N95250

Substantial
None

Taylorcraft BC12-D S/N: 9650

Accident Details

Date
Sunday, June 11, 2000
NTSB Number
ANC00LA067
Location
NINILCHIK, AK
Event ID
20001212X21140
Coordinates
60.069019, -151.420974
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 directional control during the take-off run. Factors associated with the accident were rough/uneven, soft terrain.

Aircraft Information

Registration
Make
TAYLORCRAFT
Serial Number
9650
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
BC12-D TAYB
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
BC12-D

Registered Owner (Current)

Name
SUTTON AIRCRAFT SALVAGE LLC
Address
13500 E JENSEN AVE
City
PALMER
State / Zip Code
AK 99645-9430
Country
United States

Analysis

On June 10, 2000, about 2200 Alaska daylight time, a wheel equipped Taylorcraft BC12-D airplane, N95250, sustained substantial damage during takeoff from a remote site, about 15 miles northeast of Ninilchik, Alaska, at latitude 60 degrees, 01 minutes north, and longitude 151 degrees, 35 minutes west. The airplane was being operated as a visual flight rules (VFR) personal flight under Title 14, CFR Part 91, when the accident occurred. The certificated private pilot, and the one passenger aboard, were not injured. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated about 1900, at the Soldotna Airport, Soldotna, Alaska.

During a telephone conversation with the National Transportation Safety Board investigator-in-charge on June 10, the pilot reported that he was attempting a westerly departure from a 600 feet long remote airstrip. He said that during the takeoff run, the airplane veered to the left of the narrow airstrip. He added that upon rotation, the main wheels hit a series of soft bumps, and the airplane became airborne before a safe flying speed could be reached. He said that the airplane continued to fly beyond the end of the airstrip, and then settled. The main wheels contacted soft tundra, and the airplane nosed over. The airplane sustained substantial damage to the wings and fuselage.

The pilot noted in his written report to the NTSB that wind conditions at the time of the accident were from 090 degrees, at 3 knots.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC00LA067