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 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 48 45 76 627 627 162 173 76 628 628 166 178 2000 44 41 74 598 598 159 175 75 599 599 163 179 4000 40 37 72 569 569 154 175 73 570' 570 159 180 6000 36 33 70 540 540 150 176 70 541 541 155 181 8000 32 29 67 510 510 145 175 68 511 511 150 182 10,000 28 25 64 479 479 139 174 65 481 481 145 181 12,000 24 21 61 448 448 132 171 62 450 450 140 180 14,000 20 17 57 419 419 124 166 58 422 422 134 179 16,000 16 13 53 388 388 111 156 54 392 392 127 176 18,000 12 9 --- --- --- --- --- 49 361 361 116 168 20,000 8 5 --- --- --- --- --- 45 335 335 106 159 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT08704 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 1 0 knots. Figure 7A-92.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +30°C (Sheet 2 of 2) 7A-149