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 7 5 83 629 629 149 150 83 628 628 154 154 2000 3 1 83 611 611 147 152 83 610 610 153 157 4000 -1 -3 83 594 594 145 154 83 593 586 150 160 6000 -5 -7 83 579 579 142 156 83 578 578 148 162 8000 -9 -11 83 567 567 139 158 83 565 565 146 165 10,000 -12 -15 83 555 555 136 159 83 554 554 144 167 12,000 -16 -19 83 545 545 133 161 83 544 544 141 170 14,000 -20 -23 83 539 539 130 162 83 537 537 139 172 16,000 -24 -27 81 524 524 123 159 82 527 527 135 174 18,000 -29 -31 77 496 496 107 144 78 501 501 128 170 20,000 -32 -35 --- --- --- --- --- 74 475 475 119 164 22,000 -37 -39 --- --- --- --- --- 68 442 442 103 149 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03641 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 7-130.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA -10 °C (Sheet 1 of 2)  IR Change 2  7-209