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Viewing 163861 to 163890 of 169630
Standard
1948-11-01
To specify minimum requirements for Electric Tachometers primarily for use in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aeronautical Standard covers magnetic drag tachometers with or without built-in synchroscopes.
Standard
1948-11-01
To specify minimum requirements for carbon monoxide detector instruments for use in aircraft, the operation of which may subject the instrument to the environmental conditions specified in Paragraph 3.3. This standard is not intended to cover fire detectors. This Aeronautical Standard covers the basic type of carbon monoxide detector instrument used to determine toxic concentrations of carbon monoxide by the measurement of heat changes through catalytic oxidation.
Standard
1948-11-01
This Aerospace Standard establishes the minimum sage performance standards for electrical type temperature instruments primarily for use with reciprocating engine powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.4. This Aerospace Standard covers two basic types of temperature instruments as follows: TYPE I Radiometer type, actuated by changes in electrical resistance of a temperature sensing electrical resistance element; the resistance changes being obtained by temperature changes of the temperature sensing resistance element. TYPE II: Millivoltmeter type, operated and actuated by varying E.M.F. output of a thermocouple; the varying E.M.F. input to the instrument being obtained by temperature changes of the temperature sensing thermocouple.
Standard
1948-11-01
This Aerospace Standard establishes the essential minimum safe performance standards for manifold pressure instruments primarily for use with reciprocating engine powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aerospace Standard covers two basic types of manifold pressure instruments as follows: TYPE I - Direct Indicating. TYPE II - Remote Indicating.
Standard
1948-11-01
This specification covers mixtures of methyl alcohol and/or ethyl alcohol with water in the form of liquids.
Standard
1948-11-01
This specification covers one type of methyl methacrylate in the form of extrusions, compression moldings, and injection moldings. These products have been used typically for parts requiring good dimensional stability, a high degree of optical clarity, and good resistance to outdoor weathering, but usage is not limited to such applications.
Standard
1948-11-01
This specification covers an alloy steel in the form of bars 1 inch (25.4 mm) and under in nominal diameter or distance between parallel sides. Primarily for bolts and screws requiring a coefficient of thermal expansion approaching that of aluminum alloys. This steel is hardenable only by cold working.
Standard
1948-11-01
1. ACKNOWLEDGMENT: A vendor shall mention this specification number in all quotetione and when acknowledging purchase orders. 2. FORM: Bars, billets, and forgings. 3. APPLICATION: Parts and assemblies, such as shafts, buckets, blades, and bolts, requiring high strength and oxidation resistance up to 1400 F.
Standard
1948-11-01
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.
Standard
1948-11-01
ABSTRACT
Standard
1948-11-01
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
Standard
1948-11-01
This specification covers a silicone rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
Standard
1948-11-01
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 specifications which have previously been widely used and which may be required on some 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.
Standard
1948-11-01
This specification covers established inch-pound manufacturing tolerances applicable to seamless and welded thin-wall aircraft tubing of nickel, nickel alloys, and cobalt alloys ordered to inch-pound dimensions. These tolerances apply to all conditions and are based on individual measurements, unless otherwise noted. The term "exclusive" is used to apply only to the higher figure of a specified range.
Standard
1948-11-01
This specification covers a silver alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, and chips and a viscous mixture (paste) of powder in a suitable binder. This material has been used typically for joining ferrous metals, including austenitic steels and alloys, where high joint strength up to 700 degrees F (371 degrees C) is required, and for joining nonferrous metals except those having base of aluminum or magnesium, but usage is not limited to such applications.
Standard
1948-11-01
This specification covers a denatured ethyl alcohol in the form of a liquid.
Standard
1948-11-01
This specification covers a silicone rubber in the form of sheet, strip, tubing, extrusions, and molded shapes. Primarily for parts required to operate or seal from -65 to +205C degrees (-85 to +401F degrees). Silicone elastomer is resistant to deterioration by weathering and petroleum-base lubricating oil and remains flexible over the temperature range noted. These products are not normally suitable for use in contact with gasoline or aromtic fuels and low-aniline-point petroleum-base fluids due to excessive swelling of the elastomer.
Standard
1948-11-01
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.
Standard
1948-11-01
To specify minimum requirements for Fuel Flowmeters for use primarily in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aeronautical Standard covers two basic types of instruments, or combinations thereof, intended for use in indicating fuel consumption of aircraft engines as follows: TYPE I - Measure rate of flow of fuel used. TYPE II - Totalize amount of fuel consumed or remaining.
Standard
1948-11-01
This Aeronautical Standard covers two basic types of instruments as follows: Type I - Float Instruments, Type II - Capacitance Instruments. To specify minimum requirements for Fuel and Oil Quantity Instruments for use in aircraft, the operation of which may subject the instruments to the environmental conditions specified in Paragraph 3.3.
Standard
1948-11-01
This specification covers a corrosion and heat-resistant steel in the form of seamless tubing.
Standard
1948-11-01
This Aerospace Standard establishes the essential minimum safe performance standards for fuel, oil and hydraulic pressure instruments primarily for use with reciprocating engine powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aerospace Standard covers two basic types of fuel, oil and hydraulic pressure instruments as follows: Type I - Direct Indicating, Type II - Remote Indicating. This Aerospace Standard does not apply to engine mounted torque meter systems.
Standard
1948-11-01
This specification covers an aluminum alloy in the form of seamless round tubing.
Standard
1948-11-01
This specification covers the engineering requirements for electrodeposition of nickel and the properties of the deposit. This process has been used typically to provide moderate corrosion and oxidation resistance to metal parts but without control of other characteristics and for the buildup of surfaces, but usage is not limited to such applications. If a hard plate is required, AMS 2423 should be used; if a low-stressed plate is required, AMS 2424 should be used.

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