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EFTA01735529 | EFTA01735537 FightSafety GIVI0300/0400 PILOT TRAINING MANUAL DISTRIBUTION SYSTEM poµnstream of the temperature control valves, the hot bleed air which passed through the that portion of the air which valves is joined by The hot and cold air arc d. ate µas refriger of the valves to become eam mixed downstr temperature-controlled air. The cabin and re cockpit have separate temperatu control s. calves and distribution system ribution system consists of The cockpit dist the cockpit temperature conthe ducting from duct trol valve, the refrigerated air duct, an air in the r check valve, a silencer, and fou outlets (or side le lab trol two con cockpit. There are e shoulder) outlets and two non-controllabl the and t side pilo the on foot outlets. one each copilot side. ductThe cabin distribution system consists of e, valv trol con ing from the cabin temperature two refrigerated air check valve, a silencer, and ally ctic baseboard-shaped outlets running pra A the entire length of the cabin on both sides. air the fluted skirt near the floor level allows from the baseboard to enter the compartment. Cabin and cockpit air check valves are inw stalled in the compartment ducting. They allo air to pass only in a forward direction. Should the air attempt to reverse flow, the valves close and prevent backflow. Cabin and cockpit silencers are installed in the ducting under the floor for noise attenuation. The silencer function is to suppress the air noise from the engine bleed-air ducts. REFRIGERATION SYSTEM ass the temperBleed air which does not byp into the refrigature control valves is routed unit consists of eration unit. The refrigerationents: the following major compon • Primary heat exchanger perature thermal • ACM and ACM overtem switch • Secondary heat exchanger bypass duct • Mixing muff, screen, and assembly as• Water separator anti-ice valve with sociated sensor • Water separator unit • Cooling fan hangers Cooling is accomplished by heat exc cation idifi um Deh and an expansion turbine. sepais accomplished by a mechanical water ns mea by g icin from rator, which is prevented t hea the ss acro of an anti-ice system. Airflow h wit ined inta exchangers is automatically ma a ground cooling fan. Primary Heat Exchangers The primary heat exchangers are the first stage of refrigeration. They use ram air from the dorsal fin ram-air inlet as a coolant. These single-pass heat exchangers are mounted in the tail compartment. ONLY FOR TRAINING PURPOSES 11-9 FrTA Di nrin4n.ne• EFTA01735537 Epstein Web iOS app on the App Store.
March 8, 2026 at 1:19 PM