Operation (10Th Stage) - BOMBARDIER Challenger 601-3A CL-600-2B16 Pilot Training Manual

Pressure Indication
(10th Stage)
The bleed-air manifold pressure is sensed by
two transducers (one on each side of the iso-
lation valve) which transmit to the appropri-
ate needle on the dual-scale, dual-needle
indicator on the bleed-air control panel (Figure
9-1). The transmitters receive power from DC
bus 1 and DC bus 2, respectively.

OPERATION (10TH STAGE)

Figure 9-3 illustrates that the right engine is
operating and the right bleed-air shutoff valve
is open. The isolation valve is in its normally
closed position.
ATS
LH
ATS
VALVE
10TH STAGE
LEGEND
BLEED AIR
PORTS
BLEED AIR
Figure 9-3. Bleed-Air Supply—Right Engine Operating
9-4 CL 601-3A
EMER
PRESS SOV
DUCT
SENSOR
HEAT EXCHANGER
LH FOOT-WARMER
RH FOOT-WARMER
VALVE (STBY)
VALVE (NORM)
LH 10TH STAGE
BLEED-AIR
SOV
PRESSURE
XDUCER
LH ACU
VALVE
LEFT
EXT
ACU
AIR
FOR TRAINING PURPOSES ONLY
FlightSafety Canada
CL-600-2B16 PILOT TRAINING MANUAL
The right side of the bleed-air manifold is
pressurized, and pressure indication is avail-
able on the right scale of the bleed-air pres-
sure indicator. Bleed-air supply is available
from the right engine to the right ACU pres-
sure-regulating and shutoff valve and the right
footwarmer-demist shutoff valve.
The pressurization jet pump is supplied from up-
stream of the right engine bleed-air shutoff valve.
Both sides of the manifolds can be pressurized
from one engine by opening the isolation valve.
FAN
RAM AIR
PRESSURIZATION
JET PUMP
ATS VALVE
RH 10TH STAGE
BLEED-AIR
ISOL VALVE
SOV
PRESSURE
XDUCER
RH ACU
VALVE
RIGHT
ACU
LOAD
CONTROL
VALVE (LCV)
APU
L t é e
L t d .
DEMIST
CONTROL
KNOB
FOOTWARMER
CONTROL
KNOB
RH
ATS
10TH STAGE
BLEED AIR
PORTS