SAE ARP 1947 : 2007
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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
30-09-2019
01-01-2007
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Superseded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 AMS 4249B : 2012 (R2018) | 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 AMS 4241 : 2015 | 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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