switches are not on. It is ONLY the taxi light
circuit that is routed through the main gear
down and locked switches.
Landing Gear Warning/Caution
System
The landing gear warning/caution system pro-
vides inputs to the CWP and EICAS (Table 14-
1) which activate voice and visual warnings
whenever a landing is attempted and any of the
gear are not down and locked; or, if airspeed
is excessive while the gear is in transition, or
if either main gear inboard door is not closed.
The conditions that activate gear warning and
the indications for gear warning are listed in
Table 14-2 and illustrated in Figure 14-3.
A landing gear caution is activated to alert the
crew of an unsafe gear configuration in the
event of an invalid radio altimeter, or if gear
limit speeds are exceeded while the gear is
in transition or either main gear door is not
up and locked. The conditions that activate
gear caution and the indications are listed in
Table 14-2.
For gear cautions, the master CAUT lights
may be extinguished by depressing either mas-
ter caution light, however, the amber “GEAR”
CAS message remains in view as long as the
condition exists.
For gear warnings, the WARN lights may be
extinguished by depressing either master warn-
ing light, however, the red GEAR CAS mes-
14-5
FOR TRAINING PURPOSES ONLY
LEARJET 45 PILOT TRAINING MANUAL
FlightSafety
international
LEARJET 45 PILOT TRAINING MANUAL
FlightSafety
international
GEAR, . . ." (W)
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