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 34 433 866 124 134 32 419 838 124 134 2000 43 41 35 417 834 124 138 32 403 806 124 138 4000 39 37 36 401 802 124 143 33 387 774 124 143 6000 35 33 36 386 772 124 147 33 372 744 124 147 8000 31 29 37 370 740 124 152 34 356 712 124 152 10,000 27 25 38 355 710 124 157 34 341 682 124 157 12,000 24 21 38 341 682 124 162 35 327 654 124 162 14,000 20 17 39 329 658 124 167 36 314 628 124 167 16,000 16 13 40 320 640 124 173 36 304 608 124 173 18,000 12 9 41 316 632 124 178 37 300 600 124 178 20,000 9 5 42 310 620 124 185 38 294 588 124 185 22,000 5 1 43 307 614 124 191 39 289 578 124 191 24,000 1 -3 --- --- --- --- --- 40 286 572 124 198 26,000 -3 -7 --- --- --- --- --- 41 286 572 124 205 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03611 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 1 of 2)  IR 7-188  Change 2