TM 1-1510-224-10 ONE-ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA +10°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 28 25 83 651 651 171 177 83 650 650 174 180 2000 24 21 83 629 629 169 180 83 629 629 172 183 4000 20 17 83 610 610 167 183 83 61 610 170 186 6000 16 13 83 593 593 165 186 83 593 593 168 190 8000 12 9 83 580 580 163 189 83 580 580 166 193 10,000 8 5 79 553 553 157 189 80 554 554 162 194 12,000 5 1 76 523 523 152 188 76 524 524 157 194 14,000 1 -3 72 491 491 145 187 72 493 493 151 194 16,000 -4 -7 68 462 462 139 184 69 464 464 145 193 18,000 -8 -11 64 435 435 131 181 65 437 437 139 191 20,000 -12 -15 60 409 409 123 176 61 412 412 133 189 22,000 -16 -19 56 384 384 111 165 57 388 388 126 186 24,000 -19 -23 --- --- --- --- --- 53 364 364 119 182 26,000 -24 -27 --- --- --- --- --- 50 341 341 110 176 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT068708 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 I0 knots. Figure 7A-90.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +10°C (Sheet 2 of 2) 7A-145