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Viewing 5761 to 5790 of 5903
HISTORICAL
1966-02-01
Standard
J945_196602
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
HISTORICAL
1966-01-01
Standard
J910_196601
This standard defines the test conditions, procedures and performance specifications for 6, 12 and 24-V manually actuated hazard warning signal switch.
HISTORICAL
1965-10-01
Standard
J590B_196510
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
HISTORICAL
1965-10-01
Standard
ARP881
This SAE Aerospace Recommended Practice (ARP) lists the lamps in Table 1 that are recommended for the type of service indicated. This list is not intended as a catalog and does not include many types that are now in use. This specification is not applicable to Solid State Lighting Lamp Assemblies (Based LED lamps). It does, however, reflect current practice.
HISTORICAL
1965-08-01
Standard
AS406
This standard establishes the essential minimum safe performance requirements for flight director instruments, primarily for use with turbine-powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in paragraph 3.3. This standard covers flight directors for use on aircraft to indicate to the pilot, by visual means, the correct control application for the operation of an aircraft in accordance with a preselected flight plan.
HISTORICAL
1965-07-01
Standard
J590B_196507
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
HISTORICAL
1965-07-01
Standard
J823A_196507
This SAE Standard specifies the test procedure, test circuitry, and instruments required for measuring the performance of flashers used in motor vehicles.
HISTORICAL
1965-06-01
Standard
ARP798
This recommended practice covers the general requirements and test procedures recommended for use with white incandescent integrally lighted instruments. Its use should provide uniformity of illumination from instrument to instrument and legibility under daylight operation. An appendix is provided to familiarize the designer with some of the techniques used to obtain uniformity of color and illumination in various types of instruments.
HISTORICAL
1965-05-01
Standard
J839B_196505
This SAE Recommended Practice establishes minimum performance requirements and test procedures for evaluating and testing passenger car side door latch systems. It is limited to tests that can be conducted on uniform test fixtures and equipment in commercially available laboratory test facilities. The test procedures and minimum performance requirements outlined in this document are based on currently available engineering data. It is intended that all portions of the document will be periodically reviewed and revised, as additional knowledge regarding vehicle latch performance under impact conditions is developed.
HISTORICAL
1965-05-01
Standard
AS486A
The purpose of this standard is set forth the desired location, arrangement and general requirements of aircraft circuit breakers and fuses. The recommendations of this standard apply to all civil type multi-engine transport aircraft. The definitions used herein are made as brief as possible and in familiar cockpit language. They are intended only to identify the devices mentioned rather than to prescribe their application.
HISTORICAL
1965-05-01
Standard
ARP712
HISTORICAL
1965-04-01
Standard
J565A_196504
This SAE Standard provides test procedures, performance requirements, and guidelines for semiautomatic headlamp beam switching devices.
CURRENT
1965-02-01
Standard
AS436
This Aerospace Standard covers the direct reading pressure actuated type mach meter.
HISTORICAL
1965-02-01
Standard
AS417
This Standard recommends the minimum safe operational performance requirements for Air Data Computer equipment for use in Subsonic Turbine Powered Aircraft operating up to 50,000 feet of pressure altitude and 500 knots maximum indicated airspeed. This Standard covers air data equipment (hereinafter designated the instrument) which when connected to sources of aircraft electrical power, static pressure, static pressure, total pressure and outside air temperature (singly or in combination) provides some or all of the following computed air data output signals: Pressure Altitude*, Pressure Altitude (Reporting), Baro-Corrected Pressure Altitude*, Vertical Speed*, Computed Airspeed*, Mach Number*, Maximum Allowable Airspeed*, Static Air Temperature (*when used as an alternate for total temperature), Total Temperature*, Altitude Rate, Overspeed Warning, Altitude Hold, Airspeed Hold, Mach Hold, qc (impact pressure), True Airspeed, Others.
