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Viewing 169981 to 170010 of 188251
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.
1966-05-01
Magazine
HISTORICAL
1966-05-01
Standard
AS123751A
No scope available
HISTORICAL
1966-05-01
Standard
J953_196605
The scope of this SAE Recommended Practice is to establish uniform test procedures for passenger cars, to determine whether the system is defined as a defroster or defogger, and to establish minimum performance requirements for each system. A defroster for purposes of this practice is a system which will remove moisture and/or frost from the interior surface of the backlight at -18 °C. A defogger is a system which will remove moisture and/or fog from the interior surface of the backlight at 4 °C. The test procedure is intended to simulate actual conditions by utilizing either a cold room with an appropriate device to introduce air flow over the backlight or a sufficiently large wind tunnel with ambient temperature control. The test procedure and the minimum performance requirements are based on currently available engineering data.
HISTORICAL
1966-05-01
Standard
J903A_196605
This SAE Recommend Practice establishes for passenger cars, light trucks, and multipurpose vehicles with GVW or 4500 kg (10 000 lb) or less: a. Minimum performance standards for windshield wiper systems. b. Test procedures that can be conducted on uniform test equipment by commercially available laboratory facilities. c. Uniform terminology of windshield wiper system characteristics and phenomena consistent with those found in guides for the use of engineering layout studies to evaluate system performance. d. Guides for the design and location of components of the systems for function, servicing of the system, etc. The test procedures and minimum performance standards, outlined in this document, are based on currently available engineering data. It is the intent that all portions of the document will be periodically reviewed and revised as additional data regarding windshield wiping system performance are developed.
HISTORICAL
1966-05-01
Standard
J919_196605
This SAE Standard describes the instrumentation and procedures to be used in measuring sound levels at the operator station for self-propelled sweepers as defined in SAE J2130 and self-propelled off-road work machines in categories 1, 2, 4, and 5, of SAE J1116. This SAE document is applicable to machines that have operator stations where the operator can either stand or sit and will be either transported by, or walk with the machine during its operation. The sound levels obtained using this procedure are repeatable and representative of the higher range of sound levels generated by machines under actual field operating conditions. Due to variability of field operating conditions, this data is not intended to be used for operator noise exposure evaluations. Measurement and calculation of the operator's sound exposure should follow SAE J1116.
HISTORICAL
1966-05-01
Standard
AS1043A
No scope available.
CURRENT
1966-04-26
Standard
AS12985-1
No scope available.
1966-04-01
Magazine
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
1966-03-15
Standard
AMS4767A
This specification covers a silver alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, and chips and a viscous mixture (paste) of powder in a suitable binder. This material has been used typically for brazing corrosion-resistant honeycomb structures where service temperature will not exceed 900 degrees F (482 degrees C), but usage is not limited to such applications. Oxidation of the brazed alloy may occur during long-time exposure to such temperatures.
HISTORICAL
1966-03-15
Standard
AMS4766B
This specification covers a silver alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, and chips and a viscous mixture (paste) of powder in a suitable binder. This material has been used typically for joining ferrous metals where high strength up to 800 degrees F (427 degrees C) for short-time service or up to 500 degrees F (260 degrees C) for long-time service is required, and for joining nonferrous metals except those having a base of aluminum or magnesium, but usage is not limited to such applications.
HISTORICAL
1966-03-15
Standard
AS1004
No scope available.
HISTORICAL
1966-03-15
Standard
AS1002
No scope available.
HISTORICAL
1966-03-15
Standard
AS1007
No scope available.
HISTORICAL
1966-03-15
Standard
AS1006
No scope available.
HISTORICAL
1966-03-15
Standard
AS1010
No scope available.
HISTORICAL
1966-03-15
Standard
AS1008
No scope available.
HISTORICAL
1966-03-15
Standard
AS1009
No scope available.
HISTORICAL
1966-03-15
Standard
AMS4930
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1966-03-15
Standard
AMS4935A
This specification covers a titanium alloy in the form of extruded bars and shapes, flash welded rings, and stock for flash welded rings. These products have been used typically for parts that do not require heat treatment but require high mechanical properties in the annealed condition and for which processing above the beta transus is permissible, but usage is not limited to such applications. This alloy exhibits high strength-to-weight ratios up to 750 °F (399 °C).
HISTORICAL
1966-03-15
Standard
AMS6275B
This specification has been declared 'NONCURRENT' by the Aerospace Materials Division, SAE, as of August, 1992. Alloy: 94B17 UNS Number: G94171
HISTORICAL
1966-03-15
Standard
AMS4970A
This specification covers a titanium alloy in the form of bars, wire, forgings, and forging stock.
HISTORICAL
1966-03-15
Standard
AMS4966B
This specification covers a titanium alloy in the form of forgings and forging stock. These forgings have been used typically for parts requiring strength up to 800 °F (427 °C) and that may be welded during fabrication, but usage is not limited to such applications.
HISTORICAL
1966-03-15
Standard
AMS4973
This specification covers a titanium alloy in the form of forgings and forging stock.
HISTORICAL
1966-03-15
Standard
AMS4972
This specification covers a titanium alloy in the form of bars, wire, flash welded rings, and stock for flash welded rings or heading.

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