TM 1-1510-223-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA + 20°C WEIGHT® 12,000 POUNDS 10,000 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 38 35 83 657 657 161 169 83 656 656 164 172 2000 34 31 83 636 636 159 172 83 635 635 162 175 4000 30 27 81 606 606 155 173 82 607 607 158 177 6000 26 23 78 576 576 150 173 79 577 577 154 178 8000 22 19 75 546 546 146 173 76 547 547 150 178 10,000 18 15 72 515 515 140 173 73 517 517 145 179 12,000 14 11 69 484 484 134 171 69 486 486 140 178 14,000 10 7 64 451 451 126 167 64 454 454 134 176 16,000 6 3 59 422 422 118 162 60 425 425 127 174 18,000 2 -1 56 396 396 109 156 57 400 400 121 172 20,000 -3 -5 52 369 369 94 140 53 374 374 114 168 22,000 -6 -9 --- --- --- --- --- 50 351 351 107 163 24,000 -10 -13 --- --- --- --- --- 46 328 328 97 155 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559012 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 7-137.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +20 °C (Sheet 2 of 2)  CA 7-224  Change 2