TM 1-1510-224-10 ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA -30°C WEIGHT® 16,000 POUND 14,000 POUNDS PRESSURE ALTITUDE IOAT OAT 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 -13 -15 83 642 642 169 162 83 641 641 173 166 2000 -16 -19 83 622 622 167 165 83 621 621 172 170 4000 -20 -23 83 604 604 167 170 83 603 693 171 174 6000 -24 -27 83 591 591 164 172 83 590 590 170 178 8000 -28 -31 83 580 580 162 175 83 579 579 167 180 10,000 -32 -35 83 569 569 159 177 83 568 568 165 183 12,000 -36 -39 83 558 558 157 179 83 557 557 163 186 14,000 -40 -43 83 549 549 154 182 83 548 548 160 189 16,000 -44 -47 83 542 542 150 184 83 540 540 158 192 18,000 -47 -51 83 537 537 147 186 83 535 535 155 195 20,000 -51 -55 83 530 530 143 186 83 531 531 152 198 22,000 -56 -59 76 492 492 128 173 78 496 496 143 193 24,000 -59 -63 --- --- --- --- --- 71 458 458 132 184 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05277 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 7-86.  One Engine Inoperative Max Cruise Power at 1700 RPM (Engine Anti-Ice Off) - ISA -300C (Sheet 1 of 2) 7-136