TM 1-1510-223-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA -30°C WEIGHT® 16,000 POUNDS 14,000 POUNDS TORQUE FUEL TOTAL TORQUE FUEL TOTAL PRESSURE PER FLOW FUEL PER FLOW FUEL ALTITUDE IFAT FAT ENGINE PER FLOW IAS TAS ENGINE PER FLOW IAS TAS ENGINE ENGINE FEET °C °C PERCENT LBS/HR LBS/HR KTS KTS PERCENT   LBS/HR    LBS/HR KTS KTS 0 -13 -15 83 644 644 158 152 83 643 643 162 156 2000 -17 -19 83 624 624 156 155 83 623 623 161 159 4000 -21 -23 83 607 607 155 158 83 605 605 160 163 6000 -25 -27 83 594 594 153 161 83 593 593 158 166 8000 -28 -31 83 582 582 150 163 83 581 581 156 169 10,000 -32 -35 83 571 571 148 165 83 570 570 154 171 12,000 -36 -39 83 560 560 145 167 83 559 559 152 174 14,000 -40 -43 83 551 551 142 169 83 550 550 149 177 16,000 -44 -47 83 544 544 140 171 83 542 542 147 180 18,000 -48 -51 83 539 539 137 173 83 538 538 144 182 20,000 -52 -55 82 528 528 131 172 83 530 530 141 184 22,000 -56 -59 75 487 487 111 152 77 493 493 132 179 24,000 -60 -63 --- --- --- --- --- 70 454 454 120 169 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05590 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately  7 percentage points (E.G., 67% - 7 percentage points = 60%), fuel flow will decrease approximately 25 LBS/HR/ENG, and true airspeed will be reduced approximately 15 knots. Figure 7-127.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA -30 °C (Sheet 1 of 2)  CA Change 2  7-203