TM 1-1510-223-10 ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA -30°C WEIGHT® 16,000 POUNDS 14,000 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 83 623 623 151 146 83 623 623 156 150 2000 -17 -19 83 604 604 150 149 83 603 603 154 153 4000 -21 -23 83 586 586 148 152 83 585 585 153 156 6000 -25 -27 83 571 571 146 154 83 570 570 151 159 8000 -29 -31 83 561 561 144 156 83 560 560 149 162 10,000 -33 -35 83 552 552 141 158 83 550 550 147 164 12,000 -36 -39 83 543 543 138 159 83 542 542 145 167 14,000 -40 -43 83 536 536 135 161 83 535 535 143 170 16,000 -44 -47 83 531 531 132 162 83 529 529 140 172 18,000 -48 -51 83 527 527 128 163 83 526 526 138 175 20,000 -52 -55 83 526 526 124 163 83 523 523 135 177 22,000 -56 -59 --- --- --- --- --- 78 491 491 126 172 24,000 -60 -63 --- --- --- --- --- 71 451 451 112 159 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03637 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 1 of 2)  IR Change 2  7-201