TM 1-1510-224-10 ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA -10°C WEIGHT® 12,000 POUND 10,000 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 83 648 648 176 175 83 647 647 179 178 2000 4 1 83 629 629 174 179 83 629 629 177 182 4000 0 -3 83 612 612 172 182 83 611 611 175 185 6000 -4 -7 83 596 596 170 185 83 595 595 173 188 8000 -8 -11 83 582 582 168 188 83 581 581 171 192 10,000 -11 -15 83 569 569 166 192 83 569 569 169 195 12,000 -15 -19 83 558 558 163 195 83 558 558 167 199 14,000 -19 -23 83 550 550 161 199 83 549 549 165 203 16,000 -23 -27 82 534 534 158 200 82 535 535 162 206 18,000 -27 -31 78 507 507 152 199 78 508 508 157 206 20,000 -31 -35 74 481 481 146 198 75 482 482 152 206 22,000 -35 -39 69 451 451 138 194 70 453 453 145 204 24,000 -39 -43 64 421 421 128 188 65 423 423 138 201 26,000 -44 -47 59 390 390 117 178 60 394 394 130 196 28,000 -47 -50 --- --- --- --- --- 55 364 364 121 190 29,000 -49 -52 --- --- --- --- --- 52 350 350 116 186 31,000 -54 -56 --- --- --- --- --- 47 320 320 103 172 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05282 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 2 of 2) 7-141