This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of 1-1-84. It is recommended that this specification not be specified for new designs. This cover sheet should be attached to the initial issue of the sUbject specification. Noncurrent refers to those procedures which have previously been widely used and which may be required on some existing designs in the future. The Aerospace Materials Division does not recommend these as standard procedures for future use in new designs. Each of these "Noncurrent" specifications is available from SAE upon request. This specification has been CANCELLED by the Aerospace Materials Division, SAE, as of August, 1989. By this action, subject specification number and its title will be deleted from the active specification index of Aerospace Material Specifications.
This specification covers the engineering requirements for electrodeposition of lead and indium and diffusion of the indium into the lead, and the properties of the deposit.
This specification covers the engineering requirements for electroless deposition of nickel-boron on various materials and the properties of the deposit.
This specification covers the engineering requirements for electroless deposition of nickel-boron on various materials and the properties of the deposit.
This specification covers the engineering requirements for a treatment to provide maximum attainable corrosion resistance to sheet metal parts, such as brackets, spacers, and washers, fabricated from martensitic corrosion-resistant steels, usually AMS 5504 or AMS 5508 and having hardness not higher than 40 HRC, or ferritic corrosion-resistant steels, usually AMS 5506. The treatment is not recommended for use on parts subject to impact in service.
This specification covers the requirements for computer-controlled laser peening of metal part surfaces to induce residual compressive stresses at and beneath the surface.