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 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 47 45 75 625 625 151 161 76 627 627 159 170 2000 43 41 73 595 595 146 161 74 597 597 155 170 4000 39 37 71 565 565 139 158 72 568 568 150 170 6000 35 33 68 535 535 130 153 69 538 538 144 169 8000 32 29 --- --- --- --- --- 67 508 508 138 167 10,000 28 25 --- --- --- --- --- 63 476 476 129 162 12,000 ---- --- --- --- --- --- --- --- --- --- --- --- 14,000 ---- --- --- --- --- --- --- --- --- --- --- --- 16,000 --- --- --- --- --- --- --- --- --- --- --- --- 18,000 --- --- --- --- --- --- --- --- --- --- --- --- 20,000 --- --- --- --- --- --- --- --- --- --- --- --- 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05289 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 7-92.  One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +30°C (Sheet 1 of 2) 7-148