N36044

Substantial
None

Taylorcraft BC12-65S/N: 3011

Accident Details

Date
Saturday, July 9, 2005
NTSB Number
DEN05CA107
Location
Roosevelt, UT
Event ID
20050809X01185
Coordinates
40.286109, -110.052223
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 failure to maintain control of the aircraft during landing. A factor contributing to the accident was the crosswind.

Aircraft Information

Registration
Make
TAYLORCRAFT
Serial Number
3011
Engine Type
Reciprocating
Year Built
1941
Model / ICAO
BC12-65TAYB
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
BC12-65

Registered Owner (Current)

Name
SHIPLEY JOHN L
Address
9185N 6800W
City
TREMONTON
State / Zip Code
UT 84337
Country
United States

Analysis

On July 9, 2005, at approximately 1630 mountain daylight time, a Taylorcraft BC12-65, N36044, piloted by a private pilot, was substantially damaged while landing at the Roosevelt Municipal Airport (74V), Roosevelt, Utah. Visual meteorological conditions prevailed at the time of the accident. The personal cross-country flight was being conducted under the provisions of Title 14 CFR Part 91 without a flight plan. The pilot was not injured. The flight originated at Heber City, Utah, at approximately 1530.

The pilot said he listened to the local weather observation and noted uncharacteristic northerly winds of 10 knots, gusting to 17 knots at his time of arrival. He said he then performed a crosswind landing on runway 25 (6,500 feet by 75 feet, dry asphalt). After approximately a 20 foot ground roll, a gust of wind lifted the aircraft off the runway and pivoted it left (counterclockwise). The airplane then touched down off the side of the runway, impacted a rock, and nosed down. The pilot exited the aircraft and pushed it back upright to stop fuel from leaking.

An examination of the airplane showed the airplane's propeller bent aft, and the left wing broken aft to include the left wing spar. Flight control continuity was confirmed. An examination of the engine, engine controls, and other airplane systems showed no anomalies.

At 1653, the wind conditions at Vernal, Utah (VEL), located 26 nautical miles east of the accident site, were 240 degrees at 8 knots. The wind conditions 33 minutes prior to the accident were 190 degrees at 13 knots, gusting 16 knots. The crosswind component at that time was calculated as 11 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# DEN05CA107