Kodiak 100 Series User Manual

Pilot’s Operating Handbook
5-34
DO NOT USE FOR FLIGHT OPERATIONS
Section 5
PERFORMANCE
100 SERIES
Performance
TEMP °C
2200 RPM 2000 RPM
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
40 100% 1240 343 154 100% 1360 344 155
Rng 1020 306 139 Rng 1050 295 137
75% 930 290 130 75% 1020 290 135
65% 800 269 116 65% 880 269 123
End 660 245 77 End 680 236 86
30 100% 1410 371 162 100% 1560 374 163
75% 1060 311 140 75% 1170 311 143
Rng 1040 307 139 Rng 1030 289 134
65% 920 287 128 65% 1010 287 133
End 660 243 76 End 670 234 84
20 100% 1590 402 169 100% 1750 407 170
75% 1200 331 148 75% 1320 333 150
Rng 1060 308 139 65% 1140 305 140
65% 1040 304 136 Rng 1010 285 131
End 660 241 74 End 670 231 77
13 100% 1670 415 171 100% 1840 421 172
75% 1250 340 150 75% 1380 341 152
65% 1090 311 139 65% 1190 312 142
Rng 1080 311 139 Rng 1030 286 132
End 660 239 73 End 660 229 76
10 100% 1670 414 170 100% 1840 421 171
75% 1250 339 149 75% 1380 341 151
Rng 1090 312 139 65% 1190 311 142
65% 1090 310 138 Rng 1040 288 132
End 660 239 73 End 660 228 76
0 100% 1670 412 168 100% 1840 420 169
75% 1250 337 147 75% 1380 339 150
Rng 1130 316 140 65% 1190 309 140
65% 1090 308 136 Rng 990 277 127
End 660 236 70 End 660 225 73
TEMP °C
2200 RPM 2000 RPM
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
-10 100% 1670 411 166 100% 1840 419 167
75% 1250 335 145 75% 1380 337 148
Rng 1170 320 140 65% 1190 307 138
65% 1090 306 134 Rng 1010 278 126
End 660 234 70 End 660 223 72
-20 100% 1670 409 163 100% 1840 418 165
75% 1250 332 143 75% 1380 334 146 65% 1090 304 131 65% 1190 304 136
Rng 1050 297 129 Rng 1030 278 126
End 670 233 70 End 660 221 70
-30 100% 1670 408 161 100% 1840 417 163
75% 1250 330 141 75% 1380 332 144
Rng 1090 302 130 65% 1190 302 134
65% 1090 301 130 Rng 1060 281 126
End 680 232 69 End 660 218 68
-40 100% 1670 406 158 100% 1840 416 160
75% 1250 328 138 75% 1380 330 142
Rng 1140 307 131 65% 1190 300 132
65% 1090 299 127 Rng 1090 284 126
End 680 230 69 End 660 216 66
-50 100% 1670 405 156 100% 1840 415 158
75% 1250 325 136 75% 1380 328 140
Rng 1190 314 132 65% 1190 298 130
65% 1090 296 124 Rng 1140 289 127
End 690 229 68 End 660 214 64
CRUISE PERFORMANCE (Pressure Altitude 1000 FT)
Conditions:
Weight
..................................................................................... 7255 pounds
Engine Inlet
...................................................................................NORMAL
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