Beechcraft Duchess 76 - Altimeter Correction - Normal System

ALTIMETER CORRECTION· NORMAL SYSTEM
lAS 75KTS
FLAPS DOWN (ON)
INDICATED PRESSURE ALTITUDE
: 40ooFT
ALTIMETER CORRECTION +2 FT
ACTUAL PRESSURE ALTITUDE 4002 FT
EXAMPLE:
60 70 80 90 100 110 120
lAS - INDICATED AIRSPEED - KNOTS
em
c m
o m
:To
ell J:
~ 0
...... ::0
tTI~
~
1:1
llell
'=i
~Q
3 ....
III 0
130 140:l :l
~ <
20,000
SL
~;;W-
11.0: I I
~G\PS DOWN (ON
~
50
20
10
Iii
Ie 5'
I ~
Z -
0
0
~ W
a: 0
8§
a: .,;
~ @ -10
~ ~
~ ~
::;:
o -20
IE
i
::J -30
~
150 160
80 90 100 110 120 130 140
lAS - INDICATED AIRSPEED - KNOTS
70
30
tu -
w w
u. 0
I j:?
z i=
Q :;! 20
f-
() 0
W ~
a: .,;
a: ()
o -
() 0
a: ;;;
~ 2 10
::;: 0
- 0
~ .,;
.,;-
0
Vi
60
...
--.j
.....
w
"'"
co
t..
III
:l
C
III
~