TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA +30°C WEIGHT® 12,000 POUNDS 10,000 POUNDS PRESSURE ALTITUDE IFAT FAT TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS FEET °C °C PERCENT LBS/HR LBS/HR KTS KTS PERCENT LBS/HR LBS/HR KTS KTS 0 50 45 82 635 1270 226 239 82 636 1272 227 241 2000 46 41 80 606 1212 222 242 80 606 1212 223 243 4000 43 37 78 577 1154 217 244 78 577 1154 218 245 6000 39 33 75 548 1096 212 246 75 549 1098 214 248 8000 35 29 73 521 1042 207 248 73 521 1042 209 250 10,000 31 25 70 494 988 202 249 70 494 988 204 252 12,000 27 21 66 463 926 196 250 67 463 926 198 252 14,000 23 17 63 434 868 190 250 63 435 870 192 253 16,000 19 13 59 405 810 183 248 59 405 810 185 252 18,000 15 9 54 374 748 174 245 54 375 750 177 249 20,000 11 5 50 349 698 166 243 50 350 700 170 247 22,000 7 1 47 329 658 160 241 47 330 660 164 247 24,000 3 -3 44 309 618 153 239 44 309 618 157 246 26,000 -1 -7 41 291 582 146 237 42 291 582 151 245 28,000 -5 -10 39 275 550 139 235 39 275 550 145 245 29,000 -7 -12 38 266 532 135 233 38 268 536 142 244 31,000 -12 -16 35 248 496 125 225 35 250 500 134 241 33,000 -15 -20 --- --- --- --- --- 32 231 462 126 235 35,000 -20 -24 --- --- --- --- --- 29 211 422 115 225 BT058684 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately 12%,  fuel  flow  will  decrease  approximately  8%,  and  true  airspeed  will  be  reduced by approximately 15 knots. Figure 7A-46.  Maximum Cruise Power at 1700 RPM - ISA +30°C (Sheet 2 of 2) 7A-71