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Learjet 60 - Page 90

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Pilot's
Manual
Learjet
60
Landing
gear
extension
cycle
:
When
the
LANDING
GEAR
switch
is
placed
in the
DN
position
the
following
sequence
of events
will
occur
:
1
.
28
VDC
will
be
applied
to
the
"open"
solenoid
of the
door
selec-
tor
valve
and
hydraulic
pressure
will
be
applied
to
both
inboard
main
gear
door
uplock
actuators
and door
actuators
.
2
.
When
the
main
gear
doors open,
door
open
switches
will
com-
plete
a
circuit
from
the
LANDING
GEAR
switch
to the
"down"
solenoid
of
the
gear
selector
valve
.
Hydraulic
pressure
will
be
applied
to
the
main
and
nose
gear
actuators
and
the
gear
will ex-
tend
.
3
.
When
the
main
gear
are
full
down,
gear
down
switches
will
complete
a
circuit
from
the
LANDING
GEAR
switch
to
the
"close"
solenoid
of the
door
selector
valve
.
Hydraulic
pressure
will
be
applied
to
the
inboard
main
gear
door
actuators
to
raise
the
gear
doors
.
Additionally,
a
gear
down
safety
switch
will
complete
a
circuit
to
the
"down"
solenoid
of
the
gear
selector
valve
to
maintain continuous
hydraulic
pressure
in
the
gear
ac-
tuators
.
3-8
4
.
The
gear
doors
are
latched
by
uplatch
actuator
spring
tension
.
PM-123
Original

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