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 27 25 83 633 633 156 161 83 632 632 159 164 2000 24 21 83 611 611 154 164 83 611 611 157 167 4000 20 17 83 592 592 152 167 83 591 591 155 170 6000 16 13 83 575 575 150 170 83 575 575 153 174 8000 12 9 83 564 564 148 173 83 563 563 151 177 10,000 8 5 82 548 548 144 175 82 550 550 149 179 12,000 4 1 78 518 518 139 174 78 520 520 144 179 14,000 0 -3 73 487 487 132 171 74 489 489 138 178 16,000 -4 -7 69 458 458 125 168 70 460 460 132 177 18,000 -8 -11 65 431 431 118 164 65 433 433 127 175 20,000 -12 -15 60 405 405 109 157 61 408 408 120 173 22,000 -17 -19 56 380 380 96 145 58 384 384 113 169 24,000 -20 -23 --- --- --- --- --- 54 361 361 106 164 26,000 -24 -27 --- --- --- --- --- 50 337 337 96 156 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03646 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 7-134.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +10 °C (Sheet 2 of 2)   IR 7-218  Change 2