TM 1-1510-223-10 LOITER POWER 1700 RPM ISA + 30°C WEIGHT® 12,000 POUNDS 10,000 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 27 414 828 124 134 25 404 808 124 134 2000 43 41 28 397 794 124 138 26 387 774 124 138 4000 39 37 28 380 760 124 143 26 370 740 124 143 6000 35 33 29 363 726 124 147 27 353 706 124 147 8000 31 29 29 346 692 124 152 27 336 672 124 152 10,000 27 25 30 330 660 124 157 27 320 640 124 157 12,000 24 21 30 315 630 124 162 28 304 608 124 162 14,000 20 17 31 301 602 124 167 28 290 580 124 167 16,000 16 13 31 289 578 124 173 29 279 558 124 173 18,000 12 9 32 282 564 124 178 29 270 540 124 178 20,000 9 5 33 275 550 124 185 30 262 524 124 185 22,000 5 1 33 269 538 124 191 31 256 512 124 191 24,000 1 -3 34 264 528 124 198 31 250 500 124 198 26,000 -3 -7 35 260 520 124 205 32 246 492 124 205 28,000 -6 -10 36 258 516 124 212 33 243 486 124 212 29,000 -8 -12 36 259 518 124 216 33 242 484 124 216 31,000 -12 -16 --- --- --- --- --- 34 242 484 124 224 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559414 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 2 of 2)  CA Change 2  7-191