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 -2 -5 83 641 641 174 170 83 641 641 177 173 2000 -6 -9 83 622 622 173 175 83 621 621 176 177 4000 -10 -13 83 606 606 172 178 83 605" 605 175 181 6000 -14 -17 83 592 592 170 181 83 591 591 173 184 8000 -18 -21 83 579 579 167 184 83 579 579 171 188 10,000 -22 -25 83 568 568 165 187 83 567 567 169 191 12,000 -25 -29 83 557 557 163 191 83 557 557 167 195 14,000 -29 -33 83 548 548 161 194 83 547 547 165 198 16,000 -33 -37 83 540 540 159 198 83 539 539 163 203 18,000 -37 -41 83 534 534 157 201 83 533 533 161 206 20,000 -41 -45 79 508 508 150 200 79 509 509 156 206 22,000 -45 -49 74 477 477 143 197 74 478 478 149 205 24,000 -49 -53 69 445 445 135 192 69 447 447 142 202 26,000 -53 -57 63 412 412 125 185 64 415 415 135 199 28,000 -57 -60 --- --- --- --- --- 58 381 381 126 193 29,000 -59 -62 --- --- --- --- --- 55 363 363 120 188 31,000 -64 -66 --- --- --- --- --- 49 328 328 107 176 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0587014 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 2 of 2) 7A-139