TM 1-1510-224-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA -10°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 7 5 83 649 649 164 164 83 648 648 170 169 2000 4 1 83 630 630 163 168 83 629 629 168 173 4000 0 -3 83 613 613 161 170 83 611 611 166 176 6000 -4 -7 83 597 597 158 172 83 596 596 164 178 8000 -8 -11 83 583 583 155 175 83 581 581 161 181 10,000 -12 -15 83 570 570 152 177 83 569 569 159 184 12,000 -16 -19 83 558 558 149 179 83 557 557 156 187 14,000 -20 -23 83 551 551 146 181 83 549 549 154 190 16,000 -24 -27 80 529 529 139 178 81 532 532 149 190 18,000 -27 -31 --- --- --- --- --- 77 505 505 142 187 20,000 -32 -35 --- --- --- --- --- 73 478 478 134 183 22,000 -36 -39 --- --- --- --- --- 68 447 447 121 173 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0587011 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-88.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -10°C (Sheet 1 of 2) 7A-140