CURRENT
1965-01-10
Standard
ARP497A
This recommendation establishes objectives for high performance control motors to be used with aeronautical and associated equipment in protective enclosures or completely within the shell of the aircraft so that they are subjected only to the internal climatic conditions of heat, cold, shock, vibration, altitude, and humidity. Control motors larger than size #23 are not covered in this document.
HISTORICAL
1965-01-10
Standard
AIR860
It is intended that the scope of this information report be limited to electrical heating of passenger, crew, and cargo compartments only.
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
1965-01-01
Standard
J910_196501
This standard defines the test conditions, procedures and performance specifications for 6, 12 and 24-V manually actuated hazard warning signal switch.
HISTORICAL
1965-01-01
Standard
AS486
The purpose of this standard is set forth the desired location, arrangement and general requirements of aircraft circuit breakers and fuses. The recommendations of this standard apply to all civil type multi-engine transport aircraft. The definitions used herein are made as brief as possible and in familiar cockpit language. They are intended only to identify the devices mentioned rather than to prescribe their application.
HISTORICAL
1964-12-01
Standard
AIR857
The following analysis is limited to variations in voltage, torque, temperature and altitude of the same magnitude as in MIL-M-8609.
HISTORICAL
1964-10-30
Standard
AS778
No scope available.
CURRENT
1964-10-30
Standard
AS654
This Aerospace Standard covers insulated, high-tension, shielded, special purpose cable and unshielded electrical cable for ignition systems of internal combustion engines for aircraft.
CURRENT
1964-08-01
Standard
AS415
This Aerospace Standard covers two types of compensated altimeters which indicate, by visual means, the pressure altitude compensated for the static pressure system errors of the aircraft.
HISTORICAL
1964-08-01
Standard
ARP842
This recommended practice sets forth the design objectives for handling qualities applicable to transport aircraft operating in the subsonic, transonic and supersonic speed range. These objectives are not necessarily applicable to rotor or VTOL aircraft.
HISTORICAL
1964-06-20
Standard
ARP493
This recommended practice is intended to recommend the basic shapes and dimensions for knobs used in aircraft. Two basic types of knobs, the bar shape and the round shape, are described, as well as several widely used variations of these two basic shapes.
HISTORICAL
1964-06-01
Standard
ARP450B
HISTORICAL
1964-04-01
Standard
J589_196404
A turn signal switch is that part of a turn signal system by which the operator of a vehicle causes the turn signal lamps to function. A Class A turn signal switch may be used on any vehicle but is intended for use on multipurpose passenger vehicles, trucks, and buses that are 80 in or more wide overall. A Class B turn signal switch is intended for use in passenger cars, motorcycles, and multipurpose passenger vehicles, trucks, and buses of less than 80 in overall width.
HISTORICAL
1964-04-01
Standard
J564A_196404
This SAE Standard J564 defines the test conditions, procedures and performance specification for 6, 12, and 24 V manually actuated headlamp beam control switches.
HISTORICAL
1964-04-01
Standard
AS443
This SAE Aerospace Standard (AS) covers a direct reading magnetic compass. This Aerospace Standard establishes the essential minimum safe-performance standards for non-stabilized magnetic direction instruments, primarily for use with turbine-powered, subsonic, transport aircraft that may subject the instruments to the environmental conditions specified in paragraph 3.3.
HISTORICAL
1964-04-01
Standard
AIR744
This SAE Aerospace Information Report (AIR) is a review of the general characteristics of power sources that may be used to provide secondary, auxiliary, or emergency power for use in aircraft, space vehicles, missiles, remotely piloted vehicles, air cushion vehicles, surface effect ships, or other vehicles in which aerospace technology is used. The information contained herein is intended for use in the selection of the power source most appropriate to the needs of a particular vehicle or system. The information may also be used in the preparation of a power source specification. Considerations for use in making a trade study and an evaluation of the several power sources are included. More detailed information relating to specific power sources is available in other SAE Aerospace Information Reports or in Aerospace Recommended Practices.
Viewing 5761 to 5790 of 5903