N5343G

Substantial
None

de Havilland DHC-2S/N: 862

Accident Details

Date
Sunday, September 16, 2001
NTSB Number
ANC01LA152
Location
ARCTIC VILLAGE, AK
Event ID
20011218X02417
Coordinates
68.090278, -145.599761
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 selection of unsuitable terrain for takeoff. A factor in the accident was rock(s)/boulders in the area of takeoff.

Aircraft Information

Registration
Make
DE HAVILLAND
Serial Number
862
Engine Type
Reciprocating
Year Built
1958
Model / ICAO
DHC-2DH2T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
8
FAA Model
BEAVER DHC-2 MK.1

Registered Owner (Current)

Name
COYOTE AIR LLC
Address
PO BOX 9053
City
COLDFOOT
State / Zip Code
AK 99701-9053
Country
United States

Analysis

On September 16, 2001, about 1200 Alaska daylight time, a wheel-equipped deHavilland DHC-2 airplane, N5343G, sustained substantial damage during takeoff from a remote area, about 65 miles northeast of Arctic Village, Alaska. The airplane was being operated as a visual flight rules (VFR) cross-country personal flight under Title 14, CFR Part 91, when the accident occurred. The airplane was registered to Coyote Air LLC., and operated by the pilot. The airline transport certificated pilot, and the one passenger, were not injured. Visual meteorological conditions prevailed.

During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on December 5, 2001, the pilot reported he flew to a remote gravel bar located along the Coleen River to pick up a friend who was rafting in the area. The pilot said he was departing toward the north from an area that was about 1,000 feet long. During the takeoff roll, the tailwheel struck a large rock. He continued the takeoff and landed at Coldfoot, Alaska, without incident.

A postaccident examination of the tailwheel area on December 4, revealed damage to the tailwheel casting, fuselage bulkheads, and a stringer near the tailwheel attach point. The airplane repair conducted at an FAA approved repair station, included replacement of bulkheads at fuselage stations 228 and 224, and replacement of fuselage skin at stations 228 through 204. Doublers were fabricated and installed at stations 244 through 208. An FAA Form 337, Major Repair and Alteration, was completed by the repair station.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC01LA152