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Viewing 36781 to 36810 of 38466
1952-06-01
Standard
AMS5511A
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
1952-06-01
Standard
AMS4081
This specification covers an aluminum alloy in the form of seamless, round tubing.
1952-02-15
Standard
AMS4370A
ABSTRACT
1952-02-15
Standard
AMS4210E
This specification covers an aluminum alloy in the form of sand castings.
1952-02-15
Standard
AMS3130A
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.
1952-02-15
Standard
AMS4434E
This specification covers a magnesium alloy in the form of sand castings.
1952-02-15
Standard
AMS6427
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 requiring a combination of high tensile strength and good ductility with relatively high impact strength and hardness, but usage is not limited to such applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment. ARP1110 recommends practices to minimize such conditions.
1952-02-05
Standard
AMS3150B
1. ACKNOWLEDGMENT: A vendor shall mention this specification number and its revision letter in all quotations and when acknowledging purchase orders. 2. APPLICATION: , For use in commercial aircraft hydraulic systems. 3. COMPOSITION: There shall be no restrictions on the type of materials used in the fluid except those imposed by the technical requirements of this specification.
1952-02-01
Standard
ARP265
This Aeronautical Recommended Practice provides a standard method for locating and dimensioning the airfoil portions of parts such as blades, and vanes. This method will apply to blades, or vanes with or without a base. The forms of attachment are varied; therefore, the blade bases shown in the following figures are for illustration only. All dimensions and notes shown pertaining to the common functional point, line or plane are considered to be applied to a datum, on or off the part, irrespective of the form of attachment.
1952-02-01
Standard
AMS5361A
This specification covers a corrosion and heat resistant steel in the form of sand or centrifugal castings.
1952-02-01
Standard
AMS5392D
This specification covers a moderate corrosion and heat resistant alloy iron in the form of sand castings.
1952-02-01
Standard
AMS5686A
This specification covers a corrosion-resistant steel in the form of wire. This wire has been used typically for fabricating into rivets, but usage is not limited to that application.
1952-02-01
Standard
AMS5685C
This specification covers a corrosion-resistant steel in the form of wire.
1952-02-01
Standard
AMS5721B
Primarily for parts, such as bolts, dowels and fittings, for use up to 1150 F.
1952-02-01
Standard
AMS5627
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.
1952-02-01
Standard
AMS5577
This specification covers a corrosion and heat resistant steel in the form of welded tubing. This tubing has been used typically for parts requiring both corrosion and heat resistance, especially when such parts are welded during fabrication and for parts requiring oxidation resistance up to 2000 degrees F (1093 degrees C) but useful at that temperature only when stresses are low, but usage is not limited to such applications.
1952-02-01
Standard
AMS3414A
This specification covers an aluminum welding flux in the form of powder.
1952-02-01
Standard
AMS4134A
This specification covers an aluminum alloy in the form of die forgings and forging stock.
1952-02-01
Standard
AMS3028B
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE as of March 1990.
1952-02-01
Standard
AMS3032B
This specification has been "SUPERSEDED" by the Aerospace Materials Division, SAE, as of 2 November 1990.
1952-02-01
Standard
AMS3034
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE.
1952-02-01
Standard
AMS3036B
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE.
1952-02-01
Standard
AMS3165A
This specification covers a petroleum-base liquid solvent.
1952-02-01
Standard
AMS3170A
This specification covers a blend of alcohols and esters in the form of a liquid.
1952-02-01
Standard
ARP266
This recommended practice is written to cover the installation of combustion heaters used in the following applications. Fuselage Compartment Heating: (All occupied regions, cargo space, and transparent area heating.) Thermatl Ice Prevention System Engine and Accessory Heating: (When heater is installed as part of the aircraft).
1952-02-01
Standard
AMS4125D
This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those materials which may have been widely used previously and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. “NONCURRENT” specifications are available from SAE upon request.