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 47 45 33 439 878 124 134 30 426 852 124 134 2000 43 41 33 422 844 124 138 30 409 818 124 138 4000 39 37 34 406 812 124 143 31 392 784 124 143 6000 35 33 34 389 778 124 147 31 375 750 124 147 8000 31 29 35 373 746 124 152 32 359 718 124 152 10,000 27 25 36 357 714 124 157 32 343 686 124 157 12,000 24 21 36 342 684 124 162 33 327 654 124 162 14,000 20 17 37 328 656 124 167 34 313 626 124 167 16,000 16 13 38 318 636 124 173 34 302 604 124 173 18,000 12 9 39 312 624 124 178 35 296 592 124 178 20,000 9 5 39 305 610 124 185 36 289 578 124 185 22,000 5 1 40 5301 602 124 191 37 284 568 124 191 24,000 1 -3 41 300 600 124 198 37 279 558 124 198 26,000 -3 -7 --- --- --- --- --- 38 277 554 124 205 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559413 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 7-118.  Loiter Power at 1700 RPM - ISA +30°C (Sheet 1 of 2)  CA 7-190  Change 2