SAE AMS4307B PDF

SAE AMS4307B PDF

Name:
SAE AMS4307B PDF

Published Date:
04/02/2012

Status:
Active

Description:

Aluminum Alloy, Extrusions 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T61511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Precipitation Heat Treated

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:
$19.8
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This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of February, 2005. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those specifications which have previously been widely used and which may be required on some existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs.

This specification covers an aluminum alloy in the form of extruded bars, rods, profiles, and tubing.

These extrustions have been used typically for structural parts requiring a combination of high strength, moderate fatigue strength, and moderate exfoliation corrosion resistance, but usage is not limited to such applications.
File Size : 1 file , 730 KB
Note : This product is unavailable in Ukraine, Russia, Belarus
Published : 04/02/2012

History

SAE AMS4307B
Published Date: 04/02/2012
Aluminum Alloy, Extrusions 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T61511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Precipitation Heat Treated
$19.8

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