TM 1-1510-223-10 ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA +37°C WEIGHT® 16,000 POUNDS 14,000 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 71 598 598 127 139 72 599 599 136 148 2000 50 48 --- --- --- --- --- 70 568 568 132 149 4000 46 44 --- --- --- --- --- 68 538 538 128 148 6000 42 40 --- --- --- --- --- 66 510 510 122 146 8000 38 36 --- --- --- --- --- 63 481 481 114 142 10,000 34 32 --- --- --- --- --- 59 448 448 101 131 12,000 --- --- --- --- --- --- --- --- --- --- --- --- 14,000 --- --- --- --- --- --- --- --- --- --- --- --- 16,000 --- --- --- --- --- --- --- --- --- --- --- --- 18,000 --- --- --- --- --- --- --- --- --- --- --- --- 20,000 --- --- --- --- --- --- --- --- --- --- --- --- 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03651 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 7-140.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +37 °C (Sheet 1 of 2)  IR Change 2  7-229