SS-EN-4662 Aerospace series - Test specification for vibration control components

SS-EN-4662 - 2010 EDITION - CURRENT


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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.

To find similar documents by classification:

17.160 (Vibrations, shock and vibration measurements Including measuring instruments and installations Vibration and shock with respect to human beings, see 13.160 Balancing and balancing machines, see 21.120.40 Vibration protection of buildings, see 91.120.25)

49.035 (Components for aerospace construction Tyres for aircraft, see 83.160.20)

49.040 (Coatings and related processes used in aerospace industry Coatings for general use, see 25.220)

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Designation Name

SS-EN 4662:2010

Revision Level

2010 EDITION

Status

Current

Publication Date

March 22, 2010

Language(s)

English

Page Count

20

International Equivalent

EN 4662:2010(IDT)