TM 1-1510-223-10 ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA -30°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 -13 -15 83 622 622 159 153 83 622 622 162 156 2000 -17 -19 83 603 603 158 157 83 602 602 161 159 4000 -21 -23 83 585 585 157 160 83 584 584 160 163 6000 -24 -27 83 569 569 156 163 83 569 569 159 166 8000 -28 -31 83 559 559 154 166 83 558 558 157 170 10,000 -32 -35 83 550 550 152 169 83 549 549 155 173 12,000 -36 -39 83 541 541 150 172 83 541 541 153 176 14,000 -40 -43 83 534 534 148 175 83 533 533 151 179 16,000 -44 -47 83 528 528 146 179 83 528 528 149 183 18,000 -48 -51 83 525 525 144 181 83 524 524 147 186 20,000 -51 -55 83 522 522 141 184 83 521 521 145 189 22,000 -56 -59 79 494 494 135 182 79 495 495 140 189 24,000 -60 -63 72 456 456 127 178 73 459 459 133 186 26,000 -64 -67 65 415 415 115 168 66 419 419 125 181 28,000 -68 -70 57 372 372 97 149 59 379 379 115 174 29,000 -70 -5 --- --- --- --- --- 55 359 359 110 169 31,000 -72 -9 --- --- --- --- --- 49 322 322 96 155 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03638 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 7-126.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA-30 °C (Sheet 2 of 2)  IR 7-202  Change 2