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Viewing 36781 to 36810 of 38377
1951-12-01
Standard
AMS5378A
This specification covers a corrosion and heat resistant cobalt alloy in the form of investment castings.
1951-12-01
Standard
AMS4121A
This specification covers an aluminum alloy in the form of bars, rods, and wire.
1951-12-01
Standard
AMS4291A
This specification covers an aluminum alloy in the form of die castings.
1951-12-01
Standard
AMS4122B
This specification covers an aluminum alloy in the form of rolled or cold finished bars, rods, and wire, and of flash welded rings.
1951-12-01
Standard
AMS4212D
This specification covers an aluminum alloy in the form of castings.
1951-12-01
Standard
AMS4350D
This specification covers a magnesium alloy in the form of extruded bar rods, wire, tubing, and profiles. These products have been used typically for low-strength parts requiring rigidity and low density, but usage is not limited to such applications. Special care is necessary to prevent corrosion.
1951-12-01
Standard
AMS4284B
This specification covers an aluminum alloy in the form of permanent mold castings.
1951-12-01
Standard
AMS5645F
This specification covers a corrosion and heat resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings.
1951-12-01
Standard
AMS5648B
This specification covers a corrosion and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings.
1951-12-01
Standard
AMS5651B
This specification covers a corrosion and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings.
1951-12-01
Standard
AMS2671
This specification covers the engineering requirements for producing brazed joints using metallic copper as the brazing filler metal.
1951-12-01
Standard
AMS5665B
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
1951-12-01
Standard
AMS5360A
This specification covers a corrosion and heat resistant steel in the form of investment castings.
1951-12-01
Standard
AMS5112D
This specification covers a carbon steel in the form of wire supplied as coils, spools, or cut lengths. This wire has been used typically for springs subject to high stress or requiring good fatigue properties up to 200 °F (93 °C), but usage is not limited to such applications.
1951-12-01
Standard
AMS5643A
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging, flash welded rings or heading.
1951-12-01
Standard
AMS5516C
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
1951-12-01
Standard
AMS5560C
This specification covers a corrosion-resistant steel in the form of seamless tubing. This tubing has been used typically for parts, such as fluid-conducting lines, not subjected to high pressure and requiring good corrosion resistance, but usage is not limited to such applications. Welding, brazing, or other exposure to temperatures over 800 °F (427 °C) during fabrication may impair corrosion resistance.
1951-12-01
Standard
AMS5565C
This specification covers a corrosion-resistant steel in the form of welded tubing. This tubing has been used typically for parts, such as fluid-conducting lines not subjected to high pressure, requiring good corrosion resistance, but usage is not limited to such applications. Welding, brazing, or other exposure to temperatures over 800 degrees F (427 degrees C) during fabrication may impair corrosion resistance.
1951-11-01
Standard
AMS6421
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
1951-11-01
Standard
AMS6422
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
1951-10-01
Standard
AIR13A
INTRODUCT ION Conventional internal conbustion a i r c r a f t engines require the same basic conditions for starting in cold weather as they do in warn weather. These are: (1) The engine must be cranked a t a reasonable speed. ( 2 ) A combustible mixture must be delivered t o the cylinders. (3) An ignition spark must be supplied which is capable of igniting t'ne charge a t the proper t i m e . (4) The fits and olearanoes of mating parts in the engine m u s t be such that normal Sunctions occur a t a l l temperatures. (5) The engine must receive a usable lubricant. (6) The engine must develop s u f f i c i e n t power t o overcome its own f r i c t i o n and accelerate itself t o the desired operating speed.
1951-10-01
Standard
AMS2503A
This specification covers the engineering requirements for finishing aircraft parts and assemblies with a black enamel.
1951-10-01
Standard
AMS5710B
This specification covers a corrosion and heat resistant steel in the form of bars, forgings, and forging stock.
1951-10-01
Standard
AMS5705A
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of September, 2002. Alloy: CNS UNS Number: S63005
1951-10-01
Standard
AMS4352
This specification covers a magnesium alloy in the form of extruded bars, rods, wire, tubing, and profiles. These extrusions have been used typically for parts requiring toughness and moderate abrasion resistance, but usage is not limited to such applications.
1951-10-01
Standard
AMS4424E
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of August, 1992. It is recommended, therefore, that this specification not be specified for new designs.
1951-10-01
Standard
AMS3214E
This specification covers a nitrile (NBR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.