TM 1-1510-223-10 LOITER POWER 1700 RPM ISA + 10°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 27 25 32 430 860 124 130 29 414 828 124 130 2000 23 21 32 413 826 124 134 29 397 794 124 134 4000 19 17 33 396 792 124 138 30 381 762 124 138 6000 15 13 33 379 758 124 142 30 365 730 124 142 8000 11 9 34 364 728 124 147 31 351 702 124 147 10,000 7 5 35 352 704 124 151 32 339 678 124 151 12,000 3 1 36 338 676 124 156 32 324 648 124 156 14,000 0 -3 36 325 650 124 161 33 311 622 124 161 16,000 -4 -7 37 313 626 124 166 33 299 598 124 166 18,000 -8 -11 37 303 606 124 172 34 288 576 124 172 20,000 -12 -15 38 295 590 124 178 35 280 560 124 178 22,000 -15 -19 39 294 588 124 184 35 274 548 124 184 24,000 -19 -23 40 293 586 124 190 36 271 542 124 190 26,000 -23 -27 42 294 588 124 297 37 272 544 124 197 28,000 -27 -30 43 296 592 124 204 38 272 544 124 204 29,000 -28 -32 43 297 594 124 208 39 273 546 124 208 31,000 -32 -36 --- --- --- --- --- 40 276 552 124 215 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT055949 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 7-114.  Loiter Power at 1700 RPM - ISA +10°C (Sheet 1 of 2)  CA 7-182  Change 2