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SAE ARP1947 Rev D

Dendrite Arm Spacing of Structural Aircraft Quality D357 Aluminum Alloy Castings, Determination and Acceptance of
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SAE ARP1947 Rev D

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

PUBLISH DATE 2024
SAE ARP1947 Rev D
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).
SDO SAE: SAE International
Document Number ARP1947
Publication Date May 9, 2024
Language en - English
Page Count 8
Revision Level D
Supercedes
Committee
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