ROCKWELL INTERNATIONAL 690A

Ellensburg, WA — September 16, 2012

Event Information

DateSeptember 16, 2012
Event TypeACC
NTSB NumberWPR12LA428
Event ID20120920X50809
LocationEllensburg, WA
CountryUSA
Coordinates47.02639, -120.52500
AirportBowers Field Airport
Highest InjuryMINR

Aircraft

MakeROCKWELL INTERNATIONAL
Model690A
CategoryAIR
FAR Part091
Aircraft DamageSUBS

Conditions

Light ConditionDAYL
WeatherVMC

Injuries

Fatal0
Serious0
Minor1
None2
Total Injured1

Event Location

Probable Cause

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

Full Narrative

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.

About This NTSB Record

This aviation event was investigated by the National Transportation Safety Board (NTSB). NTSB investigates all U.S. civil aviation accidents to determine probable cause and issue safety recommendations to prevent future accidents.

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