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
General
Vol. 2 01−10−5
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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 01−10−6
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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 01−10−7
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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 01−10−8
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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);
• Fully seat the door using the DOOR PULL−IN GRIP;
• Latch the door by moving the INNER HANDLE downward to its stop (confirm all four
rotary latch green marks are aligned);
• Pull the internal T-HANDLE to stow the EXTERNAL HANDLE (external handle stow is
confirmed by an audible click and a green locked indicator showing in the viewing
window); and
• Stow the internal T-HANDLE by pushing it back into its recessed position.
The door is closed from the outside by lifting and pushing it to the vertical closed position, flush
with the fuselage. The EXTERNAL HANDLE is rotated clockwise to latch the cams, and is then
stowed by pushing it into its recessed position.
The door is opened from the inside by lifting the INNER HANDLE, which releases the
EXTERNAL HANDLE from its recess. The continued upward travel of the INNER HANDLE
unlatches the door-locking mechanism. As the door opens, the handrails unfold upward. A
PULL-UP ASSIST HANDLE is attached to the rear of the door, to assist in controlling the fall of
the door as it opens.
The door is opened from outside by pressing the TRIGGER PLATE on the EXTERNAL
HANDLE, which releases the handle from its recess. Rotating the EXTERNAL HANDLE
counterclockwise unlatches the door.
A hinged pressurization flap is installed in the door, to release excess cabin pressure before the
door locks are released. When the door is fully opened, a support leg extends to the ground to
stabilize the door. The EXTERNAL HANDLE incorporates a keylock mechanism.
AIRPLANE GENERAL
General
Vol. 2 01−10−9
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
DOORS AND EMERGENCY EXIT (CONT'D)
Passenger Door
Figure 01−10−7
AIRPLANE GENERAL
General
Vol. 2 01−10−10
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
DOORS AND EMERGENCY EXIT (CONT'D)
Cargo/Baggage Door
The cargo/baggage compartment door is located on the left side of the airplane, immediately
behind the passenger compartment.
Cargo/Baggage Door Operation
The door may be opened from inside or outside. The door opens inward and upward on two
tracks attached to the structure. Balance springs and cables are attached to assist in opening.
The door is held closed by two plungers, which are operated by an external HANDLE. Two
plunger-activated proximity switches provide an indication in the flight compartment if the door is
not properly closed. The external handle provides a keyed security lock. This handle is kept
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
庞巴迪挑战者605机组操作手册 CL605-AIRPLANE_GENERAL(3)
