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Viewing 164191 to 164220 of 175603
1960-11-01
Standard
AMS3357B
This specification covers a silicone (VMQ) rubber in the form of sheet, strip, tubing, extrusions and molded shapes. Primarily for parts required to operate or seal from -55 to +230 degrees C (-67 to +446 degrees F), compounded especially for aircraft piston engine oil resistance and low compression set. Silicone elastomer is resistant to deterioration by weathering and by high-aniline-point petroleum-base oils and remains flexible over the temperature range noted. This material is not normally suitable for use in contact with gasoline or aromatic fuels and low-aniline-point petroleum-base fluids due to excessive swelling of the elastomer.
1960-10-01
Standard
AS430
This Aeronautical Standard covers the following basic types of fire detection instruments, or combinations thereof, intended for use in protecting aircraft powerplant installation, auxiliary powerplants, combustion heaters and other installations where fuel, oil or similar fires may occur. Basic Types: Definition of Type I: Thermal - Fixed Temperature, an instrument which will actuate an alarm signal when exposed to any temperature above a definite pre-established level. Type II: Thermal - Rate of Rise, an instrument which will actuate an alarm signal when exposed to any rate of temperature change abouve a definite pre-established level. Type III: Flame - Contact, an instrument which will actuate an alarm signal when exposed to physical contact with flame.
1960-10-01
Magazine
1960-10-01
Standard
ARP600
Torques to be determined for tube or hose end connections shall be specific for a material combination; however, may vary upon consideration of variables for a given tube size. These variables include tube material, fitting material, testing medium, required proof pressure and lubricant used. Resultant torques from substitution of listed variables will vary for a given tube size. Therefore, a developed torque is satisfactory only for the specific combination used in its formulation. These valves are to be used for connecting tubing and hose assemblies to each other and/or to related equipment.
1960-10-01
Standard
AMS5585
This specification covers a corrosion and heat resistant alloy in the form of welded and drawn tubing.
1960-09-01
Magazine
1960-08-01
Standard
AS678
No scope available.
1960-08-01
Magazine
1960-07-15
Standard
AS393A
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.
1960-07-01
Standard
AIR63
ABSTRACT
1960-07-01
Standard
AS665
No scope available.
1960-07-01
Magazine
1960-06-30
Standard
AMS4389
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of July, 1991.
1960-06-30
Standard
AMS4445A
This specification covers a magnesium alloy in the form of sand castings.
1960-06-30
Standard
AMS4483
This specification covers a magnesium alloy in the form of permanent mold castings.
1960-06-30
Standard
AMS2201D
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of September 1994. The requirements of this specification are embodied in the latest issue of ANSI H35.2, Dimensional Tolerances for Aluminum Mill Products.
1960-06-30
Standard
AMS2205D
This specification covers established manufacturing tolerances applicable to aluminum alloy and magnesium alloy extruded bar, rod, wire, shapes, and tubing ordered to inch/pound dimensions. Tolerances greater than standard may be necessary for some shapes; tolerances closer than standard may be possible for others. Tolerances shown here, however, apply unless otherwise agreed upon by purchaser and vendor and apply to all tempers, unless otherwise noted.
1960-06-30
Standard
AMS2202C
This specification covers established manufacturing tolerances applicable to aluminum and magnesium alloy sheet and plate ordered to inch dimensions. These tolerances apply to all conditions, unless otherwise noted. The term 'excl' applies only to the higher figure of the specified range.
1960-06-30
Standard
AMS4024
Aluminum Alloy Plate 4.3Zn - 3.3Mg - o.6Cu - o.2Mn - 0.17Cr (7o79-T651) Stress-Relief Stretched
1960-06-30
Standard
AMS6435
This specification covers a premium aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
1960-06-30
Standard
AMS6462
This specification covers a low-alloy steel in the form of welding wire.
1960-06-30
Standard
AMS6461A
This specification covers a low-alloy steel in the form of welding wire.
1960-06-30
Standard
AMS6458
This specification covers a low-alloy steel in the form of welding wire. This wire has been used typically for use as filler metal for gas-tungsten-arc and gas-metal-arc welding of low-alloy steels of similar composition where the weld area is required to have strength comparable to that of the parent metal, but usage is not limited to such applications.
1960-06-30
Standard
AMS6355F
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate. Primarily for use where welding and moderate mechanical properties are required. Sheet and strip are extensively used where minimum tensile strength of 160,000 psi (1105 MPa) is required in sections up to 0.125 in. (3.12 mm) thick and proportionately lower strength in heavier thicknesses.
1960-06-30
Standard
AMS6406
Primarily for heat treated parts and structures that may require welding during fabrication and may be through-hardened to a minimum tensile strength of 270,000 psi (1862 MPa) in sections of 2 in. (50 mm) or less in nominal thickness. This specification has been declared "Noncurrent" by the Aerospace Materials Division, SAE, as of April 1, 1987. It is recommended that this specification not be specified for new designs.

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