TEMP °C
2200 RPM 2000 RPM
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
20 100% 950 240 153 100% 1040 243 154
Rng 910 233 148 Rng 930 224 143
75% 710 199 115 75% 780 199 120
End 690 196 104 End 750 194 104
10 100% 1060 259 161 100% 1160 264 162
Rng 860 223 142 Rng 930 222 142
75% 790 211 132 75% 870 213 135
End 690 193 103 65% 750 194 114
End 730 191 102
0 100% 1150 279 167 100% 1270 286 168
Rng 880 226 143 75% 950 225 143
75% 870 223 141 Rng 910 219 139
65% 750 203 125 65% 830 204 129
End 680 191 101 End 720 187 100
-10 100% 1260 301
173 100% 1380 312 173
75% 940 236 148 75% 1040 240 150
Rng 860 221 139 Rng 900 215 137
65% 820 213 134 65% 900 215 137
End 670 188 98 End 710 184 97
-13 100% 1280 306 173 100% 1410 318 174
75% 960 239 149 75% 1060 243 151
Rng 860 220 139 65% 920 218 138
65% 830 216 136 Rng 900 214 136
End 670 188 98 End 710 183 97
TEMP °C
2200 RPM 2000 RPM
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
-20 100% 1340 321 175 100% 1470 336 176
75% 1010 247 152 75% 1110 252 154
65% 870 222 139 65% 960 224 142
Rng 860 219 138 Rng 880 211 134
End 670 186 95 End 700 181 95
-30 100% 1410 341 177 100% 1560 360 178
75% 1060 257 155 75% 1170 264 156
65% 920 229 142 65% 1010 233 145
Rng 880 222 139 Rng 870 208 132
End 660 183 93 End 690 178 95
-40 100% 1480 361 178 100% 1630 385 179
75% 1110 267 156 75% 1220 275 158
65% 960 237 144 65% 1060 241 147
Rng 840 214 132 Rng 860 204 129
End 660 181 89 End 680 176 94
-50 100% 1550 385 179 100% 1710 415 180
75% 1160 278 158 75% 1280 289 159
65% 1010 245 146 65% 1110 251 149
Rng 840 212 131 Rng 840 201 126
End 650 179 87 End 680 173 92
CRUISE PERFORMANCE (Pressure Altitude 14,000 FT)
Conditions:
Weight
..................................................................................... 7255 pounds
Engine Inlet
...................................................................................NORMAL