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 29 407 814 124 134 27 395 790 124 134 2000 43 41 30 391 782 124 138 27 381 762 124 138 4000 39 37 30 376 752 124 143 28 365 730 124 143 6000 35 33 31 360 720 124 147 28 350 700 124 147 8000 31 29 31 344 688 124 152 29 334 668 124 152 10,000 27 25 32 329 658 124 157 29 319 638 124 157 12,000 24 21 32 315 630 124 162 30 305 610 124 162 14,000 20 17 33 302 604 124 167 30 292 584 124 167 16,000 16 13 33 292 584 124 173 31 281 562 124 173 18,000 12 9 34 286 572 124 178 31 274 548 124 178 20,000 9 5 35 279 558 124 185 32 267 534 124 185 22,000 5 1 36 275 550 124 191 33 262 524 124 191 24,000 1 -3 36 270 540 124 198 34 257 514 124 198 26,000 -3 -7 37 267 534 124 205 34 253 506 124 205 28,000 -6 -10 38 268 536 124 212 35 252 504 124 212 29,000 -8 -12 --- --- --- --- --- 35 251 502 124 216 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03612 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 7-117.  Loiter Power at 1700 RPM - ISA +30°C (Sheet 2 of 2)  IR Change 2  7-189