N6465V

Substantial
None

Helio H-295 S/N: 1417

Accident Details

Date
Saturday, August 23, 1997
NTSB Number
ANC97LA128
Location
FORT YUKON, AK
Event ID
20001208X08537
Coordinates
66.560111, -145.250854
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

failure of the pilot to maintain directional control of the airplane, which resulted in a swerve and collision with a tree as the pilot continued the takeoff, subsequently jamming the stabilator and causing the plane to crash in water.

Aircraft Information

Registration
Make
HELIO
Serial Number
1417
Engine Type
Reciprocating
Year Built
1969
Model / ICAO
H-295
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
H-295

Registered Owner (Current)

Name
CORNICE LLC
Address
PO BOX 60789
City
FAIRBANKS
State / Zip Code
AK 99706-0789
Country
United States

Analysis

On August 23, 1997, about 1500 Alaska daylight time, a tundra tire equipped Helio H-295 airplane, N6465V, crashed during takeoff from a remote area of river, about 78 miles north of Fort Yukon, Alaska. The airplane was being operated as a visual flight rules (VFR) on-demand passenger flight, under Title 14 CFR Part 135, when the accident occurred. The airplane, operated by Wright Air Service Inc., Fairbanks, Alaska, sustained substantial damage. The certificated airline transport pilot, and 2 passengers, were not injured. Visual meteorological conditions prevailed. A VFR flight plan was filed. The flight originated at the Arctic Village Airport, Arctic Village, Alaska, about 1300.

The operator reported the pilot was departing a 1,000 foot long gravel bar in a southbound direction. The area, located along the Sheenjek River, had been used by the operator in the past, and the pilot was picking up two passengers from a river float trip. During the takeoff run, the airplane had just attained flying speed. Suddenly, the airplane veered to the right, and the tail struck a tree along the edge of the gravel bar, jamming the stabilator. The airplane lifted off the ground, and attained a nose high pitch attitude. The pilot pushed forward on the flight controls, but was unable to lower the nose of the airplane. The airplane climbed to about 100 feet above the ground, and then descended toward the river. The airplane collided with the river, and came to rest in about 3 feet of water. The airplane received damage to the right main landing gear, stabilator, fuselage, and engine.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC97LA128