TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA +30°C WEIGHT® 16,000 POUNDS 14,000 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 223 236 82 635 1270 224 238 2000 46 41 79 606 1212 218 238 80 606 1212 220 240 4000 42 37 77 577 1154 213 239 77 577 1154 215 242 6000 38 33 75 548 1096 208 241 75 548 1096 210 244 8000 35 29 72 520 1040 203 242 72 520 1040 205 245 10,000 31 25 69 493 986 197 243 70 493 986 200 247 12,000 27 21 66 462 924 190 243 66 462 924 194 247 14,000 23 17 62 433 866 183 242 63 434 868 187 246 16,000 19 13 58 403 806 175 238 58 404 808 179 244 18,000 14 9 53 373 746 164 232 53 374 748 170 239 20,000 10 5 49 347 694 155 227 50 348 696 161 236 22,000 6 1 46 327 654 146 222 47 328 656 154 233 24,000 2 -3 43 306 612 136 214 44 308 616 146 230 26,000 -2 -7 --- --- --- --- --- 41 290 580 138 225 28,000 -6 -10 --- --- --- --- --- 38 273 546 128 218 29,000 -8 -12 --- --- --- --- --- 37 264 528 122 212 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT058683 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 1 of 2) 7A-70