This standard specifies the procedure and the parameter for testing static and dynamic stiffness of vibration
control components (e.g. shock mounts with bushes).
This standard applies to vibration control components all installed for aircraft applications. It may be applied
when referred to in the product standard or in a design specification.
BS EN 4662:2010 history
2010BS EN 4662:2010 Aerospace series - Test specification for vibration control components