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Viewing 7201 to 7230 of 7276
HISTORICAL
1955-03-01
Standard
AMS2645C
This specification has been declared 'SUPERSEDED' by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the latest issue of ASTM E 1417.
HISTORICAL
1954-12-15
Standard
AS408A
This Aerospace Standard establishes the essential minimum safe performance standards for fuel, oil and hydraulic pressure instruments primarily for use with reciprocating engine powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. 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.
HISTORICAL
1954-12-15
Standard
AS264C
The desired system for aircraft instrument panel and cockpit lighting is one that will furnishlight of adequate intensity and distribution under all conditions of external lighting so that the crew may read instrumentation, placards, check lists, manuals, maps, instrument color coding, distinguish controls, etc., without undue interference with their vision outside of the aircraft.
HISTORICAL
1954-12-15
Standard
AS407A
To specify minimum requirements for Fuel Flowmeters for use primarily in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aeronautical Standard covers two basic types of instruments, or combinations thereof, intended for use in indicating fuel consumption of aircraft engines as follows: TYPE I - Measure rate of flow of fuel used. TYPE II - Totalize amount of fuel consumed or remaining.
HISTORICAL
1954-12-15
Standard
AS404A
To specify minimum requirements for Electric Tachometers primarily for use in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aeronautical Standard covers magnetic drag tachometers with or without built-in synchroscopes.
HISTORICAL
1954-12-01
Standard
AS413A
This Aerospace Standard establishes the minimum sage performance standards for electrical type temperature instruments primarily for use with reciprocating engine powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.4. This Aerospace Standard covers two basic types of temperature instruments as follows: TYPE I Radiometer 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 E.M.F. output of a thermocouple; the varying E.M.F. input to the instrument being obtained by temperature changes of the temperature sensing thermocouple.
HISTORICAL
1954-12-01
Standard
AS420
This Aerospace Standard establishes essential minimum safe performance standards for Flight Director instruments primarily for use with reciprocating engine powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. 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
1954-12-01
Standard
AS391B
This Aeronautical Standard covers five basic types o fairspeed instruments as follows: Type I - 1 revolution Type II - 1 revolution (unequal scale) Type III - 1 1/2 to 1 3/4 revolutions Type IV - 7 revolutions Type V - 1 3/4 to 2 revolutions
HISTORICAL
1953-06-15
Standard
AMS2645B
This specification has been declared 'SUPERSEDED' by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the latest issue of ASTM E 1417.
HISTORICAL
1952-11-01
Standard
AMS2640D
This specification has been declared 'CANCELLED' by the Aerospace Materials Division SAE, as of April 1996. and has been superseded ASTM E 1444.
HISTORICAL
1952-02-01
Standard
ARP266
This recommended practice is written to cover the installation of combustion heaters used in the following applications.
HISTORICAL
1951-10-01
Standard
AMS6372C
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing. This tubing has been used typically for parts, 0.75 inch (19 mm) and under in section thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 40 HRC when properly hardened and tempered and for parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.
HISTORICAL
1951-03-15
Standard
AS392B
This Aeronautical Standard covers two (2) basic types of instruments as follows: Type I - Range 35,000 feet. Barometric Pressure. Scale range at least 28.1 - 30.99 inches of mercury (946-1049 millibars). May include markers working in conjunction with the Barometric Pressure Scale to indicate pressure altitude. Type II - Range 50,000 feet. Barometric Pressure. Scale range at least 28.1 - 30.99 inches of mercury (946-1049 millibars). May include markers working in conjunction with the Barometric Pressure Scale to indicate pressure altitude.
HISTORICAL
1951-03-15
Standard
ARP217
This document deals with ground and flight test of airplane installed Environmental Control Systems (ECS), Figure 1. The ECS provide an environment, controlled within specified operational limits of comfort and safety, for humans, animals, and equipment. These limits include the following: pressure, temperature, humidity, ventilation air velocity, ventilation rate, wall temperature, audible noise, vibration, and environment composition (ozone, contaminants, etc.). The ECS are composed of equipment, controls, and indicators that supply, distribute, recycle and exhaust air to maintain the desired environment.
HISTORICAL
1951-03-01
Standard
AMS5032A
This specification covers a low-carbon steel in the form of wire supplied as coils of wire or, when specified, as straight lengths.
HISTORICAL
1951-03-01
Standard
AS396A
To specify the minimum requirements for gyroscopically stabilized Bank and Pitch Indicators for use in aircraft, the operation of which may subject the instrument to the environmental conditions specified in Section 3.4.
