N5203W

Substantial
None

Piper PA-28-160S/N: 28-238

Accident Details

Date
Wednesday, November 5, 2003
NTSB Number
FTW04LA018
Location
Amarillo, TX
Event ID
20031120X01931
Coordinates
35.169998, -101.825836
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 inadequate compensation for wind condition. Contributing factors were the pilot's lack of total experience in the make and model of aircraft, and the crosswind.

Aircraft Information

Registration
N5203W
Make
PIPER
Serial Number
28-238
Engine Type
Reciprocating
Year Built
1961
Model / ICAO
PA-28-160P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
DANTO PETER J
Address
3336 OAK CT
Status
Deregistered
City
LAFAYETTE
State / Zip Code
CA 94549-5204
Country
United States

Analysis

On November 5, 2003, about 1600 central standard time, a Piper PA-28-160 single-engine airplane, N5203W, was substantially damaged following a loss of directional control while landing at the Tradewind Airport (TDW), near Amarillo, Texas. The student pilot, sole occupant in the airplane, was not injured. The airplane was registered to, and operated by the pilot. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 local personal flight, which departed TDW approximately 1530.

On the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), the 30-hour student pilot stated that while landing on runway 17 after his first solo cross-country flight, right rudder pressure was applied to compensate for the prevailing crosswind conditions. After touchdown, the pilot added that he "failed to release the right rudder," and the airplane veered to the right side of the runway. The pilot further stated that he "overcompensated" with left rudder, and the airplane departed the left side of the runway. The airplane struck two fences before becoming to a stop.

Examination of the airplane by an FAA inspector, who responded to the accident site, revealed structural damage to the elevator, left aileron, left flap, and the leading edge of the left wing. The left fuel tank was found to have cracked.

Runway 17 is 5,099 feet long and 60 feet wide. The pilot reported the winds from 150 degrees at 7 to 8 knots, with gusts to 9 knots. At 1553, the reported winds at the Amarillo International Airport (AMA), located approximately five miles from the accident site, was reporting the winds from 080 degrees at 10 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# FTW04LA018