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 83 642 642 165 159 83 642 642 168 161 2000 -17 -19 83 623 623 164 163 83 622 622 167 165 4000 -20 -23 83 605 605 164 167 83 604 604 167 169 6000 -24 -27 83 592 592 162 170 83 591 591 165 173 8000 -28 -31 83 580 580 160 173 83 579 579 163 176 10,000 -32 -35 83 569 569 158 176 83 569 569 161 179 12,000 -36 -39 83 558 558 156 179 83 558 558 159 183 14,000 -40 -43 83 549 549 154 182 83 548 548 157 186 16,000 -44 -47 83 541 541 152 185 83 541 541 155 189 18,000 -47 -51 83 536 536 150 189 83 536 536 153 193 20,000 -51 -55 83 531 531 147 191 83 531 531 151 197 22,000 -55 -59 77 495 495 140 188 78 497 497 145 195 24,000 -59 -63 71 458 458 131 184 72 460 460 138 192 26,000 -64 -67 65 418 418 121 177 65 421 421 130 188 28,000 -68 -70 57 375 375 105 160 58 380 380 120 181 29,000 -70 -72 --- --- --- --- --- 55 361 361 115 177 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT055902 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 7-127.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA -30 °C (Sheet 2 of 2)  CA 7-204  Change 2