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 -11 -15 67 522 1044 205 196 64 509 1018 202 193 2000 -15 -19 64 491 982 200 197 61 479 958 198 195 4000 -19 -23 61 460 920 194 197 59 449 898 193 195 6000 -23 -27 58 430 860 189 197 56 421 842 188 196 8000 -27 -31 55 402 804 183 196 53 393 786 182 196 10,000 -31 -35 52 374 748 177 195 50 366 732 176 195 12,000 -35 -39 49 349 698 171 195 47 341 682 171 195 14,000 -39 -43 47 326 652 165 194 45 319 638 166 195 16,000 -43 -47 44 304 608 159 194 43 298 596 161 195 18,000 -47 -51 42 286 572 154 193 41 280 560 156 196 20,000 -51 -55 40 270 540 149 193 39 263 526 151 196 22,000 -55 -59 38 254 508 142 191 37 247 494 145 195 24,000 -59 -63 -38 247 494 139 194 34 231 462 138 192 26,000 -63 -67 39 246 492 139 200 32 216 432 131 189 28,000 -66 -70 40 248 496 140 208 32 213 426 129 193 29,000 -68 -72 40 248 496 140 212 33 212 424 129 196 31,000 -72 -76 40 242 484 137 215 33 210 420 128 202 33,000 -76 -80 38 231 462 130 211 33 209 418 128 208 35,000 -80 -84 38 233 466 129 217 32 202 404 124 209 BT05871168 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-64.  Maximum Range Power at 1500 RPM - ISA -300C (Sheet 2 of 2) 7A-99