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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
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
1955-07-01
Standard
ARP461
This document is limited to units meeting the definitions of para. 1.3 and covers the following general class of synchros: 26 volt, 400 cycle synchros 115 volt, 400 cycle synchros 115 volt, 60 cycle synchros
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
AS408A
This aeronautical standard covers two basic types of pressure instruments. These are intended for use in measuring fuel, oil or hydraulic pressures as follows: This aeronautical standard does not apply to engine mounted torque meter systems.
HISTORICAL
1954-12-15
Standard
AS404A
This Aeronautical Standard covers magnetic drag tachometers with or without built-in synchroscopes.
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
1954-12-01
Standard
ARP292
This purpose of this recommended practice is to provide the aerospace industry with a standard to which helicopter air conditioning systems may be designed for the civil aircraft industry. These recommendations are written to cover the general requirements for helicopter air conditioning and are sub-divided as follows: (1) Air Conditioning System - Dealing with the general design aspects. (2) Air Conditioning Equipment - Design requirements for satisfactory system function and performance. (3) Air Conditioning System Design Requirements - General information for use of those concerned in meeting requirements contained herein.
HISTORICAL
1954-12-01
Standard
AS420
This Aeronautical 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 of airspeed instruments with indication range essentially as follows:
HISTORICAL
1954-12-01
Standard
AS413A
This Aeronautical Standard covers two basic types of temperature indicators as follows:
CURRENT
1954-06-01
Standard
AIR33A
HISTORICAL
1952-08-15
Standard
AIR32
INTRODUCTION This report is intended to encourage more effort to be directed toWard improving the pilot's visibility from the cockpit of transport type aircraft wih the ultimate objective of improving safety. In the preparation of this Aeronautical Information Report, consideration Was given to pilot surveys made by the Civil Aeronautics Administration, studies made by manufacturers, and a review of the cockpit visibility provided in present day transport aircraf`t. It is recognized that a rigid specification is undesirable and may restrict development and utilization of initiative. For this reason the report is in general terms and offered as a guide.
HISTORICAL
1952-02-01
Standard
ARP266
This recommended practice is written to cover the installation of combustion heaters used in the following applications.
HISTORICAL
1951-03-15
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
1951-03-15
Standard
AS392B
This Aeronautical Standard covers two basic types of instruments as follows:
HISTORICAL
1951-03-01
Standard
AS396A
This specification covers two basic types as follows:
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
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.
CURRENT
1949-02-01
Standard
AIR4A
HISTORICAL
1949-02-01
Standard
AS391A
This specification covers six types of instruments as follows:
HISTORICAL
1949-02-01
Standard
AS392A
This Aeronautical Standard covers two basic types of instruments as follows:
HISTORICAL
1948-11-01
Standard
ARP367
HISTORICAL
1948-11-01
Standard
AS405
This Aeronautical Standard covers two basic types of instruments as follows: Type I - Float Instruments, Type II - Capacitance Instruments. To specify minimum requirements for Fuel and Oil Quantity Instruments for use in aircraft, the operation of which may subject the instruments to the environmental conditions specified in Paragraph 3.3.
HISTORICAL
1948-11-01
Standard
AS412
This specification covers the basic type of instrument for detection of toxic concentrations of carbon monoxide whose operation is based on measurement of heat changes through catalytic oxidation.
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
AS411
This specification covers instruments intended for use in airplanes to indicate engine manifold absolute pressure.
HISTORICAL
1948-11-01
Standard
AS413
This specification covers two types of instruments. These instruments are for the purpose of measuring temperature, such as those of oil coolant, carburetor air, free air and cylinder head.
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.
Viewing 1591 to 1620 of 1642