TM 1-1510-223-10 MAXIMUM RANGE POWER 1500 RPM ISA + 10°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 29 25 79 580 1160 205 210 77 571 1142 204 209 2000 25 21 76 546 1092 199 211 73 536 1072 198 210 4000 21 17 72 512 1024 194 212 70 502 1004 193 210 6000 17 13 69 480 960 188 212 66 469 938 187 210 8000 13 9 65 452 904 183 212 62 440 880 181 210 10,000 9 5 61 422 844 176 211 59 415 830 176 211 12,000 5 1 58 396 792 171 211 56 388 776 171 211 14,000 1 -3 56 372 744 165 211 53 361 722 164 210 16,000 -3 -7 53 349 698 160 211 50 336 672 158 209 18,000 -7 -11 50 328 656 154 211 47 315 630 153 209 20,000 -11 -15 48 308 616 148 210 45 296 592 148 209 22,000 -15 -19 45 289 578 141 207 42 279 558 142 209 24,000 -19 -23 42 273 546 135 206 40 262 524 136 208 26,000 -23 -27 39 254 508 127 201 38 247 494 131 207 28,000 -27 -30 38 246 492 122 201 36 232 464 125 205 29,000 -28 -32 39 249 298 123 206 34 224 448 121 203 31,000 -32 -36 41 253 506 123 214 33 213 426 115 202 33,000 -37 -40 --- --- --- --- --- 32 206 422 111 201 35,000 -40 -44 --- --- --- --- --- 33 211 412 112 210 BT0559210 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 2 of 2)   CA 7-150  Change 2