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Cessna 208B - Page 167

Cessna 208B
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CESSNA SECTION 5
MODEL
2088 (675 SHP) PERFORMANCE
TABLE OF CONTENTS
(Continued) Page
Figure 5-26 Climb Gradient
.
Takeoff Flap Setting
.............
5.66
Figure 5-27 Maximum Rate Of Climb
.
Flaps Up
..............
5.67
Figure 5-28 Takeoff Climb Gradient
.
Flaps Up
................
5.68
Figure 5-29 Cruise Climb
.
Flaps Up
.
115 KIAS
...............
5.69
Figure 5-30 Rate Of Climb
.
Balked Landing
..................
5.70
Figure 5-31 Time, Fuel, And Distance To Climb
.
Maximum Rate Of Climb
.....................
5.71
Time, Fuel, And Distance To Climb
.
Cruise Climb
.
115 KlAS
.....................
5.72
Figure 5-32 Cruise Performance
.
Notes
.....................
5.73
Cruise Performance
.
2000 Feet
.................
5.74
Cruise Performance
.
4000 Feet
.................
5.75
Cruise Performance
.
6000 Feet
.................
5.76
Cruise Performance
.
8000 Feet
.................
5.77
Cruise Performance
.
10, 000 Feet
................
5.78
Cruise Performance
.
12, 000 Feet
................
5.79
Cruise Performance
.
14, 000 Feet
................
5.80
Cruise Performance
.
16.000 Feet
................
5.81
Cruise Performance
.
18, 000 Feet
................
5.82
................
Cruise Performance
.
20, 000 Feet 5.83
................
Cruise Performance
.
22, 000 Feet 5.84
................
Cruise Performance
.
24, 000 Feet 5.85
Figure 5-32A Cruise Maximum Torque (Sheet 1 of 5)
...........
5.86
Figure 5-32A Cruise Maximum Torque (Sheet 2 of 5)
...........
5.87
Figure 5-32A Cruise Maximum Torque (Sheet 3 of 5)
...........
5.88
...........
Figure 5-32A Cruise Maximum Torque (Sheet 4 of 5)
5.89
...........
Figure 5-32A Cruise Maximum Torque (Sheet 5 of 5)
5.90
Figure 5-33 Fuel And Time Required
.
Maximum Cruise Power
(40-200 NM)
..............................
5.91
Fuel And Time Required
.
Maximum Cruise Power
............................
(200-1 000 NM) 5.92
Figure 5-34 Fuel And Time Required
.
Maximum Range Power
(40-200 NM)
..............................
5.93
Fuel And Time Required
.
Maximum Range Power
............................
(200-1000 NM) 5.94
................................
Figure 5-35 Range Profile 5.95
.............................
Figure 5-36 Endurance Profile 5.96
.............
Figure 5-37 Time, Fuel, And Distance To Descend
5.97
............
.
Figure 5-38 Landing Distance 8500 Lbs, 8000 Lbs 5.98
......
.
Landing Distance 7500 Lbs, 7000 Lbs .5.99/ 5.100
Revision 23 U.S. 5-315-4

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