TM 1-1510-223-10 ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER 1700 RPM ISA + 30°C WEIGHT® 12,000 POUNDS 10,000 POUNDS TORQUE FUEL TOTAL TORQUE FUEL TOTAL PRESSURE PER FLOW FUEL PER FLOW FUEL ALTITUDE IFAT FAT ENGINE PER FLOW IAS TAS ENGINE PER FLOW IAS TAS ENGINE ENGINE FEET °C °C PERCENT LBS/HR LBS/HR KTS KTS PERCENT   LBS/HR    LBS/HR KTS KTS 0 47 45 80 626 626 151 161 81 626 626 154 165 2000 43 41 78 596 596 147 162 79 597 597 151 166 40000 0 37 76 566 566 143 163 76 567 567 147 168 6000 36 33 73 537 537 138 163 74 538 538 143 168 8000 32 29 70 507 507 133 162 71 509 509 139 168 10,000 28 25 67 476 476 127 160 67 478 478 133 168 12,000 24 21 63 444 444 120 157 63 447 447 128 166 14,000 19 17 59 416 416 112 152 60 418 418 122 164 16,000 15 13 54 386 386 100 142 55 389 389 114 160 18,000 12 9 --- --- --- --- --- 50 358 358 104 152 20,000 7 5 --- --- --- --- --- 46 333 333 95 144 22,000 3 1 --- --- --- --- --- 43 314 314 82 131 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03650 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately  7 percentage points (E. G., 67% - 7 percentage points = 60%), fuel flow will decrease approximately 25 LBS/HR/ENG, and true airspeed will be reduced approximately 15 knots. Figure 7-138.  One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +30 °C (Sheet 2 of 2)  IR 7-226  Change 2