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Cessna 208B - Page 234

Cessna 208B
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CESSNA
MODEL
2088 (675 SHP)
SECTION
5
PERFORMANCE
U.S. 5-71
WITHOUT CARGO POD
TIME, FUEL, AND DISTANCE
TO
CLIMB
MAXIMUM RATE OF CLIMB
CONDITIONS:
FLAPS UP
1900 RPM
INERTIAL SEPARATOR
-
NORMAL
NOTE
I.
Torque set at 1865 FT-LBS or lesser value must not
exceed maximum climb ITT of 765°C or
Ng of 101.6%.
2.
Add
35
pounds of fuel for engine start, taxi, and takeoff
allowances.
3. Distances shown are based on zero wind.
4.
With inertial separator set in bypass, increase time, fuel and
distance numbers by 1% for each 2000 feet of climb and for
cabin heat ON increase time, fuel, and distance numbers by
1
%
for each 1000 feet of climb.
5.
Where time, fuel and distance values have been replaced by
dashes, an appreciable rate of climb for the weight shown
WEIGHT
LBS
8750
8300
7800
7300
cannot
PRESS
ALT
FT
SL
4000
8000
12000
16000
20000
24000
SL
4000
8000
12000
16000
20000
24000
SL
4000
8000
12000
16000
20000
24000
SL
4000
8000
12000
16000
20000
24000
Figure 5-31.
be
cLl~~
SLk:D
104
104
101
95
87
78
103
103
100
94
86
77
101
101
98
91
83
73
99
99
99
96
88
80
69
Time,
expected.
20'C
BELOW
TlME
MIN
4
8
13
19
26
4
8
12
17
24
36
4
7
11
15
21
31
6
10
14
19
27
Fuel,
CLIMB
FROM
SEA LEVEL
STANDARD
STANDARD
FUEL
LBS
30
60
92
128
173
000
27
55
84
116
155
213
25
50
76
104
138
184
3235
45
69
94
123
161
and
TlME
MIN
104000000000
4
9
14
21
33
103000000000
4
8
13
19
29
46
101000000000
4
7
12
17
25
38
7
10
15
22
32
20%
ABOVE
TEMP
DlST
NM
7
15
24
34
50
7
14
21
31
44
69
6
12
19
27
38
57
11
17
24
34
49
Distance
TlME
MIN
5
11
19
31
54
-----.......--..--
5
10
17
27
43
---
4
9
15
23
35
---
8
13
20
29
47
(Sheet 1
TEMPERATURE
FUEL
LBS
31
62
98
140
198
28
57
89
126
173
252
26
52
80
1i2
151
208
000000000
3235
47
72
100
133
177
to Climb
DlST
NM
8
16
27
42
65
7
14
24
37
56
92
6
13
21
32
47
73
11
19
28
40
60
STANDARD
FUEL
LBS
35
74
119
177
280
32
66
106
154
227
---
28
59
93
133
187
---
4257
52
81
115
158
227
of 2)
TEMP
DlST
NM
10
22
38
62
111
9
19
34
53
88
---
8
17
29
45
70
.--
15
25
38
57
93

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