Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 20

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SECTION 2
LIMITATIONS
CESSNA
MODELT210M
Propeller Manufacturer: McCauley Accessory Division.
Propeller Model Number:
D3A34C402/90DFA-10.
Propeller Diameter, Maximum: 80 inches.
Minimum: 78.5 inches.
Propeller Blade Angle at 30 Inch
Station,
Low: 12.4°.
High: 28.5°.
Propeller Operating Limits: Avoid continuous operation between 1850
and 2150 RPM above 24 inches manifold
pressure.
POWER PLANT INSTRUMENT MARKINGS
Power plant instrument markings and their color code significance
are shown in figure 2-3.
RED LINE
GREEN ARC
YELLOW ARC WHITE ARC
RED LINE
INSTRUMENT
MINIMUM
NORMAL
CAUTION
NORMAL
MAXIMUM
LIMIT
OPERATING
RANGE
CLIMB
LIMIT
RANGE
Tachometer
-
-
-
2200 -
2600 -
-
-
-
2700 RPM
2500 RPM
2700 RPM
Manifold Pressure
-
- -
15 - 30
35 - 36.5
- - -
36.5 in. Hg
in. Hg
in. Hg
Oil Temperature
-
-
-
100° - 240°F
- - -
- - -
240°F
Cylinder Head
-
- -
200°
-
460°F
- - -
- - -
460°F
Temperature
Fuel Flow
(3.0 psi)
36 - 120
- - -
120 - 162
186 lbs/hr
(Pressure)
lbs/hr
lbs/hr
(19.5 psi)
Oil Pressure
10 psi
30 - 60 psi
-
- -
-
- -
100 psi
Figure 2-3. Power Plant Instrument Markings
2-6

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