Cessna 402B 1973 - Page 47

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TEMPEFIATURE
-
DEG.
F,
{€sranoeno
CONDITIONS
1. Propeller
Controls
f\ll High
nPM
-
F\rlI
Low Pitch
2. Manifold
Pressure
Adjusted
to
Obtain
Proper
RPM
'
1600
2000
2400
PROPELLEFI
SPEED
-
RPM
TEMPERATURE
EXAMPLE A. Temperature
-
80"F.
B.
Pressure
Altitude
-
4000 ft.
C.
Airspeed -
100
MPH
IAS.
D.
Propeller
Speed -
1880
RPM.