SECTION
5
CESSNA
PERFORMANCE MODEL
2088 (675
SHP)
AIRSPEED
CALIBRATION
NORMAL STATIC SOURCE
CONDITIONS:
8750Pounds
Power required for level flight or maximum rated RPM dive
NOTE
Where airspeed values have been replaced by dashes, the
airspeed would be either below stall speed at maximum
weight or above the maximum approved operating limit
s~eed for the condition.
FLAPS UP
1
KlAS
I
-.
-
80 100 120 140 160 175
---
I
/
KlAS
175 80 100 120 140 160 175
---
I
KCAS
FLAPS
10"
KCAS
179 83 100 120 140 160 175
---
FLAPS
20'1
--
-
85 100 120 140 160 175
---
ks
1
i:
f3:
:.
I00 I10 130 150
1
KCAS
100 110 130 150
FLAPS
30"
Figure
5-1.
Airspeed Calibration (Sheet
I
of
2)
1
5-12
U.S. Revision
23
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