SS-EN-4710-03 › Historical Revision Information
Aerospace series - Quick release fastening systems for non-structural applications - Part 03: Spring clamp
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This standard specifies the dimensions, mass, tolerances and static values of catch spring for use in fuselage interior equipment and non-structural or secondary structural area. This standard part shall be used in conjunction with EN 4710-06 and EN 4710-07 as described in EN 4710-02. The applicable temperature range is -55 °C to 85 °C.
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49.035 (Components for aerospace construction Tyres for aircraft, see 83.160.20)
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Designation Name
SS-EN 4710-03:2015
Revision Level
2015 EDITION
Status
Superseded
Publication Date
Oct. 12, 2015
Language(s)
English
Page Count
16
International Equivalent
EN 4710-03:2015(IDT)