CESSNA
MODEL
2088 (675 SHP)
SECTION 5
PERFORMANCE
WITHOUT
CARGO
POD
CRUISE
CLIMB
FLAPS UP
-
115
KlAS
CONDITIONS:
1900 RPM
INERTIAL SEPARATOR
-
NORMAL
NOTE
I.
Torque set at
1865
foot-pounds or lesser value must not
exceed maximum climb
ITT of
765°C
or N, of
101.6%.
2. With climb power set below the torque limit, decrease rate-of-
climb by 50 FPM for inertial separator set in BYPASS and 70
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Where rate of climb values have been replaced by dashes, an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.
U.S. 5-69
WEIGHT
LBS
~j
,
~ ~
PRESS
ALT
CI
8750
8300
7800
7300
RATE
OF
CLIMB
-
FPM
400C
I
-2O'C
I
O'C
1
20°C
I
40°C
.
.
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
Figure
1000
980
960
910
935
880
845
1085
1065
1040
1015
990
960
925
1185
1165
1140
1115
1090
1060
1025
1300
1275
1255
1230
1200
ll70
1135
5-29. Cruise
980
960
935
905
880
845
705
1060
1040
1015
990
960
925
780
1165
1140
1115
1090
1060
1025
870
1275
1255
1230
1200
1170
1135
970
Climb
-
960
935
910
880
790
640
485
1040
1020
990
960
870
710
550
1145
1120
1090
1060
965
795
630
1255
1230
1205
1170
1070
890
715
Flaps Up
940
910
795
650
505
370
235
1020
995
870
720
570
430
285
1120
1095
965
805
645
500
350
1235
1205
1065
900
730
575
41 5
-
115 KlAS
705
570
435
305
190
. . .
. . .
780
635
495
360
235
120
...
865
715
565
420
295
175
...
960
800
645
490
355
230
...
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