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SAE AMS4241

Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Dendrite Arm Spacing (DAS) Controlled

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Organization: SAE
Publication Date: 1 December 2015
Status: active
Page Count: 10
scope:

Form

This specification covers an aluminum alloy in the form of castings.

Application

These castings have been used typically for structural aircraft components (see 8.3) requiring DAS quality control, but usage is not limited to such applications.

Document History

SAE AMS4241
December 1, 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
Form This specification covers an aluminum alloy in the form of castings. Application These castings have been used typically for structural aircraft components (see 8.3) requiring DAS quality...
November 1, 2009
Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Dendrite Arm Spacing (DAS) Controlled
Form This specification covers an aluminum alloy in the form of castings. Application These castings have been used typically for structural aircraft components (See 8.3) requiring DAS quality...
July 1, 2002
Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Dendrite Arm Spacing (DAS) Controlled
Form: This specification covers an aluminum alloy in the form of castings. Application: These castings have been used typically for structural aircraft components (See 8.3) requiring DAS quality...
July 1, 2002
Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Dendrite Arm Spacing (DAS) Controlled
Form: This specification covers an aluminum alloy in the form of castings. Application: These castings have been used typically for structural aircraft components (See 8.3) requiring DAS quality...
March 1, 2002
(R) Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Dendrite Arm Spacing (DAS) Controlled
Form: This specification covers an aluminum alloy in the form of castings. Application: These castings have been used typically for structural aircraft components (See 8.3) requiring DAS quality...
July 1, 1992
Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Dendrite Arm Spacing (DAS) Controlled
SCOPE: Form: This specification covers an aluminum alloy in the form of castings. Application: Primarily for structural aircraft components (See 8.3) requiring DAS quality control. Safety - Hazardous...
July 1, 1986
ALUMINUM ALLOY CASTINGS, SAND COMPOSITE 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Aircraft Structural Quality
Form: This specification covers an aluminum alloy in the form of sand castings Application: Primarily for structural aircraft components. Alloy D357.0 has restricted composition within the limits...

References

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