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Cessna 208B - Page 191

Cessna 208B
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I
I
I
Figure 5-12. Maximum Rate of Climb
-
Flaps Up
I
SECTION
5
CESSNA
PERFORMANCE MODEL
2088
(675
SHP)
CARGO POD INSTALLED
MAXIMUM RATE
OF
CLIMB
FLAPS
UP
CONDITIONS:
1900 RPM
INERTIAL SEPARATOR-NORMAL
NOTE
1.
Torque set at
1865
foot-pounds or lesser value must not
exceed maximum climb ITT of
765°C
or
Ng
or
101.6%.
2. With climb power set below the torque limit, decrease rate of
climb by 30 FPM for inertial separator in BYPASS and
65
FPM
for cabin heat ON.
3.
Where rate of climb values have been replaced by dashes, an
appreciable rate of climb for the weight shown cannot be
expected or operating temperature limits of the airplane would
be greatly exceeded. Those rates of climb which are included
but the operation slightly exceeds the temperature limit are
provided for interpolation purposes only.
1
5-28 U.S. Revision 23
WEIGHT
LBS
8750
PRESS
ALT
FT
SL
4000
8000
12000
16000
20000
24000
CLIMB
SPEED
KlAS
104
104
104
101
95
87
78
MTE
OF
CLIMB
-
FPM
40%
975
940
890
840
610
345
95
-20'C
960
915
865
710
445
195
...
O'C
940
890
780
510
260
20
. .
-
20%
920
785
515
275
50
...
...
40'C
705
450
215
15
...
. .
-
-. .

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