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 9 5 79 575 1150 217 215 54 488 976 187 185 2000 5 1 76 542 1084 211 215 58 481 962 191 195 4000 1 -3 72 507 1014 205 215 58 458 916 189 199 6000 -3 -7 66 469 938 197 213 56 431 862 184 200 8000 -7 -11 62 435 870 189 211 53 404 808 179 200 10,000 -11 -15 58 403 806 182 209 50 376 752 173 200 12,000 -15 -19 54 375 750 175 208 47 349 698 167 199 14,000 -19 -23 51 350 700 169 208 45 324 648 161 198 16,000 -23 -27 49 329 658 164 208 42 301 602 155 197 18,000 -27 -31 47 309 618 158 207 39 280 560 149 196 20,000 -31 -35 45 295 590 154 208 37 263 526 144 196 22,000 -34 -39 45 285 570 151 212 37 253 506 141 199 24,000 -38 -43 44 276 552 148 214 36 245 490 139 202 26,000 -42 -47 43 266 532 145 217 36 236 472 136 205 28,000 -46 -50 42 257 514 141 219 36 230 460 134 209 29,000 -48 -52 41 251 502 138 218 35 '227 454 133 212 31,000 -52 -56 38 238 476 130 214 35 221 442 130 215 33,000 -56 -60 38 237 474 127 217 34 215 430 127 217 35,000 -60 -64 40 244 488 128 227 32 203 406 119 213 BT0587112 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-66.  Maximum Range Power at 1500 RPM - ISA -10°C (Sheet 2 of 2) 7A-1 03