N6134X

Substantial
None

Cessna TU206GS/N: U20605826

Accident Details

Date
Wednesday, June 14, 2006
NTSB Number
DEN06CA089
Location
Alamosa, CO
Event ID
20060713X00934
Coordinates
37.384723, -105.851387
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

the pilot's failure to maintain aircraft control during the landing. Contributing factors include the gusty winds, the crosswind, and the pilot exceeding the maximum demonstrated crosswind component for the airplane.

Aircraft Information

Registration
N6134X
Make
CESSNA
Serial Number
U20605826
Engine Type
Reciprocating
Year Built
1980
Model / ICAO
TU206GC206
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
POLKOWSKE LEROY A DBA
Address
PO BOX 80
Status
Deregistered
City
LA JARA
State / Zip Code
CO 81140-0080
Country
United States

Analysis

According to the accident report submitted by the pilot, he encountered a gust of wind during the landing flare to runway 20 (8,519 feet by 100 feet, asphalt). The pilot stated that a gust brought the left wing up and he added power to recover and the airplane "straightened out." He stated that he reduced power to land and encountered a second gust of wind, bringing the left wing up again. The right wing impacted the runway and the airplane "ground looped." The engine separated from the airplane, the right wing tip was crushed, and the left tire separated. An examination of the airplane's systems, conducted by the FAA Inspector, revealed no anomalies. The pilot did not report any problems with the airplane or its systems.

The closest official weather observation station was San Luis Valley regional Airport/Bergman field (ALS), Alamosa, Colorado. The routine aviation weather report (METAR) for ALS, issued at 1152, reported, winds, 240 degrees at 27 knots, gusting 36 knots; visibility, 10 statute miles; sky condition, clear; temperature 27 degrees Celsius (C); dewpoint, 01 degrees C; altimeter, 30.25 inches. The crosswind component was calculated to be between 17 and 23 knots. According to the Cessna Pilot Operating Handbook, the maximum demonstrated crosswind component for this airplane is 20 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# DEN06CA089