Cessna 402C - Page 114

(.O;:,402C
AIRSPEED CALIBRATION
SECTION 5
PERFORMANCE
- NORMAL STATIC SOURCE
NOTE:
1. Indicated airspeed assumes zero instrument error.
2.
The following calibrations are not valid in the prestal1 buffet.
3.
The following calibrations are valid for the pilotls and copilot's
airspeed indicators when the standard or optional dual static system
is installed.
Gear Up
Gear Down
Gear Down
Flaps 00
Flaps 150 Flaps 450
KIAS
KCAS
KIAS
KCAS
KIAS KCAS
70
72 70 71 70 71
80
81
80
80
80
80
90
90 90
90
90
89
---
--- ---
---
95*
93*
100
99 100 99 100
98
llO
109 llO
108 llO 107
120
ll8 120 ll8 120
ll6
140
137
130
127
130
126
160
157
140
137
140 136
180 175 150 146
149 145
200 195 160 156
---
---
220
216
170
165
---
---
235
231
180 174
--- ---
*Recommended Minimum All Engines Approach Speed at 6850 Pounds
with 450 Win9 Flaps.
Figure
5-1
1 November 1979
5-13