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1963-12-15
Standard
AS522
No scope available.
1963-12-15
Standard
AS523
No scope available.
1963-12-15
Standard
AS520
No scope available.
1963-12-15
Standard
ARP726
This recommended practice covers a self-contained detection system which is capable of pressurizing a closed system up to 70 psig with halogen (tracer) gas and up to 3500 psig with nitrogen. An external tracer gas supply may be used to increase the capacity of the system. The detector shall be capable of detecting leaks as small as .05 ounce of tracer gas per year, with a system pressure of 70 psig or less. The purpose of this document is to provide a recommended practice for the design of a universal leak detector which will pressurize a closed system with a mixture of inert and tracer gas and provide a probe and detector to indicate location and rate of system leakage with a high degree of accuracy.
1963-12-01
Standard
ARP699B
This Recommended Practice is intended to outline the design, installation, testing, and field maintenance criteria for a high temperature metal pneumatic duct system, for use as a guide in the aircraft industry. These recommendations are to be considered as currently applicable and necessarily subject to revision from time to time, as a result of the rapid development of the industry.
1963-11-01
Standard
AIR764
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.
1963-10-01
Magazine
1963-09-01
Standard
AIR797
This document lists military and industry specifications and standards which are used in aerospace systems and for ground servicing equipment. The characteristic limitations of the hose, which are of major importance to designers, and the sizes in which the hoses are standard are shown. Revisions and amendments, which are current for these specifications and standards are not listed.
1963-08-30
Standard
AS408B
This Aerospace Standard covers two basic types of fuel, oil and hydraulic pressure instruments as follows: Type I - Direct Indicating Type II - Remote Indicating. This Aerospace Standard does not apply to engine mounted torque meter systems.
1963-08-15
Standard
ARP461B
In order to ease the equipment design engineer's problem and at the same time provide a basis for comparing measurements by manufacturer and user this recommended practice sets up standard test procedures for acceptance testing. These conditions and the basic tests to which the characteristics refer are grouped in Section 2 and compose a complete list of defining characteristics of the synchro. Specifications written around synchros have specified certain necessary characteristics for production acceptance testing, such as null voltage and accuracy, under test conditions and techniques that are mainly and properly concerned with accuracy and the shortest possible test time. These characteristics are inherently degraded when the synchro is operating for a period of time at other than room temperature. In synchros this degradation is a factor of high importance
1963-08-01
Standard
AS756
No scope available.
1963-08-01
Standard
AS758
No scope available.
1963-08-01
Standard
AS429
This Aerospace Standard establishes essential minimum safe performance standards for pressure actuated Rate of Climb (Vertical Speed) Indicators primarily for use with turbine powered subsonic transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aerospace Standard covers four basic types of direct reading pressure actuated rate of climb (vertical speed) indicators as follows: TYPE I - Range 0-2000 feet per minute climb and descent, TYPE II - Range 0-3000 feet per minute climb and descent, TYPE III - Range 0-4000 feet per minute climb and descent, TYPE IV - Range 0-6000 feet per minute climb and descent.
1963-08-01
Standard
AS432A
This SAE Aerospace Standard (AS) covers tachometer instruments (RPM indicator, 0-110 percent RPM and 0-120 percent RPM indicators and generator) for remote indication of engine speed. This Aerospace Standard establishes the essential minimum safe performance standards for Tachometer Instruments primarily for use on turbine-powered subsonic transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3.
1963-08-01
Magazine
1963-07-25
Standard
AS1043
No scope available.
1963-06-01
Standard
AS390
This aerospace standard covers the following basic instrument types: Type I - Pitot Pressure, straight and L-shaped "28 and 115 volt, 60 to 400 cycles AC or DC", 1 or 2 wire circuit. Type II - Pitot and Static Pressures, straight and L-shaped "28 and 115 volt, 60 to 400 cycle AC or DC", 1 or 2 wire circuit.
1963-06-01
Standard
J857_196306
ABSTRACT
1963-05-01
Standard
ARP731
The purpose of this SAE Aerospace Recommended Practice (ARP) is to establish recommendations for the design, installation and testing of air vehicle vapor cycle refrigeration systems. These recommendations are representative of the refrigerant cycles.
1963-04-15
Standard
AS411A
This Aerospace Standard covers two basic types of mainfold pressure instruments as follows: Type I - Direct Indicating Type II - Remote Indicating
1963-04-01
Standard
AS437
This Aerospace Standard covers one type of maximum-allowable-airspeed instrument which gives a continuous indication of both indicated airspeed and maximum allowable airspeed not exceeding 650 knots. This Aerospace Standard establishes the essential minimum safe performance standards for pitot-static type of maximum-allowable-airspeed instruments primarily for use with turbine powered subsonic transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3.
1963-04-01
Standard
J587A_196304
This SAE Standard provides test procedures, requirements, and guidelines for vehicular license plate illumination devices.
1963-04-01
Magazine
1963-03-01
Standard
AIR818
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.
1963-02-28
Standard
AS470B
No scope available.
1963-02-28
Standard
AS468B
No scope available.
1963-02-28
Standard
AS473B
No scope available.
1963-02-28
Standard
ARP416
This recommended practice covers the requirements for gyroscopically stabilized Directional Indicating Systems, which will operate as a 1°/hour latitude corrected, free directional gyro or as a slaved gyro, magnetic compass with 1/2° accuracy.
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