TM 1-1510-223-10 LOITER POWER 1700 RPM ISA +20°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 37 35 34 430 860 124 132 31 415 830 124 132 2000 33 31 34 413 826 124 136 31 398 796 124 136 4000 29 27 35 395 790 124 140 32 382 764 124 140 6000 25 23 36 379 758 124 145 33 366 732 124 145 8000 21 19 36 364 728 124 149 33 351 702 124 149 10,000 17 15 37 350 700 124 154 34 336 672 124 154 12,000 14 11 38 336 672 124 159 34 323 646 124 159 14,000 10 7 39 327 654 124 164 35 313 626 124 164 16,000 6 3 39 318 636 124 170 36 304 608 124 170 18,000 2 -1 40 312 624 124 175 36 294 588 124 175 20,000 -2 -5 41 308 616 124 181 37 289 578 124 181 22,000 -5 -9 42 306 612 124 187 38 287 574 124 187 24,000 -9 -13 43 304 608 124 194 39 285 570 124 194 26,000 -13 -17 45 305 610 124 201 40 283 566 124 201 28,000 --- --- --- --- --- --- --- 41 285 570 124 208 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03609 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 7-115.  Loiter Power at 1700 RPM - ISA +20°C (Sheet 1 of 2)  IR 7-184  Change 2