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Viewing 36781 to 36810 of 42945
1968-04-01
Standard
ARP922
The recommendations set forth herein are the results of the combined efforts of engineers associated with manufacturing of lamps, instrumentation, aircraft, aerospace equipment and vehicles, Air Transport and interested Government Agencies. The information contained in this initial release of the ARP is general in nature and will suffice as an introduction to this type of lighting. However, it is recommended that it be developed, in further revisions, into a more specific document.
1968-04-01
Standard
J823B_196804
This SAE Standard specifies the test procedure, test circuitry, and instruments required for measuring the performance of flashers used in motor vehicles.
1968-04-01
Standard
J590C_196804
This SAE Standard defines the test conditions, procedures, and minimum design requirements for nominal 6, 12, and 24 V turn signal flashers. Document cancelled in 1999. Information now contained in J1690
1968-04-01
Standard
J1402_196804
This recommended practice covers minimum requirements for air brake hose assemblies made from reinforced elastomeric hose and suitable fittings for use in automotive air brake systems including flexible connections from frame to axle, tractor to trailer, trailer to trailer and other unshielded air lines with air pressures up to 1 MPa, that are exposed to potential pull or impact. This hose is not to be used where temperatures, external or internal, fall outside the range of -40 °C to +100 °C.
1968-04-01
Standard
J1703A_196804
This SAE Standard covers motor vehicle brake fluids of the nonpetroleum type for use in the braking system of any motor vehicle such as a passenger car, truck, bus, or trailer. These fluids are not intended for use under arctic conditions. These fluids are designed for use in braking systems fitted with rubber cups and seals made from styrene-butadiene rubber (SBR), or a terpolymer of ethylene, propylene, and a diene (EPDM).
1968-03-01
Standard
ARP862
This Aerospace Recommended Practice (ARP) provides recommended methods for measuring performance of skid control systems. It includes test items and equipment.
1968-03-01
Standard
AIR822
This SAE Aerospace Information Report (AIR) provides a general overview of oxygen systems for general aviation use. Included are a brief review of the factors and effects of hypoxia, system descriptions and mission explanations for system or component selection, and techniques for safe handling of oxygen distribution systems.
1968-03-01
Standard
ARP958
This SAE Aerospace Recommended Practice (ARP) outlines a standard method for the checkout and calibration of electromagnetic interference measurement antennas. Its primary application is for use when measuring a source 1 m from the antenna in a shield room versus a source at a greater distance (far field). This is the typical distance used in performing military EMC testing. Thus, this is a method of calibration. Shield room characteristics are not considered. It does not address an unknown distributed source. Yet it is close to reality since it is based on another antenna that represents a distributed source. This document presents a technique to determine antenna factors for antennas used primarily in performing measurements in accordance with 2.1 and 2.2. The purpose of Revision B is to include the calibration of other antennas, such as small loop antennas that are also specified for use in these same references.
1968-03-01
Standard
ARP901
This test method describes a procedure for measuring the largest pore or hole in a filter or similar fluid-permeable porous structure. A standard referee test method for precise determination or resolution of disputes is specified. A simpler inspection test procedure for quality assurance 'go-no-go' measurement is also given. Bubble-point testing physics, analysis of bubble-point test data, and correlation with other methods of pore size determination are separately discussed in the appendix.
1968-03-01
Standard
J328_196803
This SAE Recommended Practice provides minimum performance requirements and uniform procedures for fatigue testing of wheels intended for normal highway use and temporary use on passenger cars, light trucks, and multipurpose passenger vehicles. For heavy truck wheels and wheels used as duals, see SAE J267. For wheels used on trailers drawn by passenger cars, light trucks, or multipurpose vehicles, see SAE J1204. These minimum performance requirements apply only to wheels made of materials included in Tables 1 to 4.
1968-02-27
Standard
RS571-4
No scope available.
1968-02-27
Standard
RS589-3
No scope available.
1968-02-15
Standard
ARP498A
This document is intended to cover the design of plastic lighted panels, mounting plates, and their installation.
1968-02-15
Standard
AS269F
This SAE Aerospace Standard (AS) provides material identification codes for aluminum alloys, copper alloys, carbon steels, alloy steels, titanium alloys, corrosion resistant materials, and heat resistant materials that are used to make AN, MS, and AS engine and propeller standard utility parts. This document also provides similar material codes for company parts (such as nuts, bolts, etc.) having design configuration similar to other company parts or the engine and propeller standard utility parts (AN, MS, and AS) that are not of the same material.
1968-02-01
Standard
ARP465
This SAE Aerospace Recommended Practice (ARP) provides guidance for the design of flanges on temperature sensors intended for use in gas turbine engines. Three figures detail the configuration of standard size flange mounts with bolt holes, slotted flanges, and miniaturized flanges for small probes.
1968-02-01
Standard
AS82A
This SAE Aerospace Standard (AS) defines an external thread with a rounded root radius based on a minimum root radius of .108 x Pitch.
1968-02-01
Standard
J945_196802
This SAE Standard defines the test conditions, procedures, and minimum design requirements for nominal 6, 12, and 24 V hazard warning flashers. Document cancelled 1999. Information now contained in J1690
1968-02-01
Standard
J980_196802
This SAE Recommended Practice is to establish uniform impact test procedures for passenger vehicle bumpers by use of a pendulum as the impacting object. Other methods of impacting, or the use of other impacting objects, are acceptable.
1968-02-01
Standard
J573C_196802
Most lighting devices on motor vehicles today are required by law and are essential to operation on public roadways. Additionally, most lighting devices have replaceable light sources (bulbs). To assure field replacement, it is important that bulb types employed be readily available in normal service channels. This document attempts to define the physical, electrical, and photometric characteristics necessary to achieve a proper replacement for popular types of bulbs. Some of the design characteristics in this document are listed solely for the sake of standardization and are not intended to describe the performance of lighting devices (lamp assemblies) on the vehicle.
1968-02-01
Standard
J381_196802
This SAE Recommended Practice establishes uniform test procedures and performance requirements for the defrosting system of enclosed cab trucks, buses, and multipurpose vehicles. It is limited to a test that can be conducted on uniform test equipment in commercially available laboratory facilities. Current engineering practice prescribes that for laboratory evaluation of defroster systems, an ice coating of known thickness be applied to the windshield and left- and right-hand side windows to provide more uniform and repeatable test results, even though under actual conditions such a coating would necessarily be scraped off before driving. The test condition, therefore, represents a more severe condition than the actual condition, where the defroster system must merely be capable of maintaining a cleared viewing area.
1968-02-01
Standard
J593C_196802
This SAE Standard provides installation requirements, test procedures, design guidelines, and performance requirements for backup lamps.
1968-01-31
Standard
ARP24B
This ARP is intended to serve as an instrument to determine hydraulic pressure drop, utilizing the best known practices for accessories in the hydraulic, fuel, oil, and coolant systems to aerospace vehicles.