Kodiak 100 Series User Manual

Pilot’s Operating Handbook
5-53
DO NOT USE FOR FLIGHT OPERATIONS
Section 5
PERFORMANCE
100 SERIES
Performance
CRUISE PERFORMANCE (Pressure Altitude 20,000 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% 790 195 134 100% 860 199 135
End 750 189 117 End 820 191 117
0 100% 870 211 149 100% 960 216 150
Rng 870 211 149 Rng 920 208 145
End 740 186 113 End 810 188 113
-10 100% 960 229 159 100% 1050 237 159
Rng 850 207 146 Rng 910 206 143
End 730 183 111 End 790 184 111
-20 100% 1020 245 164 100% 1130 256 165
Rng 830 202 142 Rng 900 204 142
75% 770 190 131 75% 840 193 133
End 720 180 109 End 780 180 110
-25 100% 1050 252 166 100% 1160 264 167
Rng 830
202 142 Rng 890 202 141
75% 790 193 135 75% 870 197 137
End 710 178 107 End 770 179 109
-30 100% 1090 261 168 100% 1190 275 169
Rng 820 198 139 75% 900 202 141
75% 810 198 139 Rng 880 200 139
End 710 177 105 65% 780 179 118
End 760 177 108
-40 100% 1140 277 170 100% 1260 295 171
75% 860 206 143 75% 940 212 145
Rng 820 199 139 Rng 860 195 135
65% 740 183 125 65% 820 186 128
End 700 174 105 End 750 173 106
-50 100% 1200 297 173 100% 1320 320 174
75% 900 215 147 75% 990 223 149
Rng 810 196 136 65% 860 194 134
65% 780 190 131 Rng 840
191 132
End 690 171 104 End 730 170 102
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