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Viewing 36781 to 36810 of 43551
HISTORICAL
1969-11-01
Standard
AMS6423A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1969-11-01
Standard
AMS6426
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. Primarily for parts, such as bearing components, for service up to 500 degrees F (260 degrees C) and requiring a through-hardening steel capable of developing hardness not lower than 60 HRC in cross-sections 3 inches (76 mm) and under.
HISTORICAL
1969-11-01
Standard
AMS4004
This specification covers an aluminum alloy in the form of foil. This foil has been used typically for corrugated or expanded honeycomb core material for use in sandwich construction, but usage is not limited to such applications.
HISTORICAL
1969-11-01
Standard
AMS4970B
This specification covers a titanium alloy in the form of bars, wire, forgings, and forging stock.
HISTORICAL
1969-11-01
Standard
AMS4070G
This specification covers an aluminum alloy in the form of drawn, round seamless tubing. This tubing has been used typically for parts, such as brackets, conduits, and low-pressure fluid lines, requiring good weldability, moderate strength, and good resistance to corrosion, but usage is not limited to such applications.
HISTORICAL
1969-11-01
Standard
AMS7498D
This specification covers flash welded rings made of titanium and selected titanium alloys.
HISTORICAL
1969-11-01
Standard
AMS4921B
This specification covers one grade of commercially-pure titanium in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1969-11-01
Standard
AMS5613K
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, flash welded rings, or heading.
HISTORICAL
1969-11-01
Standard
AMS4967B
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging, heading, or flash welded rings.
HISTORICAL
1969-11-01
Standard
AMS2406E
This specification covers the requirements for electrodeposited hard chromium plate.
HISTORICAL
1969-11-01
Standard
AMS5578
This specification covers a premium-quality corrosion and heat resistant steel in the form of welded tubing. This tubing has been used typically for parts requiring corrosion resistance and high strength up to 800 degrees F (427 degrees C) after precipitation heat treatment, but usage is not limited to such applications. Certain design and processing procedures may cause this tubing to become susceptible to stress-corrosion cracking after precipitation heat treatment; SAE ARP 1110 recommends practices to minimize such conditions.
HISTORICAL
1969-11-01
Standard
AMS5355B
This specification covers a corrosion resistant steel in the form of investment castings. These castings have been used typically for parts requiring good corrosion resistance and strength up to 600 °F (316 °C), but usage is not limited to such applications (See 8.3). Certain processing procedures and service conditions may cause these castings to become subject to stress-corrosion cracking; ARP1110 recommends practices to minimize such conditions. Where stress-corrosion is considered to be a factor, precipitation heat treatment should be performed at a temperature not lower than 1000 °F (538 °C).
HISTORICAL
1969-11-01
Standard
AMS5336A
This specification covers a low-alloy steel in the form of investment castings. These castings have been used typically for small structural parts of intricate design requiring heat treatment to minimum tensile strengths up to 150 ksi (1034 MPa), but usage is not limited to such applications.
HISTORICAL
1969-11-01
Standard
AMS2816G
This specification covers procedures for tab marking of bare welding wire to provide positive identification of cut lengths and spools.
HISTORICAL
1969-11-01
Standard
AMS2231E
This specification covers established inch/pound manufacturing tolerances applicable to carbon steel bars 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.
HISTORICAL
1969-11-01
Standard
AMS2371
null, null
This specification covers quality assurance sampling and testing procedures used to determine conformance to applicable specification requirements of wrought corrosion and heat-resistant steel and alloy products and of forging stock.
HISTORICAL
1969-11-01
Standard
AMS4928D
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings.
CURRENT
1969-11-01
Standard
AMS4906A
This specification has been Cancelled by the Aerospace Materials Division, SAE, as of August 1994.
HISTORICAL
1969-11-01
Standard
AMS4096
This specification covers an aluminum alloy in the form of sheet and plate clad on two sides.
HISTORICAL
1969-11-01
Standard
AMS4229
This specification covers an aluminum alloy in the form of sand, permanent mold, and composite mold castings.
HISTORICAL
1969-11-01
Standard
AMS5640J
This specification covers three types of a free-machining, corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
HISTORICAL
1969-11-01
Standard
AMS4173
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing. These extrusions have been used typically for parts requiring moderate strength and where distortion during machining must be minimized, but usage is not limited to such applications.
HISTORICAL
1969-10-31
Standard
AS478C
This standard provides the following: a. Definition of terms pertaining to marking. b. Symbols for marking location. c. Requirements and restrictions for permanent markings. d. Types of marking methods. e. Rules for designating marking methods. f. Table listing marking methods.
CURRENT
1969-10-15
Standard
ARP1111
This concept for measuring worn splines provides a direct wear depth dimension by utilizing the unworn involute surface as a contact point from which to measure the depth of wear on the spline tooth at the pitch diameter. Fig. 1 shows spline wear patterns and pitch diameter gaging points.
HISTORICAL
1969-10-01
Standard
J857A_196910
ABSTRACT
HISTORICAL
1969-10-01
Standard
J410C_196910
ABSTRACT
HISTORICAL
1969-10-01
Standard
AIR1083
The purpose of this document is to provide design guides for increasing survivability of military Air Vehicle Hydraulic Systems when subjected to ground fire.
CURRENT
1969-10-01
Standard
AIR1090
This report includes a procedure for typical pulse voltage measurement using the pressurized ball gap, calibration procedure, and a description of the pressurized ball gap.