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 27 25 83 634 634 146 152 83 633 633 152 157 2000 23 21 83 613 613 144 154 83 612 612 149 160 4000 19 17 83 594 594 141 156 83 593 593 147 162 6000 15 13 83 577 577 138 157 83 576 576 145 165 8000 12 9 83 566 566 135 159 83 564 564 143 167 10,000 7 5 80 543 543 128 156 81 546 546 138 167 12,000 3 1 76 512 512 118 149 77 516 516 131 165 14,000 0 -3 --- --- --- --- --- 72 484 484 123 160 16,000 -5 -7 --- --- --- --- --- 68 454 454 112 152 18,000 --- --- --- --- --- --- --- --- --- --- --- --- 20,000 --- --- --- --- --- --- --- --- --- --- --- --- 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- 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 7-134.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +10 °C (Sheet 1 of 2)  IR Change 2  7-217