TM 1-1510-223-10 MAXIMUM RANGE POWER 1500 RPM ISA + 37°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 56 52 76 581 1162 198 213 71 563 1126 194 209 2000 52 48 74 551 1102 194 215 67 527 1054 189 209 4000 48 44 67 520 1040 190 217 64 495 990 184 210 6000 44 40 62 484 968 183 216 61 464 928 179 211 8000 40 36 57 448 896 176 214 57 430 860 172 210 10,000 36 32 54 412 824 168 211 52 393 786 164 206 12,000 32 28 51 383 766 161 210 49 365 730 158 206 14,000 28 24 49 357 714 155 209 46 339 678 152 205 16,000 24- 20 48 337 674 151 210 43 316 632 146 204 18,000 21 16 48 324 648 148 213 41 294 588 140 203 20,000 17 12 48 311 622 145 216 41 284 568 138 207 22,000 12 8 --- --- --- --- --- 39 271 542 134 208 24,000 9 4 --- --- --- --- --- 38 259 518 130 210 26,000 4 0 --- --- --- --- --- 31 221 442 113 191 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559216 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 7-103.  Maximum Range Power at 1500 RPM - ISA +37 °C (Sheet 2 of 2)   CA 7-162  Change 2