Cessna 402C - Page 319

I\uher lll<JO 402C
No[~:
AIRSPEED CALIBRATION
ALTERNATE STATIC SOURCE
f'OH$ 82-2
Page 5-3
1.
3.
..
Indicated airllp.!ed assumes zero inatrtaent error.
Tb .. folluwjn~ ndibrat.ions are not valid in the pt'f!-stall
buffet.
The foll..:lwl11g calibrations a..e valid for the pUotlto and
co-pilot'l:I a1t"6pecd indicAtor. wben·,the standard or (Ce •• n.)
optional dual static ~y.tem i~ inatailed.
&!fer to bssle POH for gear up nap. 0° configuration
RAM AIR CONTKOL .IN AND
PILOT'S WIHDOWCLOSED'
C~AR' DOWN GEAR DOWN,,'
.
FlAPS
100
FLAPS 30°·
,;,
"AS
KCAS XIAS . KCAS'
70
b'
70
71
....
80 79
80 81
90
09 90
90
100
99 100 100'
110 108
110
110·
12u
II'
120,
120
- -
123
123
140 138
-
-
160
1>7
-
-
173 170
-
-
RAt'! AIR
CONTROL
(lUT AIllJ
PILOT'S WINDOW
CLOSED
70 72
70
73
80
82 80
83
% 92 90
92
lUU 101
lUO 102
110 III
HO 112
12lj
121 120
122
- -
121
123
140 140
-
-
lun 1bO
-
-
17\" 110
-
-
RAl1 AIR CONTROL
OUT ANI)
PILOT'S WINDOW
OPEN
70 65 70
66
81i
"
80 76
91)
8S
90
85
lUO
9,
100
95
111)
~ (J~ 110
105
120 114 120 115
-
- 125
119
1411 ),h
-
-
t6ij
1."11
-
-
1 7U
H,l
-
-
",'
--- :.;
FA:\ Approved: ArK] .... :ll, 1980
19