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Standard

BRAZING, SILVER For Use Up to 800°F (427°C)

1991-07-01
HISTORICAL
AMS2664E
This specification covers the engineering requirements for producing brazed Joints in parts made of steels, iron alloys, nickel alloys, and cobalt alloys by use of silver alloy filler metals, and the properties of such Joints.
Standard

COPPER BRAZING

1991-07-01
HISTORICAL
AMS2670G
This specification covers the engineering requirements for producing brazed joints using copper as the brazing filler metal.
Standard

Fluoroscopic X-Ray Inspection

1991-01-01
CURRENT
AMS2650A
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.
Standard

Aviation Fuel, Grade 100/130

1991-01-01
CURRENT
AMS3032D
This specification has been "SUPERSEDED" by the Aerospace Materials Division, SAE, as of 2 November 1990.
Standard

NICKEL-CADMIUM PLATING Diffused

1990-10-01
HISTORICAL
AMS2416G
This specification covers the engineering requirements for a diffused electrodeposit of cadmium into an electrodeposit of nickel on carbon, low-alloy, and corrosion-resistant steels and the properties of the diffused deposit.
Standard

SHOT PEENING, COMPUTER MONITORED

1990-10-01
HISTORICAL
AMS2432
This specification establishes the engineering requirements for computer monitored peening of surfaces of parts.
Standard

HEAT TREATMENT OF TITANIUM ALLOY PARTS

1990-07-01
HISTORICAL
AMS2801
This specification covers the engineering requirements for heat treatment by part fabricators (users) or their vendors or subcontractors of parts (See 1.1.2) made from the following titanium alloys.
Standard

Oxygen, Liquid, Propellant Grade

1990-01-01
CURRENT
AMS3012A
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE as of January 1990.
Standard

Oil, Carburetor Flushing

1990-01-01
CURRENT
AMS3070E
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE as of January 1990.
Standard

Aviation Fuel, Grade 91/98

1990-01-01
CURRENT
AMS3028D
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE as of March 1990.
Standard

Standards and Test Methods

1989-10-01
CURRENT
AMS2350BA
To establish the issue of specifications, standards, and recommended practices published by standardizing agencies other than divisions and committees of the Aerospace Council of SAE approved for use in determining conformance to requirements of Aerospace Material Specifications (AMS) and other specifications in which this specification is referenced.
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