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Viewing 163861 to 163890 of 185272
HISTORICAL
1969-05-01
Standard
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.
HISTORICAL
1969-05-01
Standard
AMS4917B
This specification covers a titanium alloy in the form of sheet, strip, and plate.
HISTORICAL
1969-05-01
Standard
AMS6520
This specification covers a premium aircraft-quality, maraging steel in the form of sheet, strip, and plate. These products have been used typically for large booster rocket applications, pressure vessels, and other components requiring through-hardening, without quenching, to a yield strength of 245 ksi (1689 MPa) or higher, but usage is not limited to such applications.
HISTORICAL
1969-05-01
Standard
AMS6433A
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
HISTORICAL
1969-05-01
Standard
AMS6460A
This specification covers a low-alloy steel in the form of welding wire. Primarily for use as filler metal for gas-tungsten-arc and gas-metal-arc welding of low-alloy steels requiring a joint capable of being heat treated to strength levels consistent with the metals joined. Alloy: NAX-9115-AC UNS Number: K11365
HISTORICAL
1969-05-01
Standard
AMS7310E
This specification covers piston rings fabricated from cast iron.
HISTORICAL
1969-05-01
Standard
AMS5029
This specification covers a low-alloy steel in the form of welding wire. This wire has been used typically as filler metal for gas-tungsten-arc welding of basis metal of similar composition and quality requiring heat treatment response in the weld joint approximating strength of the basis metal, but usage is not limited to such applications.
HISTORICAL
1969-05-01
Standard
AMS5110B
This specification covers a carbon steel in the form of wire supplied as coils of wire or as finished springs.
HISTORICAL
1969-05-01
Standard
AMS5388C
This specification covers a corrosion and heat-resistant nickel alloy in the form of investment castings.
HISTORICAL
1969-05-01
Standard
ARP1135
The purpose of this recommended practice is to provide recommendations for the design of a series of components which, when used as prescribed, will provide a wrench capable of producing up to 500,000 in.-lb of torque. This recommended practice covers the dimensions of an inside splined driver-wrench adapter, envelope of the housing-wrench reaction, the mechanical method of adapting the driver-wrench adapter to the wrench adapter driven end, and the housing-wrench reaction to the holder-counter torque.
HISTORICAL
1969-05-01
Standard
AMS6428A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1969-05-01
Standard
AMS6429A
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1969-05-01
Standard
AMS6430A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1969-05-01
Standard
AMS6299A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts to be carburized requiring high minimum core hardness with wide range in sections 0.375 inch (9.5 mm) and under in thickness, but usage is not limited to such applications. The core may or may not be machinable after hardening.
HISTORICAL
1969-05-01
Standard
AMS4956
This specification covers a titanium alloy in the form of wire for welding filler metal.
HISTORICAL
1969-05-01
Standard
AMS6276C
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1969-05-01
Standard
AMS2370
null, null
This specification covers quality assurance sampling and testing procedures used to determine conformance to applicable specification requirements of wrought carbon and low-alloy steel products and of forging stock.
HISTORICAL
1969-05-01
Standard
J916_196905
ABSTRACT
HISTORICAL
1969-05-01
Standard
AMS5080D
This specification covers a carbon steel in the form of bars, forgings, mechanical tubing, and forging stock. This product has been used typically for parts requiring moderate strength and high ductility, but usage is not limited to such applications.
HISTORICAL
1969-05-01
Standard
AMS7312C
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, oil scraper rings, and dual oil control rings in aircraft piston engines.
HISTORICAL
1969-05-01
Standard
AMS3611B
This specification covers a polycarbonate resin in the form of sheet. This sheet has been used typically for parts, such as aircraft heating ducts, cabin liners, fairings, storage boxes, and decorative laminates, requiring high impact strength, high strength, and dimensional stability, but usage is not limited to such applications. This material is sensitive to some solvents; each application must be evaluated on its own metrics.
HISTORICAL
1969-05-01
Standard
AMS4080J
This specification covers an aluminum alloy in the form of drawn seamless tubing. This tubing has been used typically for parts, such as conduits and low-pressure fluid lines, where moderate strength, ductility, and good weldability are required, but usage is not limited to such applications.
HISTORICAL
1969-05-01
Standard
AMS3693A
This specification covers a modified epoxy adhesive in the form of supported film supplied in rolls or sheets.
HISTORICAL
1969-05-01
Standard
AMS3823
This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of April 1994. It is recommended, therefore, that this specification not be specified for new designs.
HISTORICAL
1969-05-01
Standard
AMS5115C
This specification covers a carbon steel in the form of wire supplied as coils of wire or as finished springs. Primarily for springs, such as valve springs, subject to moderate stresses and requiring good fatigue properties.
HISTORICAL
1969-05-01
Standard
AMS4027G
This specification covers an aluminum alloy in the form of sheet and plate.
HISTORICAL
1969-05-01
Standard
AMS5622
This specification covers a premium aircraft-quality corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging, flash welded rings, or heading.
HISTORICAL
1969-05-01
Standard
AMS4082H
This specification covers an aluminum alloy in the form of seamless, drawn tubing.
HISTORICAL
1969-05-01
Standard
AMS6434A
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
HISTORICAL
1969-05-01
Standard
AMS2232D
This specification covers established inch/pound manufacturing tolerances applicable to carbon steel sheet, strip, and plate ordered to inch/pound dimensions. These tolerances apply to all conditions unless otherwise noted. The term 'excl' is used to apply only to the higher figure of the specified range. Tolerances for products sizes not listed herein shall be as agreed upon by purchaser and vendor.

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