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 IFAT FAT 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 54 52 68 599 599 152 164 68 600 600 157 169 2000 51 48 66 570 570 148 166 67 571 571 154 171 4000 47 44 65 541 541 145 167 65 542 542 151 174 6000 43 40 63 513 513 141 168 64 515 515 148 175 8000 39 36 61 485 485 136 167 62 487 487 143 176 10,000 35 32 58 454 454 129 164 59 457 457 138 175 12,000 31 28 54 422 422 121 159 55 425 425 132 173 14,000 27 24 --- --- --- --- --- 52 396 396 125 170 16,000 23 20 --- --- --- --- --- 48 367 367 117 165 18,000 19 16 --- --- --- --- --- 44 337 337 106 156 20,000 --- --- --- --- --- --- --- --- --- --- --- --- 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT058702 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 7A-93.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +37°C (Sheet 2 of 2) 7A-151