TM 1-1510-223-10 LOITER POWER 1700 RPM ISA 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 17 15 26 394 788 124 128 24 383 766 124 128 2000 13 11 26 379 758 124 132 24 368 736 124 132 4000 9 7 27 364 728 124 136 24 353 706 124 136 6000 5 3 27 350 700 124 140 25 338 676 124 140 8000 1 -1 28 336 672 124 144 25 324 648 124 144 10,000 -3 -5 28 322 644 124 149 26 310 620 124 149 12,000 -7 -9 29 307 614 124 153 26 296 592 124 153 14,000 -10 -13 29 294 588 124 158 27 283 5666 124 158 16,000 -14 -17 30 281 562 124 163 27 271 542 124 163 18,000 -18 -21 30 271 542 124 169 28 260 520 124 169 20,000 -22 -25 31 262 524 124 174 28 251 502 124 174 22,000 -26 -29 32 256 512 124 180 29 244 488 124 180 24,000 -29 -33 32 251 502 124 186 30 239 478 124 186 26,000 -33 -37 33 247 494 124 193 30 234 468 124 193 28,000 -37 -40 34 245 490 124 200 31 230 460 124 200 29,000 -39 -42 34 246 492 124 203 31 229 458 124 203 31,000 -42 -46 35 249 498 124 211 32 230 460 124 211 33,000 -46 -50 36 252 504 124 218 33 233 466 124 218 35,000 -50 -54 37 256 512 124 226 34 236 472 124 226 BT055948 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 7-112.  Loiter Power at 1700 RPM - ISA (Sheet 2 of 2)  CA Change 2  7-179