SAE AMS4249A PDF

SAE AMS4249A PDF

Name:
SAE AMS4249A PDF

Published Date:
04/02/2012

Status:
Active

Description:

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)

Publisher:
SAE International

Document status:
Active

Format:
Electronic (PDF)

Delivery time:
10 minutes

Delivery time (for Russian version):
200 business days

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Choose Document Language:
$26.1
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This specification covers an aluminum alloy in the form of castings.

These castings have been used typically for durability and damage tolerance structural aircraft components requiring fatigue resistance and fracture toughness, but usage is not limited to such applications.
File Size : 1 file , 1.3 MB
Note : This product is unavailable in Ukraine, Russia, Belarus
Published : 04/02/2012

History

SAE AMS4249B
Published Date: 04/02/2018
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)
$27.3
SAE AMS4249A
Published Date: 04/02/2012
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)
$26.1

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