TM 1-1510-224-10 MAXIMUM RANGE 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 -12 -15 83 639 639 175 168 83 639 639 178 170 2000 -16 -19 83 620 620 174 172 83 619 619 177 174 4000 -20 -23 83 601 601 173 176 83 601 601 176 176 6000 -24 -27 83 588 588 171 179 83 587 587 174 182 8000 -28 -31 83 576 576 169 182 83 576 576 172 186 10,000 -32 -35 83 566 566 167 185 83 565 565 170 189 12,000 -35 -39 83 555 555 165 189 83 554 554 168 193 14,000 -39 -43 83 545 545 163 192 83 545 545 167 196 16,000 -43 -47 83 538 538 161 195 83 537 537 165 165 18,000 -47 -51 83 533 533 158 199 83 532 532 163 204 20,000 -51 -55 83 529 529 156 203 83 527 527 161 208 22,000 -55 -59 78 498 498 149 200 79 499 499 155 207 24,000 -59 -63 72 461 461 141 196 73 464 464 148 205 26,000 -63 -67 65 421 421 130 188 66 425 425 139 200 28,000 -68 -70 58 378 378 115 174 59 384 384 129 193 29,000 -69 -72 - - - - - - - - - - - - - - - 56 364 364 123 188 31,000 -74 -76 - - - - - - - - - - - - - - - 49 327 327 111 176 33,000 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 35,000 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - BT0587016 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately 10%,  fuel  flow  will  decrease  approximately  6%,  and  true  airspeed  will  be  reduced by approximately 10 knots. Figure 7A-86.  One Engine Inoperative Max Cruise Power at 1700 RPM (Engine Anti-Ice Off) - ISA -30°C (Sheet 1 of 2) 7A-136