Kodiak 100 Series User Manual

Pilot’s Operating Handbook
5-4
DO NOT USE FOR FLIGHT OPERATIONS
Section 5
PERFORMANCE
100 SERIES
Performance
5-2 AIRSPEED CALIBRATION
Conditions:
Power for level ight or maximum power for descent, whichever is less.
Weight
..................................................................................... 7255 pounds
Example:
Flaps
..........................................................................................................0°
Indicated Airspeed
.........................................................................140 KIAS
Calibrated Airspeed
..................................................................... 141 KCAS
KIAS
KCAS
Flaps 0° Flaps 10° Flaps 20° Flaps 35°
60 69 63 63
70 78 73 72 72
80 81 80 82 82
90 91 90 91 92
100 100 100 100 101
110 110 111 110
120 120 121 120
130 130 131
140 141
150 151
160 162
170 171
180 179
Table 5-1 – Airspeed Calibration
NOTES:
• Indicated airspeed values assume zero instrument error.
• KIAS = Knots Indicated Airspeed
• KCAS = Knots Calibrated 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• Where airspeeds have been replaced by shaded areas, the airspeed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

Kodiak 100 Series Specifications

General

Manufacturer	Daher
Engine	Pratt & Whitney Canada PT6A-34
Service Ceiling	25, 000 feet
Seating Capacity	10
Crew	1-2
Range	1, 132 nautical miles
Type	Utility aircraft
Length	34 feet 2 inches
Wingspan	45 feet
Max takeoff weight	7, 255 pounds
Power Output	750 shp
Cabin Width	4 feet 6 inches