Kodiak 100 Series User Manual

Pilot’s Operating Handbook
5-54
DO NOT USE FOR FLIGHT OPERATIONS
Section 5
PERFORMANCE
100 SERIES
Performance
CRUISE PERFORMANCE (Pressure Altitude 21,000 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
0 100% 830 202 144 100% 920 207 145
End 750 186 117 End 830 189 117
-10 100% 920 219 156 100% 1010 227 156
Rng 850 205 146 Rng 910 205 143
End 740 183 115 End 810 186 113
-20 100% 980 235 162 100% 1080 245 163
Rng 840 202 143 Rng 900 203 142
75% 740 182 122 75% 810 185 124
End 730 180 111 End 790 182 111
-27 100% 1020 245 165 100% 1120 258 165
Rng 830 199 142 Rng 900 202 142
75% 770 187 131 75% 840 191 133
End 720 178 110 End 780 179 111
-30 100% 1040 250 166 100% 1150 264 167
Rng 830 200 142 Rng 890 201 141
75% 780 190 134 75% 860 195 136
End 720 177 109 End 780 178 110
-40 100% 1100 267 169 100% 1210 284 170
75% 820 198 140 75% 910 204 142
Rng 820 197 139 Rng 870 195 136
65% 710 176 115 65% 780 179 121
End 710 174 105 End 760 174 108
-50 100% 1160 287 171 100% 1270 309 172
75% 870 207 145 75% 950 215 147
Rng 810 195 137 Rng 850 191 133
65% 750 183 127 65% 830 187 130
End 700 171 104 End 750 171 106
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