TM 1-1510-223-10 ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA 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 17 15 83 629 629 148 151 83 628 628 153 156 2000 13 11 83 613 613 146 153 83 612 612 151 159 4000 9 7 83 597 597 143 155 83 596 596 149 161 6000 5 3 83 581 581 140 157 83 580 580 146 163 8000 1 -1 83 568 568 137 158 83 567 567 144 166 10,000 -2 -5 83 556 556 134 160 83 555 555 142 168 12,000 -6 -9 83 547 547 131 161 83 545 545 140 171 14,000 -11 -13 79 515 515 120 154 80 519 519 133 169 16,000 -14 -17 --- --- --- --- --- 75 490 490 125 165 18,000 -18 -21 --- --- --- --- --- 71 464 464 116 159 20,000 -23 -25 --- --- --- --- --- 66 437 437 101 144 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 7-132.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA (Sheer 1 of 2)    IR Change 2  7-213