TM 1-1510-223-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA  -10°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 7 5 83 652 652 156 156 83 651 651 160 160 2000 3 1 83 633 633 154 159 83 632 632 159 164 4000 -1 -3 83 616 616 152 161 83 615 615 157 166 6000 -4 -7 83 600 600 149 163 83 599 599 155 169 8000 -8 -11 83 586 586 146 165 83 585 585 152 172 10,000 -12 -15 83 573 573 144 167 83 572 572 150 175 12,000 -16 -19 83 561 561 141 169 83 560 560 148 177 14,000 -20 -23 83 554 554 138 171 83 553 553 145 180 16,000 -24 -27 79 525 525 129 166 80 529 529 140 179 18,000 -28 -31 75 498 498 116 156 77 502 502 133 177 20,000 -32 -35 --- --- --- --- --- 73 476 476 125 172 22,000 -36 -39 --- --- --- --- --- 67 444 444 112 160 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT055905 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 7-131.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA -10 °C (Sheet 1 of 2)  CA Change 2  7-211