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 -1 -5 67 527 1054 203 198 59 499 998 195 190 2000 -5 -9 64 496 992 198 198 57 471 942 191 191 4000 -9 -13 61 466 932 192 199 55 443 886 186 192 6000 -13 -17 58 436 872 187 199 53 416 832 182 193 8000 -17 -21 55 407 814 181 198 51 390 780 177 194 10,000 -21 -25 52 378 756 174 197 48 364 728 172 194 12,000 -25 -29 49 352 704 169 197 46 339 678 166 194 14,000 -29 -33 46 328 656 162 196 43 315 630 161 194 16,000 -33 -37 44 307 614 157 195 41 294 588 155 194 18,000 -37 -41 42 289 578 152 195 39 277 554 151 194 20,000 -41 -45 41 275 550 147 196 37 260 520 146 194 22,00G -45 -49 41 269 538 146 200 35 244 488 140 192 24,000 -49 -53 41 263 526 144 205 34 231 462 135 192 26,000 -52 -57 41 258 516 142 209 33 224 448 132 195 28,000 -56 -60 41 254 508 141 214 33 219 438 130 199 29,000 -58 -62 41 251 502 140 216 33 217 434 129 202 31,000 -62 -66 40 244 488 135 218 34 215 430 129 208 33,000 -66 -70 38 232 464 128 214 34 213 426 128 214 35,000 -70 -74 39 238 476 128 221 33 204 408 123 213 BT0587114 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-65.  Maximum Range Power at 1500 RPM - ISA -20°C (Sheet 2 of 2) 7A-101