ARP1947D: Dendrite Arm Spacing of Structural Aircraft Quality D357 Aluminum Alloy Castings, Determination and Acceptance of - Recommended Practice

Features

Issuing Committee: AMS D Nonferrous Alloys 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 ksi (345 MPa).

Rationale

Content: ARP1947D results from an SAE Five-Year Review and update of this specification with changes to relocate Definitions (see 2.3), correct typographical errors (see Title and 2.3.2) and strength units consistent with related material specifications (see 1.1 and 4.1.1), and update Applicable Documents (see Section 2).

Meta Tags

Topics: Aluminum alloys
Casting alloys
Aircraft

Details

DOI: https://doi.org/10.4271/ARP1947D

Pages: 8

Citation: SAE International Recommended Practice, Dendrite Arm Spacing of Structural Aircraft Quality D357 Aluminum Alloy Castings, Determination and Acceptance of, SAE Standard ARP1947D, Revised May 2024, Reaffirmed July 1996, Issued October 1985, https://doi.org/10.4271/ARP1947D.

Additional Details

Publisher: SAE International

Published: May 09

Product Code: ARP1947D

Content Type: Recommended Practice

Status: Revised

Language: English

Historical