Kodiak 100 Series - CRUISE PERFORMANCE (Pressure Altitude 18,000 FT)

Pilot’s Operating Handbook
5-51
DO NOT USE FOR FLIGHT OPERATIONS
Section 5
PERFORMANCE
100 SERIES
Performance
CRUISE PERFORMANCE (Pressure Altitude 18,000 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% 870 216 149 100% 960 220 150
End 720 189 111 Rng 930 214 145
End 790 189 111
0 100% 960 233 158 100% 1060 239 159
Rng 870 214 147 Rng 910 210 143
75% 720 187 117 75% 790 189 121
End 710 186 107 End 770 186 110
-10 100% 1060 252 165 100% 1160 262 166
Rng 860 213 146 Rng 910 208 142
75% 790 199 135 75% 870 202 137
End 700 183 105 End 760 182 108
-20 100% 1130 270 169 100% 1240 282 170
75% 850 208 142 75% 930 212 144
Rng 820 203 139 Rng 900 206 140
65% 730
187 123 65% 810 189 127
End 690 180 105 End 750 179 106
-21 100% 1130 271 170 100% 1250 284 170
75% 850 209 142 75% 930 213 144
Rng 830 205 140 Rng 900 206 140
65% 740 188 124 65% 810 190 127
End 690 180 104 End 750 179 106
-30 100% 1190 287 172 100% 1310 303 173
75% 900 217 146 75% 990 223 148
Rng 830 204 139 Rng 860 199 135
65% 780 194 131 65% 850 197 134
End 690 178 103 End 730 176 103
-40 100% 1250 305 174 100% 1380 326 175
75% 940 226 149 75% 1030 233 151
Rng 830 203 137 65% 900 204 138
65% 820 200 135 Rng 860 197 133
End 680 175 100 End
720 172 100
-50 100% 1320 327 176 100% 1450 352 177
75% 990 236 152 75% 1090 245 154
65% 860 208 139 65% 940 213 142
Rng 820 200 134 Rng 840 193 130
End 670 173 98 End 710 169 97
Uncontrolled if printed