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CONTROL OF WATER CARRYOVER FROM THE ENVIRONMENTAL CONTROL SYSTEM AND CONDENSATION ON THE STRUCTURE

2007-12-03

HISTORICAL

AIR1204

This publication will discuss water carryover from the environmental control system with respect to causes and indicated corrective or preventative action. In addition, condensation on structure will be reviewed with possible preventative action described.

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Aircraft Electrical Heating Systems

2011-10-17

CURRENT

AIR860B

It is intended that the scope of this information report be limited to electrical heating of passenger, crew, and cargo compartments only. No attempt has been made to develop the complete electrical circuitry associated with the electrical heating components; however, the electrical circuitry required for heating component operation, safety, and monitoring will be included as available. Specific design information is given for various modern aircraft utilizing electrical heating. Each aircraft discussed will be identified by alphabetical letter designation and included in the appropriate appendix.

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Aircraft Electrical Heating Systems

2006-03-24

HISTORICAL

AIR860A

It is intended that the scope of this information report be limited to electrical heating of passenger, crew, and cargo compartments only. No attempt has been made to develop the complete electrical circuitry associated with the electrical heating components; however, the electrical circuitry required for heating component operation, safety, and monitoring will be included as available. Specific design information is given for various modern aircraft utilizing electrical heating. Each aircraft discussed will be identified by alphabetical letter designation and included in the appropriate appendix.

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AIRCRAFT ELECTRICAL HEATING SYSTEMS

1992-03-01

HISTORICAL

AIR860

It is intended that the scope of this information report be limited to electrical heating of passenger, crew, and cargo compartments only.

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TEMPERATURE CONTROL EQUIPMENT, AUTOMATIC, AIRPLANE CABIN

1956-03-15

HISTORICAL

ARP89B

This recommended practice covers automatic cabin temperature control systems of the following types for pressurized and unpressurized cabins: Type I - Proportioning. Type II - On-Off, or Cycling. Type III - Floating, including modifications thereof.

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TEMPERATURE CONTROL EQUIPMENT, AUTOMATIC, AIRCRAFT COMPARTMENT

1992-03-01

HISTORICAL

ARP89C

The recommendations of this ARP are primarily intended to be applicable to temperature control of compartments, occupied or unoccupied, of civil aircraft whose prime function is the transporting of passengers or cargo. The recommendations will apply, however, to a much broader category of civil and military aircraft where automatic temperature control systems are applicable.

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Aircraft Compartment Automatic Temperature Control Systems

2018-08-23

CURRENT

ARP89D

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.

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TEMPERATURE CONTROL EQUIPMENT, AUTOMATIC, AIRPLANE CABIN

1949-02-01

HISTORICAL

ARP89A

These recommendations are written to cover automatic cabin temperature controls under three classifications, namely:

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GUIDE FOR QUALIFICATION TESTING OF AIRCRAFT AIR VALVES

1990-02-28

HISTORICAL

ARP986B

This Aerospace Recommended Practice (ARP) defines tests to be performed on hydraulically, electrically, pneumatically, and mechanically actuated air valves. They may be further defined as those valves that function in response to externally applied forces or in response to variations in upstream and/or downstream duct air conditions in order to maintain a calibrated duct air condition (e.g., air flow, air pressure, air temperature, air pressure ratio, or air shutoff).

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Guide for Qualification Testing of Aircraft Air Valves

2008-11-06

HISTORICAL

ARP986C

This Aerospace Recommended Practice (ARP) defines tests to be performed on hydraulically, electrically, pneumatically, and mechanically actuated air valves. They may be further defined as those valves that function in response to externally applied forces or in response to variations in upstream and/or downstream duct air conditions in order to maintain a calibrated duct air condition (e.g., air flow, air pressure, air temperature, air pressure ratio, or air shutoff).

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AIR CONDITIONING, HELICOPTERS, GENERAL REQUIREMENTS FOR

1961-08-15

HISTORICAL

ARP292A

These recommendations are written to cover the general requirements of helicopter air conditioning and are subdivided as follows:

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Aircraft Humidification

2015-11-09

HISTORICAL

AIR1609A

This SAE Aerospace Information Report (AIR) covers the design parameters for various methods of humidification applicable to aircraft, the physiological aspects of low humidities, the possible benefits of controlling cabin humidity, the penalties associated with humidification, and the problems which must be solved for practical aircraft humidification systems. The design information is applicable to commercial and military aircraft. The physiological aspects cover all aircraft environmental control applications.

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AIRCRAFT HUMIDIFICATION

2010-05-03

HISTORICAL

AIR1609

This report covers the design parameters for various methods of humidification applicable to aircraft, the physiological aspects of low humidities, the possible benefits of controlling cabin humidity, the penalties associated with humidification, and the problems which must be solved for practical aircraft humidification systems. The design information is applicable to commercial and military aircraft. The physiological aspects cover all aircraft environmental control applications.

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Aircraft Humidification

2021-01-14

CURRENT

AIR1609B

This SAE Aerospace Information Report (AIR) covers the design parameters for various methods of humidification applicable to aircraft, the physiological aspects of low humidities, the possible benefits of controlling cabin humidity, the penalties associated with humidification, and the problems which must be solved for practical aircraft humidification systems. The design information is applicable to commercial and military aircraft. The physiological aspects cover all aircraft environmental control applications.

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ENVIRONMENTAL CONTROL FOR CIVIL SUPERSONIC TRANSPORT

1993-06-01

HISTORICAL

AIR746A

This document supplements and in some cases supersedes the recommendations presented in ARP 85D, which refers to subsonic civil transports.

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ELECTRONIC EQUIPMENT COOLING DESIGN CONCEPTS FOR HIGH MACH NUMBER AIRCRAFT

1963-01-31

HISTORICAL

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.

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Electronic Equipment Cooling Design Concepts for High Mach Number Aircraft

1984-03-01

CURRENT

AIR728A

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AIR CONDITIONING OF AIRCRAFT AT HIGH ALTITUDE

1975-04-15

HISTORICAL

AIR795

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AIR CONDITIONING OF SUBSONIC AIRCRAFT AT HIGH ALTITUDE

1984-03-01

CURRENT

AIR795A

This report is limited to the special problems of air quantity, purity, movement, pressure, temperature, and humidity which arise from the requirements of the human body during high altitude flight, together with the associated aircraft design problems.

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The Control of Excess Humidity in Avionics Cooling

2003-10-31

HISTORICAL

ARP987A

The purpose of this document is threefold: (1) to review the problem of moisture in avionics equipment, (2) to outline methods for correcting conditions of excess moisture in existing avionics installations, and (3) to recommend design practices for new avionics cooling system installations which will minimize the adverse effects of moisture.