TM 1-1510-223-10 LOITER POWER 1700 RPM ISA -30°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 -14 -15 32 408 816 124 121 30 396 792 124 121 2000 -18 -19 33 390 780 124 125 30 379 758 124 125 4000 -21 -23 33 373 746 124 128 30 362 724 124 128 6000 -25 -27 34 358 716 124 132 31 346 692 124 132 8000 -29 -31 34 343 686 124 136 31 331 662 124 136 10,000 -33 -35 35 329 658 124 140 32 317 634 124 140 12,000 -37 -39 35 316 632 124 144 32 304 608 124 144 14,000 -41 -43 36 306 612 124 149 33 293 586 124 149 16,000 -45 -47 37 298 596 124 153 33 283 566 124 153 18,000 -48 -51 37 292 584 124 158 34 275 550 124 158 20,000 -52 -55 38 287 574 124 163 35 270 540 124 163 22,000 -56 -59 39 284 568 124 169 36 267 534 124 169 24,000 -60 -63 40 281 562 124 174 36 263 526 124 174 26,000 -63 -67 40 279 558 124 180 37 261 522 124 180 28,000 -67 -70 41 278 556 124 186 37 259 518 124 186 29,000 -69 -72 42 281 562 124 190 37 258 516 124 190 31,000 -73 -76 43 286 572 124 196 39 263 526 124 196 33,000 -77 -80 44 291 582 124 203 40 267 534 124 203 35,000 -80 -84 --- --- --- --- --- 41 271 542 124 210 BT03599 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 7-105.  Loiter Power at 1700 RPM - ISA -30°C (Sheet 1 of 2)  IR 7-164  Change 2