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 33 420 840 124 130 30 406 812 124 130 2000 23 21 33 404 808 124 134 31 389 778 124 134 4000 19 17 34 388 776 124 138 31 373 746 124 138 6000 15 13 35 374 748 124 142 32 359 718 124 142 8000 11 9 36 361 722 124 147 32 348 696 124 147 10,000 7 5 37 350 700 124 151 33 337 674 124 151 12,000 3 1 37 337 674 124 156 34 324 648 124 156 14,000 0 -3 38 325 650 124 161 35 311 622 124 161 16,000 -4 -7 39 314 628 124 165 35 300 600 124 166 18,000 -8 -11 39 305 610 124 172 36 291 582 124 172 20,000 -12 -15 40 299 598 124 178 37 283 566 124 178 22,000 -16 -19 41 299 598 124 184 37 278 556 124 184 24,000 -19 -23 43 300 600 124 190 39 279 558 124 190 26,000 -23 -27 44 302 604 124 197 40 280 560 124 197 28,000 -27 -30 45 305 610 124 204 41 281 562 124 204 29,000 -28 -32 46, 307 614 124 208 41 283 566 124 208 31,000 -42 -46 --- --- --- --- --- 43 286 572 124 215 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03607 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 7-113.  Loiter Power at 1700 RPM - ISA +10°C (Sheet 1 of 2)  IR 7-180  Change 2