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SAE ARP 1947C:2018-08-22

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SAE ARP 1947C:2018-08-22

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

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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 50000 psi (345 MPa).
Author SAE
Editor SAE
Document type Standard
Format File
ICS 49.025.20 : Aluminium
Number of pages 7
Replace SAE ARP 1947B:2007-08-17
Set AEROPAKS10U-10
Year 2018
Document history SAE ARP 1947B:2007-08-17
Country USA
Keyword SAE 1947;SAE ARP1947C;SAE ARP1947C;SAE ARP 1947