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Standard

Induction Hardening of Steel Parts

2007-12-17
CURRENT
AMS2745A
This specification defines the requirements for locally hardening steel parts by the induction hardening method.
Standard

Heat Treatment, Carbon, Low-Alloy and Specialty Steels

1976-01-01
HISTORICAL
AMS2760
This specification covers the procedure for through-hardening and related heat treatments of carbon, low-alloy, and specialty steel parts to produce specified mechanical properties within the capability of each respective steel. Heat treating processes such as induction hardening, flame hardening, carburizing, nitriding, austempering, and martempering are recognized processes but are not covered by this specification.
Standard

Induction Hardening of Steel Parts

2001-01-01
HISTORICAL
AMS2745
This specification defines the requirements for locally hardening steel parts by the induction hardening method.
Standard

Piston Rings, Centrifugally-Cast Alloyed Iron, 0.50Mo - 0.50Cu

1948-05-01
HISTORICAL
AMS7311
This specification covers a centrifugally-cast, alloyed iron in the form of sleeves for the fabrication of piston rings. Primarily for use as top compression rings in aircraft piston engines. Rings usually require chromium plating for compatibility with the cylinder barrel material.
Standard

Piston Rings, Centrifugally-Cast Alloyed Iron, 0.50Mo - 0.50Cu

1952-06-01
HISTORICAL
AMS7311A
This specification covers a centrifugally-cast, alloyed iron in the form of sleeves for the fabrication of piston rings. Primarily for use as top compression rings in aircraft piston engines. Rings usually require chromium plating for compatibility with the cylinder barrel material.
Standard

Piston Rings, Centrifugally-Cast Alloyed Iron, 0.50Mo - 0.50Cu

1969-05-01
HISTORICAL
AMS7311C
This specification covers a centrifugally-cast, alloyed iron in the form of sleeves for the fabrication of piston rings. Primarily for use as top compression rings in aircraft piston engines. Rings usually require chromium plating for compatibility with the cylinder barrel material.
Standard

Piston Rings, Centrifugally-Cast Alloyed Iron, 0.50Mo - 0.50Cu

1958-01-01
HISTORICAL
AMS7311B
This specification covers a centrifugally-cast, alloyed iron in the form of sleeves for the fabrication of piston rings. Primarily for use as top compression rings in aircraft piston engines. Rings usually require chromium plating for compatibility with the cylinder barrel material.
Standard

Piston Rings, Centrifugally-Cast Alloyed Iron, 0.50Mo - 0.50Cu

1974-12-01
HISTORICAL
AMS7311D
This specification covers a centrifugally-cast, alloyed iron in the form of sleeves for the fabrication of piston rings. Primarily for use as top compression rings in aircraft piston engines. Rings usually require chromium plating for compatibility with the cylinder barrel material.
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