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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; and
• 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.
AIRPLANE GENERAL
General
Vol. 2 01−10−3
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
FUSELAGE (CONT'D)
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; and
• Aft underfloor pressurized area.
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
General
Vol. 2 01−10−4
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
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.
Doors and Emergency Exit − Location
Figure 01−10−2
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 fitting to raise the door.
AIRPLANE GENERAL
General
Vol. 2 01−10−5
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
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, foreward 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.
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
　
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