ARP1947A DENDRITE ARM SPACING OF STRUCTURAL AIRCRAFT QUALITY D357 ALUMINUM ALLOY CASTINGS, DETERMINATION AND ACCEPTANCE OF

Reaffirmed

7/1/1996

Features
Issuing Committee
Scope
Content
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 50,000 psi (345 MPa).
Meta TagsDetails
DOI
https://doi.org/10.4271/ARP1947A
Citation
SAE International Recommended Practice, DENDRITE ARM SPACING OF STRUCTURAL AIRCRAFT QUALITY D357 ALUMINUM ALLOY CASTINGS, DETERMINATION AND ACCEPTANCE OF, SAE Standard ARP1947A, Revised October 1989, Issued October 1985, https://doi.org/10.4271/ARP1947A.
Additional Details
Publisher
Published
7/1/1996
Product Code
ARP1947A
Content Type
Recommended Practice
Status
Reaffirmed
Language
English

Revisions