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incorporated into the polished aluminum wing leading edges. The attached winglets are made of
Kevlar, and significantly reduce drag.
Components
Fuel Tanks
The wing contains fuel in three areas. The right and left wings contain the main tanks (between
the spars), and the wing center section forms the auxiliary tank. A bulkhead on either side of the
wing center section separates the auxiliary and wing tanks.
Main Landing Gear
The main landing gear, mounted in the wings, are conventional oleopneumatic, shock-absorbing
struts, fitted with two wheels on each strut.
FUSELAGE
Description
The CL–605 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 radome incorporating dual landing lights, and which protects the radar antenna
pedestal on the front bulkhead; and
• The main battery, main battery chargers, and the AC to DC transformer rectifier units are
located behind the radar.
AIRPLANE GENERAL
General
Vol. 2 01−10−3
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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:
• The APU battery;
• APU battery charger;
• 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.
PRO LINE 21 DATA MANAGEMENT
Display data in Pro Line 21 cockpit is controlled using the display control panel (DCP) for the PFD
and the cursor control panel (CCP) for the MFD. General operation of the panels is as follows:
• Menu buttons (MENU, UPR MENU, LWR MENU, RDR MENU) provide direct access to
on-screen menus.
• Selection within these menus are made using MENU ADV/DATA/PUSH SELECT knobs.
• Memory buttons (MEM 1, 2, 3) store preferred MFD configurations for easy recall.
• The remainder of the buttons provide shortcuts to menus, EICAS functions, radio tuning and
radar control.
Detailed panel operations are covered in their respective systems chapters, where applicable.
AIRPLANE GENERAL
General
Vol. 2 01−10−4
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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
　
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