MIL-C-5778D
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MIL-C-5778D, MILITARY SPECIFICATION, COVERS, AIRCRAFT COMPONENTS, GENERAL REQUIREMENTS FOR (8 MAY 1992) [S/S BY SAE-AS5778]., This specification covers general requirements for covers intended to protect the following aircraft parts: Cockpit, Fuselage, Canopy, Engine, Armament, Propeller or Rotor, Miscellaneous.
Product Code:SAE MAM2221
Title:Tolerances, Metric, Copper and Copper Alloy Bars and Rods (Cancelled Jan 2008, Superseded by AMS2221)
Issuing Committee:Ams D Nonferrous Alloys Committee
Scope:This specification covers established metric manufacturing tolerances applicable to bars and rods of copper and copper alloys ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term 驴exclusive驴 is used to apply only to the higher figure of a specified range.Product Code:SAE AMS7735
Title:Alloy Wire, Round, 35Pd - 30Ag - 14Cu - 10Au - 10Pt - 0.85Zn, Solution Heat Treated
Issuing Committee:Ams D Nonferrous Alloys Committee
Scope: This specification covers a palladium-silver alloy in the form of round wire.
Rationale: This specification covers a palladium-silver alloy in the form of round wire.