TM 1-1510-223-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA + 20°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 37 35 83 659 659 152 160 83 658 658 157 165 2000 33 31 83 636 636 148 161 83 637 637 263 168 4000 29 27 80 603 603 143 160 81 605 605 150 168 6000 25 23 77 572 572 136 158 78 574 574 145 167 8000 21 15 70 509 509 118 147 75 544 544 139 166 10,000 17 15 70 509 509 118 147 71 513 513 132 164 12,000 14 11 --- --- --- --- --- 68 481 481 125 160 14,000 9 7 --- --- --- --- --- 62 447 447 112 150 16,000 --- --- --- --- --- --- --- --- --- --- --- --- 18,000 --- --- --- --- --- --- --- --- --- --- --- --- 20,000 --- --- --- --- --- --- --- --- --- --- --- --- 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559011 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 1 of 2)  CA Change 2  7-223