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 47 47 75 625 625 152 163 75 626 626 156 167 2000 44 41 73 596 596 148 164 74 597 597 153 168 4000 40 37 71 567 567 144 165 72 568 568 149 170 6000 36 33 69 538 538 140 165 69 539 539 145 171 8000 32 29 66 508 508 135 164 67 509 509 141 171 10,000 28 25 63 477 477 129 163 64 478 478 136 171 12,000 24 21 60 445 445 123 160 61 448 448 131 170 14,000 20 17 57 416 416 115 156 58 419 419 125 168 16,000 15 13 52 386 386 104 147 53 390 390 118 164 18,000 12 9 --- --- --- --- --- 48 359 359 108 157 20,000 7 5 --- --- --- --- --- 45 333 333 99 150 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559014 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- Figure 7-139.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +30 °C (Sheet 2 of 2)  CA 7-228  Change 2