shaft
Year Built
1999
Model / ICAO
AS-350B2
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
6
FAA Model
AS 350 B2

Registered Owner (Current)

Name
ERA HELICOPTERS LLC
Address
600 AIRPORT BLVD
City
LAKE CHARLES
State / Zip Code
LA 70607-0610
Country
United States

Analysis

On November 11, 2000, about 1300 Alaska standard time, a high skid equipped Eurocopter AS-350-B2 helicopter, N216EH, sustained substantial damage while maneuvering over snow-covered terrain, about four miles east of Girdwood, Alaska. The helicopter was being operated as a visual flight rules (VFR) on-demand passenger flight under Title 14, CFR Part 135 when the accident occurred. The helicopter was operated by ERA Aviation Inc., Anchorage, Alaska. The airline transport certificated pilot, and the sole passenger, were not injured. Visual meteorological conditions prevailed. VFR company flight following procedures were in effect. The flight originated at the Girdwood airport, about 1115.

During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on November 21, 2000, the vice president of safety for the operator reported that the pilot was conducting a photo flight in the area of Mount Alyeska. According to the vice president, the pilot related that he was maneuvering along a mountain ridge. The end of the ridge line was in a shadow. While flying in the area of shadow, the pilot began to lose depth perception, and he added engine power to move away from the ridge. The left landing gear skid tube made contact with snow on the ridge, and the pilot felt a vibration. He landed on lower terrain and shut down the helicopter. A subsequent inspection of the helicopter disclosed internal damage to the tail rotor spars, and a torsional twist in the tail rotor drive shaft.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC01LA020