TM 1-1510-224-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER. 1700 RPM ISA +20°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 38 35 83 653 653 170 178 83 653 653 173 182 2000 34 31 83 632 632 168 181 83 632 632 171 185 4000 30 27 82 609 609 165 184 82 610 610 168 188 6000 26 23 79 578 578 160 184 80 580 580 164 189 8000 22 19 76 548 548 155 184 77 550 550 160 189 10,000 18 15 73 518 518 150 183 73 519 519 155 189 12,000 14 11 69 487 487 144 182 70 489 489 150 189 14,000 10 7 65 454 454 136 178 65 456 456 143 187 16,000 6 3 60 425 425 127 173 61 427 427 136 185 18,000 2 -1 57 398 398 118 166 58 402 402 130 183 20,000 -2 -5 --- --- --- --- --- 54 376 376 123 179 22,000 -6 -9 --- --- --- --- --- 50 353 353 115 174 24,000 -10 -13 --- --- --- --- --- 47 330 330 105 166 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT068706 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-91.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +20°C (Sheet 2 of 2) 7A-147