TM 1-1510-223-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA -20°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 -3 -5 83 645 645 164 161 83 644 644 167 164 2000 -6 -9 83 626 626 164 165 83 625 625 167 168 4000 -10 -13 83 609 609 162 168 83 609 609 165 171 6000 -14 -17 83 595 595 160 172 83 595 595 163 175 8000 -18 -21 83 582 582 158 175 83 582 582 1629 178 10,000 -22 -25 83 571 571 156 178 83 571 571 160 181 12,000 -26 -29 83 560 560 154 181 83 560 560 158 184 14,000 -30 -33 83 551 551 152 184 83 550 550 156 188 16,000 -33 -37 83 543 543 150 187 83 542 542 154 192 18,000 -37 -41 83 535 535 147 190 83 536 536 151 195 20,000 -41 -45 78 505 505 141 188 79 507 507 146 194 22,000 -45 -49 73 474 474 134 185 74 476 476 140 193 24,000 -50 -53 68 443 474 126 181 69 445 445 133 190 26,000 -54 -57 63 410 410 116 174 63 413 413 126 187 28,000 -58 -60 56 373 373 99 156 58 379 379 117 181 29,000 -60 -62 --- --- --- --- --- 55 361 361 112 177 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT055904 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 7-129.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA -20 °C (Sheet 2 of 2)  CA 7-208  Change 2