TM 1-1510-223-10 ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA +20°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 37 35 83 636 636 145 153 83 635 635 150 158 2000 33 31 83 616 616 142 155 83 614 614 148 161 4000 29 27 83 596 596 139 157 83 595 595 146 163 6000 26 23 82 571 571 134 156 83 573 573 142 165 8000 21 19 78 540 540 126 152 83 543 543 136 163 10,000 17 15 74 508 508 115 144 82 512 512 130 161 12,000 13 11 --- --- --- --- --- 71 480 480 122 156 14,000 9 7 --- --- --- --- --- 65 446 446 109 145 16,000 --- --- --- --- --- --- --- --- --- --- --- --- 18,000 --- --- --- --- --- --- --- --- --- --- --- --- 20,000 --- --- --- --- --- --- --- --- --- --- --- --- 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03647 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 7-136.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +20 °C (Sheet 1 of 2)  IR Change 2  7-221