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Viewing 7081 to 7110 of 7254
HISTORICAL
1963-02-28
Standard
AS470B
No scope available.
HISTORICAL
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.
HISTORICAL
1963-02-01
Standard
AS440
This SAE Aerospace Standard (AS) covers autoatic pilots intended for use on aircraft to automatically operate the primary and trim aerodynamic controls to maintain stable flight and/or to provide maneuvering about any of the three axes through servo control. Automatic control functions essential for primary or augmented flight control are excluded. To establish essential minimum safe performance standards for automatic pilots primarily for use with turbine powered subsonic transport aircraft, the operation of which may subject the instrument to the environmental conditions specified in Section 3.3.
HISTORICAL
1963-02-01
Standard
ARP785
This procedure describes a gravimetric method for the determination of particulate contaminant in hydraulic fluids by the control filter technique. With this method detectable contamination levels down to 0.2 mg per sample can be obtained with a standard deviation of ± 0.1 mg.
HISTORICAL
1963-01-31
Standard
AIR728
This publication outlines general design concepts considered the minimum acceptable standards for use in electrical and electronic equipment. The objective is increased reliability of the equipment without penalizing the aircraft performance.
HISTORICAL
1963-01-01
Standard
J843_196301
This SAE Recommended Practice establishes a uniform procedure for the level road test of the brake systems of new light-duty trucks and new multipurpose passenger vehicles up to and including 2700 kg (6000 lb) GVW and all classes of new passenger cars. The purpose of the test code is to establish brake system capabilities with regard to: a. Deceleration versus input, as affected by vehicle speed, brake temperature, and usage; b. brake system integrity; c. Stopping ability during emergency or inoperative power assist conditions; d. Water recovery characteristics.
HISTORICAL
1962-12-01
Standard
AIR746
This document supplements ARP85, to extend its use in the design of ECS for supersonic transports. The ECS provides an environment controlled within specified operational limits of comfort and safety, for humans, animals and equipment. These limits include pressure, temperature, humidity, conditioned air velocity, ventilation rate, thermal radiation, wall temperature, audible noise, vibration, and composition (ozone, contaminants, etc.) of the environment. The ECS is comprised of equipment, controls, and indicators that supply and distribute conditioned air to the occupied compartments. This system is defined within the ATA 100 specification, Chapter 21. It interfaces with the pneumatic system (Chapter 36 of ATA 100), at the inlet of the air conditioning system shutoff valves.
HISTORICAL
1962-11-01
Standard
J840_196211
This SAE Recommended Practice covers equipment and procedures for qualification of bonded brake shoe and lining assemblies and for quality control on materials and processes used in their manufacture.
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
1962-10-30
Standard
AS515
No scope available.
HISTORICAL
1962-10-30
Standard
AS516
No scope available.
HISTORICAL
1962-10-30
Standard
AS517
No scope available.
HISTORICAL
1962-10-30
Standard
AS534
No scope available.
HISTORICAL
1962-10-30
Standard
AS533
No scope available.
HISTORICAL
1962-10-30
Standard
AS532
No scope available.
HISTORICAL
1962-08-30
Standard
ARP743
This method describe the procedure for (1) sampling air in contamination controlled spaces for air-borne particulate contamination 5u or greater in size and for (2) the microscopic determination of the concentration and size range distribution of the particulate material removed from the air sample.
HISTORICAL
1962-04-01
Standard
J823_196204
This SAE Standard specifies the test procedure, test circuitry, and instruments required for measuring the performance of flashers used in motor vehicles.
CURRENT
1962-03-01
Standard
AS420B
This Aerospace 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 pre-selected flight plan.
HISTORICAL
1962-02-15
Standard
AS400A
This Aerospace Standard covers three basic types of cargo compartment fire detector instruments. Basic Types - Definition of: Type I: Carbon Monoxide, an instrument which will actuate an alarm signal when the concentration of carbon monoxide in air exceeds a specified value. Type II: Smoke Detector, Electronic, an instrument operating on the principle of smoke particles modifying the relationship between a light beam and electronic light sensor which will actuate an alarm signal when the concentration of smoke in air exceeds a specified value. Type III: Smoke Detector, Visual, an instrument which, by visual means, will show in a positive manner the presence of smoke when the concentration of smoke in air exceeds a specified value.
HISTORICAL
1962-02-01
Standard
AS431A
This SAE Aerospace Standard (AS) covers three basic types of true mass flow indicating instruments. Each may consist of an indicator, transmitter and other auxiliary means such as a power supply or amplifier as required. This Aerospace Standard establishes the essential minimum safe performance standards for True Mass Fuel Flow 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.
HISTORICAL
1961-12-31
Standard
ARP719
Gas for the purpose of this ARP shall be defined as the gaseous produces) resulting from the decomposition, dissociation, or combustion of liquid or solid mono or bi-propellants. Where other gases such as heated N2, H2, H2O (steam), etc., which may have similar physical and/or chemical properties as the defined "gas", are used to effect testing economies; they may be considered as being included in this ARP.
CURRENT
1961-11-30
Standard
ARP727
HISTORICAL
1961-10-15
Standard
ARP219
This procedure will be generally applicable to three classes of hydraulic components as listed below:
HISTORICAL
1961-08-15
Standard
ARP85D
Air Conditioning System - General - Dealing with Design Features
HISTORICAL
1961-07-01
Standard
AMS3388A
This specification covers a synthetic rubber in the form of a non-rigid, smooth bore, noncollapsing-type hose. This hose has been used typically for fueling aircraft, but usage is not limited to such applications. This hose is not intended for flexible connection between tractor and trailer, to be collapsed for drainage, or for operating pressures higher than 185 psi (1276 kPa).
HISTORICAL
1961-07-01
Standard
AMS3389A
This specification covers a synthetic rubber in the form of a nonrigid, smooth bore, noncollapsing-type hose. This hose has been used typically for fueling aircraft, but usage is not limited to such applications. This hose is not intended for flexible connection between tractor and trailer, to be collapsed for drainage, or for operating pressures higher than 250 psi (1724 kPa).
HISTORICAL
1961-07-01
Standard
AMS3386A
This specification covers a synthetic rubber in the form of soft wall, smooth bore, collapsing-type hose. This hose has been used typically for fueling aircraft from tank trucks or pits where the hose will be rolled flat for stowage on a reel, but usage is not limited to such applications. Not recommended for operating pressures higher than 125 psi (862 kPa).
HISTORICAL
1961-07-01
Standard
AMS3159
This specification covers a liquid oxygen compatible gas-leak deteching compound in the form of a liquid.
HISTORICAL
1961-06-01
Standard
J30_196106
This SAE standard covers fuel, oil, or emission hose for use in coupled and uncoupled applications, for use with gasoline, oil, diesel fuel, lubrication oil, or the vapors present in either the fuel system or in the crankcase of internal combustion engines in mobile or stationary applications. This standard covers the hose portion only. If assembly / coupling is required, that is to be agreed to between the customer and assembler, along with the specific requirements.
HISTORICAL
1961-06-01
Standard
AS414
This SAE Aerospace Standard (AS) covers two basic types of temperature instruments as follows: type I: ratiometer type, actuated by changes in electrical resistance of a temperature sensing electrical resistance element; the resistance changes being obtained by temperature changes of the temperature sensing resistance element. Type II: millivoltmeter type, operated and actuated by varying EMF output of a thermocouple; the varying EMF input to the instrument being obtained by temperature changes of the temperature sensing thermocouple. This document establishes the essential minimum safe performance standards for electrical type temperature 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 3.4.
Viewing 7081 to 7110 of 7254