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 -12 -15 67 523 1046 195 187 63 509 1018 192 184 2000 -16 -19 64 492 984 190 187 61 479 958 188 185 4000 -20 -23 61 461 922 185 187 58 450 900 183 186 6000 -24 -27 58 432 864 179 187 56 422 844 178 186 8000 -28 -31 55 403 806 174 187 53 395 790 173 187 10,000 -32 -35 52 375 750 168 186 50 367 734 168 186 12,000 -40 -39 49 348 696 161 185 47 343 686 163 186 14,000 -44 -43 47 327 654 157 185 45 320 640 157 186 16,000 -48 -47 44 306 612 151 185 43 300 600 152 186 18,000 -51 -51 42 288 576 146 185 41 281 562 148 187 20,000 -55 -55 40 271 542 141 184 39 264 528 143 186 22,000 -55 -59 38 256 512 135 183 37 248 496 137 185 24,000 -59 -63 38 250 500 133 186 34 231 462 130 183 26,000 -63 -67 39 247 494 133 190 32 217 434 124 180 28,000 -67 -70 39 246 492 131 196 32 214 428 123 185 29,000 -69 -72 40 246 492 131 200 33 213 426 122 187 31,000 -73 -76 39 242 484 129 203 33 210 420 121 191 33,000 -77 -80 37 229 458 121 199 33 207 414 120 197 35,000 -80 -84 39 235 470 122 208 32 200 400 116 197 BT055922 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 7-89.  Maximum Range Power at 1500 RPM - ISA -30°C (Sheet 2 of 2)CA 7-134  Change 2