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OIL PRESSURE GAGE.
Idling Pressure
Normal Operating Range
Maximum Pressure
FUEL QUANTITY INDICATORS.
Empty
.
(2.5 gallons unusable each tank in normal flight maneuvers
with fuel selector valve on "BOTH.
CYLINDER HEAD TEMPERATURE GAGE.
Normal Operating Range
Do Not Exceed .
TACHOMETER.
Normal Operating Range
Do Not Exceed (Engine rated speed)
MANIFOLD PRESSURE GAGE.
Normal Operating Range
CARBURETOR AIR TEMPERATURE
Icing Range
SUCTION GAGE (GYRO SYSTEM).
Normal Operating Range
WEIGHT AND BALANCE.
The following information will enable you to operate your C essna
within the prescribed weight and center of gravity limitations.
weight and balance, use the Sample Loading Problem, Loading Graph,
and C enter of Gravity Moment En velope as follows:
Take the licensed empty weight and moment from appropriate weight
and balance records carried in your airplane, and write them down in the
column titled "YOUR AIRPLANE" on the Sample Loading Problem.
The licensed empty weight and moment are recorded on the
Weight and Balance and Installed Equipment Data sheet, or
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GAGE (OPT).
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NOTE
10 psi (red line)
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30-60 psi (green arc)
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100 psi (red line)
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200 -460°F (green arc)
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460°F (red line)
RPM ( gre en arc )
220 0-2 450
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.2600 RPM (red line)
.15-23 in. Hg (green arc)
-15" to 5°C (yellow arc)
4.6- 5. 4 in. Hg (green arc)
E ( red
line)
To figure
4- 3
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