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Viewing 5671 to 5700 of 5822
HISTORICAL
1966-12-01
Standard
J537D_196612
This SAE Standard serves as a guide for testing procedures of automotive 12 V storage batteries and as a publication providing information on container holddown configuration and terminal geometry. The ratings submitted are to be based on procedures described in this document. The ratings submitted must be of a level that when any subsequent significant sample is tested in accordance with this document, that at least 90% of the batteries shall meet the ratings. The choice of 90% compliance recognizes that batteries consist of many plates and require chemical-electrical formation procedures and small variations in test conditions and procedures can affect the performance of individual batteries. Future Considerations - In order to expedite the release of this revision of the Standard, several topic areas were deferred for consideration in future revisions.
HISTORICAL
1966-09-01
Standard
ARP914
HISTORICAL
1966-08-01
Standard
AIR818A
This Aerospace Information Report, (AIR) is intended to provide the sponsors of Aerospace Standards, (AS), with standard wording, formatting, and minimum environment and design requirements for use in the preparation of their document. The individual shall use only those parts of this AIR which apply to their particular document. The individual sponsor may expand the standard wording, especially under Sections 4, 5, and 6 as required. The paragraphs of this AIR shall be used verbatim wherever possible. Unless otherwise directed by SAE, cross referenced documents shall be called out by specific revision letter, e.g. "shall be in accordance with AS XXXXB." In addition, all non-SAE documents called out shall include the document title when initially identified. However, every effort shall be made to keep cross-referencing to an absolute minimum.
HISTORICAL
1966-07-01
Standard
AS916
This SAE Aerospace Standard (AS) defines the overall requirements applicable to oxygen flow indicating devices intended to operate in conjunction with an oxygen regulator and mask system. Flow indicators covered by this document are for use with pressure demand, diluter-demand and continuous flow oxygen systems.
HISTORICAL
1966-06-20
Standard
AIR764A
This technical report documents three surveys to determine realistic vibration requirements for skid control systems specifications and obtain updated vibration information for locations in aircraft where skid control system components are mounted.
CURRENT
1966-06-01
Standard
AS428
The exhaust gas temperature instruments covered by this standard are of the electrical servo null balance type, actuated by a varying emf output of one or more parallel connected Chromel-Alumel thermocouples.
HISTORICAL
1966-05-15
Standard
AS793
This standard covers three basic types of total-temperature-measuring instruments used as a means of determining the total temperature developed by adiabatic heating of the air due to motion of the aircraft through the air. This standard establishes essential minimum safe performance requirements for total temperature measuring instruments, primarily for use with turbine-powered subsonic transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in this report.
HISTORICAL
1966-04-01
Standard
AIR512
This document covers the general recommendations for cabin lighting in order to provide satisfactory illumination for, but not limited to: a. Boarding and deplaning b. Movement about the cabin c. Reading d. Use of lavatories e. Use of work areas f. Exiting under emergency conditions g. Using stowage compartments, coat rooms, and closets h. Using interior stairways and elevators (lifts)
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
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
1965-10-01
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
1965-08-01
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
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
1965-07-01
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
1965-06-01
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
ARP712
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
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
1965-04-01
Standard
J565A_196504
This SAE Standard provides test procedures, performance requirements, and guidelines for semiautomatic headlamp beam switching devices.
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
1965-02-01
Standard
AS436
This Aerospace Standard covers the direct reading pressure actuated type mach meter.
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
1965-01-10
Standard
AIR860
It is intended that the scope of this information report be limited to electrical heating of passenger, crew, and cargo compartments only.
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
1965-01-01
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
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
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.
Viewing 5671 to 5700 of 5822