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SAE ARP85 Rev G

Current Revision

Air Conditioning Systems for Subsonic Airplanes

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This SAE Aerospace Recommended Practice (ARP) contains guidelines and recommendations for subsonic airplane air conditioning systems and components, including requirements, design philosophy, testing, and ambient conditions. The airplane air conditioning system comprises that arrangement of equipment, controls, and indicators that supply and distribute air to the occupied compartments for ventilation, pressurization, and temperature and moisture control. The principal features of the system are: a A supply of outside air with independent control valve(s). b A means for heating. c A means for cooling (air or vapor cycle units and heat exchangers). d A means for removing excess moisture from the air supply. e A ventilation subsystem. f A temperature control subsystem. g A pressure control subsystem. Other system components for treating cabin air, such as filtration and humidification, are included, as are the ancillary functions of equipment cooling and cargo compartment conditioning. The interface with the major associated system, the pneumatic system (Chapter 36 of ATA 100) is at the inlet of the air conditioning shutoff valves. This boundary definition aligns with that in the ATA 100 Specification.

SDO SAE: SAE International
Document Number ARP85
Publication Date Sept. 25, 2019
Language en - English
Page Count 50
Revision Level G
Supercedes
Committee
Publish Date Document Id Type View
Sept. 25, 2019 ARP85G Revision
Oct. 9, 2012 ARP85F Revision
Aug. 1, 1991 ARP85E Revision
Aug. 15, 1961 ARP85D Revision
March 15, 1956 ARP85C Revision
Aug. 1, 1948 ARP85B Revision
Nov. 1, 1943 ARP85A Revision
Jan. 1, 1943 ARP85 Revision