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Viewing 36781 to 36810 of 43384
HISTORICAL
1969-05-01
Standard
AMS2242C
This specification covers established manufacturing tolerances applicable to sheet, strip, and plate of corrosion and heat resistant steels, iron alloys, titanium, and titanium alloys ordered to inch dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl " is used to apply only to the higher figure of the specified range.
HISTORICAL
1969-05-01
Standard
AMS2412E
This specification covers the requirements for silver deposited on metal parts with a copper strike between the basis metal and the silver deposit. This process has been used typically to provide a bearing surface and to prevent galling or seizing of metal surfaces of parts made of materials where a high baking temperature may be detrimental to the properties of the basis material.
HISTORICAL
1969-05-01
Standard
AMS2430F
This specification covers the engineering requirements for automatic peening of surfaces of parts by impingement of metallic shot, glass beads, or ceramic shot. To induce residual compressive stress in surface layers of parts, thereby increasing fatigue strength and resistance to stress-corrosion cracking but usage is not limited to such applications.
HISTORICAL
1969-05-01
Standard
AMS5640H
This specification covers three types of a free-machining, corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
HISTORICAL
1969-05-01
Standard
AMS6411
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts requiring high tensile strength and good ductility with relatively high impact strength, superior transverse properties, and hardness, but usage is not limited to these applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment. ARP1110 recommends practices to minimize such conditions.
HISTORICAL
1969-05-01
Standard
AMS6520
This specification covers a premium aircraft-quality, maraging steel in the form of sheet, strip, and plate. These products have been used typically for large booster rocket applications, pressure vessels, and other components requiring through-hardening, without quenching, to a yield strength of 245 ksi (1689 MPa) or higher, but usage is not limited to such applications.
HISTORICAL
1969-05-01
Standard
AMS4027G
This specification covers an aluminum alloy in the form of sheet and plate.
HISTORICAL
1969-05-01
Standard
AMS2410E
This specification covers the engineering requirements for electrodeposition of silver on other metals, usually with a nickel strike between the basis metal and the silver.
CURRENT
1969-04-10
Standard
RS430-5
No scope available.
HISTORICAL
1969-04-01
Standard
AIR839B
Liquid propellant fuels and oxidizers are, in general, highly reactive chemicals. Consequently, the propellants and their reaction products possess certain hazardous properties which must be fully understood by all who are required to handle them. This manual is intended as a guide to help establish rules as needed to fit actual cases. The fitting of details into this framework must be left to personnel assigned to specific operations. Accordingly, information on the properties of these materials is given so that hazards will be recognized and understood.
HISTORICAL
1969-04-01
Standard
J377_196904
This SAE Standard establishes the minimum operational life cycles, corrosion resistance, and sound level output for traffic horns (electric) on new automotive highway vehicles. Test equipment, environment, and procedures are specified.
HISTORICAL
1969-04-01
Standard
AIR984
This SAE Aerospace Information Report (AIR) defines the helicopter bleed air requirements which may be obtained through compressor extraction and is intended as a guide to engine designers.
HISTORICAL
1969-04-01
Standard
ARP1109
This SAE Aerospace Recommended Practice (ARP) recommends performance requirements for test equipment used in dynamic testing of aviation oxygen breathing equipment. This document describes test equipment and methods used for testing continuous flow, demand and pressure demand regulators and their associated masks as well as filtered protective breathing devices; such articles of oxygen breathing or protective breathing equipment may be tested as individual components or as a complete system.
HISTORICAL
1969-04-01
Standard
ARP1070
This document recommends minimum requirements for antiskid brake control to provide total aircraft systems compatibility. Design and operational goals, general theory, and functions, which should be considered by the aircraft brake system engineer to attain the most effective skid control performance, are covered in detail. Methods of determining and evaluating antiskid system performance are discussed. While this document specifically addresses antiskid systems which are a part of a hydraulically actuated brake system, the recommended practices are equally applicable to brakes actuated by other means, such as electrically actuated brakes.
HISTORICAL
1969-03-15
Standard
AS686
To provide design criteria and an index of parts and standards for piloted ring seal tube swivel connections. This standard presents the designer with sufficient information to fully define the configuration for the connection and to determine the limits of application for given conditions.
HISTORICAL
1969-03-15
Standard
AS1078
No scope available.
HISTORICAL
1969-03-01
Standard
J388_196903
This SAE Recommended Practice describes a laboratory test procedure for evaluating the loss of thickness and the amount of structural breakdown of slab polyurethane foam seating materials. A test specimen is measured for thickness under a specified load and subsequently subjected simultaneously to compressive and shear deformation in a controlled atmosphere. This is accomplished by subjecting the foam to a rolling shearing action under a constant load for a specified number of cycles. Specimen thickness under a constant load is obtained after a 1hr recovery period following dynamic fatigue to determine loss in foam thickness.
