TM 1-1510-223-10 MAXIMUM RANGE POWER 1500 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 49 45 76 577 1154 199 212 70 556 1112 194 207 2000 45 41 71 538 1076 192 211 67 523 1046 189 208 4000 41 37 66 501 1002 185 209 62 488 976 183 207 6000 37 33 62 466 933 178 208 59 455 910 177 207 8000 33 29 58 433 866 172 207 56 424 848 172 206 10,000 29 25 55 403 806 166 206 53 395 790 166 206 12,000 25 21 52 376 752 160 206 51 369 738 161 207 14,000 21 17 49 349 698 154 205 48 342 684 155 206 16,000 17 13 47 328 656 148 204 45 319 638 149 205 18,000 13 9 45 314 628 144 205 40 293 586 140 200 20,000 9 5 45 304 608 142 209 38 275 550 135 199 22,000 6 1 45 294 588 139 212 36 260 520 130 199 24,000 2 -3 44 285 570 136 215 35 246 492 125 199 26,000 -3 -7 --- --- --- --- --- 35 237 474 122 202 28,000 -7 -10 --- --- --- --- --- 34 230 460 119 204 29,000 -8 -12 --- --- --- --- --- 34 228 456 119 207 31,000 -12 -16 --- --- --- --- --- 33 214 428 113 205 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559214 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 7-101.  Maximum Range Power at 1500 RPM - ISA +30 °C (Sheet 2 of 2)   CA 7-158  Change 2