TM 1-1510-223-10 MAXIMUM RANGE POWER 1500 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 29 25 83 595 1190 205 210 82 590 1180 205 211 2000 25 21 79 560 1120 199 211 78 554 1108 200 211 4000 21 17 75 523 1046 193 210 74 519 1038 194 211 6000 17 13 71 490 980 186 209 70 488 976 188 212 8000 -3 9 68 462 924 180 209 66 457 914 181 211 10,000 9 5 64 434 868 173 207 62 428 856 175 209 12,000 5 1 61 408 816 167 207 60 403 806 169 210 14,000 1 -3 58 383 766 161 206 57 378 756 164 209 16,000 -3 -7 56 363 726 155 206 54 354 708 157 208 18,000 -7 -11 55 348 696 151 206 52 335 670 152 208 20,000 -11 -15 54 340 680 148 209 48 313 626 144 205 22,000 -14 -19 55 338 676 146 214 46 298 5960 138 203 24,000 -18 -23 56 336 672 144 219 46 291 582 135 205 26,000 -22 -27 --- --- --- --- --- 48 294 588 135 213 28,000 -26 -30 --- --- --- --- --- 49 295 590 134 218 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT055929 NOTE During operations with ice vanes extended, torque will decrease approximately 10 percentage points (E.G., 64% - 10 percentage points = 54%), fuel flow will decrease approximately 20 LBS/HR/ENG, and true airspeed will be reduced approximately 10 knots. Figure 7-97.  Maximum Range Power at 1500 RPM - ISA +10 °C (Sheet 1 of 2)   CA Change 2  7-149