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GENERAL
General Airplane Description 01−10−1
Wing 01−10−3
Description 01−10−3
Components 01−10−3
Fuselage 01−10−3
Description 01−10−3
Components 01−10−3
Doors and Emergency Exit 01−10−5
Description 01−10−5
Components and Operation 01−10−5
EICAS Messages 01−10−14
Service Panels and Accesses 01−10−15
Airplane Antennas 01−10−16
Flight Compartment Controls and Indicators 01−10−16
Crew Seats 01−10−29
Description 01−10−29
Taxiing and Turning Radii 01−10−33
Hazard Areas 01−10−34
LIST OF ILLUSTRATIONS
GENERAL
Figure 01−10−1 Airplane Basic Dimensions 01−10−2
Figure 01−10−2 Doors and Emergency Exit − Location 01−10−5
Figure 01−10−3 Passenger Door 01−10−7
Figure 01−10−4 Cargo/Baggage Door 01−10−9
Figure 01−10−5 Aft Equipment Bay Door 01−10−11
Figure 01−10−6 Emergency Exit 01−10−13
Figure 01−10−7 Service Doors And Panels − Location 01−10−15
Figure 01−10−8 Airplane Antennas 01−10−16
Figure 01−10−9 General Arrangement 01−10−17
Figure 01−10−10 Overhead Panel 01−10−19
AIRPLANE GENERAL
Table of Contents
Vol. 2 01−00−1
REV 66, Feb 01/07
CHAPTER 1 - AIRPLANE GENERAL
01−00−1
CL−604 Operating Manual
PSP 604−6
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
LIST OF ILLUSTRATIONS
GENERAL
Figure 01−10−11 Centre Pedestal 01−10−21
Figure 01−10−12 Glareshield and Side Panels 01−10−23
Figure 01−10−13 Instrument Panels 01−10−25
Figure 01−10−14 Side Consoles 01−10−27
Figure 01−10−15 Seat/Harness Assembly 01−10−30
Figure 01−10−16 Eye Locator − Seat Adjustment 01−10−32
Figure 01−10−17 Taxiing and Turning Radii 01−10−33
Figure 01−10−18 Hazard Areas 01−10−34
AIRPLANE GENERAL
Table of Contents
Vol. 2 01−00−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
Page
GENERAL AIRPLANE DESCRIPTION
The Challenger 604 is a sweptwing, twin-engine monoplane, certified in accordance with FAR 25,
FAR 36 and their amendments. Maximum ramp and takeoff weights are 48,300 and 48,200 lb
respectively. The airplane is designed for two crew members with accommodation for up to 19
passengers, and is powered by two General Electric CF34-3B engines.
The following sections will be addressed:
• Wing
• Fuselage
• Doors and emergency exit
• Service panels and accesses
• Antennas
• Cockpit controls and indicators
• Crew seats and eye locator
• Taxiing and turning radii
• Hazard areas
AIRPLANE GENERAL
General
Vol. 2 01−10−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
GENERAL AIRPLANE DESCRIPTION (CONT'D)
Airplane Basic Dimensions
Figure 01−10−1
AIRPLANE GENERAL
General
Vol. 2 01−10−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
WING
Description
The wing is an all-metal, advanced-technology airfoil manufactured as a single unit and bolted to
the bottom of the fuselage. The wing incorporates ailerons, flaps, flight and ground spoilers,
internal fuel tanks and the support structure for the main landing gear. Thermal anti-icing is
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–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,
　
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