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Viewing 36781 to 36810 of 37724
1947-12-01
Standard
AMS6372A
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing. This tubing has been used typically for parts, 0.75 inch (19 mm) and under in section thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 40 HRC when properly hardened and tempered and for parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.
1947-12-01
Standard
AMS5514
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate. These products have been used typically for parts manufactured by deep drawing or spinning and requiring corrosion resistance up to 800 degrees F (427 degrees C), but usage is not limited to such applications.
1947-12-01
Standard
AMS2670
This specification covers the engineering requirements for producing brazed joints using copper as the brazing filler metal.
1947-12-01
Standard
AMS3110A
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
1947-12-01
Standard
AMS3128A
This specification covers a pigment material in the form of a paste comprising aluminium powder mixed in a suitable binder.
1947-12-01
Standard
AMS4071A
This specification covers an aluminum alloy in the form of drawn, round seamless tubing. This tubing has been used typically for parts, such as hydraulic systems and fuel and oil lines, but usage is not limited to such applications.
1947-12-01
Standard
AMS4139B
This specification has been declared 'CANCELLED' by the Aerospace Materials Division, SAE, as of September 1996, and has been superseded by AMS 4126. Alloy: 7075-T6 UNS Number: A97075
1947-12-01
Standard
AMS4135E
This specification covers an aluminum alloy in the form of die forgings, hand forgings, rolled rings, and stock for forgings on rolled rings. Primarily for applications, such as aircraft structural members, requiring material with moderately high strength. Certain design and processing procedures may cause these forgings to become susceptible to stress corrosion cracking; ARP 823 recommends practices to minimize such conditions.
1947-12-01
Standard
AMS2221A
This specification covers established inch/pound manufacturing tolerances applicable to bars and rods of copper alloys ordered to inch/pound dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "exclusive" is used to apply only to the higher figure of a specified range.
1947-12-01
Standard
AMS2222A
This specification covers established inch/pound manufacturing tolerances applicable to copper and copper alloy sheet, strip, and plate ordered to inch/pound dimensions. These tolerances apply to all conditions, unless otherwise noted.
1947-12-01
Standard
AMS4360B
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of September 1996. Alloy: AZ80A-T5 UNS Number: M11800
1947-12-01
Standard
AMS4555A
This specification covers a copper alloy (leaded brass) in the form of seamless tubing.
1947-12-01
Standard
AMS4530A
This specification covers one type of copper-beryllium alloy in the form of sheet, strip, and plate.
1947-12-01
Standard
AMS4532
This specification covers one type of copper-beryllium alloy in the form of sheet and strip.
1947-12-01
Standard
AMS4710A
This specification covers one type of brass in the form of wire.
1947-12-01
Standard
AMS4650C
This specification covers one type of copper-beryllium alloy in the form of bars, rods, forgings, and forging stock. These products have been used typically for parts requiring a combination of high strength, good wear resistance, and corrosion resistance and where electrical conductivity or low magnetic susceptibility may be important, but usage is not limited to such applications.
1947-12-01
Standard
AMS4725
This specification covers one type of copper-beryllium alloy in the form of wire.
1947-12-01
Standard
AMS3685
null, null
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of June, 1996.
1947-12-01
Standard
AMS5362
This specification covers a corrosion and heat resistant steel in the form of investment castings. These castings have been used typically for structural parts, where welding during fabrication may be required, for use up to 1500 °F (816 °C), but usage is not limited to such applications.
1947-12-01
Standard
AS393
The purpose of this Aeronautical Standard is to specify minimum requirements for pitot-static type of electrically heated Airspeed Tubes primarily for use in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in paragraph 3.3. This aeronautical standard covers two basic types of instruments as follows: Type I - Pitot Pressure, straight and L-shaped, 12 and 14 volt nominal, 2 wire circuit. Type II - Pitot and Static Pressured, straight and L-shaped, 12 and 24 volt nominal, 2 wire circuit.
1947-12-01
Standard
AMS5667
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading.
1947-12-01
Standard
AMS5350
This specification covers a corrosion and moderate heat-resistant steel in the form of investment castings.
1947-12-01
Standard
AMS2665
This specification covers the engineering requirements for producing brazed joints in parts fabricated from steels, iron alloys, nickel alloys, cobalt alloys, and copper alloys by use of silver alloys, and the properties of such joints. This procedure has been used typically for joints requiring high strength up to 400 degrees F (204 degrees C), but usage is not limited to such applications.
1947-12-01
Standard
AMS5521
This specification covers a corrosion and heat-resistant steel in the form of sheet, strip, and plate.
1947-09-01
Standard
AMS5366
This specification covers a corrosion and heat-resistant steel in the form of investment castings.
1947-09-01
Standard
AMS5365
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of January 1995. It is recommended, therefore, that this specification not be specified for new designs.
1947-09-01
Standard
AMS5380
This specification covers a corrosion and heat-resistant cobalt alloy in the form of investment castings.
1947-09-01
Standard
AMS5378
This specification covers a corrosion and heat resistant cobalt alloy in the form of investment castings.
1947-09-01
Standard
AMS5375
This specification covers a corrosion and heat resistant cobalt alloy in the form of investment castings.