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Learjet 60 - Fuel Control Panel Switches and Annunciators; JET PUMP Switches; STBY PUMP Switches; XFLO VALVE Switch

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Learjet
60
Pilot's
Manual
FUEL
CONTROL
PANEL
SWITCHES
AND
ANNUNCIATORS
The
fuel
control
panel
(Figure
2-7)
incorporates
all
the
necessary
switches
to fuel
the
aircraft
(when
using
the
over-the-wing
method)
and
to
maintain
proper
fuel
management
.
JET
PUMP
SWITCHES
The
JET
PUMP
switches,
on
the
fuel
control
panel,
control
the
motive
flow
valves
.
The
switches
are
an
alternate
action
type
.
Selecting
On,
opens
the
corresponding motive
flow
valve
and
allows
high-pressure
fuel
from
the
corresponding
engine-driven
fuel
pump
to
flow
to the
corresponding
jet
pumps
.
Selecting
OFF,
closes
the
corresponding
mo-
tive
flow
valve
and
renders
the
associated
jet
pumps
inoperative
.
When
OFF
is
selected,
an
OFF
annunciation
(on
the switch)
will
illuminate
and
the
Master
CAUT
lights
will flash
(Master
CAUT
will
not
illumi-
nate
during
engine
start)
.
If
a
motive
flow
valve
is
neither
open
nor
closed,
the
corresponding
OFF
annunciator
will flash
.
The
motive
flow
valves
operate
on
28
VDC
supplied
through
the
5-amp
L
and
R
JET
PUMP-XFR
VALVE
circuit
breakers
on
the
pilot's
and
copilot's
circuit
breaker
panels
.
Loss
of
power
to
the
motive
flow
valve
causes
the
valve
to
remain
in
its
last
position
.
Motive
flow
valves
are
operative
during
EMER
BUS
mode
.
STBY
PUMP
SWITCHES
The
STBY
PUMP
switches,
on
the
fuel
control
panel,
control
the
opera-
tion
of the
standby
electric
pumps
.
The
switches
are
an
alternate
action
type
.
The
switches
normally remain
Off
except
in
the
event
of
a
jet
pump
failure
or
during
fuel
crossflow
.
Regardless
of
switch
position,
the
standby
pumps
are
automatically
de-energized
during
fuselage
fuel transfer
operations
.
The
standby
pumps
are
automatically
ener-
gized
when
the
fuselage
tank
FILL
function
is
selected
or
the
START-
GEN
switch
is
set
to
START
.
An
ON
annunciation
(on
the switch)
will
illuminate
whenever
power
is
applied
to the
corresponding
standby
pump
.
The
green
FUEL
SYS
light,
on
the glareshield
annunciator
panel,
will
also
illuminate
whenever
a
standby
pump
is
on
.
The
standby
pumps
operate
on
28
VDC
supplied
through
the
15-amp
L
and
R
STBY
SCAV
PUMP
circuit
breakers
on
the
pilot's
and
copilot's
circuit
breaker
panels
.
XFLO
VALVE
SWITCH
The
XFLOVALVE
switch,
on
the
fuel
control
panel,
controls
the
crossflow
valve
.
The
switch
is
an
alternate
action
type
.
Selecting
PM-123
2-29
Change
5

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