N7053K

Substantial
None

Piper PA-20S/N: 20-160

Accident Details

Date
Thursday, April 28, 2005
NTSB Number
ATL05LA076
Location
Thomaston, GA
Event ID
20050602X00709
Coordinates
32.954723, -84.263053
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The unapproved repair of the tailwheel rudder arm assembly, which resulted in an overload failure during touchdown and subsequent loss of control of the airplane and on-ground collision with an object.

Aircraft Information

Registration
Make
PIPER
Serial Number
20-160
Engine Type
Reciprocating
Year Built
1950
Model / ICAO
PA-20PA20
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-20

Registered Owner (Current)

Name
MATLAD INC
Address
3511 SILVERSIDE RD STE 105
City
WILMINGTON
State / Zip Code
DE 19810-4902
Country
United States

Analysis

On April 28, 2005, at 0935 eastern daylight time, a Piper PA-20, N7053K, registered to Matlad, Inc., and operated by the airline transport pilot, veered off the runway during landing roll at Thomaston - Upson County Airport, Thomaston, Georgia. The personal flight was operated under the provisions of Title 14 CFR Part 91 with no flight plan filed. Visual meteorological conditions prevailed. The airline transport pilot and the passenger were not injured, and the airplane sustained substantial damage. The flight departed Aiken Municipal Airport, Aiken, South Carolina, about 0815.

The pilot stated the approach to runway 30 was normal, and the main wheels touched down normally. The pilot stated that, when the tailwheel touched down, the airplane pulled hard to the left, application of the rudder had no effect, and the airplane continued left off the side of the runway. The airplane continued through the grass, and the empennage collided with the runway's precision approach path indicator lights.

Examination of the airplane revealed damage to the empennage and fuselage. The tailwheel rudder arm assembly was found fractured and separated on the right side, and evidence of a previous weld repair outboard of the fracture was observed. The weld repair was observed at the thickest area of the tapered rudder arm, and the fracture was observed at a smaller-diameter area. Metallurgical examination of the rudder arm revealed the aluminum component showed deformation near the fracture surfaces with no evidence of fatigue.

The pilot stated he had purchased the airplane two days before the accident, and the airplane had accumulated approximately 1.9 hours since annual inspection. Review of maintenance records for the airplane revealed no record of the rudder arm assembly repair.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL05LA076