Beechcraft Baron 58 - Page 145

ALTIMETER
CORRECTION
-
NORMAL
SYSTEM
."
(!l
~cn
o
CD
~
0
3
::t.
III 0
::s
::s
£ <
cnaJ
(!l m
:::l·m
!!?O
-l:%:
:%:0
......
:0
......
J>
W~
III
-l
::s
aJ
Q.III
J>~
.... 0
..
::S
(!len
~
QI)
·21 FT
(3965-21)
+
3944
FT
91 KTS
DOWN
3965
FT
-60
I I I I I I I
60 70 80 90 100
110 120
lAS - INDICATED
AIRSPEED~KNOTS
-50
lAS
FLAPS
INDICATED
PRESSURE
ALTITUDE
ALTIMETER
CORRECTION
ACTUAL PRESSURE
ALTITUDE
EXAMPLE
o 40
W
...
~
~w
30
woO
u. z:::>
~
-t:::
20
z
O~
o ...«
>=
8 10
u «
~
----0
o -
o
~~
a: 0:::> -10'
W
a:'"
tu
u,
5
~
t;
-c
-20
...
«0
;j
~~
m«
:::>u
~~
-41
FLAPS UP
70
80
90 100
110
120 130 140 150 160
170 180 190
200
lAS - INDICATED AIRSPEED
~KNOTS
-30
-40 -50
w
::;0
0:::>
a:t:::
u. ...
tJ;i
«0
a:W
lii~
:::>u
~i5
~
NOTE
INDICATED ALTITUDE AND
INDiCATED
AIRSPEED
ASSUME
ZERO
INSTRUMENT
ERROR
en
,
...
en
o
o
..
o
a'
(!l
~
...
CO
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0)