AIRPLANE GENERAL
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 01-02-01
INTRODUCTION
The Challenger 300 aircraft, manufactured by Bombardier Aerospace, is an all metal, pressurized, low-wing, turbofanpowered
monoplane. The high-aspect ratio, fully cantilevered, swept-back wings with winglets are of conventional riveted
construction except for the upper section of the winglets, which utilize full-depth honeycomb core bonded to the outer skin.
The fuselage is of semimonocoque construction and utilizes a constant circular cross-sectional shape fuselage.
Thrust is provided by two pod-mounted AS907 turbofan engines manufactured by Honeywell. Independent fuel systems
supply fuel to the engines with fuel storage provided in wing tanks. Engine-driven hydraulic pumps provide hydraulic power
for braking, extending or retracting the landing gear, nosewheel steering, wing flaps, spoilers, thrust reversers, elevator,
and rudder. The landing gear system is a fully retractable tricycle-type trailing link landing gear with dual main gear wheels,
nosewheel steering, and a brake-by-wire brake control/anti-skid braking system.
The ailerons are manually controlled, and the elevator and rudder are controlled via hydraulic actuators. An electrically
actuated trim tab is installed on the left aileron to provide lateral trim. Longitudinal trim is accomplished by changing the
incidence of the horizontal stabilizer with an electrically operated linear actuator. Rudder trim is accomplished via an electromechanical
actuator which moves the rudder surface independent of the rudder pedal position. Aircraft air-conditioning
systems which include an air-cycle machine, provide heating, cooling, and pressurization for the cockpit,
passenger compartment, and lavatory.
REV 1
AIRPLANE GENERAL
Volume 2 Flight Crew Operating Manual Sep 13/2004
01-02-02 CSP 100-6 REV 1
AIRCRAFT DIMENSION SCHEMATIC
CFO0101002_015
NOTES
Measurement at manufacturer
empty weight.
WING AREA
WING BASE
522 ft (48.5 m )
27.8 ft (8.5 m)
27°
25% CHORD LINE
10 ft 6 in
(3.20 m)
63 ft 10 in
(19.46 m)
3 ft 9 in
(1.14 m)
23 ft 9 in
(7.24 m)
13 ft 2 in
(4.01 m)
7 ft 8 in
(2.34 m)
28 ft 1 in
(8.56 m)
2 2
1
OTHER DIMENSIONS
12 ft
(3.66 m)
AIRPLANE GENERAL
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 01-02-03
AIRCRAFT DIMENSION SCHEMATIC (Cont)
CFO0101002_016
2 ft 6 in
(0.76 m)
4 ft 3 in
(1.3 m) 61 ft 1 in
(18.62 m) 68 ft 8 in
(20.92 m)
20 ft
(6.1 m)
23.7 ft
(7.7 m)
16.5 ft
(5.0 m)
28.6 ft
(8.7 m)
NOTES
Measurement at manufacturer
empty weight.
1
1
6 ft 3 in
(1.89 m)
REV 1
AIRPLANE GENERAL
Volume 2 Flight Crew Operating Manual Sep 13/2004
01-02-04 CSP 100-6 REV 1
AIRCRAFT DIMENSION SCHEMATIC (Cont)
CFO0101002_017
6.1 ft
(1.9 m)
5.1 ft
(1.6 m)
7.2 ft
(2.2 m)
PASSENGER COMPARTMENT
DIMENSIONS
LENGTH
WIDTH (FLOOR LINE)
WIDTH CENTERLINE
HEIGHT
VOLUME
FLOOR AREA
28 ft 7 in
5 ft 1 in
7 ft 2 in
6 ft 1 in
896 ft
146 ft
8.71 m
1.55 m
2.18 m
1.85 m
25.37 m
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