Kodiak 100 Series User Manual

Pilot’s Operating Handbook
5-56
DO NOT USE FOR FLIGHT OPERATIONS
Section 5
PERFORMANCE
100 SERIES
Performance
CRUISE PERFORMANCE (Pressure Altitude 23,000 FT)
Conditions:
Weight
..................................................................................... 7255 pounds
Engine Inlet
...................................................................................NORMAL
TEMP
°C
2200 RPM 2000 RPM
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
-10 100% 840 201 145 100% 920 207 145
End 770 186 121 End 850 191 120
-20 100% 900 216 155 100% 990 225 155
Rng 850 203 147 Rng 910 205 144
End 750 182 118 End 830 187 118
-30 100% 960 230 160 100% 1050 243 161
Rng 830 200 144 Rng 900 203 142
End 740 179 115 End 810 183 115
-31 100% 960 231 161 100% 1060 244 161
Rng 830 199 144 Rng 900 202 142
End 740 179 115 End 810 183 115
-40 100% 1010 245 164 100% 1110 261 165
Rng 810 194 139 Rng 880 199 139
75%
760 182 127 75% 830 188 130
End 730 176 111 End 790 179 111
-50 100% 1070 265 168 100% 1180 286 169
Rng 810 194 139 75% 880 199 139
75% 800 192 137 Rng 860 194 136
End 720 173 109 End 770 175 110
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