CRUISE PERFORMANCE (Pressure Altitude 11,000 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
20 100% 1070 271 159 100% 1180 275 160
Rng 910 242 144 Rng 950 235 141
75% 800 224 131 75% 880 225 134
65% 700 206 111 65% 770 206 118
End 680 203 100 End 710 198 97
10 100% 1200 294 166 100% 1320 300 167
75% 900 239 141 75% 990 241 144
Rng 880 236 140 Rng 930 232 139
65% 780 218 127 65% 860 219 130
End 670 200 97 End 700 195 95
0 100% 1310 315 171 100% 1440 324 172
75% 980 252 148 75% 1080 255 150
Rng 890 237 140 65% 930 231 138
65% 850 229 135 Rng 920 228 136
End 660 198 96 End 690 192 94
-7 100% 1380 331 174 100% 1520 343 175
75% 1040 262 151 75% 1140 265 153
Rng 900 237 139 65% 990 239 142
65% 900 237 139 Rng 920 228 136
End 660 196 92 End 690 190 94
-10 100% 1420 339 176 100% 1560 352 176
75% 1060 266 153 75% 1170 270 155
65% 920 240 141 65% 1010 242 143
Rng 900 236 138 Rng 910 225 134
End 660 196 90 End 690 189 94
TEMP °C
2200 RPM 2000 RPM
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
-20 100% 1510 360 178 100% 1660 377 179
75% 1130 278 156 75% 1240 283 158
65% 980 249 144 65% 1080 252 147
Rng 880 231 135 Rng 890 221 131
End 650 193 88 End 680 187 94
-30 100% 1590 382 179 100% 1740 403 180
75% 1190 288 158 75% 1310 296 159
65% 1030 257 146 65% 1130 261 149
Rng 880 230 133 Rng 880 217 129
End 650 190 87 End 670 184 91
-40 100% 1660 403 180 100% 1820 429 181
75% 1240 298 159 75% 1370 308 160
65% 1080 265 148 65% 1180 270 150
Rng 900 233 134 Rng 870 214 126
End 640 188 86 End 670 182 88
-50 100% 1670 409 178 100% 1840 438 179
75% 1250 300 157 75% 1380 310 159
65% 1090 265 146 65% 1190 271 149
Rng 870 224 127 Rng 890 216 126
End 650 187 83 End 660 179 85