TM 1-1510-224-10 ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA -30°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 -12 -15 83 640 640 177 170 83 640 640 180 172 2000 -16 -19 83 621 621 176 174 83 620 620 179 177 4000 -20 -23 83 603 603 175 178 83 602 602 178 181 6000 -24 -27 83 589 589 174 181 83 589 589 177 184 8000 -28 -31 83 578 578 171 184 83 577 577 175 188 10,000 -32 -35 83 567 567 169 188 83 567 567 173 191 12,000 -35 -39 83 557 557 167 191 83 556 556 171 195 14,000 -39 -43 83 547 547 165 194 83 546 546 169 199 16,000 -43 -47 83 539 539 163 198 83 539 539 167 203 18,000 -47 -51 83 534 534 161 202 83 533 533 165 207 20,000 -51 -55 83 530 530 158 205 83 529 529 163 210 22,000 -55 -59 78 498 498 151 203 79 500 500 157 210 24,000 -59 -63 73 462 462 143 199 73 465 465 150 207 26,000 -63 -67 66 422 422 132 191 67 426 426 141 203 28,000 -68 -70 58 380 380 118 178 59 384 384 131 195 29,000 -69 -72 --- --- --- --- --- 56 365 365 125 191 31,000 -73 -76 --- --- --- --- --- 50 328 328 113 179 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05278 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately 100%, fuel flow will decrease approximately 6%, and true airspeed will be reduced by approximately 10 knots. Figure 7-86.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -30°C (Sheet 2 of 2) 7-137