TEMP °C
2200 RPM 2000 RPM
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
20 100% 990 250 155 100% 1090 253 156
Rng 880 232 144 Rng 940 228 143
75% 740 207 123 75% 810 208 127
End 690 198 103 End 730 195 102
10 100% 1100 271 163 100% 1210 276 164
Rng 890 232 144 Rng 940 227 142
75% 830 220 136 75% 910 222 139
65% 720 202 117 65% 790 202 122
End 680 195 101 End 720 192 100
0 100% 1210 291 169 100% 1330 299 170
75% 900 233 144 75% 990 235 146
Rng 870 227 140 Rng 920 223 139
65% 780 212 129 65% 860 213 132
End 670 193 100 End 710 189 97
-10 100% 1310 314 174 100% 1440 325 174
75% 980 246 150 75% 1080 250 152
Rng 870 225 139 65% 940 224 139
65% 850 222 137 Rng 900 217 135
End 670 190 96 End 700 185 95
-11 100% 1320 315 174 100% 1450 327 175
75% 990 247 150 75% 1090 251 152
Rng 870 225 139 65% 940 225 140
65% 860 223 137 Rng 900 217 135
End 670 190 96 End 700 185 95
TEMP °C
2200 RPM 2000 RPM
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
-20 100% 1400 334 176 100% 1540 350 177
75% 1050 257 154 75% 1150 262 155
65% 910 231 141 65% 1000 234 144
Rng 880 226 139 Rng 890 216 134
End 660 188 93 End 690 183 95
-30 100% 1470 354 178 100% 1620 375 179
75% 1100 267 156 75% 1210 274 158
65% 960 239 144 65% 1050 242 146
Rng 860 221 135 Rng 860 208 129
End 660 186 89 End 680 180 94
-40 100% 1540 375 179 100% 1690 400 180
75% 1150 277 157 75% 1270 286 159
65% 1000 246 146 65% 1100 251 148
Rng 840 216 131 Rng 860 206 127
End 650 183 87 End 680 177 93
-50 100% 1610 399 180 100% 1770 430 181
75% 1210 289 158 75% 1330 299 160
65% 1050 254 147 65% 1150 260 150
Rng 870 221 132 Rng 850 205 126
End 650 181 87 End 670 175 90
CRUISE PERFORMANCE (Pressure Altitude 13,000 FT)
Conditions:
Weight
..................................................................................... 7255 pounds
Engine Inlet
...................................................................................NORMAL