Beechcraft Baron 58 - Page 144

U'I
AIRSPEED
CALIBRATION
-
NORMAL
SYSTEM
EXAMPLE
~C/)
,
NOTE INDICATED AIRSPEED
ASSUMES
ZERO
INSTRUMENT
ERROR
lAS
91 KNOTS
CD
CD
~
~n
oIlo
FLAPS
DOWN
o
::t.
CAS
89 KNOTS
... 0
200
200_
3 ::l
FLAPS UP
l» <
::l
190
190
n
CD
180
180
170
170
(f)
(f)
f-
f-
~
160
~
160
'"
'"
( 150
(
150
§
§
85
140
~
140
a:
a:
<i'130
<i'130
0
fiJ
w
tD
~
120
~
120
a:
a:
C/)m
'"
'"
CD
m
~
110
~110
:!. 0
u
u
!':J:
.;,
100
~100
-10
«
«
u
u
:J:::o
0
90
90
......
J>
n
...
80
80
......
."
0
W-I
C"
l»
tD
CD
70
70
::l l»
...
c. ...
~
60
60
J>O
CD
70
80 90
100
110 120 130 140 150
160
170 180 190
200
_::l
......
60
70
80
90
100 110 120
130
"'U'1
en
lAS·
INOICATED
AIRSPEED~
KNDTS
lAS·
INDICATED
AIRSPEED~KNOTS
~Q)