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 37 35 32 439 878 124 132 30 426 852 124 132 2000 33 31 33 420 840 124 136 30 407 814 124 136 4000 29 27 33 401 802 124 140 31 388 776 124 140 6000 25 23 34 384 768 124 145 31 371 742 124 145 8000 21 19 35 368 736 124 149 32 354 676 124 149 10,000 17 -15 35 352 704 124 154 32 338 646 124 154 12,000 14 -11 36 337 674 124 159 33 323 624 124 159 14,000 10 -7 37 327 654 124 164 33 312 604 124 164 16,000 6 3 37 316 632 124 170 34 302 584 124 170 18,000 2 -1 38 308 616 124 175 34 292 570 124 175 20,000 -2 -5 39 303 606 124 181 35 285 562 124 181 22,000 -5 -9 40 300 600 124 187 36 281 552 124 187 24,000 -9 -13 41 297 594 124 194 37 278 556 124 194 26,000 -13 -17 42 296 592 124 201 38 276 552 124 201 28,000 -16 -20 --- --- --- --- --- 39 276 552 124 208 29,000 -18 -22 --- --- --- --- --- 39 277 554 124 212 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559411 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 7-116.  Loiter Power at 1700 RPM - ISA +20°C (Sheet 1 of 2)  CA 7-186  Change 2