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 69 547 1094 184 198 62 523 1046 179 193 2000 52 48 66 516 1032 180 200 61 499 998 177 196 4000 48 44 64 488 976 176 201 59 469 938 172 197 6000 44 40 64 467 934 174 205 58 446 892 169 199 8000 40 36 62 440 880 169 206 56 420 840 165 201 10,000 36 32 58 409 818 162 204 53 393 786 160 201 12,000 32 28 54 379 758 155 202 50 365 730 154 200 14,000 28 24 51 353 706 149 201 47 340 680 148 199 16,000 24 20 49 336 672 145 203 44 315 630 141 197 18,000 20 16 49 325 650 143 206 41 296 592 136 197 20,000 16 12 49 313 626 140 210 40 281 562 132 198 22,000 13 8 47 300 600 135 210 39 270 540 128 200 24,000 8 4 38- --- --- --- --- 38 259 518 125 201 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03598 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 7-102.  Maximum Range Power at 1500 RPM - ISA +37 °C (Sheet 2 of 2)   IR 7-160  Change 2