TM 1-1510-223-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA 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 17 15 83 652 652 152 157 83 651 651 159 162 2000 13 11 83 635 635 152 160 83 634 634 157 165 4000 9 7 83 618 618 150 162 83 617 617 155 168 6000 6 3 83 601 601 147 164 83 601 601 153 170 8000 2 -1 83 586 586 144 166 83 585 585 151 173 10,000 -2 -5 83 574 574 142 168 83 573 573 149 176 12,000 -6 -9 81 550 550 135 166 82 553 553 145 177 14,000 -10 -13 76 517 517 125 160 77 521 521 138 174 16,000 -15 -17 72 486 486 109 145 73 492 492 130 171 18,000 -18 -21 --- --- --- --- --- 69 466 466 121 165 20,000 -22 -25 --- --- --- --- --- 65 439 439 109 155 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT055907 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 7-133.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA (Sheet 1 of 2)   CA Change 2  7-215