TM 1-1510-224-10 MAXIMUM RANGE 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 50 45 79 584 1168 213 225 74 568 1136 209 222 2000 46 41 72 539 1078 203 222 68 524 1048 200 219 4000 42 37 67 503 1006 196 221 64 490 980 194 219 6000 38 33 63 466 932 189 219 60 455 910 187 218 8000 34 29 59 433 866 182 218 56 423 846 181 217 10,000 30 25 56 404 808 176 218 53 394 788 175 217 12,000 26 21 53 376 752 170 217 51 367 734 170 217 14,000 22 17 50 349 698 163 216 48 342 684 164 217 16,000 18 13 47 327 654 157 215 44 316 632 157 214 18,000 14 9 46 315 630 153 216 41 295 590 149 212 20,000 10 5 45 303 606 149 219 39 278 556 144 212 22,000 6 1 45 292 584 146 222 37 263 526 139 212 24,000 2 -3 44 283 566 143 225 36 248 496 134 212 26,000 -2 -7 - - - - - - - - - - - - - - - 35 238 476 130 214 28,000 -6 -10 - - - - - - - - - - - - - - - 34 230 460 126 215 29,000 -8 -12 - - - - - - - - - - - - - - - 34 227 454 125 217 31,000 -12 -16 - - - - - - - - - - - - - - - 33 212 424 119 215 33,000 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 35,000 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - BT058714 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-70.  Maximum Range Power at 1500 RPM - ISA +30°C (Sheet 2 of 2) 7A-111