N70AF

Substantial
None

Ayres S2R-600S/N: 2547R

Accident Details

Date
Thursday, June 1, 2006
NTSB Number
DFW06CA158
Location
Childress, TX
Event ID
20060719X00966
Coordinates
34.433612, -100.286109
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 inability to maintain directional control while landing due to the failure of the rudder horn due to corrosion.

Aircraft Information

Registration
Make
AYRES
Serial Number
2547R
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
S2R-600A660
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
S2R-600

Registered Owner (Current)

Name
N70AF LLC
Address
47563 815TH RD
City
ORD
State / Zip Code
NE 68862-5362
Country
United States

Analysis

While in cruise flight, the 19,620-hour commercial pilot lost control of the rudder pedals and experienced trouble maintaining directional control of the single-engine, turbine powered agricultural airplane. The pilot reported that "he dumped his chemical load at a safe location" and elected to discontinue the aerial application flight. The pilot proceed to a larger airport for a landing. The pilot added that he made several attempts to land as he was having trouble keeping the airplane aligned with runway 35 unless he maintained a much higher than normal airspeed on final approach. On his final attempt, the pilot was able to land, but as the airplane slowed down, it veered off the right side of the 5,949-foot long, by 75-foot wide asphalt runway. Following the loss of control, the left wing of the airplane collided with a tractor. A Federal Aviation Administration (FAA) safety inspector performed an on-scene examination of the airplane and found that the rudder horn was corroded and had completely separated. According to the pilot, the rudder horn is covered by fabric and it was difficult to inspect during a preflight inspection. The pilot added that even though the operator has a procedure in place to wash the airplane after spraying corrosive chemicals, he suggested that somehow chemicals had made contact with the rudder horn which caused the corrosion. At the time of the last 100 hour inspection, which was completed less than 11 days prior to the mishap, the tailwheel-equipped airplane had accumulated a total of 11,107.8 hours since new. The wind at the time of the accident was reported from 030 degrees at 8 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# DFW06CA158