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Viewing 1711 to 1740 of 1766
HISTORICAL
1965-01-10
Standard
AIR839
No scope available.
HISTORICAL
1965-01-10
Standard
AIR786
This document contains data relative to the chemical nature of aerospace fluids and relates each to its effect upon elastomeric components. Since the compatibilities of elastomers are determined by the compounding as well as the nature of the base polymer, the elastomers considered are limited to finished compounds for which material or performance specifications could be referenced.
HISTORICAL
1964-09-01
Standard
J447A_196409
This SAE Information Report provides automotive engineers with the basic principles of corrosion, design guidelines to minimize corrosion, and a review of the various materials, treatments, and processes available to inhibit corrosion of both decorative and functional body and chassis components.
HISTORICAL
1964-06-01
Standard
AMS3156A
This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of December 2008 and has been superseded by AMS2644. The requirements of the latest issue of AMS2644 shall be fulfilled whenever reference is made to the cancelled AMS3156. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by AMS2644.
HISTORICAL
1964-06-01
Standard
J900_196406
The purpose of this SAE STandard is to provide standard test procedures for crankcase emission control systems and/or devices. The procedures included are for determining: a. The flow rate of the blowby of an engine; b. The flow rates through the crankcase emission control system inlet and outlet. This code is written to cover crankcase emission control systems which are designed to reduce the emission of engine blowby gases to the atmosphere. The code includes the following sections: 3. Definitions and Terminology; 4. Test Equipment; 5. Test Procedures; 6. Information and Data to be Recorded; 7. Data Analysis; 8. Presentation of Information and Data.
HISTORICAL
1964-06-01
Standard
J533A_196406
This SAE Standard covers specifications and performance requirements for 37-degree and 45-degree single and double flares for tube ends intended for use with SAE J512, SAE J513, SAE J514 and ISO 8434-2 connectors. Considerations such as the effects of wall thickness selection for specific working pressures, identifying appropriate length of thread engagements for specific applications with mating connectors and other associated criteria, shall be the responsibility of the user. For applicable nominal reference working pressures for hydraulic tubing, see SAE J1065 and ISO 10763.
HISTORICAL
1964-04-20
Standard
AIR790
In the past, incidents and accidents occurred in the operation of military and civil aircraft which were attributed to the formation of ice in the engine fuel supply system resulting in intermittent or complete starvation of fuel flow. Considerable effort was devoted by many airframe companies, engine and accessory manufacturers and government agencies to study the problem of ice formation and to evolve corrective measures. By its very nature, the problem of ice formation was difficult to identify and analyze. However, corrective measures were developed which virtually eliminated serious icing problems in aircraft fuel systems. For many years incidents and accidents have not occurred on aircraft equipped with fuel heaters and/or operated with fuel containing anti-icing additive.
HISTORICAL
1963-06-01
Standard
J688_196306
The procedure has been developed to provide a practical method for the prediction of truck performance using accepted data. It Is designed to help anyone concerned with the problem of truck selection. By following directions, it is possible to determine the necessary information for intelligent truck selection without being concerned with the origin or derivation of the complex factors involved. With readily available specification of a truck, information provided in the tables, and minimum of calculation, it is possible to predict: (a) The performance obtainable from a truck of given characteristics under given operating conditions. (b) The characteristics required in a truck to meet different performance requirements under given operating conditions. This report comprises a procedure form and 10 tables of data.
HISTORICAL
1963-06-01
Standard
J30_196306
This SAE standard covers fuel, oil, or emission hose for use in coupled and uncoupled applications, for use with gasoline, oil, diesel fuel, lubrication oil, or the vapors present in either the fuel system or in the crankcase of internal combustion engines in mobile or stationary applications. This standard covers the hose portion only. If assembly / coupling is required, that is to be agreed to between the customer and assembler, along with the specific requirements.
HISTORICAL
1963-04-01
Standard
J90A_196304
The classification system provides a means for specifying or describing pertinent properties of commercial nonmetallic gasket materials. Materials composed of asbestos, cork, cellulose, and other organic or inorganic materials in combination with various binders or impregnants are included. Materials normally classified as rubber compounds are not included, since they are covered in SAE J200 - ASTM D 2000. Gasket coatings are not covered, since details thereof are intended to be given on engineering drawings or in separate specifications. Since all of the properties that contribute to gasket performance are not included, use of the classification system as a basis for selecting materials is limited. The values stated in SI units are to be regarded as the standard. The values given in parentheses are for information only. This SAE Recommended Practice may involve hazardous materials, operations, and equipment.
