TM 1-1510-223-10 LOITER POWER 1700 RPM ISA + 37°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 54 52 27 414 828 124 136 27 403 806 124 136 2000 50 48 28 396 792 124 140 26 386 772 124 140 4000 46 44 28 379 758 124 144 26 369 738 124 144 6000 42 40 29 364 728 124 149 27 353 706 124 149 8000 38 36 29 348 696 124 154 27 337 674 124 154 10,000 35 32 30 333 666 124 158 27 322 644 124 158 12,000 31 28 30 318 636 124 164 28 307 614 124 164 14,000 27 24 31 304 608 124 169 28 293 586 124 169 16,000 23 20 31 292 584 124 175 29 281 562 124 175 18,000 19 16 32 282 564 124 181 30 271 542 124 181 20,000 16 12 33 274 548 124 187 30 262 524 124 187 22,000 12 8 33 268 536 124 193 31 256 512 124 193 24,000 8 4 34 263 526 124 200 31 250 500 124 200 26,000 5 0 35 260 520 124 207 32 246 492 124 207 28,000 1 -3 --- --- --- --- --- 33 243 486 124 215 29,000 -1 -5 --- --- --- --- --- 33 243 486 124 219 31,000- --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559416 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 2 of 2)   CA Change 2  7-195