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SAE ARP 1947D:2024-05-09

Dendrite Arm Spacing of Structural Aircraft Quality D357 Aluminum Alloy Castings, Determination and Acceptance of

Summary

This document covers the recommended practice for determining the acceptability of the dendrite arm spacing (DAS) of D357-T6 aluminum alloy castings required to have tensile strength not lower than 50 ksi (345 MPa).

Notes

Technical characteristics

Publisher SAE International
Publication Date 05/09/2024
Page Count 8
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Weight (in grams) ---