TM 1-1510-224-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA WEIGHT® 12,000 POUNDS 10,000 POUNDS PRESSURE ALTITUDE IFAT FAT 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 18 15 83 646 646 173 175 83 646 646 176 178 2000 14 11 83 630 630 171 178 83 629 629 174 181 4000 10 7 83 614 614 169 181 83 613 613 172 185 6000 6 3 83 597 597 166 184 83 596 596 170 188 8000 2 -1 83 582 582 164 188 83 582 582 168 191 10,000 -1 -5 83 569 569 162 191 83 568 568 166 195 12,000 -5 -9 83 557 557 160 194 83 557 557 164 199 14,000 -9 -13 79 526 526 154 193 79 528 528 159 199 16,000 -13 -17 75 498 498 148 192 75 500 500 153 199 18,000 -17 -21 71 472 472 141 190 72 474 474 148 198 20,000 -21 -25 67 447 447 134 187 68 449 449 142 197 22,000 -25 -29 63 420 420 126 182 64 422 422 135 195 24,000 -30 -33 59 393 393 116 174 60 396 396 128 192 26,000 -33 -37 --- --- --- --- --- 55 370 370 120 187 28,000 -37 -40 --- --- --- --- --- 51 343 343 111 179 29,000 -40 -42 --- --- --- --- --- 48 329 329 104 173 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0587010 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 7A-89.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA (Sheet 2 of 2) 7A-143