N8514W

Substantial
Minor

PIPER PA-28-235 S/N: 28-10015

Accident Details

Date
Saturday, March 11, 1995
NTSB Number
FTW95LA135
Location
HOBART, OK
Event ID
20001207X03116
Coordinates
35.019496, -99.089836
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
3
Total Aboard
4

Probable Cause and Findings

THE PILOT'S INADEQUATE COMPENSATION FOR THE WIND CONDITIONS. A FACTOR WAS THE GUSTY WIND CONDITION.

Aircraft Information

Registration
N8514W
Make
PIPER
Serial Number
28-10015
Engine Type
Reciprocating
Model / ICAO
PA-28-235 P28B
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BORTECH LTD
Address
PO BOX 3083
Status
Deregistered
City
BORGER
State / Zip Code
TX 79008
Country
United States

Analysis

On March 11, 1995, at 1600 central standard time, a Piper PA-28- 235, N8514W, was substantially damaged during landing at Hobart, Oklahoma. The private pilot and two passengers were not injured. One passenger received minor injuries. Visual meteorological conditions prevailed for the personal cross country flight from Borger, Texas to Mena, Arkansas.

The pilot reported the information in the following paragraph. He decided to land at Hobart Municipal Airport due to deteriorating visibility. While he was flaring the airplane for landing on runway 17, a wind gust raised the left wing. Full power was added in an attempt to go around; however, the right wing tip contacted the ground. The airplane then "bellied in at a 90 degree angle to the runway on the grass." After exiting the airplane, the pilot noticed that the wind direction was "changing abruptly by about 30 degrees."

A Federal Aviation Administration Inspector examined the wreckage and made the following observations. The first ground strike was 425 yards south and 94 yards west of the north end of runway 17 where a panel from the left wing was located. The airplane came to rest a total distance of 168 yards west of the runway. Damage included separation of the engine, the left main landing gear, and the nose landing gear, deformation of the firewall, and an upward bending of the outboard left and right wings.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW95LA135