TEMP °C
2200 RPM 2000 RPM
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
20 100% 900 230 149 100% 990 232 151
Rng 890 226 147 Rng 940 222 145
End 700 194 105 End 760 193 107
10 100% 1010 248 159 100% 1110 253 160
Rng 880 225 146 Rng 920 219 142
75% 760 202 127 75% 830 203 130
End 690 192 104 End 750 190 105
0 100% 1100 267 165 100% 1210 274 166
Rng 860 220 142 Rng 930 219 142
75% 830 214 138 75% 910 216 140
65% 720 194 118 65% 790 195 123
End 690 189 104 End 730 186 102
-10 100% 1210 288 171 100% 1330 299 172
75% 900 226 146 75% 990 230
147
Rng 860 218 141 Rng 900 213 138
65% 780 205 131 65% 860 206 133
End 680 186 102 End 720 183 100
-15 100% 1240 297 173 100% 1370 309 173
75% 930 231 148 75% 1030 235 150
Rng 850 217 140 Rng 900 212 137
65% 810 208 134 65% 890 210 136
End 680 185 99 End 720 182 99
TEMP °C
2200 RPM 2000 RPM
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
-20 100% 1290 307 174 100% 1410 322 175
75% 960 237 150 75% 1060 241 152
Rng 860 217 139 65% 920 215 139
65% 840 213 136 Rng 890 210 136
End 670 184 98 End 710 180 97
-30 100% 1360 327 176 100% 1490 346 177
75% 1020 247 153 75% 1120 253 155
65% 880 220 140 65% 970 224 143
Rng 850 214 137 Rng 870 206 133
End 670 181 95 End 700 177 95
-40 100% 1420 347 178 100% 1570 370 179
75% 1070 257 155 75% 1170 265 157
65% 930 227 143 65% 1020 232 145
Rng 850 213 135 Rng 840 199 128
End 660 179 93 End 690 174 94
-50 100% 1490 371 179 100% 1640 400 180
75% 1120 268 157 75% 1230 278 159
65% 970 235 145 65% 1070 241 147
Rng 810 204 129 Rng 840 199 127
End 660 177 89 End 680 171 94
CRUISE PERFORMANCE (Pressure Altitude 15,000 FT)
Conditions:
Weight
..................................................................................... 7255 pounds
Engine Inlet
...................................................................................NORMAL