SAE ARP1947C
Dendrite Arm Spacing of Structural Aircraft Quality D357 Aluminum Allow Castings, Determination and Acceptance of
Historical
Standard by SAE International, 2018-08-22
Quick Links
Norma
Get answers for your technical
Standart Library
Find standards for your sector
Standart Chek
Verify updates for your standards
|
Name |
Available Formats |
Availability |
Language |
|---|---|---|---|
| ARP1947C.pdf |
Secure PDF |
Immediate Download | English |
| ARP1947C.pdf |
Online Access |
Request Quote | English |
Customers Who Bought This Also Bought
About This Item
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).
ARP1947C completely revises Metallographic DAS Test Procedure (4.4) to provide more metallographic technique flexibility, and results from a Five-Year Review and update of this recommended practice.
Please request information about the document. Contact Page
Standard Details
- Publication Date: 2018-08-22
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Standard
- Subject: Heat treatment, Casting, Tensile strength, Aluminum alloys, Hazardous materials, Casting alloys, Arm, Particulate matter (PM), Test procedures
- Official SAE: Doi link
