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 30 412 824 124 121 28 400 800 124 121 2000 -18 -19 30 394 788 124 125 28 382 764 124 125 4000 -21 -23 31 376 752 124 128 28 364 728 124 128 6000 -25 -27 31 360 720 124 132 29 347 694 124 132 8000 -29 -31 32 345 690 124 136 29 332 664 124 136 10,000 -33 -35 33 330 660 124 140 30 317 634 124 140 12,000 -37 -39 33 316 632 124 144 30 303 606 124 144 14,000 -41 -43 34 305 610 124 149 31 291 582 124 149 16,000 -45 -47 35 295 590 124 153 32 281 562 124 153 18,000 -48 -51 35 288 576 124 158 33 272 544 124 158 20,000 -52 -55 36 282 564 124 163 34 266 532 124 163 22,000 -56 -59 37 279 558 124 169 34 261 522 124 169 24,000 -60 -63 38 275 550 124 174 34 257 514 124 174 26,000 -63 -67 38 273 546 124 180 35 254 508 124 180 28,000 -67 -70 39 270 540 124 186 35 252 504 124 186 29,000 -69 -72 39 272 544 124 190 35 251 502 124 190 31,000 -73 -76 41 278 556 124 196 37 254 508 124 196 33,000 -77 -80 42 282 564 124 203 38 258 516 124 203 35,000 -80 -84- --- --- --- --- --- 39 261 522 124 210 BT05594 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 7-106.  Loiter Power at 1700 RPM - ISA -30°C (Sheet 1 of 2)   IR 7-166  Change 2