N57112

Substantial
Minor

ROCKWELL INTERNATIONAL 690AS/N: 11263

Accident Details

Date
Sunday, September 16, 2012
NTSB Number
WPR12LA428
Location
Ellensburg, WA
Event ID
20120920X50809
Coordinates
47.026390, -120.525001
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
2
Total Aboard
3

Probable Cause and Findings

The pilot’s failure to avoid a turbulent smoke column, which resulted in an overstress failure of the left aileron control rod.

Aircraft Information

Registration
Make
ROCKWELL INTERNATIONAL
Serial Number
11263
Engine Type
Turbo-prop
Year Built
1975
Model / ICAO
690AAC90
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
11
FAA Model
690A

Registered Owner (Current)

Name
SKYSTAR INC
Address
PO BOX 1196
City
COLUMBIA
State / Zip Code
CA 95310-1196
Country
United States

Analysis

On September 16, 2012, about 1600 Pacific daylight time, an Aero Commander 690A, N57112, encountered turbulence and an aileron control system failure while maneuvering above a wild land fire near Ellensburg, Washington (ELN). The airline transport pilot (ATP) sustained minor injuries, and the two passengers sustained no injuries. A precautionary landing was made at ELN after the turbulence encounter. The airplane was registered to Skystar, Inc., and operated by Courtney Aviation under the provisions of Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed and a company flight plan was filed for the local flight that departed ELN at 1545.

The pilot reported that while in a right turn around a wild land fire at 7,500 feet the airplane circled into a dark, narrow, ascending smoke column that was turbulent. The pilot quickly leveled the wings and continued to fly through the turbulent smoke column. After exiting the smoke column, the pilot noticed that the flight controls had a significant deflection to the right to keep the airplane’s wings level. The pilot elected to make a precautionary landing at ELN. After landing, the airplane was inspected, and the left aileron control rod was found separated along the threaded portion of the shaft, about 2.5 inches from the rod end.

The two portions of the aileron control rod were removed from the airplane and shipped to the National Transportation Safety Board Materials Laboratory for further examination. The examination revealed no apparent wear marks along the shaft of the rod; the rod ends exhibited dirt and similar contamination. The fracture surfaces of the control rod were rough with a dull, clean luster, which was indicative of overstress. The fracture surfaces displayed no indications of fatigue or corrosion.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR12LA428