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曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
ACTION RESULT
PAX rotactor fully counter clockwise CABIN air conditioning in manual mode MAN status light in amber REMOTE status de-selected
COLD PAX pushbutton pressed and maintained CABIN temperature valve position 100 % blue CABIN air flow line in green
AIR CONDITIONING WITH ECU OVERHEAT Abnormal status
ECS SYNOPTIC
After procedure complete
AIR CONDITIONING OVERHEAD PANEL
ECS SYNOPTIC
ACTION RESULT
PAX rotactor fully counter clockwise CABIN air conditioning in manual mode MAN status light in amber REMOTE status de-selected
COLD or HOT PAX pushbutton pressed and maintained -CABIN temperature valve position select above 40% brown position to reduce the air flow in the ECU -COLD AIR UNIT air flow lines in green. If not, refer to CODDE 2 / ABNORMAL PROCEDURES / ATA 21
CAS MESSAGES
DESCRIPTION
GENERAL
The purpose of pressurization is to maintain a certain level of pressure inside the fuselage that is comfortable for the passengers and crew, taking into account structural limits of the airframe, whatever the flying conditions.
The air conditioning system provides the pressurized areas with air at mild temperature. The pressurization system can operate in three modes:
-automatic mode (AUTO),
-manual mode (MAN),
-rapid depressurization mode (DUMP).
The airplane comprises three pressurized areas:
-
the cockpit, passenger cabin and toilets, from frame 0 to frame 25, supplied with air by the air conditioning system,
-
the baggage compartment, from frame 25 to frame 30, which can be accessed in flight through a door usually closed, and pressurized with the passenger cabin air through an interconnection device,
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本文链接地址：DASSAULT FALCON 900EX EASY SYSTEMS SUMMARY Air Conditioning & Pressurization(9)
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