TM 1-1510-224-10 ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA -20°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 -3 -5 83 644 644 168 164 83 643 643 172 169 2000 -6 -9 83 625 625 167 168 83 624 624 172 173 4000 -10 -13 83 609 609 165 171 83 608 609 170 176 6000 -14 -17 83 595 595 162 174 83 594 -.594 168 179 8000 -18 -21 83 582 582 160 176 83 581 581 165 182 10,000 -22 -25 83 571 571 157 178 83 570 570 163 185 12,000 -26 -29 83 560 560 154 180 83 560 560 161 188 14,000 -30 -33 83 551 551 151 182 83 550 550 158 191 16,000 -34 -37 83 543 543 148 185 83 542 542 156 194 18,000 -38 -41 83 534 534 143 185 83 536 536 153 196 20,000 -42 -45 77 503 503 132 176 78 506 506 145 193 22,000 -45 -49 --- --- --- --- --- 73 474 474 135 187 24,000 -50 -53 --- --- --- --- --- 68 442 442 123 176 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05279 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 7-87.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -20°C (Sheet 1 of 2) 7-138