Cessna Skylane 182T User Manual

CESSNA
SECTION
7
MODEL
182T
NAV
III
AIRPLANE
AND
SYSTEM
DESCRIPTION
GFC
700
AFCS
FUEL
SYSTEM
(Continued)
FUEL
INDICATING
SYSTEM
(Continued)
Fuel
flow
is
measured
by
use
of
a
turbine
type
transducer
mounted
on
the
centerline
of
the
engine
between
the
fuel/air
control
unit
and
the
fuel
distribution
unit.
This
flow
meter
produces
a
signal
that
is
displayed
as
the
rate
of
fuel
flow
on
the
FFLOW
GPH
indicator
on
the
EIS
pages.
FFLOW
GPH
is
shown
as
either
a
horizontal
analog
indicator
or
a
digital
value,
depending
on
the
active
EIS
page.
FUEL CALCULATIONS
NOTE
Fuel
calculations
do
not
use
the
airplane’s
fuel
quantity
indicators
and
are
calculated
from
the
last
time
the
fuel
was
reset.
For fuel consumption information, a fuel used totalizer function is
provided
on
the
EIS
SYSTEM
page
as
GAL
USED.
This
digital
indicator
shows
total
fuel
used
since
last
reset
of
the
totalizer.
To
reset
the
GAL
USED,
the
EIS
SYSTEM
page
must
be
active
and
the
RST
USED
softkey
must
be
selected.
GAL
USED
is
calculated
after
reset
using
information
from
the
fuel
flow
transducer
signal.
For
fuel
remaining
information,
a
count
down
fuel
totalizer
function
is
provided
on
the
EIS
System
page
as
GAL
REM.
This
digital
indicator
shows
calculated
fuel
remaining
since
last
GAL
REM
pilot
adjustment.
To
adjust
GAL
REM,
the
EIS
SYSTEM
page must
be
active
and
the
[GAL
REM
softkey
must
be
selected
followed
by
the
appropriate
quantity
adjustment
softkeys,
Refer
to
the
Garmin
G1000
CRG
for
details
for
resetting
and
adjusting
fuel
calculations.
GAL
REM
is
calculated
after
pilot
adjustment
using
information
from
the
fuel
flow
transducer
signal.
NOTE
GAL
USED
and
GAL
REM
provide
no
indication
of
the
actual
amount
of
fuel
remaining
in
each
tank
and
should
only
be
used
in
conjunction
with
other
fuel
management
procedures
to
estimate
total
fuel
remaining.
(Continued Next Page)
1482TPHBUS-01
U.S.
7-45

Cessna Skylane 182T Specifications

General

Manufacturer	Cessna
Model	Skylane 182T
Type	Single-engine piston
Engine	Lycoming IO-540-AB1A5
Horsepower	230 hp
Maximum Takeoff Weight	3, 100 lb (1, 406 kg)
Wingspan	36 ft (11.0 m)
Length	29 ft (8.8 m)
Seating Capacity	4
Category	Aircraft
Maximum Speed	148 knots
Stall Speed (with flaps)	49 knots
Rate of Climb	924 feet per minute
Empty Weight	1, 970 pounds
Fuel Capacity	87 gallons
Height	9 feet 4 inches
Maximum Cruise Speed	145 knots
Service Ceiling	18, 100 feet