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 35 433 866 124 136 32 419 838 124 136 2000 50 48 35 418 836 124 140 32 404 808 124 140 4000 46 44 36 402 804 124 144 33 388 776 124 144 6000 42 40 36 388 776 124 149 33 373 746 124 149 8000 38 36 37 374 748 124 154 34 359 718 124 154 10,000 35 32 38 360 720 124 158 35 345 690 124 158 12,000 31 28 39 345 690 124 164 35 331 662 124 164 14,000 27 24 39 333 666 124 169 36 318 636 124 169 16,000 23 20 40 322 644 124 175 37 307 614 124 175 18,000 19 16 41 314 628 124 181 37 299 598 124 181 20,000 16 12 42 307 614 124 187 38 292 584 124 187 22,000 12 8 --- --- --- --- --- 39 287 574 124 193 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03619 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 7-119.  Loiter Power at 1700 RPM - ISA +37°C (Sheet 1 of 2)  IR 7-192  Change 2