TM 1-1510-223-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA  + 10°C WEIGHT® 12,000 POUNDS 10,000 POUNDS TORQUE FUEL TOTAL TORQUE FUEL TOTAL PRESSURE PER FLOW FUEL PER FLOW FUEL ALTITUDE IFAT FAT ENGINE PER FLOW IAS TAS ENGINE PER FLOW IAS TAS ENGINE ENGINE FEET °C °C PERCENT LBS/HR LBS/HR KTS KTS PERCENT   LBS/HR    LBS/HR KTS KTS 0 28 25 83 654 654 162 167 83 653 653 165 170 2000 24 21 83 632 632 160 170 83 632 632 163 174 4000 20 17 83 613 613 158 173 83 612 612 161 177 6000 16 13 83 596 596 156 177 83 596 596 159 180 8000 12 9 83 584 584 154 180 83 583 583 157 183 10,000 8 5 78 549 549 148 178 79 551 551 152 183 12,000 4 1 75 520 520 142 178 76 521 521 147 183 14,000 0 -3 71 488 488 136 176 72 490 490 142 182 16,000 -4 -7 67 459 459 130 173 68 461 461 136 181 18,000 -8 -11 63 432 432 122 170 64 434 434 130 180 20,000 -12 -15 59 406 406 114 164 60 409 409 124 178 22,000 -16 -19 55 381 381 102 154 57 386 386 118 176 24,000 -20 -23 --- --- --- --- --- 53 362 362 110 171 26,000 -24 -27 --- --- --- --- --- 49 338 338 101 164 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559010 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately  7 percentage points (E.G., 67% - 7 percentage points = 60%), fuel flow will decrease approximately 25 LBS/HR/ENG, and true airspeed will be reduced approximately 15 knots. Figure 7-135.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +10 °C (Sheet 2 of 2)  CA 7-220  Change 2