Cessna 208B - Page 229

1 5-66 U.S.
Revision 23
SECTION 5 CESSNA
PERFORMANCE MODEL
2088 (675 SHP)
WITHOUT CARGO POD
CLIMB GRADIENT-TAKEOFF FLAP SETTING
FLAPS 20"
CONDITIONS:
TAKEOFF POWER
1900 RPM
INERTIAL SEPARATOR
- NORMAL
NOTE
1. Do not exceed torque limit for takeoff per Engine Torque
for Takeoff chart. When ITT exceeds
765"C, this power
setting is time limited to
5 minutes.
2. With climb power set below the torque limit, decrease climb
gradient by 10
FTINM for inertial separator in BYPASS and 30
FTINM for cabin heat ON.
3. Where climb gradient values have been replaced by dashes,
operating temperature limits of the airplane would be greatly
exceeded. Those climb gradients which are included, but the
operation slightly exceeds the temperature limit, are provided
for interpolation purposes only.
WEIGHT
LBS
8750
8300
7800
7300
PRESS
ALT
FT
SL
2000
4000
6000
6000
10000
12000
SL
2000
4000
6000
8000
10000
12000
SL
2000
4000
6000
8000
10000
12000
SL
2000
4000
6000
8000
10000
12000
Figure 5-26.
40.C
575
51 5
445
370
290
...
...
645
580
95
430
340
. . .
...
730
660
580
500
405
...
. . .
830
755
670
580
475
...
...
.200C
685
€45
610
570
530
490
445
760
720
680
635
595
555
505
860
81 5
7-70
725
680
635
580
965
920
870
820
770
725
665
CLIMB
SPEED
KlAS
70
71
71
71
72
72
72
68
69
69
69
69
69
69
65
65
66
66
66
67
67
62
62
63
63
63
€4
64
Climb Gradient -Takeoff Flap Setting
CLIMB GRADIENT
0%
€45
605
570
530
495
435
345
720
660
640
595
555
495
400
810
765
725
680
635
570
470
915
870
820
775
725
655
545
- FTlNM
2O0C
610
570
535
495
410
325
245
680
640
600
560
465
375
290
770
725
680
640
540
445
350
870
825
775
730
620
520
420