Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 19

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CESSNA
MODELT210M
SECTION2
LIMITATIONS
MARKING
KIAS VALUE
SIGNIFICANCE
OR RANGE
White Arc
55-115
Full Flap Operating Range. Lower limit is
'
maximum weight Vs
0
in landing configu-
ration. Upper limit is maximum speed per-
missible with flaps extended.
Green Arc
68 - 165
Normal Operating Range. Lower limit is
maximum weight Vs
at most forward C.G.
with flaps retracted. Upper limit is maxi-
mum structural cruising speed.
Yellow Arc 165 -
195 Operations must be conducted with
caution and only in smooth air.
Red Line 195 Maximum speed for all operations.
Figure 2-2. Airspeed Indicator Markings
POWER PLANT LIMITATIONS
Engine Manufacturer: Teledyne Continental.
Engine Model Number: TSIO-520-R.
Engine Operating Limits for Takeoff and Continuous Operations:
Maximum Power, 5 Minutes - Takeoff: 310 BHP.
Continuous: 285 BHP
Maximum Engine Speed, 5 Minutes - Takeoff: 2700 RPM.
Continuous: 2600 RPM.
Maximum Manifold Pressure, 5 Minutes - Takeoff: 36.5 inches Hg.
Continuous: 35 inches Hg.
NOTE
For manifold pressure limitations above 17,000 feet, refer
to the Maximum Power Setting and Fuel Flow placard in
this section.
Maximum Cylinder Head Temperature: 238°C (460°F).
Maximum Oil Temperature: 116°C (240°F).
Oil Pressure, Minimum: 10 psi.
Maximum: 100 psi.
Fuel Pressure, Minimum: 3.0 psi.
Maximum: 19.5 psi (186 lbs/hr).
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