TM 1-1510-224-10 ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA +20°C 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 38 35 83 654 654 172 181 83 654 654 175 184 2000 34 31 83 633 633 170 184 83 633 633 173 187 4000 30 27 82 609 609 167 186 83 610 610 170 190 6000 26 23 80 579 579 162 186 80 580 580 166 191 8000 22 19 76 549 549 157 186 77 550 550 162 191 10,000 18 15 73 519 519 152 186 74 520 520 157 192 12,000 14 11 70 487 487 146 184 70 489 489 151 191 14,000 10 7 65 455 455 138 180 65 457 457 144 189 16,000 6 3 60 425 425 129 176 61 428 428 138 187 18,000 2 -1 57 399 399 120 170 58 403 403 132 185 20,000 -2 -5 --- --- --- --- --- 54 377 377 125 181 22,000 -6 -9 --- --- --- --- --- 51 354 354 117 177 24,000 -10 -13 --- --- --- --- --- 47 331 331 108 170 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000-- --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- 6T0528 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 0 knots. Figure 7-91.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +20°C (Sheet 2 of 2) 7-147