N350ST

Substantial
None

AIRBUS A350S/N: 2789

Accident Details

Date
Monday, February 18, 2019
NTSB Number
GAA19CA139
Location
Eureka, AK
Event ID
20190219X80927
Coordinates
61.774166, -147.123336
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's selection of unsuitable terrain for landing on snow-covered mountainous terrain with steep rocks above, which resulted in loose rocks damaging the main rotor blades and the subsequent loss of helicopter controllability. 

Aircraft Information

Registration
N350ST
Make
AIRBUS
Serial Number
2789
Engine Type
None
Year Built
1994
Model / ICAO
A350A350
No. of Engines
0

Registered Owner (Historical)

Name
ROTA AVIATION CONSULTING LLC
Address
172 RED BLUFF VISTA
Status
Deregistered
City
GLENWOOD SPRINGS
State / Zip Code
CO 81601
Country
United States

Analysis

The helicopter pilot reported that, while transporting snow skiers, he landed on a 20º slope below the mountain peak, where he directed the guide and two skiers to unload with the engine running. The pilot saw loose rocks from the peak above fall into the main rotor disk, and after the skiers were clear of the helicopter, he raised the collective and brought the helicopter to a hover. While hovering, he did not feel any controllability issues, so he repositioned the helicopter up the mountain about 30 feet and "toed in" to unload additional skiers. After the remaining skiers unloaded, the pilot flew the helicopter down the mountain to shut down and examine the main rotor blades.

About 10 seconds into the flight, the helicopter began to shake violently. He initiated a forced landing, but about 150 feet above the trees, the "flight controls became progressively hard to control", and the helicopter pitched nose up. Immediately, he lowered the nose and collective and about 30 feet above the snow-covered ground, the main rotor disk struck trees and the helicopter impacted the terrain.

The helicopter sustained substantial damage to the main rotor blades, fuselage, tail boom and tail rotor blades.

The director of operations reported that there were no preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# GAA19CA139