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GYRO FAST ERECT
SWITCH/LIGHT"
RIGHT ENGINE RRE WARNING LIGHT
/EXTINGUISHER ARM SWITCH
FLIGHT DIRECTOR SELECTION.
AND ANNUNCIATOR PANEL
AUTOMATIC FLIGHT CONTROL _
SYSTEM DISENGAGE SWITCH
AUTOPILOT FAIL INDICATORS—N
SPS TEST INDICATORAUDIO
CONTROL PANEL -
LIGHTING CONTROL PANEL -
AIR OUTLET -
LEFT ENGINE REVERSE THRUST
SYSTEM UNLOCKED INDICATOR
LEFT ENGINE REVERSE THRUST SYSTEM EMERGENCY STOW PUSH- BUTTON
RIGHT ENGINE REVERSE THRUST SYSTEM EMERGENCY STOW PUSH- BUTTON
CO-PILOTS
COMPLEMENT OF FLIGHT
• INSTRUMENTS AS PER
THOSE OF PILOT
STALL
WARNING
TEST PANEL
NOSE WHEEL
STEERING ARM •
SWITCH
WARNING AND
FLOODUGHT
SWITCHES
CABIN ALTITUDE AND PRESSURE
' DIFFERENCE/RATE OF CLIMB
WINDOW DEMIST
"CONTROL KNOB
WARNING AND
-FLOODLIGHTS
SWITCHES
.STALL WARNING
TEST PANEL
FOOT WARMER
V CONTROL KNOB
OXYGEN MASK.
LOCATION
PANOSE WHEEL
I 2 j STEER .
• FAIL LIGHT
VERTICAL NAVIGATION.
COMPUTER/CONTROLLER
OXYGEN MASKLOCATION
Flight Compartment Instrument and
Control Panels
Figure 15 (Sheet 2)
SECTION 1
Page 31/32
f4ar 01/85
canatiair
cfiawenger
AC POWER MANAGEMENT PANEL .
THROTTLE SAFETY
LOCKS
PITCH DISCONNECT MECHANISM
OPERATING HANDLE
OPERATING MANUAL
PSP 606
AC METERING PANEL
/
SPOILER OPERATING LEVER —^-
SPOILERS WARNING LIGHT
DOOR WARNING LIGHTS
AND CABIN SIGNS SWITCH ,
PANEL
ENGINE RELIGHT SWITCH
NAV 2/COMM 2
CONTROL PANEL"
DC METERING PANEL
DC POWER MANAGEMENT PANEL
ROLL DISCONNECT MECHANISM
OPERATING HANDLE
THROTTLE QUADRANT
FLAP OPERATING LEVER
REVERSE THRUST AR'/:
LIGHTS AND SWITCHES
LANDING AND TAXI LIGHTS
'CONTROL PANEL
^COMM 1 CONTROL PANEL
NAV 1 CONTROL PANEL
TRANSPONDER CONTRC
" PANEL
REMOTE COURSE
SELECTOR PANEL
ADF CONTROL PANEL
TRIM CONTROL PANEL
LIGHTING CONTROL PANEL
WARNING LIGHT TEST PANEL
SERVO MONITOR AND
STABILITY AUGMENTATION
PANEL
AIR DRIVEN GENERATOR
CONTROL PANEL
AIR DRIVEN GENERATOR (ADG)
MANUAL DEPLOY ASSEMBLY
LANDING GEAR
MANUAL RELEASE
HANDLE
Flight Compartment Instrument and
Control Panels
Figure 15 (Sheet 3)
SECTION 1
Page 33
Mar 01/85
cacnhaatiiiaeinr Qer
OPERATING MANUAL
PSP 606
HYDRAULIC SYSTEMS
CONTROL PANEL
ENGINE IGNITION. ENGINE
START AND ELECTRICAL
POWER PANELS
AUXILIARY
POWER UNIT
(APU) CONTROL
PANEL
CABIN
PRESSURIZATION
CONTROL PANEL
LIGHTING
CONTROL
PANEL
ENGINE
BLEED AIR
CONTROL
PANEL
ANTUCE SYSTEM
CONTROL PANE f[0
\
AlP DATA SENSOR
M£ ATI R CONTROL
PANEL
PI LOT'S EYE LOCATOR
WINDSHIELD CENTRE POST EFFECTIVITY
FT} AIRCRAFT INCORPORATING
^ ^ SB 600-0495. FOR OTHER
A/C, REFER TO SECTION 14.
Flight Compartment Instrument and
Control Panels
Figure 15 (Sheet 4)
SECTION 1
Page 34
Feb 12/88
canadair
chanenQer
OPERATING MANUAL
PSP 606
QUICK-RELEASE BUCKLE
Front of buckle can be turned to simultaneously
release shoulder straps, crotch strap and one part of
lap belt; buckle remains attached to other part of lap
belt. Snap-in attachments are incorporated at strap
ends so that safety harness can be easily connected.
SHOULDER STRAPS
LAP BELT.
LUMBAR SUPPORT
ARMREST CONTROL BUTTON
Releases armrest lock to allow angular adjustment
of armrests.
RECLINE CONTROL LEVER
Releases seatback lock to allow adjustment
from upright to recline. Seatback locks in
position when lever is released.
LUMBAR SUPPORT CONTROL VALVE
Releases air from lumbar support to suit contour of
pilot's back.
With pilot's back pressed against support, opening
valve allows support to match contour of pilot's back,
and closing valve allows support to maintain selected
shape. With no pressure on support, opening valve
allows support to return to original shape.
HEIGHT CONTROL LEVER
Releases height lock to allow vertical adjustment
of seat. Seat locks in selected position
when lever is released. NOTE
Pilot's seat shown, copilot's seat identical but opposite.
Crew Seats
Figure 16 (Sheet 1)
SECTION 1
Page 35
Mar 01/85
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Bombardier-Challenger_00-Aircraft_General(7)