CURRENT
1969-03-01
Standard
J345_196903
This SAE Recommended Practice defines the best known techniques for evaluating peak and locked wheel braking traction. It covers an important phase of tire braking traction, namely, the wet or dry pavement straight ahead conditions. However, this is but a small portion of the whole field of tire traction. As test procedures are established for other phases of this complex study, additional supplementary procedures will be written. A discussion of this entire subject is contained in Appendix B to this recommended practice.
HISTORICAL
1969-03-01
Standard
J345A_196903
This SAE Recommended Practice defines the best known techniques for evaluating peak and locked wheel braking traction. It covers an important phase of tire braking traction, namely, the wet or dry pavement straight ahead conditions. However, this is but a small portion of the whole field of tire traction. As test procedures are established for other phases of this complex study, additional supplementary procedures will be written. A discussion of this entire subject is contained in Appendix B to this recommended practice.
HISTORICAL
1969-03-01
Standard
J386_196903
This standard provides performance and test requirements for operator restraint systems provided for off-road self-propelled work machines. This document applies to pelvic restraint systems (Type 1) for off-road, self-propelled work machines fitted with ROPS and commonly used in construction, earthmoving, forestry, and mining as referred to in SAE J1040 and industrial machines fitted with ROPS as referred to in SAE J1042.
HISTORICAL
1969-03-01
Standard
J369_196903
This SAE Standard pertains to automotive vehicles and off-road, self-propelled work machines used in construction, general purpose industrial, agriculture, forestry, and specialized mining machinery. This standard does not address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this document to establish safety and health practices and determine the applicability of regulatory limitations prior to use. Purpose This test method is intended for burning rate measurement of polymeric materials used in the operator and passenger compartments as specified by the applicable standard. SAE J369 is technically equivalent to ISO 3795, ASTM D 5132 and FMVSS 302.
HISTORICAL
1969-03-01
Standard
J387_196903
This SAE Recommended Practice provides definitions of common terms used in SAE Technical Reports pertaining to motor vehicle lighting. It covers not only basic lighting terms but also terms which identify major segments of technical reports.
HISTORICAL
1969-03-01
Standard
J587D_196903
This SAE Standard provides test procedures, requirements, and guidelines for vehicular license plate illumination devices.
HISTORICAL
1969-02-01
Standard
J380_196902
Specific gravity is a nondestructive test used as a quality control check of the consistency of formulation and processing of brake lining. The specific gravity and the range of specific gravity are peculiar to each formulation and, therefore, the acceptable values or range must be established for each formulation by the manufacturer. Specific gravity alone shows nothing about a materials in use performance. The specific gravity of sintered metal powder friction materials, particularly those which have steel backing members, is usually determined somewhat differently. Reference ASTM B 376. Purpose To establish a uniform procedure for determining the specific gravity of brake friction material.
HISTORICAL
1969-02-01
Standard
AIR1047A
The factors involved in the selection of a quick-disconnect are grouped into the following classifications for the purpose of discussion: a. functional considerations; b. weight considerations; c. environmental performance factors; d. end fitting types; and e. additional considerations. A quick-disconnect coupling as used in this AIR is one that can be rapidly and repetitively connected and disconnected without excessive fluid loss. The relative importance of the design factors depends upon the fluid medium of the particular system in which quick-disconnect is to be used. The effect of the fluid media on each factor is discussed in this report where applicable. The purpose of this AIR is to guide users in the proper selection of quick-disconnect couplings for their specific application in fluid systems.
HISTORICAL
1969-02-01
Standard
ARP993A
The scope of this document is limited to encompass terminology, symbols, performance criteria and methods reflecting the current status of the technology. The purpose of this document is to promote the use of a common terminology and useful symbols and to encourage users and manufacturers of fluidic devices and systems to conform to meaningful standards of performance. This document is intended for use as the basis for a procurement specification for fluidic devices and systems when the need for such a specification arises. This document shall be the starting point for future SAE documents, either through revision or addition, in the field of fluidics as such documents become necessary.
HISTORICAL
1969-02-01
Standard
J910A_196902
This standard defines the test conditions, procedures and performance specifications for 6, 12 and 24-V manually actuated hazard warning signal switch.
HISTORICAL
1969-02-01
Standard
J589A_196902
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
1969-02-01
Standard
J565B_196902
This SAE Standard provides test procedures, performance requirements, and guidelines for semiautomatic headlamp beam switching devices.