BOMBARDIER Challenger 601-3A CL-600-2B16 Pilot Training Manual page 115

ANNUNCIATOR
ENV CONT
HYD
AUTO CB FAIL
ANTI-SKID
MLG BAY
OVHT FAIL
NAV
4-6 CL 601-3A/R
Table 4-1. CAUTION ANNUNCIATORS (Cont)
ASSOCIATED
ANNUNCIATOR
CABIN
PRESS LOW
AUTO
FAULT
OFF OFF
FAIL FAIL
HI
TEMP
ELEC
PUMP
L ENG
PUMP
R ENG
PUMP
INBD OUTBD
FAIL FAIL
INBD OUTBD
TEST TEST
OVHT
WARN
FAIL
DGRAD
ALIGN FAULT
NAV RDY NO AIR
ON BATT BATT FAIL
IRS IRS IRS
1 2 3
COMP
MON
FOR TRAINING PURPOSES ONLY
FlightSafety Canada
CL-600-2B16 PILOT TRAINING MANUAL
CAUSE FOR ILLUMINATION
Cabin pressurization has failed.
The pressurization controller has failed.
Indicated air-conditioning unit has been shut
down automatically.
Hydraulic system 1, 2, or 3 overtemped.
Indicated hydraulic system electric pump pressure is
below 1,800 psi with the flaps selected or pump
pressure is below 1,800 psi with switch selected ON.
Indicates hydraulic No. 1 system pressure
is below 1,800 psi.
Indicates hydraulic No. 2 system pressure
is below 1,800 psi.
An electronic circuit-breaker channel has failed.
Indicated antiskid system has failed.
The main landing gear bay overheat detection
system has failed.
DGRAD—Accuracy of display data cannot
be guaranteed.
FAULT—Fault has occurred in the IRS system.
ON BATT—IRS is powered by backup battery.
BATT FAIL—Battery voltage less than required
for IRS operation.
IRS 1,2, 3—IRS backup battery charger
has failed.
COMP MON—There is a difference between
pilot's and copilot's ATT, LOC, GS or IAS.
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