TM 1-1510-224-10 NORMAL CRUISE POWER 1500 RPM ISA -30°C WEIGHT® 12,000 POUNDS 10,000 POUNDS PRESSURE ALTITUDE IFAT FAT TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS FEET C° C° PERCENT LBS/HR LBS/HR KTS KTS PERCENT LBS/HR LBS/HR KTS KTS 0 20 15 86 594 1188 223 225 75 556 1112 212 214 2000 16 11 81 559 1118 216 224 73 533 1066 209 217 4000 12 7 77 527 1054 210 225 71 508 1016 206 220 6000 8 3 72 491 982 203 223 68 475 950 199 220 8000 4 -1 68 459 918 196 223 63 440 880 191 217 10,000 0 -5 63 425 850 188 221 58 406 812 183 215 12,000 -4 -9 59 395 790 181 220 54 375 750 176 213 14,000 -8 -13 56 369 738 175 219 50 347 694 169 212 16,000 -12 -17 53 346 692 169 219 47 323 646 163 211 18,000 -16 -21 51 327 654 164 219 45 302 604 157 211 20,000 -20 -25 49 309 618 159 220 42 284 568 152 210 22,00C -24 -29 47 296 592' 154 221 41 270 540 147 211 24,000 -28 -33 45 282 564 150 222 39 257 514 143 213 26,000 -32 -37 43 267 534 143 220 38 246 492 140 215 28,000 -36 -40 40 252 504 136 217 37 237 474 136 217 29,000 -38 -42 39 246 492 132 215 36 232 464 134 218 31,000 -42 -46 39 241 482 128 217 35 221 442 128 217 33,000 -46 -50 40 245 490 128 224 33 209 418 122 214 35,000 -49 -54 42 252 504 129 234 32 201 402 116 213 BT0587110 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately 10%,  fuel  flow  will  decrease  approximately  5%,  and  true  airspeed  will  be  reduced by approximately 10 knots. Figure 7A-67.  Maximum Range Power at 1500 RPM - ISA (Sheet 2 of 2) 7A-105