CESSNA
MODEL
2088 (675 SHP)
SECTION 5
PERFORMANCE
CARGO POD INSTALLED
CLIMB
GRADIENT-TAKEOFF FLAP SETTING
FLAPS
20"
CONDITIONS:
TAKEOFF POWER
1900 RPM
INERTIAL SEPARATOR-NORMAL
ZERO
WIND
NOTE
1.
Do not exceed torque limit for takeoff per Engine Torque
for Takeoff chart. When
ITT
exceeds
765°C.
this Dower
setting is time limited to
5
minutes.
2. With climb power set below the torque limit, decrease climb
gradient bv
10 FlNM for inertial seDarator 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Where climb gradient values have been replaced by dashes, operating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
gadients which are included, but the operation slightly exceeds the
temperature limit, are provided for interpolation purposes only.
'
1
Revision 23
e
-,
2
-,
U.S.
5-27
CLIMB GRADIENT
-
FTlNM
-200C
I
0'C
I
20°C
I
40°C
WEIGHT
LBS
8750
8300
7800
7300
PRESS
ALT
FT
CLIMB
SPEED
KIAS
SL
2000
4000
6000
8000
10000
12000
SL
2000
4000
6000
8000
10000
12000
SL
2000
4000
6000
8000
10000
12000
SL
2000
4000
6000
8000
10000
12000
Flgure 5-11
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
64
64
Cllmb
670
630
590
555
515
475
430
745
705
665
620
580
540
490
840
795
750
705
660
620
565
950
900
855
805
755
710
650
Gradlent
-
630
590
555
515
475
420
330
705
660
620
580
540
475
385
795
750
705
665
620
550
450
900
855
805
755
710
635
530
Takeoff Flap
595
555
520
480
390
310
225
665
625
585
545
450
360
275
755
710
665
625
525
430
335
855
805
760
715
605
505
405
Settlng
560
500
430
355
270
...
...
630
565
490
410
325
...
.
-.
715
645
565
480
390
...
...
810
735
650
560
460
...
.--
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