TM 1-1510-224-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA -10°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 8 5 83 647 647 173 173 83 646 646 176 176 2000 4 1 83 628 628 172 177 83 627 627 175 180 4000 0 -3 83 611 611 170 180 83 610 610 173 183 6000 -4 -7 83 595 - 595 168 183 83 594 594 171 186 8000 -8 -11 83 581 581 166 186 83 580 580 169 190 10,000 -12 -15 83 568 568 164 189 83 567 567 167 193 12,000 -15 -19 83 557 557 161 192 83 556 556 165 197 14,000 -19 -23 83 549 549 159 196 83 548 548 163 201 16,000 -23 -27 82 534 534 156 198 82 535 535 160 204 18,000 -27 -31 78 507 507 150 197 78 508 508 155 204 20,000 -31 -35 74 481 481 144 195 74 482 482 150 203 22,000 -35 -39 69 451 451 136 191 70 453 453 143 201 24,000 -39 -43 64 420 420 126 185 65 423 423 136 198 26,000 -44 -47 59 389 389 114 175 60 393 393 128 194 28,000 -47 -50 --- --- --- --- --- 55 364 364 119 187 29,000 -49 -52 --- --- --- --- --- 52 349 349 114 183 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0587012 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 2 of 2) 7A-141