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Cessna 208B - Page 157

Cessna 208B
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CESSNA SECTION 4
MODEL
2088 (675 SHP) NORMAL PROCEDURES
CRUISE
(Continued)
I
Pitot-static heat should be ON anytime the OAT is below 5°C (40°F). If
lclng conditions are encountered, ensure that the additional anti-icing
systems (stall vane and inertial separator) are ON and in the BYPASS
mode before encountering visible moisture below approximately 4°C
(40°F). Windshield and propeller anti-ice systems should also be turned
I
ON.
I
SAMPLE CRUISE PERFORMANCE TABLE
PARAMETERS:
I
Standard Conditions
1900
RPM
Zero Wind
(WITHOUT CARGO POD)
ALTITUDE
(in Feet)
Maximum Cruise Power
1
Maximum Range Power
KTAS
I
NMPP
I
KTAS
1
NMPP
-
I
(WITH CARGO POD)
s
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ALTITUDE Maximum Cruise Power Maximum Range Power
d
(in Feet)
H
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Figure 4-4*. Sample Cruise Performance Table
KTAS
(Continued Next Page)
d
-
1
Revision
23
9
*
NMPP
U.S. 4-57
-
KTAS
I
NMPP
5,000
10.000
149 0.45
173
151
I
0.50
0.41
172
I
0.46

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