EasyManua.ls Logo

Cessna 208B - Page 166

Cessna 208B
488 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
,-
.
-.
SECTION 5
CESSNA
,-
PERFORMANCE
MODEL 208B (675 SHP)
..
TABLE
OF
CONTENTS
(Continued) Page
,
.
Figure 5-17 Cruise Performance
-
Notes.
. . . . . .
.
.
.
.
. .
.
. .
.
. .
.
5-34
Cruise Performance
-
2000 Feet
.
.
.
. . .
.
. .
.
. . . .
.
.
5-35
,
.
Cruise Performance
-
4000 Feet
.
. .
.
. .
.
.
. .
. . . . . .
5-36
Cruise Performance
-
6000 Feet
.
. . . . . . . .
. .
. . . . .
5-37
,-
Cruise Performance
-
8000 Feet
.
. .
.
. . . .
.
.
. . .
. . .
5-38
,.
Cruise Performance
-
10,000 Feet.
.
. .
.
. . .
.
. . . . . .
5-39
Cruise Performance
-
12,000 Feet.
.
. . .
.
. . . . . . .
.
.
5-40
,-
Cruise Performance
-
14,000 Feet.
.
.
. . . . . . . . . . . .
5-41
,-
Cruise Performance
-
16,000 Feet.
. .
. . . . . . .
.
. . .
.
5-42
Cruise Performance
-
18,000 Feet.
.
.
. . .
. . . .
.
. .
.
.
5-43
.
.
Cruise Performance
-
20,000 Feet.
.
. . . .
. . .
.
.
. .
.
.
5-44
.-
Cruise Performance
-
22,000 Feet.
. . . . . .
. .
.
.
.
.
. .
5-45
Cruise Performance
-
24,000 Feet.
. . . . . . . . . .
.
.
. .
5-46
,;
Figure 5-17A Cruise Maximum Torque (Sheet 1 of 5)
. . .
. . . .
.
.
.
547
Figure 5-17A Cruise Maximum Torque (Sheet 2 of 5)
.
. . .
. . . . .
.
548
Figure 5-17A Cruise Maximum Torque (Sheet 3 of 5)
.
.
. . . . .
. .
.
549
Figure 5-17A Cruise Maximum Torque (Sheet 4 of 5)
.
.
. . .
. . . .
.
5-50
Figure 5-17A Cruise Maximum Torque (Sheet 5 of 5)
.
. . . .
.
.
.
. .
5-51
Figure 5-18 Fuel And Time Required
-
Maximum Cruise Power
(40-200 Nm).
. .
.
.
. . . .
.
. .
.
.
.
. .
.
.
. .
. . . . . .
. .
.
5-52
Fuel And Time Required
-
Maximum Cruise Power
(200-1 000 Nm).
. . .
.
. . . . .
. .
.
. .
. .
.
. . .
.
. . . .
.
.
5-53
Figure 5-19 Fuel And Time Required
-
Maximum Range Power
(40-200 Nm).
. . . .
.
. .
.
.
. .
. . . . . . . . . .
.
. . .
.
.
. .
5-54
Fuel And Time Required
-
Maximum Range Power
(200-1000
Nm).
. .
.
.
.
. .
. . . . . .
.
.
.
. .
. .
.
. .
.
.
. .
5-55
Figure 5-20 Range Profile
. . . . .
.
. .
.
. . . . . . .
.
. .
.
. .
.
. . . .
. . . .
5-56
Figure 5-21 Endurance Profile.
. . . . . .
.
. .
.
. .
.
. . . .
.
. .
.
.
.
.
. .
.
5-57
Figure 5-22 Time, Fuel, And Distance To Descend
. .
.
. .
.
. .
.
. . .
5-58
Figure 5-23 Landing Distance
-
8500 Lbs, 8000 Lbs
. .
.
. . . .
. .
.
.
5-59
Landing Distance
-
7500 Lbs, 7000 Lbs.
. . . . .
.
. .
.
.
5-60
Airplanes Without Cargo Pod
Figure 5-24 Takeoff Distance Short Field
-
8750 Lbs, 8300 Lbs
.
.
5-61
Takeoff Distance Short Field
-
7800 Lbs, 7300 Lbs
. .
5-62
Figure 5-24A Takeoff Distance, Flaps
O"
-
8750 Lbs
. . . . . . . . .
.
.
5-63
Takeoff Distance, Flaps
O"
-
8300, 7800 And
7300Lbs
................................
5-64
Figure 5-25 Rate Of Climb -Takeoff Flap Setting
.
.
. .
.
. .
.
. . . . .
5-65
(Continued Next Page)
5-2 U.S. Revision
23

Table of Contents

Related product manuals