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HISTORICAL
1966-08-01
Standard
ARP699C
HISTORICAL
1966-08-01
Standard
J796A_196608
CURRENT
1965-12-01
Standard
J936
HISTORICAL
1965-12-01
Standard
J936_196512
HISTORICAL
1965-11-01
Standard
AIR910
The purpose of this report is to provide information on ozone and its control in high altitude aircraft environmental systems. Sources of this information are listed in the selected bibliography appearing at the end of this report, to which references are made throughout.
HISTORICAL
1965-04-20
Standard
ARP750
The purpose of this Aerospace Recommended Practice (ARP) is to provide design criteria that will lead to seat designs which provide maximum safety for air transportation passengers. It is not the purpose of this ARP to specify design methods or specific designs to be followed in the accomplishment of the stated objectives.
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
1964-08-01
Standard
ARP690
The thermocouple design recommended herein is presented as one for which the correction to the observed emf, because of thermal conduction along the stem and wires, is within the limits presented in the accompanying figure. On referring to the figure, it is seen that no restriction is placed upon the diameter of the thermocouple or stem, and the longitudinal dimensions are expressed in terms of wire and stem diameters. The type of stem, such as packed ceramic stock, refractory insulating tubing, etc., also is left open to choice. Thus the sizes of wires and supporting stems may be varied over wide ranges to match particular requirements where conduction errors are to be limited or controlled.
CURRENT
1964-08-01
Standard
ARP691
The ice bath recommended herein is similar to that described in SAE AIR 46.* Some material not presented in AIR 46, including preferred dimensions, has been added.
HISTORICAL
1964-02-01
Standard
AIR805
The purpose of this information report is to present factors which affect the design and development of jet blast windshield rain removal systems for commercial transport aircraft. A satisfactory analytical approach to the design of these systems has not yet been developed. Although detailed performance data are available for some test configurations, rain removal systems will generally be unique to specific aircraft. This, then, requires a preliminary design for the system based on available empirical data to be followed with an extensive laboratory development program.
HISTORICAL
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.
HISTORICAL
1963-06-30
Standard
AS580
This Aerospace Standard (AS) assures that new transport type aircraft will provide adequate visibility from the flight deck. Background - Prior to updating this AS, the committee re-evaluated flight deck visibility angles existing in transport aircraft produced up to 1975. In addition, studies and evaluations made by various airframe manufacturers were reviewed. As a result, this standard has been modified to provide more visibility in the critical areas that are most effective for collision avoidance. The "three second rule" for landing has been retained unmodified even though some late model aircraft do not completely meet the rule. The SAE Committee S-7, whose members represent a good cross section of operations personnel of the airline operators and manufacturers feel that it is still a desirable goal and no technical studies have been presented to show that a better standard would be more desirable.
HISTORICAL
1963-05-01
Standard
ARP780
These recommendations provide a list of graphical symbols for use on environmental systems schematic diagrams. The symbols listed are those most commonly employed on engineering drawings.
HISTORICAL
1962-11-01
Standard
ARP755
This SAE Aerospace Recommended Practice (ARP) provides performance station designation and nomenclature systems for aircraft propulsion systems and their derivatives.
HISTORICAL
1961-08-15
Standard
ARP85D
Air Conditioning System - General - Dealing with Design Features
CURRENT
1958-02-15
Standard
ARP464
HISTORICAL
1956-03-15
Standard
ARP85C
Air Condiitioning System - General - Dealing with Design Features. Air Conditioning Equipment - Commercial Passenger - Delaing with features. Applicable only to commercial passenger carrying aircraft. Desirable Design Features - General information for use of those concerned in meeting requirements contained herein.
HISTORICAL
1956-03-15
Standard
ARP89B
This recommended practice covers automatic cabin temperature control systems of the following types for pressurized and unpressurized cabins:
HISTORICAL
1952-02-01
Standard
ARP266
This recommended practice is written to cover the installation of combustion heaters used in the following applications.
HISTORICAL
1949-02-01
Standard
ARP89A
The recommendations of this SAE Aerospace Recommended Practice (ARP) for aircraft compartment automatic temperature control systems are primarily intended to be applicable to occupied or unoccupied compartments of civil and military aircraft.
HISTORICAL
1948-08-01
Standard
ARP85B
Air Condiitioning System - General - Dealing with design features. Air Conditioning Equipment - Commercial Passenger - Delaing with features. Applicable only to commercial passenger carrying aircraft. Desirable Design Features - General information for use of those concerned in meeting requirements contained herein.
CURRENT
1948-03-01
Standard
ARP175
CURRENT
1947-02-01
Standard
ARP388
HISTORICAL
1943-11-01
Standard
ARP85A
This specification is written to cover heating and ventilating equipment under four main classifications, namely; A. HEATING AND VENTILATING EQUIPMENT - GENERAL - Dealing with features applicable to all makes and uses. B. HEATING AND VENTILATING EQUIPMENT - MILITARY - Dealing with features applicable only to military aircraft. C. HEATING AND VENTILATING EQUIPMENT - COMMERCIAL - Dealing with features applicable only to commercial aircraft. D. DESIRABLE DESIGN FEATURES - General information for use of those concerned in meeting requirements contained herein.
HISTORICAL
1943-01-01
Standard
ARP85
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