HISTORICAL
1950-12-01
Standard
AMS6372B
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing. This tubing has been used typically for parts, 0.75 inch (19 mm) and under in section thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 40 HRC when properly hardened and tempered and for parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.
HISTORICAL
1950-10-01
Standard
AMS6352B
This specification covers an aircraft quality, low alloy steel in the form of sheet, strip, and plate. These products have been used typically for heat treated parts and structures that may require welding during fabrication, but usage is not limited to such applications. It may be through-hardened to a minimum tensile strength of 180 ksi (1241 MPa) in sections 0.125 inch (3.18 mm) and under in nominal thickness and proportionately lower strength in heavier section thicknesses.
HISTORICAL
1950-06-15
Standard
AMS2645A
This specification has been declared 'SUPERSEDED' by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the latest issue of ASTM E 1417.
HISTORICAL
1950-06-01
Standard
AMS2640C
This specification has been declared 'CANCELLED' by the Aerospace Materials Division SAE, as of April 1996. and has been superseded ASTM E 1444.
HISTORICAL
1949-02-01
Standard
AS392A
This Aeronautical Standard covers two (2) basic types of instruments as follows: Type I - Range 35,000 feet. Barometric Pressure. Scale range at least 28.1 - 30.99 inches of mercury (946-1049 millibars). May include markers working in conjunction with the Barometric Pressure Scale to indicate pressure altitude. Type II - Range 50,000 feet. Barometric Pressure. Scale range at least 28.1 - 30.99 inches of mercury (946-1049 millibars). May include markers working in conjunction with the Barometric Pressure Scale to indicate pressure altitude.
HISTORICAL
1949-02-01
Standard
AS143B
These standards are written to cover internal combustion heat exchanger type heaters used in the following applications:
HISTORICAL
1949-02-01
Standard
AS391A
This Aeronautical Standard covers five basic types o fairspeed instruments as follows: Type I - 1 revolution Type II - 1 revolution (unequal scale) Type III - 1 1/2 to 1 3/4 revolutions Type IV - 7 revolutions Type V - 1 3/4 to 2 revolutions
HISTORICAL
1948-11-01
Standard
AS411
This Aerospace Standard establishes the essential minimum safe performance standards for manifold pressure instruments primarily for use with reciprocating engine powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aerospace Standard covers two basic types of manifold pressure instruments as follows: TYPE I - Direct Indicating. TYPE II - Remote Indicating.
HISTORICAL
1948-11-01
Standard
AS408
This Aerospace Standard establishes the essential minimum safe performance standards for fuel, oil and hydraulic pressure instruments primarily for use with reciprocating engine powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. 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.
HISTORICAL
1948-11-01
Standard
AS245
.This specification covers the following types and classes of extinguishers: Type I Stored pressure type, Category A - Temperature range -40 to +140, Category B - Temperature range +35 to +140. Type II Cartridge operated type, Category A - Temperature range -40 to +140, Category B - Temperature range +35 to +140. To specify minimum requirements for a water solution type hand fire extinguisher which shall be suitable for use on incipient fires which may occur in an airplane cabin interior. The type of fire for which these units are intended is one involving combustible materials such as paper, textiles and similar materials
HISTORICAL
1948-11-01
Standard
AS413
This Aerospace Standard establishes the minimum sage performance standards for electrical type temperature instruments primarily for use with reciprocating engine powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.4. This Aerospace Standard covers two basic types of temperature instruments as follows: TYPE I Radiometer 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 E.M.F. output of a thermocouple; the varying E.M.F. input to the instrument being obtained by temperature changes of the temperature sensing thermocouple.
HISTORICAL
1948-11-01
Standard
AS412
To specify minimum requirements for carbon monoxide detector instruments for use in aircraft, the operation of which may subject the instrument to the environmental conditions specified in Paragraph 3.3. This standard is not intended to cover fire detectors. This Aeronautical Standard covers the basic type of carbon monoxide detector instrument used to determine toxic concentrations of carbon monoxide by the measurement of heat changes through catalytic oxidation.
HISTORICAL
1948-11-01
Standard
AS404
To specify minimum requirements for Electric Tachometers primarily for use in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aeronautical Standard covers magnetic drag tachometers with or without built-in synchroscopes.
HISTORICAL
1948-11-01
Standard
AS407
To specify minimum requirements for Fuel Flowmeters for use primarily in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aeronautical Standard covers two basic types of instruments, or combinations thereof, intended for use in indicating fuel consumption of aircraft engines as follows: TYPE I - Measure rate of flow of fuel used. TYPE II - Totalize amount of fuel consumed or remaining.
Viewing 7201 to 7230 of 7276