TM 1-1510-224-10 ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA -10°C 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 8 5 83 650 650 167 167 83 649 649 172 171 2000 4 -1 83 631 631 166 170 83 630 630 171 175 4000 0 -3 83 614 614 163 172 83 613 613 168 178 6000 -4 -7 83 598 598 161 175 83 597 597 166 181 8000 -8 -11 83 584 584 158 177 83 583 583 164 183 10,000 -12 -15 83 571 571 155 179 83 570 570 161 186 12,000 -16 -19 83 560 560 152 181 83 559 559 159 189 14,000 -20 -23 83 552 552 149 184 83 551 551 156 192 16,000 -24 -27 80 529 529 142 181 81 532 532 151 193 18,000 -28 -31 76 502 502 130 173 77 505 505 144 190 20,000 -31 -35 --- --- --- --- --- 73 479 479 136 186 22,000 -36 -39 --- --- --- --- --- 68 448 448 125 177 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05281 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 7-88.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -10°C (Sheet 1 of 2) 7-140