Cessna 208B - Page 177

SECTION 5
PERFORMANCE
CESSNA
MODEL
2088 (675 SHP)
ALTIMETER CORRECTION
ALTERNATE STATIC SOURCE
NOTES:
1. Add correction to desired altitude to obtain indicated altitude to fly.
2. Where altimeter correction values have been replaced by dashes, the
correction is unnecessary because of conditions in
wh~ch airspeed is
not attainable in level flight.
VENTSCLOSED
Figure 5-2. Altimeter Correction
CONDITION
FLAPS UP
Sea Level
10,000 FT
20,000 FT
FLAPS 20"
Sea Level
10,000 FT
FLAPS 30"
Sea Level
10,000 FT
VENTS OPEN
1 5-14 U.S. Revision 23
CONDITION
FLAPS UP
Sea Level
10,000 FT
20,000 FT
FLAPS 20"
Sea Level
10,000 FT
FLAPS 30"
Sea Level
10,000 FT
CORRECTION TO BE ADDED-FEET
KlAS
CORRECTION TO BE ADDED-FEET
KIAS
140
55
75
---
75
---
---
---
80
---
---
--.
20
25
15
20
80
---
---
.--
-20
-25
-15
-20
160
80
---
---
---
---
---
---
100
20
30
40
35
50
35
50
90
15
20
25
25
35
25
35
100
-10
-20
-25
-5
-5
0
0
90
-15
-20
-30
-10
-15
-10
-10
120
40
50
70
55
75
60
85
120
-10
-15
-15
10
15
20
25
140
5
10
---
25
---
---
---
160
10
---
---
---
--.
---
---