TM 1-1510-224-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA -20°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 -3 -5 83 643 643 165 162 83 642 642 170 166 2000 -6 -9 83 624 624 164 166 83 623 623 169 171 4000 -10 -13 83 608 608 162 169 83 607 607 168 174 6000 -14 -17 83 594 594 160 171 83 592 592 166 177 8000 -18 -21 83 581 581 157 173 83 580 580 163 180 10,000 -22 -25 83 570 570 155 176 83 569 569 161 182 12,000 -26 -29 83 559 559 152 178 83 558 558 158 185 14,000 -30 -33 83 549 549 149 180 83 548 548 156 188 16,000 -34 -37 83 542 542 146 182 83 540 540 153 191 18,000 -38 -41 82 533 533 141 182 83 535 535 151 194 20,000 -41 -45 --- --- --- --- --- 78 506 506 143 190 22,000 -45 -49 --- --- --- --- --- 73 474 474 133 184 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0587013 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-87.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -20°C (Sheet 1 of 2) 7A-138