Power Plant Limitations - Cessna TR182 1979 Pilot Operating Handbook

CESSNA
MODEL TR182
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SECTION 2
LIMITATIONS
MARKING
KIAS VALUE
SIGNIFICANCE
OR RANGE
White Arc 43 - 95
Full Flap Operating Range. Lower
limit is maximum weight VSo in
landing configuration. Upper limit
is maximum speed permissible with
flaps extended.
Green Arc 43 - 157
Normal Operating Range. Lower limit
is maximum weight Vs at most forward
C.G. with flaps retracted.
Upper limit
is maximum structural cruising speed.
Yellow Arc 157 - 179
Operations must be conducted with
caution and only in smooth air.
Red Line 179
Maximum speed for all operations.
Figure 2-2. Airspeed Indicator Markings
POWER PLANT LIMITATIONS
Engine Manufacturer: Avco Lycoming.
Engine Model Number: 0-540-L3C5D.
Engine Operating Limits for Takeoff and Continuous Operations:
Maximum Power: 235 BHP.
Maximum Engine Speed: 2400 RPM.
Maximum Manifold Pressure: 31 in. Hg.
Maximum Cylinder Head Temperature: 500°F (260°C).
Maximum Oil Temperature: 245°F (118°C).
Oil Pressure, Minimum: 25 psi.
Maximum: 100psi.
Fuel Pressure, Minimum: 0.5 psi.
Maximum: 30.0 psi.
Propeller Manufacturer: McCauley Accessory Division.
Propeller Model Number: B2D34C217/90DHB-8
Propeller Diameter, Maximum: 82 inches.
Minimum: 80.5 inches.
Propeller Blade Angle at 30 Inch Station, Low: 15.8°.
High: 31.9°.
1 October 1978 2-5