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庞巴迪挑战者605公务机机组操作手册 CL605-AIRPLANE_GENERAL(4)

时间:2011-10-26 21:44来源:蓝天飞行翻译 作者:公务机
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PRO LINE 21 DATA MANAGEMENT (CONT'D)


Display Control Panel (DCP)
Figure 01.10.2


Cursor Control Panel
Figure 01.10.3


INTEGRATED FLIGHT INFORMATION SYSTEM (IFIS)
IFIS is a combination of data management platforms that handles all of the databases required by aircraft systems.
Database management is performed through a file server unit (FSU) using a laptop computer which contains relevant databases (some optional) such as:
.
Jeppview charts;

.
Maintenance data computer;

.
Graphic weather GWX;

.
Geopolitical map;

.
Airspace map;

.
Airways maps; and

.
Terrain/obstacle databases.


IFIS is the primary data source for electronic flight bag charts (Jeppview). The charts are displayed on the multi function display, and are controlled using the chart section of the CCP.


 AIRPLANE GENERAL General  Vol. 2  01.10.6 
Oct 05/06 

INTEGRATED FLIGHT INFORMATION SYSTEM (IFIS) (CONT'D)


Integrated Flight Information System (IFIS)
Figure 01.10.4


CABIN ELECTRONIC SYSTEM
The Rockwell Collins CES 5000 cabin electronic system has a backup control in the cockpit using the side console cockpit touch screen. In addition to cabin management functions, the side screen also acts as the secondary display location for Electronic Flight Bag (Jeppview) charts to comply with class III EFB standards.


 AIRPLANE GENERAL General  Vol. 2  01.10.7 
Oct 05/06 

CABIN ELECTRONIC SYSTEM (CONT'D)


Cabin Electronic System
Figure 01.10.5

DOORS AND EMERGENCY EXIT Description
The airplane is equipped with a passenger door, a cargo/baggage door, an aft equipment bay door and an emergency exit.


 AIRPLANE GENERAL General  Vol. 2  01.10.8 
Oct 05/06 

DOORS AND EMERGENCY EXIT (CONT'D)


Doors and Emergency Exit . Location
Figure 01.10.6

Components and Operation
Passenger Door
The passenger door is a manually-operated, downward-opening door with stairs integral to the door structure. The weight of the door is counterbalanced by gas springs and a spring-loaded cable drum. An electric door-closing mechanism is fitted to raise the door.


 AIRPLANE GENERAL General  Vol. 2  01.10.9 
Oct 05/06 

DOORS AND EMERGENCY EXIT (CONT'D)


Passenger Door Operation
The door is closed from inside by an electrically-powered assist mechanism. The mechanism is activated by a two-position switch, located on the interior of the fuselage, forward of the top corner of the door.
To close the passenger door from the inside:
.  
Operate the cabin door switch to raise the door (use the DOOR PULL-UP ASSIST HANDLE, if required);
 
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