TM 1-1510-223-10 MAXIMUM RANGE POWER 1500 RPM ISA 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 19 15 82 585 1170 209 211 67 530 1060 192 195 2000 15 11 78 552 1104 203 211 66 511 1022 191 199 4000 11 7 74 518 1036 196 210 65 489 978 188 202 6000 7 3 70 486 972 190 210 64 465 930 185 204 8000 3 -1 66 453 906 184 209 59 431 862 178 203 10,000 -1 -5 62 421 842 177 208 55 398 796 171 201 12,000 -5 -9 58 392 784 171 207 51 368 684 164 200 14,000 -9 -13 55 366 7328 165 207 48 342 636 158 198 16,000 -13 -17 52 344 688 159 207 45 318 596 152 197 18,000 -17 -21 50 325 650 154 207 43 298 560 146 197 20,000 -21 -25 48 308 616 150 208 41 280 534 142 197 22,000 -24 -29 47 297 594 146 210 39 267 534 138 198 24,000 -28 -33 45 284 568 142 211 38 254 508 134 200 26,000 -32 -37 43 267 534 135 209 37 244 488 131 202 28,000 -37 -40 40 252 504 128 206 37 236 472 128 206 29,000 -39 -42 39 246 492 125 204 36 231 462 126 206 31,000 -42 -46 39 243 486 122 207 35 221 442 121 206 33,000 -46 -50 40 247 494 121 214 33 209 418 115 203 35,000 -50 -54 41 250 500 120 220 31 201 402 109 202 BT055928 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/HRIENG, and true airspeed will be reduced approximately 10 knots. Figure 7-95.  Maximum Range Power at 1500 RPM - ISA (Sheet 2 of 2)   CA 7-146  Change 2