BOMBARDIER Challenger 601-3A CL-600-2B16 Pilot Training Manual page 117

ANNUNCIATOR
FLT CONT
FUEL
4-8 CL 601-3A/R
Table 4-1. CAUTION ANNUNCIATORS (Cont)
ASSOCIATED
ANNUNCIATOR
CHAN 1
INOP
CHAN 2
INOP
OVSP
CHANGE
CHAN
MACH
TRIM
OFF
ROLL
MON
SAFE
PITCH
YAW
FLAPS
FAIL
OVHT
MOT 1
OVHT
MOT 2
SPLR
INOP
SCAV
MAIN
ON
INOP
VALVE
CLOSED
FILTER
LOW
PRESS
NOT
ARMED
SEC
TRANS
FOR TRAINING PURPOSES ONLY
FlightSafety Canada
CL-600-2B16 PILOT TRAINING MANUAL
CAUSE FOR ILLUMINATION
Indicated pitch trim channel has failed.
Pitch trim has overspeed failure; and the
channel 1 brake has been applied.
Mach trim is not engaged.
The aileron PCU control valve has jammed or
one hydraulic system is unpressurized.
The elevator PCU control valve has jammed.
The rudder PCU has jammed, or one hydraulic
system is unpressurized.
The flaps have failed.
Indicated flap motor has overheated.
The ground spoiler is inoperative.
Indicated scavenge ejector fuel pump
is inoperative.
Indicated main ejector fuel pump is inoperative.
Indicated standby electric pump is inoperative.
Indicated engine fuel filter is clogged.
Indicated engine fuel pump inlet pressure is low.
Tail tank system not armed for auto transfer.
Tail tank system has switched to secondary
transfer (included on AC5135 and subsequent
incorporating SB 601-0355).
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