Kodiak 100 Series User Manual

Pilot’s Operating Handbook
5-55
DO NOT USE FOR FLIGHT OPERATIONS
Section 5
PERFORMANCE
100 SERIES
Performance
CRUISE PERFORMANCE (Pressure Altitude 22,000 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% 800 193 135 100% 880 198 135
End 770 187 121 End 840 192 120
-10 100% 880 210 151 100% 960 217 151
Rng 860 207 149 Rng 920 207 145
End 750 184 117 End 830 188 117
-20 100% 940 225 159 100% 1040 235 159
Rng 840 202 145 Rng 900 203 142
End 740 181 115 End 810 184 114
-20 100% 940 225 159 100% 1040 235 159
Rng 840 202 145 Rng 900 203 142
End 740 181 115 End 810 184 114
-29 100% 990 238 163 100% 1090 251 164
Rng 830 199 143 Rng 890 201 141
75% 740
181 123 75% 820 185 126
End 730 178 112 End 800 181 112
-30 100% 1000 240 163 100% 1100 253 164
Rng 820 197 141 Rng 890 201 141
75% 750 182 126 75% 830 187 128
End 730 178 111 End 790 180 111
-40 100% 1050 256 167 100% 1160 273 168
Rng 810 195 139 Rng 880 198 139
75% 790 190 135 75% 870 196 137
End 720 175 109 End 780 176 110
-50 100% 1110 276 170 100% 1220 297 171
75% 830 200 142 75% 920 207 144
Rng 820 195 139 Rng 850 193 135
65% 720 176 120 65% 800 180 124
End 710 172 107 End 760 173 108
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