TM 1-1510-223-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA 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 18 15 83 650 650 163 166 83 649 649 166 169 2000 14 11 83 633 633 161 169 83 633 633 164 172 4000 10 7 83 617 617 159 172 83 616 616 162 175 6000 6 3 83 600 600 157 175 83 599 599 161 178 8000 2 -1 83 585 585 155 178 83 584 584 159 182 10,000 -2 -5 83 572 572 153 181 83 572 572 157 185 12,000 -6 -9 82 554 554 150 183 83 555 555 154 188 14,000 -10 -13 78 523 523 144 182 78 525 525 149 187 16,000 -14 -17 74 495 495 138 181 74 496 496 143 187 18,000 -18 -21 70 469 469 132 179 71 471 471 138 187 20,000 -22 -25 67 444 444 126 177 67 446 446 133 186 22,000 -26 -29 62 417 417 117 171 63 420 420 127 184 24,000 -30 -33 58 390 390 106 162 59 394 394 120 181 26,000 -34 -37 --- --- --- --- --- 55 368 368 113 176 28,000 -38 -40 --- --- --- --- --- 50 340 340 102 168 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT055908 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 7-133.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA (Sheet 2 of 2)   CA 7-216    Change 2