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SAE ARP1947B

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

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

Superseded date

30-09-2019

Superseded by

SAE ARP1947C

Published date

01-01-2007

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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).

Committee
AMS-D
DocumentType
Standard
PublisherName
SAE International
Status
Superseded
SupersededBy

SAE AMS4249A ALUMINUM ALLOY CASTINGS 7.0SI - 0.58MG - 0.15TI - 0.06BE (D357.0-T6) SOLUTION AND PRECIPITATION HEAT TREATED (REQUIRING FATIGUE AND FRACTURE TOUGHNESS TESTING)
SAE AMS4241E ALUMINUM ALLOY CASTINGS, 7.0SI - 0.58MG - 0.15TI - 0.06BE (D357.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED, DENDRITE ARM SPACING (DAS) CONTROLLED
SAE AMS 4288 : 2016 ALUMINUM ALLOY CASTINGS, 7.0SI - 0.58MG - 0.15TI (E357.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED

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