HISTORICAL
1963-02-01
Standard
ARP785
This procedure describes a gravimetric method for the determination of particulate contaminant in hydraulic fluids by the control filter technique. With this method detectable contamination levels down to 0.2 mg per sample can be obtained with a standard deviation of ± 0.1 mg.
HISTORICAL
1962-11-01
Standard
J73_196211
HISTORICAL
1962-08-30
Standard
ARP743
This method describe the procedure for (1) sampling air in contamination controlled spaces for air-borne particulate contamination 5u or greater in size and for (2) the microscopic determination of the concentration and size range distribution of the particulate material removed from the air sample.
HISTORICAL
1962-02-01
Standard
AS431A
This SAE Aerospace Standard (AS) covers three basic types of true mass flow indicating instruments. Each may consist of an indicator, transmitter and other auxiliary means such as a power supply or amplifier as required. This Aerospace Standard establishes the essential minimum safe performance standards for True Mass Fuel Flow Instruments primarily for use with turbine powered, subsonic transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3.
HISTORICAL
1961-12-31
Standard
ARP719
Gas for the purpose of this ARP shall be defined as the gaseous produces) resulting from the decomposition, dissociation, or combustion of liquid or solid mono or bi-propellants. Where other gases such as heated N2, H2, H2O (steam), etc., which may have similar physical and/or chemical properties as the defined "gas", are used to effect testing economies; they may be considered as being included in this ARP.
HISTORICAL
1961-06-01
Standard
J30_196106
This SAE standard covers fuel, oil, or emission hose for use in coupled and uncoupled applications, for use with gasoline, oil, diesel fuel, lubrication oil, or the vapors present in either the fuel system or in the crankcase of internal combustion engines in mobile or stationary applications. This standard covers the hose portion only. If assembly / coupling is required, that is to be agreed to between the customer and assembler, along with the specific requirements.
CURRENT
1961-04-01
Standard
AS445
This Aeronautical Standard covers the capacitance sensor type of instrument.
HISTORICAL
1960-11-01
Standard
AMS3326A
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the latest issue of AMS 3325.
HISTORICAL
1960-03-01
Standard
AS407B
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
HISTORICAL
1959-06-15
Standard
AMS3326
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the latest issue of AMS 3325.
HISTORICAL
1959-02-01
Standard
ARP575
These recommendations are written to cover the subject of obtaining filter patch test samples from aircraft hydraulic pumps of the categories shown below. The same procedure shall apply regardless of the pump drive category.
HISTORICAL
1958-08-01
Standard
AMS3156
This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of December 2008 and has been superseded by AMS2644. The requirements of the latest issue of AMS2644 shall be fulfilled whenever reference is made to the cancelled AMS 3156. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by AMS2644.
HISTORICAL
1958-07-15
Standard
AS405B
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. This Aeronautical Standard covers two basic types of instruments as follows: Type I - Float Instruments, Type II - Capacitance Instruments.
HISTORICAL
1957-11-15
Standard
ARP492
This SAE Aerospace Recommended Practice (ARP) defines procedures for testing aircraft engine fuel pumps for th epurpose of determining their resistance to eterioration, during steady state endurance test, while receiving MIL-T-5624 Grade JP-4 fuel as a homogenous mixture of gas and liquid expressed as a ratio of vapor volume to liquid volume (V/L). The procedure recommended herin is based on experience gathered by a number of laboratories conducting component qualification tests to MIL-E-5009, currently MIL-E-5007. It is intendd to produce a uniform reproducible steady state test condition for fuel pump cavitation testing as required by various military engine specifications. This test is NOT intended to establish altitude, climb rate, starting, or other transient performance of the article tested.
HISTORICAL
1956-12-15
Standard
AS405A
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.
CURRENT
1955-03-01
Standard
AIR39
CURRENT
1955-03-01
Standard
AIR40
The objective of this work was to develop a relatively simple screening or bench test, or a combination of such tests, which would evaluate aircraft greases in respect to corrosion protection under the operating conditions described above.
CURRENT
1955-03-01
Standard
AIR42
Certain techniques involved in determining the dirt or abrasive content of aircraft greases are considered inadequate. It is desirable to develop a method of analysis which will definitely identify the quantity, size, and degree of abrasiveness of foreign substances in lubricating greases.
Viewing 1711 to 1740 of 1766