TM 1-1510-223-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA + 10°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 23 25 83 656 656 153 159 83 655 655 158 164 2000 23 21 83 634 634 150 161 83 633 633 156 166 4000 20 17 83 614 614 148 163 83 613 613 154 169 6000 16 13 83 598 598 145 165 83 597 597 152 172 8000 12 9 82 580 580 141 166 83 582 582 149 174 10,000 8 5 77 544 544 131 160 78 547 547 142 171 12,000 3 1 73 513 513 122 153 74 517 517 135 169 14,000 0 -3 --- --- --- --- --- 70 485 485 127 165 16,000 -4 -7 --- --- --- --- --- 66 455 455 117 158 18,000 -9 -11 --- --- --- --- --- 62 427 427 101 143 20,000 --- --- --- --- --- --- --- --- --- --- --- --- 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT055909 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 7-135.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +10 °C (Sheet 1 of 2)  CA Change 2  7-219