TM 1-1510-224-10 ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA +30°C WEIGHT® 12,000 POUNDS 10,000 POUNDS PRESSURE ALTITUDE IOAT OAT TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS FEET °C °C PERCENT LBS/HR LBS/HR KTS KTS PERCENT LBS/HR LBS/HR KTS KTS 0 48 45 76 628 628 165 176 77 629 629 168 179 2000 44 41 74 599 599 161 177 75 599 599 165 181 4000 40 37 72 569 569 156 177 73 570 570 161 182 6000 36 33 70 540 540 152 178 71 541 541 157 183 8000 32 29 67 511 511 147 177 68 512 512 152 184 10,000 28 25 64 480 480 141 176 65 481 481 147 184 12,000 24 21 61 449 449 134 173 62 451 451 142 183 14,000 20 17 58 420 420 126 169 58 422 422 136 181 16,000 16 13 53 389 389 114 159 54 393 393 128 178 18,000 12 9 --- --- --- --- --- 49 362 362 118 170 20,000 8 5 --- --- --- --- --- 45 336 336 109 163 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 -- --- --- --- --- --- --- --- --- --- --- --- 26,000 -- --- --- --- --- --- --- --- --- --- --- --- 28,000- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 -- --- --- --- --- --- --- --- --- --- --- --- 33,000 -- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05292 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately 10%, fuel flow will decrease approximately  6%,  and  true  airspeed  will  be  reduced by approximately 10 knots. Figure 7-92.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +300C (Sheet 2 of 2) 7-149