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Viewing 5761 to 5790 of 6169
HISTORICAL
1980-06-01
Standard
J1283_198006
This SAE Standard defines the requirements for a plug and receptacle used in an auxiliary starting system. The connector facilitates the application of supplemental electrical power for starting or charging a machine from another machine or suitable external source. This system provides: proper polarity during connector mating, secure electrical connections, and standard circuit color coding. Purpose This document establishes the connector interface dimensions and performance requirements for the electrical plug and receptacle system and its component parts.
HISTORICAL
1980-06-01
Standard
J917_198006
This SAE Standard covers dimensions and nomenclature of a push-pull control cable used in inboard marine engine applications. The dimensions are representative of existing design practice prevalent in the industry. The flexible push-pull cable is a common motion transfer device for the remote operation of the throttle and clutch levers (hydraulically applied clutches) on marine propulsion units. Satisfactory function of remote controls depend upon observing the limitations of this cable and providing adequate connection to the propulsion unit. This standard, therefore, establishes nomenclature, dimensions, and installation recommendations for marine push-pull control cables.
HISTORICAL
1980-06-01
Standard
J928_198006
This SAE Standard covers general requirements and terminal interface dimensions of various sizes of pin and receptacle type terminals.
HISTORICAL
1980-06-01
Standard
J561_198006
This SAE Standard covers general requirements and dimensions of various sizes of eyelet and spade type terminals.
HISTORICAL
1980-06-01
Standard
J1292_198006
This document is being revised to remove the references made to Truck, Truck Tractor and Trailer per the agreement between the SAE Truck and Bus Electrical Systems Subcommittee and the SAE Electrical Distribution System Standards Committee. The Truck and Bus committee has replaced the referenced documents with newer SAE documents. The documents that supersede SAE J1292 are SAE 2174 "Heavy Duty Wiring Systems for Trailers more than 2032 MM or More in Width" and SAE J2202 "Heavy Duty Wiring Systems For On Highway Trucks".
HISTORICAL
1980-06-01
Standard
J1127_198006
This standard covers low voltage battery cable intended for use at a nominal system voltage of 60 V DC (25 V AC) or less in surface vehicle electrical systems. The tests are intended to qualify cables for normal applications with limited exposure to fluids and physical abuse.
HISTORICAL
1980-04-01
Standard
J107_198004
This SAE Recommended Practice applies to two- and three-wheeled motorcycles intended for highway use. Vehicles commonly known as mpoeds and mini-bikes are included in this vehicle category if they are intended for highway use. This document is intended to provide guides toward standard location and operation of motorcycle controls and standard identification of displays to reduce the possibility of operator confusion.
HISTORICAL
1980-04-01
Standard
J1294_198004
This recommended practice covers distributors used on marine engines. To provide recommendations and guidelines for the evaluation, design, and testing of distributors to be used on marine engines.
HISTORICAL
1980-04-01
Standard
J1286_198004
To establish a uniform test method to measure static thrust of an electric outboard. This method covers all electric outboards.
HISTORICAL
1980-04-01
Standard
J297_198004
This SAE Standard is intended to improve operator efficiency and convenience by providing guidelines for the uniformity of location and direction of motion of operator controls used on industrial wheeled equipment. The controls covered are those centrally located at the operator's normal position. General These guidelines are based on the principle that a given direction of movement of any control produces a consistent and expected effect. Where confusion may result from the motion of the control, the effect from movement of the control shall be clearly and permanently identified.
HISTORICAL
1980-03-01
Standard
J819_198003
This SAE Standard applies to all self-propelled construction and industrial machines using liquid-cooled internal combustion engines. The purpose of this code is to provide a procedure to determine the cooling system reserve capacity under the conditions existing when tested.
CURRENT
1980-01-01
Standard
AS8020
This Aerospace Standard (AS) covers the general minimum performance standards for generators/starter-generators and associated voltage regulators for use in direct current (DC) electric systems for civil aircraft.
HISTORICAL
1979-12-01
Standard
J1284_197912
The fuses shown are for use in motor vehicles, boats, and trailers to protect electrical wiring and equipment. This standard is for the construction shown and is not intended to restrict the design and use of other configurations and materials capable of meeting the vehicle requirements. A fuse is a device designed to interrupt the electrical circuit when subjected to overcurrents. This action is to be nonreversible, and the fuse is intended to be replaced after the circuit malfunction has been corrected.
HISTORICAL
1979-10-01
Standard
J1230_197910
It is recognized that a malfunction in any one of the specified areas can degrade intended performance, but that levels of malfunction or combinations thereof must be considered by the vehicle designer in determining the point at which a failure indication is warranted. Consequently, the minimum reaction recommended by this document consists of making available a malfunction signal. This SAE Recommended Practice establishes a uniform minimum set of functional areas to be monitored in the process of detecting malfunctions in discrete wheel-slip brake-control systems for motor vehicles, and establishes a minimum reaction to those detected malfunctions.
HISTORICAL
1979-10-01
Standard
AIR1557
This AIR defines aircraft vibration areas, the vibration spectrum for those areas and a coupling mechanism recommendation for circular electrical connectors.
