canadair
ctiauentjer
OPERATING MANUAL
PSP 606
SECTION 1
AIRCRAFT - GENERAL
TABLE OF CONTENTS
Subject Page
MODEL DESIGNATION AND TYPE 1
OPERATING ROLE AND DESIGN CONCEPT 1
WING 1
IFUSELAGE 2
Nose Section
Centre Section
I Tail Section 3
AIRCRAFT DIMENSIONS 3
AIRCRAFT TURNING RADII 3 IDANGER AREAS 4
AIRCRAFT PARKING AND MOORING 4
SERVICING POINTS 4
AIRCRAFT ANTENNAS 4
DOORS 4
Passenger/Crew Upward Opening Door 5
Airstair
Passenger/Crew Downward Opening Door 6
Emergency Exit Door 6 I Baggage Compartment Door 7
Rear Equipment Bay Door
Service Doors
|FLIGHT COMPARTMENT 8
Instrument and Control Panels
Crew Seats
Cabin Sign Controls
cacnhaadllaeinr ger
OPERATING MANUAL
PSP 606
LIST OF ILLUSTRATIONS
Figure
Number Title Page
1 Aircraft General Details 9/10
2 Aircraft Basic Dimensions and Ground Clearances (2 sheets) 11
[3 Aircraft Turning Radii 13
4 Engine Intake and Exhaust Danger Areas 14
5 Aircraft Parking and Mooring 15/16
6 Aircraft Covers and Plugs 17/18
7 Aircraft Servicing Points 19/20
8 Aircraft Antenna Locations 21
9 Passenger/Crew Upward Opening Door (2 Sheets) 22
10 Passenger/Crew Downward Opening Door 24
111 Door Warning Indication (2 Sheets) 25
12 Baggage Compartment Door 27
13 Rear Equipment Bay Door 28
114 Service Doors and Panels 29
15 Flight Compartment Instrument and Control Panels (4 Sheets) 30
116 Crew Seats (2 Sheets) 35
J17 Cabin Sign Control Switches 37
1 - CONTENTS
Page 2
Mar 01/85
cacnhaadllaeinr ger
OPERATING MANUAL
PSP 606
SECTION 1
AIRCRAFT - GENERAL
MODEL DESIGNATION AND TYPE
The aircraft, manufactured by Canadair Limited, is designated Model CL-600 and
named Challenger. The Challenger is a swept-wing monoplane powered by two Avco
Lycoming ALF 502L-2 Turbofan engines.
OPERATING ROLE AND DESIGN CONCEPT
Primarily, the Challenger is a long-range (transcontinental) business aircraft
with a crew of two. The design concept is orientated toward carrying up to 19
passengers in spacious comfort oyer long distances. The combination of an
advanced technology supercritical wing, quiet and efficient engines, and a wide
body enables the Challenger to achieve a high standard of performance, economy
and passenger comfort.
WING (Figure 1)
The aircraft wing is an advanced technology symmetrical airfoil structure
manufactured as a single unit and bolted to the underside of the fuselage. The
wing comprises left and right swept-back airfoils connected by a central box
structure, and consists of skinned spars and ribs. Ailerons, flaps, spoilers,
integral fuel tanks and the support structure of the main landing gear are
incorporated into the wing. Wing leading edges are of aluminum alloy and
incorporate thermal anti-icing. Wing tips are of Kevlar to save weight and to
facilitate repair. On aircraft incorporating Canadair Service Bulletin
600-0401, the wing leading edge tapers toward a winglet. Each winglet is
constructed from aluminum alloy with a Kevlar leading edge.
Fuel for the aircraft is stored in three tank areas. The deep section airfoil
each side is used as a main tank and the centre section is used as an auxiliary
tank. A fuel-tight bulkhead each side of the centre section separates the
tanks, and all tanks are compartmented to ensure a continuous supply of fuel to
the engines under all normal flight conditions. On aircraft so modified,
additional auxiliary tanks are installed, one forward and one aft of the main
auxiliary tank.
The main landing gear (MLG) assemblies, mounted under the wing left and right
airfoils inboard of the trailing edge flaps, are conventional oleo-pneumatic,
shock-absorbing struts, each fitted with two wheels. The MLG retracts inward
into bins in a well in the underside of the fuselage.
SECTION 1
Page 1
Mar 01/85
canatiair
ctianenQer
OPERATING MANUAL
PSP 606
FUSELAGE (Figure 1)
The fuselage is an all-metal, semi-monocoque structure comprising nose, centre
and tail sections riveted together. The fuselage consists of externally
skinned frames, stringers and longerons. The nose section is mainly the flight
compartment area, the centre section is the passenger cabin area and avionics
bay under which the wing is bolted, and the tail section is mainly an equipment
bay to which the engines and empennage are attached.
A. Nose Section
The nose section is effectively divided by the flight compartment floor into
upper and lower halves. The upper half comprises the flight compartment and
　
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