CRUISE PERFORMANCE (Pressure Altitude 17,000 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% 920 227 153 100% 1010 231 154
Rng 880 219 148 Rng 920 214 144
End 710 189 107 End 770 189 110
0 100% 1010 244 161 100% 1110 251 162
Rng 880 218 147 Rng 920 212 143
75% 760 196 128 75% 830 198 131
End 700 187 105 End 760 186 108
-10 100% 1110 264 168 100% 1220 274 168
Rng 840 210 141 75% 910 211 141
75% 830 208 140 Rng 910 211 141
65% 720 188 119 65% 790 189 123
End 690 184 104 End 750 182 106
-19 100% 1170 280 171 100% 1290 292 172
75% 880 216 145 75% 970
220 146
Rng 840 209 140 Rng 890 206 138
65% 760 195 128 65% 840 197 131
End 690 181 103 End 740 179 103
-20 100% 1180 282 171 100% 1300 295 172
75% 890 218 145 75% 970 222 147
Rng 840 209 140 Rng 880 205 137
65% 770 196 129 65% 840 198 132
End 690 181 102 End 730 179 102
-30 100% 1250 300 174 100% 1370 318 175
75% 940 227 149 75% 1030 233 151
Rng 840 208 138 65% 890 206 137
65% 810 203 135 Rng 870 201 135
End 680 178 100 End 720 176 100
-40 100% 1310 319 175 100% 1440 341 177
75% 980 236 152 75% 1080 244 154
65% 850 209 139 65% 940 213 141
Rng
820 203 134 Rng 850 198 132
End 670 176 98 End 710 173 97
-50 100% 1380 342 177 100% 1510 369 178
75% 1030 247 154 75% 1140 256 156
65% 890 217 141 65% 980 222 144
Rng 830 203 134 Rng 830 192 128
End 660 174 96 End 700 170 95
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