FUEL
QUANTITY
INDICATORS.
Empty
(2.
0 gallons unusable each tank) . . . · · · · E (red line)
TACHOMETER.
Normal Operating Range:
At
sea
level . . .
At
5000
feet . .
At
10,
000
feet . . .
Maximum Allowable
..
. 2200-
2500
RPM (inner green arc)
. . . . 2200-
2600
RPM (middle green arc)
. . 2200-2700 RPM (outer green arc)
. . . . . • . 2700 RPM (red line)
CARBURETOR
AIR
TEMPERATURE
GAGE (OPT).
Icing Range . . . . . . . . . . . . . -15° to 5°C (yellow arc)
WEIGHT
AND
BALANCE.
The following information will enable
you
to
operate
your Cessna
within the prescribed weight and center of gravity limitations.
To
figure
weight and .balance, use the Sample· Loading Problem,
Loa~g
Graph,
anq
.Center of Gravity Moment Envelope
as
follow~:
·
"Take the licensed empty weight and moment from appropriate
weight
and
balance records
carried
in your aircraft, and
write
them
down
in the
column
titled
YOUR
AIRPLANE
on
the Sample Loading Problem.
NOTE
The
licensed empty weight and moment
are
recorded
on
the Weight and Balance and Installed Equipment
Data sheet,
or
on
revised weight and balance
records,
and
are
included in the
aircraft
f
il~.
In
a~dition
to
the licensed empty weight and moment noted on these
records, the c.
g.
arm
(fuselage station)
is
also
shown,
but
need not .be used
on
the Sample Loading Problem.
·
The
momen.t which ·
is
shown must be divided
by
1000
and this
va~ue
used
as
the moment/1000 on the
loading problem.
.
Use
the Loading Graph
to
determine the moment/1000 for each addi- ·
tional iteiµ
to
}?e
car~ied,
then
li~t
these on the loading P!Oblem.
' .
4-4
. I
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