TM 1-1510-223-10 LOITER POWER 1700 RPM ISA + 37°C WEIGHT® 16,000 POUNDS 14,000 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 54 52 32 440 880 124 136 30 426 852 124 136 2000 50 48 33 423 846 124 140 30 409 818 124 140 4000 46 44 34 406 812 124 144 31 392 784 124 144 6000 42 40 34 391 782 124 149 31 376 752 124 149 8000 38 36 35 376 752 124 154 32 361 722 124 154 10,000 35 32 36 361 722 124 158 33 346 692 124 158 12,000 31 28 36 345 690 124 164 33 331 662 124 164 14,000 27 24 37 332 664 124 169 34 317 634 124 169 16,000 23 20 38 320 640 124 175 34 305 610 124 175 18,000 19 16 39 311 622 124 181 35 296 592 124 181 20,000 16 12 39 303 606 124 187 36 287 574 124 187 22,000 12 8 --- --- --- --- --- 36 282 564 124 193 24,000 8 4 --- --- --- --- --- 37 280 560 124 200 26,000- --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559415 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 20 LBS/HR/ENG, and true airspeed will be reduced approximately 20 knots. Figure 7-120.  Loiter Power at 1700 RPM - ISA +37°C (Sheet 1 of 2)  CA 7-194  Change 2