To view this page ensure that Adobe Flash Player version
9.0.124 or greater is installed.
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
Cabin temperature indication
Cabin temperature indication is presented on the right of the PAX label. The indication is based on the air cabin temperature measurement. The temperature spacing is 1°. The readout ranges from 0 to 40°C. When the signal is invalid, two amber dashes are displayed in place of temperature indication.
CREW and PAX indications during emergency pressurization
The activation of the EMERG pressurization pushbutton simultaneously:
-closes the CABIN conditioning valve,
-drives the CKPT temperature control valve into full hot position,
Airflow admission to the ECU is shut off. Conditioning is therefore only achieved by mixing ambient cabin air with hot bleed air. Temperature control at high altitude may not present a problem. But, at lower altitude, cabin and cockpit ambient temperature will naturally increase. In this case, temperature may be manually controlled by using the COLD CREW pushbutton that commands hot bleed airflow reduction but consequently affects cabin pressurization.
SYSTEM PROTECTION
INTRODUCTION
Electrical circuit protection is provided by conventional trip-free circuit breakers located above the overhead panel.
CIRCUIT BREAKERS
AIR CONDITIONING CIRCUIT BREAKERS
NORMAL OPERATION
In the following, typical situation has been selected to help the crew to understand the symbols provided in the various panels and displays.
ECS SYNOPTIC
ABNORMAL OPERATION
INTRODUCTION
In the following, abnormal operations have been selected to help the crew to understand the symbols provided in the various panels and displays.
AIR CONDITIONING WITH CABIN OVERHEAT Abnormal status
ECS SYNOPTIC
After procedure complete
AIR CONDITIONING OVERHEAD PANEL
ECS SYNOPTIC
中国公务机网 www.gongwuji.com
公务机翻译 www.aviation.cn
本文链接地址:DASSAULT FALCON 900EX EASY SYSTEMS SUMMARY Air Conditioning & Pressurization(8)
|