TM 1-1510-224-10 ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA +37°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 55 52 68 600 600 154 166 68 600 600 159 171 2000 51 48 67 570 570 151 168 67 571 571 156 174 4000 47 44 65 541 541 147 169 66 542 542 153 176 6000 43 40 63 514 514 143 170 64 515 515 150 177 8000 39 36 61 485 485 138 169 62 487 487 145 178 10,000 35 32 58 455 455 131 167 59 457 457 140 177 12,000 31 28 55 423 423 123 316 56 426 426 134 175 14,000 26 24 51 393 393 112 153 52 397 397 127 173 16,000 23 20 --- --- --- --- --- 49 368 368 119 168 18,000 19 16 --- --- --- --- --- 44 338 338 108 158 20,000 --- --- --- --- --- --- --- --- --- --- --- --- 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 ---- --- --- --- --- --- --- --- --- --- --- --- 33,000 ---- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05291 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 I0 knots. Figure 7-93.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +37°C (Sheet 2 of 2) 7-151