TM 1-1510-223-10 MAXIMUM CRUISE POWER 1700 RPM ISA + 30°C WEIGHT® 16,000 POUNDS 14,000 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 50 45 81 634 1268 210 223 81 634 1268 212 225 2000 46 41 78 605 1210 206 225 79 605 1210 208 227 4000 42 37 76 576 1152 202 227 76 576 1151 204 229 6000 38 33 74 547 1094 197 229 74 547 1094 199 231 8000 34 29 71 519 1038 192 230 72 519 1038 194 233 10,000 30 25 69 490 980 186 231 69 491 982 189 234 12,000 26 21 65 460 920 180 230 65 460 920 183 234 14,000 22 17 62 431 862 173 229 62 432 864 177 234 16,000 18 13 57 401 8026 165 226 58 402 804 169 231 18,000 14 9 52 371 7428 155 219 53 372 744 160 226 20,000 10 5 48 345 690 146 214 49 346 692 152 223 22,000 6 1 45 325 650 137 210 46 327 654 145 221 24,000 1 -3 43 305 610 127 203 43 307 614 137 217 26,000 -3 -7 40 286 572 114 189 41 289 578 129 213 28,000 -6 -10 --- --- --- --- --- 38 272 544 120 206 29,000 -9 -12 --- --- --- --- --- 37 263 526 114 200 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559313 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 7-55.  Maximum Cruise Power at 1700 RPM - ISA +30 °C (Sheet 1 of 2)  CA Change 2  7-79