N5426J

Substantial
None

Cessna 172NS/N: 5426J

Accident Details

Date
Saturday, July 31, 2004
NTSB Number
DEN04LA114
Location
Hurricane, UT
Event ID
20040805X01149
Coordinates
37.133609, -113.300552
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the student pilot's failure to maintain aircraft control during the landing. Contributing factors include the crosswind, the wind gusts, and the exceeded maximum demonstrated crosswind component.

Aircraft Information

Registration
Make
CESSNA
Serial Number
5426J
Engine Type
Reciprocating
Model / ICAO
172NC172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
172N

Registered Owner (Current)

Name
MEDIA STEW LLC
Address
2101 ARROWHEAD DR
City
CARSON CITY
State / Zip Code
NV 89706-0402
Country
United States

Analysis

On July 31, 2004, at approximately 1440 mountain daylight time, a Cessna 172N, N5426J, piloted by a student pilot, was substantially damaged when it impacted terrain after departing the runway during landing at Hurricane Airport, Hurricane, Utah. Visual meteorological conditions prevailed at the time of the accident. The solo training flight was being conducted under the provisions of Title 14 CFR Part 91 without a flight plan. The student pilot reported no injuries. The local flight originated at 1300.

According to the accident report submitted by the student pilot, he was landing on runway 18 "too fast." The pilot wrote that he "lost control and veered off to the west" side of the runway. The right main landing gear was bent, the left wing tip and wing spar were bent up and the firewall was wrinkled. A postaccident examination of the airplane systems revealed no anomalies.

The winds at St. George Municipal Airport, 14 nautical miles west of Hurricane, were reported as 260 degrees at 18 knots with gusts to 25 knots. The calculated crosswind component was between 19 and 25 knots. According to the Cessna Pilot Operating Handbook, the maximum demonstrated crosswind component for this airplane is 15 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# DEN04LA114