TM 1-1510-224-10 ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA WEIGHT® 12,000 POUNDS 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 18 15 83 647 647 175 177 83 647 647 178 180 2000 14 11 83 631 631 173 181 83 631 631 176 183 4000 10 7 83 615 615 171 184 83 614 614 174 187 6000 6 3 83 598 598 168 187 83 598 598 172 190 8000 2 -1 83 583 583 166 190 83 583 583 170 194 10,000 -1 -5 83 570 570 164 193 83 570 570 168 198 12,000 -5 -9 83 558 558 162 197 83 558 558 166 201 14,000 -9 -13 79 527 527 156 196 79 528 528 160 201 16,000 -13 -17 75 498 498 150 194 75 500 500 155 201 18,000 -17 -21 71 473 473 143 193 72 474 474 149 200 20,000 -21 -25 67 447 447 136 190 68 449 449 144 200 22,000 -25 -29 63 420 420 128 185 64 423 423 137 198 24,000 -30 -33 59 393 393 118 178 60 397 397 130 195 26,000 -33 -37 --- --- --- --- --- 56 370 370 122 190 28,000 -37 -40 --- --- --- --- --- 51 343 343 113 182 29,000 -40 -42 --- --- --- --- --- 49 329 329 107 177 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05285 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 2 of 2) 7-143