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 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 28 25 83 652 652 173 179 83 651 651 176 182 2000 24 21 83 631 631 171 182 83 630 630 174 185 4000 20 17 83 611 611 169 185 83 611 611 172 189 6000 16 13 83 595 595 167 189 83 594 594 170 192 8000 13 9 83 582 582 165 192 83 581 581 168 196 10,000 9 5 80 553 553 159 191 80 555 555 164 196 12,000 5 1 76 523 523 154 191 77 525 525 159 197 14,000 1 -3 72 492 492 147 189 73 493 493 153 196 16,000 -3 -7 68 462 462 141 187 69 464 464 147 195 18,000 -8 -11 64 435 435 133 183 65 437 437 141 194 20,000 -12 -15 60 409 409 125 179 61 412 412 135 191 22,000 -16 -19 56 385 385 114 169 57 389 389 128 189 24,000 -19 -23 --- --- --- --- --- 54 365 365 121 185 26,000 -24 -27 --- --- --- --- --- 50 341 341 112 179 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05286 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 7-90.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +10°C (Sheet 2 of 2) 7-145