TM 1-1510-224-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA 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 18 15 83 648 648 163 166 83 647 647 169 171 2000 14 11 83 632 632 161 169 83 631 631 167 174 4000 10 7 83 615 615 159 171 83 614 614 165 177 6000 6 3 83 599 599 156 173 83 598 598 162 180 8000 2 -1 83 584 584 153 176 83 583 583 160 183 10,000 -2 -5 83 571 571 150 178 83 570 570 157 185 12,000 -6 -9 82 553 553 146 178 83 555 555 154 188 14,000 -10 -13 77 520 520 135 171 78 524 524 147 185 16,000 -14 -17 --- --- --- --- --- 74 495 495 139 182 18,000 -18 -21 --- --- --- --- --- 70 469 469 131 177 20,000 --- --- --- --- --- --- --- --- --- --- --- --- 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT058709 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-89.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA (Sheet 1 of 2) 7A-142