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for the baggage compartment door, with the exception that the rear
equipment bay door must be supported during opening because of opening
direction.
Service Doors (Figure 14)
Quick-release service doors and panels are provided for easy access to the
servicing points throughout the aircraft.
SECTION 1
Page 7
Jun 12/86
cftaHencjer
OPERATING MANUAL
PSP 606
12. FLIGHT COMPARTMENT
The flight compartment contains the aircraft instrument, warning light, control
and circuit breaker panels, two crew seats and the flight control columns,
wheels and pedals. The compartment structure incorporates the windshield,
including a pilot's eye locator to enable seat adjustment for optimum field of
vision.
Miscellaneous items in the flight compartment include a portable fire
extinguisher, located behind the copilot's seat on the bulkhead that separates
the flight and passenger compartments, two oxygen masks, two cup holders, and
storage boxes and pouches for checklists, etc.
A. Instrument and Control Panels (Figure 15)
Details of panels, controls, switches, lights and instruments are given in
the appropriate sections of this manual.
B. Crew Seats (Figure 16)
The pilot's and copilot's seats are identical except that certain controls
are installed on opposite sides; on both seats, inertia reel and forward/
rearward controls are located inboard, and lumbar support, height and
rreevc, li iinni nnigg lcuorniitrruoilds aarrce lloucuaatiecdu oi utboard.
C. Cabin Sign Controls (Figure 17)
The NO SMOKING and FASTEN SEAT BELT signs in the passenger cabin are
controlled manually or automatically through switches located on the centre
pedestal.
SECTION 1
Page 8
Mar 01/85
OPERATING MANUAL
PSP 606
VERTICAL STABIUZER/REAR FUSELAGE FRAME STRUCTURE
HORIZONTAL
STABILIZER
PRESSURIZED PASSENGER
COMPARTMENT
(FUSELAGE CENTRE SECTION)
PILOTSBULKHEAD
FLIGHT COMPARTMENT
ENGINE COWLINGS
FORWARD AVIONICS
BAY (UNPRESSURIZED)
RADOME
FLIGHT COMPARTMENT FLOOR
ADG COMPARTMENT
HYDRAULICALLY
OPERATED NOSE
GEAR DOORS
WINGLET
NOSE LANDING GEAR REMOVABLE LEADING EDGES
Aircraft General Details
Figure 1
SECTION 1
Page 9/10
Feb 12/88
canadair
chanenQer
OPERATING MANUAL
PSP 606
19 ft 2 in
7 ft Oin
1 _ Pain
[—10 ft Bin—1
-61 ft 10 in k
5 ft 0 in
L_
8 ft 10 in
26 ft 6 in
}T CABIN INTERIOR DIMENSIONS _|
Length
Width (maxdia)
I Headroom (floor to
Volume
Floor Area
I Floor Width
max height)
28 ft 3 in I
8 ft 2 in
6 ft 1 in
1150 cu ft
202.5 sq ft
7 ft 2 in ]
EFFECTIVITY: Aircraft not incorporating SB 600-0401
-3ft Oin
5 ft 6 in
0 D D 0 D C
•60ft Oin
-68 ft 5 in
STATIC GROUND LINE
20 ft 4 in
20 ft 8 in
Aircraft Basic Dimensions
and Ground Clearances
Figure 2 (Sheet 1)
SECTION 1
Page 11
Feb 12/88
canaaair
chatiencjer
OPERATING MANUAL
PSP 606
Aircraft Basic Dimensions
and Ground Clearances
Figure 2 (Sheet 2)
20 ft 4 in
20 ft 8 in
SECTION 1
Page 12
Feb 12/88
canadair
chanencjer
OPERATING MANUAL
PSP 606
61 FT. MINIMUM TAXI STRIP
WIDTH FOR 180 DEGREE TURN
NOTES
* ' •. S3 ti for aircraft with winglets.
/7'\ y* •: for aircraft with winglets.
3 L»M«f steering angles require
taxi strip for 180° turn.
MINIMUM TURNING RADII WITH NOSE WHEEL
AT 90° (AIRCRAFT MAXIMUM TOWING ANGLE)
Aircraft Turning Radii
Figure 3-
SECTION 1
Page 13
Mar 01/85
canadair
chaiienqer
OPERATING MANUAL
PSP 606
IDLE
THRUST
0 T
10 4
20 4
30 4
150 FT/SEC
(102 MPH)
100FT/SEC
40 4 (68 MPH)
50FT4
60
70 4
80 4
90 4
100 FT f 35 FT/SEC
(24 MPH)
110
120
130 +
140 +
150 FT -L
350 FT/SEC
(238 MPH)
4 10
4 20
+ 30
4 40
T 50 FT
200 FT/SEC 4 60
(136 MPH)
4 70
4 80
4 90
- 4 100 FT
-f 110
j l S g p ] 38<>C
MAXIMUM! (100°F)
THRUST
50 FT/SEC
(34 MPH)
+ 120
+ 130
+ 140
-1-150 FT
18 FT
Engine Intake and Exhaust Danger Areas
Figure 4
SECTION 1
Page 14
Feb 12/88
cacnhaadiiaeinr cte_r _
OPERATING MANUAL
　
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