Kodiak 100 Series - Altitude Correction

Pilot’s Operating Handbook
5-5
DO NOT USE FOR FLIGHT OPERATIONS
Section 5
PERFORMANCE
100 SERIES
Performance
5-3 ALTITUDE CORRECTION
Conditions:
Power for level ight or maximum power for descent, whichever is less.
Weight
..................................................................................... 7255 pounds
Example:
Flaps
..........................................................................................................0°
Indicated Airspeed
.........................................................................100 KIAS
Desired Altitude
.......................................................................... 10,000 feet
Altitude Correction
............................................................................ -11 feet
Altitude to Fly: 9,989 feet
FLAPS
PRESS
ALT.
(FEET)
CORRECTION TO BE ADDED
NORMAL STATIC SOURCE - KIAS
60 80 100 120 140 160 180
0
°
S.L.
+7 -9 +1 +8 +2 -24
10000
+10 -11 +2 +10 +3 -38
20000
+18 -20 +3 +18 +4 -62
10°
S.L.
+7 +1 +3 +7
10000
+8 +1 +3 +8
20000
+9 +1 +4 +9
20°
S.L.
+11 -2 0
10000
+13 -2 0
20000
+17 -3 0
35°
S.L.
+12 +10 +8
10000
+14 +12 +9
20000
+18 +15 +10
Table 5-2 – Altitude Correction
NOTES:
• Indicated airspeed values assume zero instrument error.
• KIAS = Knots Indicated Airspeed
• Where airspeeds have been replaced by shaded areas, the airspeed
would either be below the maximum weight stall speed or above
the maximum approved operating limits speed for the aircraft
conguration.
Uncontrolled if printed