返回首页

庞巴迪挑战者300公务机机组操作手册 Bombardier Challenger-语音和视觉警报 Aural and Visual Alerts(8)

时间:2011-11-02 15:06来源:蓝天飞行翻译 作者:公务机
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
  
-Non-pilot selected automatic activation of certain critical systems (L or R FUEL PUMP ON)
-Loss of system redundancy
-Needed information not related to a change of system status (SELCAL)
-May have a tone associated (i.e. cabin call or voice SELCAL) STATUS (S) MESSAGES White status messages appear directly below any advisory messages that may be present. White status messages:
-Indicate the state of a specific system that has been manually activated
INHIBITED EICAS MESSAGES
Takeoff and landing are the most critical phases of flight, and the most workload intensive. Accidents can occur during these phases of flight due to the crew becoming distracted by minor non-relevant system problems. To reduce the possibility of this occurring, some warning messages, most caution messages, and all advisory messages are inhibited during the take-off and landing phase.
Selected messages are inhibited for takeoff when airspeed is above 80 kts, and the aircraft reaches 400 ft AGL.
Selected messages are inhibited during landing when the aircraft descends below 400 ft AGL and airspeed decreases to less than 40 kts. Inhibited messages are indicated with a X in the respective column.
When a message is triggered during an inhibit period, the message and the master/caution (if appropriate) illuminates as the aircraft exits the inhibit envelope.
SYNOPTIC PAGES
The synoptic pages can be selected for presentation on the bottom half of either MFD by using the individual switches lo-cated on the MCP control panel. The synoptic pages provide the pilot real-time indication of aircraft system operation. Each synoptic page displays the aircraft systems as a schematic diagram.
ANTI-ICE
The anti-ice synoptic page displays the operation of the following systems:
-Bleed air system
-Wing anti-ice system
-Engine anti-ice system ECS
The ECS synoptic page displays information for the following systems:
-Bleed air
-Air conditioning
-Pressurization
ELECTRICAL
The electrical synoptic page displays the system using a block diagram.
FLIGHT CONTROLS
The flight control synoptic page displays the positions of the ailerons, elevator, rudder and spoilers.
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
03-02-08 ENGINE INDICATING AND CREW ALERTING SYSTEM (EICAS) (Cont)

MULTIFUNCTION DISPLAY (MFD) (Cont)
FUEL
The fuel synoptic page displays fuel quantities, fuel temperature, and fuel system operation.
HYDRAULIC
The hydraulic system synoptic page displays the engine pumps, auxiliary pumps, status of reservoirs, and hydraulic fluid temperature and pressure. The synoptic pages represent actual valve operation using color to identify the state and service-ability of the valve. Red indicates failure, yellow indicates a cautionary status, white indicates normal with no dynamic flow, green indicates normal with dynamic flow, and magenta invalid or unknown status. Each valve has an outline and a flowline.
 
中国公务机网 www.gongwuji.com
公务机翻译 www.aviation.cn
本文链接地址:庞巴迪挑战者300公务机机组操作手册 Bombardier Challenger-语音和视觉警报 Aural and Visual Alerts(8)
 

------分隔线----------------------------