HISTORICAL
1979-10-01
Standard
ARP1612
This document describes the materials, equipment, and processing techniques utilized in the fabrication of polyimide printed wiring boards. Included are recommendations for both double-sided and multi-layer boards.
HISTORICAL
1979-10-01
Standard
J68_197910
This SAE Recommended practice covers standardized basic tests, test methods, and requirements applicable to electromechanical switching devices which may be used on snowmobiles as defined in SAE J33.
HISTORICAL
1979-09-01
Standard
ARP914A
HISTORICAL
1979-09-01
Standard
J99_197909
To provide specifications for lighting and marking of industrial wheeled equipment whenever such equipment is operated or traveling on a highway.
HISTORICAL
1979-07-16
Standard
AMS3582A
This specification covers a crosslinked polyvinyl chloride plastic in the form of flexible, thin-wall, heat-shrinkable tubing.
HISTORICAL
1979-06-01
Standard
J551_197906
This SAE Standard covers the measurement of broadband electromagnetic radiation over the frequency range of 30 to 1000 MHz from a vehicle or other device powered by an internal combustion engine or electric motor. Operation of all engines (main and auxiliary) of a vehicle or device is included. All equipment normally operating when the engine is running is also included except operator-controlled equipment, which is excluded. The recommended level applies only to complete vehicles or devices in their final manufactured form. Vehicle mounted rectifiers used for battery charging in electric vehicles are included in this document when operated in their charging mode.
HISTORICAL
1979-05-01
Standard
AMS3579
This specification covers a non-crosslinked polyvinyl chloride plastic in the form of flexible, thin-wall, heat-strinkable tubing with a low recovery temperature. These products have been used typically as a flexible, electrical insulation tubing whose diameter can be reduced to a predetermined size by heating to 150 degrees C (302 degrees F) or higher, but usage is not limited to such applications. This tubing is stable for continuous exposure from -20 to +105 degrees C (-4 to 221 degrees F).
HISTORICAL
1979-05-01
Standard
AIR1204
This publication will discuss water carryover from the environmental control system with respect to causes and indicated corrective or preventative action. In addition, condensation on structure will be reviewed with possible preventative action described.
HISTORICAL
1979-05-01
Standard
AS8009
This SAE Aerospace Standard (AS) specifies minimum performance requirements for primary pressure altimeter systems other than air data computers. This document covers altimeter systems that measure and display altitude as a function of atmospheric pressure. The pressure transducer may be contained within the instrument display case or located remotely. Requirements for air data computers are specified in AS8002. Some requirements for nontransducing servoed altitude indicators are included in AS791. The instrument system specified herein does not include aircraft pressure lines. Unless otherwise specified, whenever the term "instrument" is used, it is to be understood to be the complete system of pressure transducer components, any auxiliary equipment, and display components. The test procedures specified herein apply specifically to analog type instruments. Digital instruments or automatic test instrumentation may require other test procedures.
HISTORICAL
1979-03-01
Standard
J180B_197903
This SAE document describes alternator physical, performance and application requirements for heavy-duty electrical charging systems for off road work machines including those defined in SAE J1116. The purpose of this SAE document is to provide information on which to base machine and component design and to establish minimum requirements which will result in the most satisfactory operation of charging systems in construction, agricultural, and industrial machinery environments.
HISTORICAL
1979-03-01
Standard
ARP1311
This SAE Aerospace Recommended Practice (ARP) applies to landing gear structures and mechanisms (excluding wheels, tires, and brakes and other landing gear systems) for all types and models of civil and military aircraft. All axles, wheel forks, links, arms, mechanical and gas/oil energy absorbers, downlock and uplock assemblies, braces, trunnion beams, and truck beams etc., that sustain loads originating at the ground, and that are not integral parts of the airframe structure, should be designed and validated in accordance with this document. Hydraulic actuators (retraction, main and nose gear steering, positioning, damping, etc.) should also be included in this coverage. System level, non structural components such as retraction/extension valves, controllers, secondary structure and mechanisms in the airframe (e.g. manual release mechansims, slaved doors) as well as equipment that is located in the cockpit is not addressed in this ARP.
HISTORICAL
1979-02-15
Standard
AIR764B
HISTORICAL
1979-02-01
Standard
J1253_197902
The electrical cranking system components, which include the battery, cables, and cranking motor, must be carefully selected to provide the necessary speed to start an engine under the most severe climatic conditions for which the system is intended. Engine cranking loads increase with cold temperatures, therefore, the initial selection of these components needs to consider low temperature engine torque requirements. To insure an adequate electrical cranking system is obtained, it is important that proper test procedures are used for obtaining the cranking load requirements of the engine.
HISTORICAL
1978-12-01
Standard
J542C_197812
The purpose of this SAE Recommended Practice is to provide standardized dimensions for mounting starting motors. It is recommended that a full register diameter having a minimum depth of 2.54 mm (0.100 in) be provided in the flywheel housing to insure proper control of gear center distance and clearance between pitch diameters. The clearance between the starting motor pilot diameter and the register diameter in the flywheel housing should be 0.03 mm (0.001 in) minimum to 0.25 mm (0.010 in) maximum.