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
19ft 2in.
(5.84m).
P604_01_001
AIRPLANE GENERAL
1-4 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
Fuselage
Description
The CL-604 fuselage is a semimonocoque structure and is made up of three sections:
the nose, center and tail sections. The nose section includes the nose landing gear and
flight compartment, while the center section includes the avionics area and cabin. The
wing, which contains the main landing gear, is bolted to the fuselage behind the
avionics bay. The tail section encloses an equipment bay, and supports the engines and
empennage.
Components
Nose Section
The nose section contains:
• the flight compartment, comprising instrument panels, airplane controls, and crew
stations
• the underfloor area, with compartments for brake accumulators and controls, an
air-driven generator, the forward avionics bay, flight control mechanisms and the
nosewheel well
• a weather radar antenna pedestal which is located on the front bulkhead and is
covered by a Kevlar radome incorporating conductive paths to reduce the risk of
damage from lightning strikes. The airplane has dual landing lights in the radome
Center Section
The center section is divided by the cabin floor into a pressurized passenger
compartment and underfloor area. The passenger compartment comprises a passenger
door, an emergency exit and a cargo/baggage compartment door. The underfloor area
is divided into three areas:
• pressurized avionics bay
• unpressurized main landing gear bay
• aft underfloor pressurized area
AIRPLANE GENERAL
For Training Purposes Only
May 03
1-5
P I LOT T R A I N I N G GU I D E
Tail Section
The tail section is unpressurized and includes the following three main areas:
• an aft equipment bay which contains:
• two batteries
• two battery chargers
• electric junction box 5 (JB-5)
• Auxiliary Power Unit (APU)
• two air conditioning packs
• two hydraulic systems
• three fire extinguisher bottles
• saddle fuel tanks and
• empennage and engine support structures
• a tail cone consisting of:
• Emergency Locator Transmitter (ELT) and
• tail fuel tank
• vertical stabilizer, horizontal stabilizer, rudder and elevator assemblies and
components
AIRPLANE GENERAL
1-6 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
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
For Training Purposes Only
May 03
1-7
P I LOT T R A I N I N G GU I D E
Doors and Emergency Exit - Location
Figure 1-2
Passenger
Door
Cargo /
Baggage Door
Aft Equipment
Bay Door
Emergency Exit
Passenger Door
Overwing
Emergency Exit
Cargo/baggage
Door
91 x 178 cm
51 x 91 cm
109 x 84 cm
36 x 70 inch
20 x 36 inch
43 x 33 inch
Type I Exit
Type III Exit
P604_01_002
AIRPLANE GENERAL
1-8 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
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.
Passenger Door Operation
The door is closed from the 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)
• 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.
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CL_604-AIRPLANE_GENERAL(3)
