This ARP discusses design philosophy, system and equipment requirements, and ambient conditions and design considerations for systems within the ATA 100 Specification, Chapter 21 (Reference 1). This chapter is principally concerned with passenger and crew environment and the air conditioning system that maintains this environment. 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.
SAE ARP85E-2007 history
2019SAE ARP85G-2019 Air Conditioning Systems for Subsonic Airplanes
2018SAE ARP85F-2018 Air Conditioning Systems for Subsonic Airplanes
2012SAE ARP85F-2012 Air Conditioning Systems for Subsonic Airplanes
2007SAE ARP85E-2007 Air Conditioning Systems For Subsonic Airplanes
1991SAE ARP85E-1991 Air Conditioning Systems For Subsonic Airplanes
1961SAE ARP85D-1961 AIR CONDITIONING EQUIPMENT@ GENERAL REQUIREMENTS FOR SUBSONIC AIRPLANES
1956SAE ARP85C-1956 AIR CONDITIONING EQUIPMENT@ AIRPLANE GENERAL REQUIREMENTS FOR
1948SAE ARP85B-1948 AIR CONDITIONING EQUIPMENT@ AIRPLANE GENERAL REQUIREMENTS FOR
1943SAE ARP85A-1943 HEATING AND VENTILATING EQUIPMENT@ AIRPLANE-GENERAL REQUIREMENTS FOR
1943SAE ARP85-1943 HEATING AND VENTILATING EQUIPMENT, AIRPLANE-GENERAL REQUIREMENTS FOR