TM 1-1510-223-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA + 37°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 54 52 67 598 598 142 154 67 598 598 147 159 2000 50 48 65 568 568 139 156 66 569 569 144 161 4000 46 44 64 539 539 136 157 64 540 540 141 163 6000 42 40 62 512 512 132 158 63 513 513 138 165 8000 38 36 60 483 483 127 157 61 484 484 134 165 10,000 34 32 57 452 452 120 154 58 454 454 129 164 12,000 30 28 54 420 420 112 149 55 423 423 123 162 14,000 26 24 50 391 391 102 141 51 394 394 117 160 16,000 23 20 --- --- --- --- --- 48 365 365 109 155 18,000 18 16 --- --- --- --- --- 43 336 336 99 146 20,000 --- --- --- --- --- --- --- --- --- --- --- --- 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559016 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 7-141.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +37 °C (Sheet 2 of 2)  CA 7-232  Change 2