Cessna 150 - ENGINE INSTRUMENT MARKINGS.; WEIGHT AND BALANCE.

(
~ JGINE INSTRUMENT MARKINGS.
OIL TEMPERATURE GAGE.
Normal Operating Range
Maximum Allowable • .
OIL PRESSURE GAGE.
Minimum Idling . . . .
Normal Operating Range
Maximum ..•....
FUEL QUANTITY INDICATORS.
. , Gr · een Arc
225 oF Red Line
10 PSI (red line)
30-60 PSI (green arc)
. . 100 PSI (1•ed line)
Empty (1. 75 gallons unusable each standard tank) • E (red line)
(1. 50 gallons unusable each long range tank)
TACHOMETER.
Normal Operating Range:
At sea level .
At
5000 feet . .
At 10,000 feet •
Maximum
Allowable
WEIGHT AND BALANCE.
• 2000-2550 (inner green arc)
• 2000-2650 (middle green arc)
2000-2750 (outer green arc)
. . . . . . . 2750 (red line)
The following information will enable you to operate your Cessna
within the prescribed weight and center of gravity limitations. To figure
the weight and balance for your particular airplane, use the Sample Prob-
lem, Loading Graph, and Center of Gravity Moment Envelope as follows:
Tal~e the licensed Empty Weight and Moment/1000 from the Weight
and
Balance Data sheet, plus any changes noted on forms FAA-337,
~arried in your airplane, and write them down in the proper columns.
ling the Loading Graph, determine the moment/1000 of each item to be
a.rried. Total the weights and moments/1000 and use the Center of
Gravity Moment :Envelope to determine whether the point falls within the
envelope, and if the loading is acceptable,
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