Abstract
Includes the external diameters and thicknesses of tubes, for all metallic materials, to be selected for all uses in aircraft structural and system design. They shall be selected from those specified in the table. The tolerances shall be specified in the relevant standard appropriate to the material and intended application.
General information
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Status: Under developmentStage: DIS registered [40.00]
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Edition: 3Number of pages: 2
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Technical Committee :ISO/TC 20/SC 10ICS :49.080
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Life cycle
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Previously
PublishedISO 2964:1985
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Now