Operational Shock test verified if the equipment or instrument will continue to function in accordance to its specifications after being subject to shocks during normal aircraft operation.

Such tests are conducted by Thermodyne Engineering Ltd. in accordance with RTCA/DO-160 Section 7.for all Categories and Procedures.

Saw tooth, half sine or square shocks can be applied from 6g to 20g in 11 or 20 milliseconds and in all 6 directions.



For more information, please contact JYeremian@thermodyne.ca.
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