TM 1-1510-224-10 MAXIMUM RANGE POWER 1500 RPM ISA +37°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 57 52 77 582 1164 210 225 77 582 11164 212 227 2000 53 48 75 551 1102 206 227 75 552 1104 208 229 4000 49 44 72 519 1038 200 228 67 502 1004 197 249 6000 45 40 68 483 966 194 227 63 467 934 190 223 8000 41 36 62 445 890 185 224 57 426 852 181 219 10,000 37 32 58 412 824 177 222 53 394 788 173 218 12,000 33 28 54 382 764 170 220 49 364 728 167 216 14,000 29 24 51 356 712 164 220 46 338 676 161 215 16,000 25 20 49 336 672 159 220 44 316 632 155 215 18,000 21 16 48 321 642 155 223 42 296 592 149 215 20,000 17 12 47 308 616 152 226 40 282 564 146 217 22,000 13 8 - - - - - - - - - - - - - - - 39 269 538 141 218 24,000 9 8 - - - - - - - - - - - - - - - 38 257 514 137 219 26,000 5 0 - - - - - - - - - - - - - - - 33 232 464 126 209 28,000 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 29,000 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 31,000 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 33,000 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 35,000 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - BT058712 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately 10%/e, fuel flow will decrease approximately 5%, and true airspeed will be reduced by approximately 10 knots. Figure 7A-71.  Maximum Range Power at 1500 RPM - ISA +37°C (Sheet 2 of 2) 7A-113