TM 1-1510-223-10 LOITER POWER 1700 RPM ISA -20°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 -4 -5 30 415 830 124 123 27 402 804 124 123 2000 -7 -9 31 397 794 124 127 28 384 768 124 127 4000 -11 -13 31 380 760 124 131 28 367 734 124 131 6000 -15 -17 32 364 728 124 125 29 351 702 124 135 8000 -19 -21 32 349 698 124 139 29 336 672 124 139 10,000 -23 -25 33 335 670 124 143 30 321 642 124 143 12,000 -27 -29 34 321 642 124 147 30 307 614 124 147 14,000 -31 -33 34 310 620 124 152 31 295 590 124 152 16,000 -34 -37 35 300 600 124 157 32 285 570 124 157 18,000 -38 -41 36 293 586 124 162 33 277 554 124 162 20,000 -42 -45 37 287 574 124 167 33 270 540 124 167 22,000 -46 -49 37 282 564 124 173 34 265 530 124 173 24,000 -50 -53 38 278 556 124 178 35 261 522 124 178 26,000 -53 -57 39 276 552 124 185 35 258 516 124 185 28,000 -57 -60 40 276 552 124 191 36 255 510 124 191 29,000 -59 -62 40 278 556 124 194 36 254 508 124 194 31,000 -63 -66 42 283 566 124 201 37 258 516 124 201 33,000 -66 -70 43 288 576 124 208 38 263 526 124 208 35,000 -70 -74 --- --- --- --- --- 40 268 536 124 216 BT055943 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 7-108.  Loiter Power at 1700 RPM - ISA -20°C (Sheet 1 of 2)   CA 7-170  Change 2