CESSNA SECTION
5
MODEL 2088 (675 SHP) PERFORMANCE
CARGO POD INSTALLED
TAKEOFF
CLIMB
GRADIENT
FLAPS
UP
~
~
CONDITIONS:
TAKEOFF POWER
1900 RPM
INERTIAL SEPARATOR-NORMAL
NOTE
I.
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 rate of
climb by 10
FlNM for inertial separator in BYPASS and 40 FTI
NM 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 Where climb gradient values have been replaced by dashes,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
interpolaGon purposes only.
1
Revision 23
U.S.
5-29
8750
8300
7800
7300
CLIMB GRADIENT
-
FTlNM
-20aC
I
O'C 20°C
I
40°C
WEIGHT
LBS
. .
SL
2000
4000
6000
8000
10000
12000
SL
2000
4000
6000
8000
I0000
12000
SL
2000
4000
6000
8000
10000
12000
SL
2000
4000
6000
8000
I0000
12000
Figure
PRESS
ALT
FT
CLIMB
SPEED
KlAS
68
69
69
70
70
71
72
66
66
67
68
68
69
69
61
62
62
62
63
63
63
59
59
59
59
59
59
59
5-13. Takeoff
695
655
615
580
540
505
420
770
730
690
645
605
570
475
860
820
775
730
690
645
550
970
920
875
830
780
735
630
Climb
655
615
580
545
475
390
305
725
685
650
610
540
445
355
81 5
775
730
690
615
515
420
920
875
830
780
700
595
490
Gradlent
-
620
580
500
41 0
330
250
180
690
650
565
470
380
300
225
775
735
640
540
445
360
280
875
830
730
620
520
430
340
Flaps Up
475
390
305
230
165
..*
...
535
445
360
280
210
. .
.
. . .
615
51 5
425
340
265
-..
-
-.
700
595
500
405
330
. . .
. . .
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