TM 1-1510-223-10 MAXIMUM CRUISE POWER 1700 RPM ISA + 37°C WEIGHT® 12,000 POUNDS 10,000 POUNDS TORQUE FUEL TOTAL TORQUE FUEL TOTAL PRESSURE PER FLOW FUEL PER FLOW FUEL ALTITUDE IFAT FAT ENGINE PER FLOW IAS TAS ENGINE PER FLOW IAS TAS ENGINE ENGINE FEET °C °C PERCENT LBS/HR LBS/HR KTS KTS PERCENT   LBS/HR    LBS/HR KTS KTS 0 56 52 73 606 1212 204 219 73 606 1212 206 221 2000 53 48 71 576 1152 201 222 71 576 1152 203 224 4000 49 44 69 548 1096 197 225 69 548 1096 199 227 6000 45 40 68 521 1042 193 227 68 521 1042 195 229 8000 41 36 65 494 988 189 229 66 494 988 191 231 10,000 37 32 63 467 934 184 230 63 467 934 186 233 12,000 33 28 60 435 870 178 230 60 436 872 180 233 14,000 29 24 56 406 812 172 230 56 407 814 174 233 16,000 25 20 53 378 756 165 228 53 378 756 168 232 18,000 21 16 48 349 698 157 225 49 350 700 160 230 20,000 17 12 45 324 648 149 222 45 324 648 153 227 22,000 13 8 42 303 606 142 219 42 304 608 147 226 24,000 9 4 38 283 566 134 215 39 284 568 140 223 26,000 5 0 36 267 534 127 212 36 267 534 133 222 28,000 1 -3 34 253 506 120 209 35 254 508 128 222 29,000 -1 -5 33 246 492 117 207 34 247 494 126 221 31,000 -6 -9 31 229 458 106 198 32 232 464 119 218 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559316 NOTE During operations with ice vanes extended, torque will decrease approximately 10 percentage points (E. G., 64% - 10 percentage points = 54%), fuel flow will decrease approximately 35 LBS/HRIENG, and true airspeed will be reduced approximately 20 knots. Figure 7-57.  Maximum Cruise Power at 1700 RPM - ISA +37 °C (Sheet 2 of 2)   CA 7-84  Change 2