TM 1-1510-224-10 ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA WEIGHT® 16,000 POUND 14,000 POUNDS PRESSURE ALTITUDE IOAT OAT TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS FEET °C °C PERCENT LBS/HR LBS/HR KTS KTS PERCENT LBS/HR LBS/HR KTS KTS 0 18 15 83 649 649 166 169 83 648 648 171 174 2000 14 11 83 633 633 164 171 83 632 632 169 177 400010 10 7 83 616 616 161 174 83 615 615 167 179 6000 6 3 83 500 600 159 176 83 599 599 164 182 8000 2 -1 83 585 585 156 178 83 584 584 162 185 10,000 -2 -5 83 572 572 153 180 83 571 571 159 188 12,000 -6 -9 82 553 553 148 180 83 556 556 156 190 14,000 -10 -13 77 521 521 138 175 78 525 525 149 188 16,000 -14 -17 --- --- --- --- --- 74 496 496 142 184 18,000 -18 -21 --- --- --- --- --- 70 470 470 133 180 20,000 -22 -25 --- --- --- --- --- 66 443 443 122 171 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05283 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately 10%,  fuel  flow  will  decrease  approximately  6%,  and  true  airspeed  will  be  reduced by approximately 10 knots. Figure 7-89.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA (Sheet 1 of 2) 7-142