TM 1-1510-224-10 ONE-ENGINE INOPERATIVE: MAXIMUM CRUISE POWER 1700 RPM ISA -30°C WEIGHT® 16,000 POUNDS 14,000 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 -13 -15 83 641 641 166 160 83 640 640 171 164 2000 -17 -19 83 621 621 165 163 83 620 620 170 168 4000 -20 -23 83 603 603 164 167 83 602 602 169 172 6000 -24 -27 83 590 590 162 170 83 589 589 168 175 8000 -28 -31 83 578 578 159 172 83 577 577 165 178 10,000 -32 -35 83 568 568 157 175 83 566 566 163 181 12,000 -36 -39 83 557 557 154 177 83 556 556 160 184 14,000 -40 -43 83 548 548 151 179 83 546 546 158 186 16,000 -44 -47 83 540 540 148 181 83 539 539 155 189 18,000 -48 -51 83 536 536 145 183 83 534 534 153 192 20,000 -52 -55 83 530 530 140 183 83 530 530 150 195 22,000 -55 -59 --- --- --- --- --- 77 495 495 141 190 24,000 -60 -63 --- --- --- --- --- 71 457 457 129 181 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0587015 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-86.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA -30°C (Sheet 2 of 2) 7A-137