BOMBARDIER Challenger 601-3A CL-600-2B16 Pilot Training Manual page 317

LEGEND
COLD AIR
CABIN CONDITIONED AIR
COCKPIT CONDITIONED AIR
CABIN AIR EXHAUST—
VENTED UNDERFLOOR
ACU'S AND RAM AIR
UNDERFLOOR
AVIONICS BAY
INSTRUMENT
COOLING
SIDE PANEL
VENT
FOOTWARMER
electors are set at the desired position. Pushing
t h e A P U B L E E D
(Figure 11-4) will cause the APU surge valve
to close and, at the same time, the APU load
control valve (LCV) to open (the OPEN light
will illuminate) and pressurize the left side of
the bleed-air manifold. This can be verified by
checking the left pressure indicator on the
bleed-air panel. Pressure will be approxi-
mately 50 psi. APU bleed air can be supplied
to the right side of the bleed-air manifold by
pushing the ISOL switchlight. The green
OPEN light will illuminate and the right pres-
sure indicator will also read approximately
50 psi.
LEFT ACU SUPPLIES:
RIGHT ACU SUPPLIES:
SIDE CONSOLE VENT
DEMIST
Figure 11-3. Air-Conditioning Distribution
A I R s w i t c h l i g h t
FOR TRAINING PURPOSES ONLY
FlightSafety Canada
CL-600-2B16 PILOT TRAINING MANUAL
COLD AIR FOR CABIN
CONDITIONED AIR FOR
CABIN AND COCKPIT
COLD AIR FOR CABIN
AND COCKPIT
CONDITIONED AIR FOR
CABIN
BLEED ADPTR
AIR OIL
LO
FAILED
PRESS
HI
OPEN
TEMP
PUSH
A
P
%RPM
U
100
80
60 20
40
Figure 11-4. APU Control Panel
RAM-AIR
EXHAUST
RAM-AIR SCOOP
PWR FUEL APU START/
ON/OFF OIL STOP
SOV LO
STARTER
CLOSED PRESS
PUMP HI APU
INOP TEMP READY
PUSH PUSH
10 EGT
°C X 100
8
0
0
6
2
4
CL 601-3A 11-5
L t é e
L t d .
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