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Learjet 60 - Fuel; Fuel Indicator; Fuel Quantity Probes

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Learjet60'
Pilot's
Manual
FUEL
GAGING
SYSTEM
The
fuel
gaging
system
consist
of
a
fuel
quantity
indicator
installed
in
the
cockpit,
fuel
quantity
probes
located in the
various
fuel
tanks,
and
an
optional
total
quantity
indicator
located
near
the
single
point
pres-
sure
refueling controls
.
The
fuel
gaging
system
operates
on
28
VDC
supplied
through
the
2-amp
FUEL
QTY
PWR
1
and
FUEL
QTY
PWR
2
circuit
breakers
an
the
pilot's
and
copilot's circuit
breaker
panels
.
The
fuel
gaging system
is
operative
during
EMER
BUS
mode
.
FUEL
QUANTITY
INDICATOR
The
fuel
quantity
indicator,
on
the
instrument
panel,
indicates fuel
quantity
in
pounds
(or
optionally
kilograms)
of
fuel
.
The
indicator
has
four
digital
readouts
-
one
for
the
left
wing
tank,
one
for
the
right
wing
tank,
one
for the fuselage
tank,
and
one
which
shows
the
total
of
e
other three
summed
together
.
On
aircraft
60-159
and
subsequent
and
prior
aircraft
modified
by
SB
60-28-10
(Installation
of
Improved
Fuel
Quanti-
ty
Indicator),
inputs
from
the
attitude
heading
reference
system
are
used
to
correct
the
fuel
quantity
indication
for
aircraft
pitch
attitude
.
The
in-
dicator
incorporates
a
feature to
alert
the
crew
of
a
fuel
imbalance
be-
een
the
left
and
right
wing
tanks
.
Should
a
fuel
imbalance
of
500
pounds,
(200
pounds
if
flaps
are or
lower)
or
more
occur,
the
fuel
quantity
reading
representing
the
heavy wing
and
the
IMB
annuncia-
tor,
on
the
fuel
quantity
indicator,
will flash
.
The
flashing
annunciations
may
be
cancelled
by
depressing
and
releasing
the
mute
switch
in
the
right
thrust
lever
.
FUEL
QUANTITY
PROBES
Fuel
quantity
is
sensed
by
four
capacitance-type
fuel
quantity
probes
in
each
wing
tank
and a
capacitance-type
fuel
quantity
probe
in
the
fuse-
lage
fuel
tank
.
The
left
inboard
fuel
quantity
probe
incorporates
a
fuel
temperature
compensater
which
compensates
for
fuel
density
changes
due
to
temperature
.
TOTAL
QUANTITY
INDICATOR
(SPPR)
The
optional
total
quantity
indicator,
located
with
the
single
point
pres-
sure refueling
controls,
indicates
total
fuel
quantity
in
pounds
of
fuel
.
The
system
may
also
be
configured
to
indicate
kilograms
of fuel
.
The
indicator
has
a
digital
readout
which
repeats
the
total
indication
shown
on
the
cockpit
indicator
.
Refueling personnel
can use
the
indicator
to
determine
the
total
fuel
load
without
reference
to
the
cockpit
indicator
.
PM-123
2-35
Change
4

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