SAE MAM2243D

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This specification has been declared “CANCELLED” and superseded by the Aerospace Materials Division, SAE, as of September, 2007, and has been superseded by AMS 2243. The requirements of the latest issue of AMS 2243 shall be fulfilled whenever reference is made to the cancelled MAM 2243C. By this action, this document will remain listed inthe Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”.

This specification covers manufacturing tolerances applicable to seamless and welded tubing of corrosion and heat resistant steel ordered to metric dimensions. These tolerances apply to all conditions and are based on individual measurements, unless otherwise noted. Tubing may be specified by two dimensions only (OD and wall thickness, ID and wall thickness, or OD and ID).

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Published:
09/13/2007
File Size:
1 file , 450 KB

SAE MAM5706C

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This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading procured in SI (metric) units.

AMS 5706 is the inch/pound version of this MAM.

These products have been used typically for parts, such as fasteners, flanges, and rings, requiring high strength up to 815 degrees C and oxidation resistance up to 955 degrees C, particularly those parts which are formed or welded and then heat treated to develop required properties, but usage is not limited to such applications.

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Published:
03/12/2003
File Size:
1 file , 78 KB

SAE RB4A

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A guide for the use by companies contracting for design of electronic products with the Department of Defense (DOD) and other government agencies.

This Bulletin present concepts and techniques for quantifying electronic equipment reliability. The techniques are responsive to the requirements of various branches of the Department of Defense and are also useful with regard to other Government agencies (e.g., NASA).

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Published:
06/17/2016
File Size:
1 file , 1.7 MB

SAE MAM2232C

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This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2007, and has been superseded by AMS 2232. The requirements of the latest issue of AMS 2232 shall be fulfilled whenever reference is made to the cancelled MAM 2232. By this action, this document will remain listed in the Numercial Section of the Index of Aerospace Material Specifications noting that it is superseded by AMS 2232.

This specification covers established metric manufacturing tolerances applicable to carbon steel sheet, strip, and plate ordered to metric dimensions. These tolerances apply to all conditions unless otherwise noted. The term “excl” is used to apply only to the higher figure of the specified range. Tolerances for product sizes not listed herein shall be as agreed upon by purchaser and vendor.

AMS 2232 is the inch/pound version of this MAM.

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Published:
06/18/2007
File Size:
1 file , 170 KB

SAE MAM4131B

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This specification covers an aluminum alloy in the form of die forgings and hand forgings procured to metric (SI) units.

AMS 4131 is the inch/pound verison of this MAM.

These forgings have been used typically for parts requiring a combination of good strength and resistance to stress-corrosion cracking, but usage is not limited to such applications.

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Published:
03/12/2003
File Size:
1 file , 76 KB