Cessna 182S Skylane Information Manual page 116

CESSNA
MODEL
182S
SECTION 5
PERFORMANCE
ALTIMETER CORRECTION
ALTERNATE STATIC SOURCE
NOTE:
Add correction to desired altitude to
obtain indicated altitude to
flv.
Windows closed, ventilators closed,
cabin
heater,
cabin air, ánd
defroster
on
maxrmum.
CONDITIONS:
Power required
for
level flight or
maximum
power
descent
cruise
configura-
tion.
Altimeter corrections
Tor
the takeoff and
landing configuration
are
less
than 50 feet.
CONDITION
FLAPS
UP
CORRECTION
TO
BE
ADDED-FEET
KIAS - alternate static source
ON
60 80 100 120 140
160
S.L.
2000 ft.
4000 ft.
6000 ft.
8000 ft.
10,000 Ít.
12,000 ft.
14,000 ft.
20
20
20
30
30
30
30
30
-10
-10
-10
-10
-10
-10
-10
-10
-30
-30
-30
-40
-40
-40
-40
-50
-60
-60
-70
-70
-80
-80
-80
-90
-90
-90
100
110
110
't20
120
't20
-120
-1
30
-140
-140
-150
-160
-170
-1
80
Feb
3/97
Figure 5-2. Altimeter Correction
5-11