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.
Status: PublishedPublication date: 1985-04
Edition: 2Number of pages: 2
Technical Committee: ISO/TC 20/SC 10 Aerospace fluid systems and components
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|std 1 38|
|std 2 38||Paper|