TM 1-1510-224-10 MAXIMUM RANGE POWER 1500 RPM ISA +37°C WEIGHT® 16,000 POUNDS 14,000 POUNDS PRESSURE ALTITUDE IOAT OAT 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 84 607 1214 214 230 84 607 1214 216 232 2000 53 48 82 577 1154 210 232 82 576 1152 217 236 4000 49 44 80 547 1094 211 235 79 534 1068 209 233 6000 45 40 78 511 1022 203 234 72 498 996 202 233 8000 41 36 72 478 956 196 232 71 463 926 194 230 10,000 37 32 72 451 902 191 233 65 436 872 190 232 12,000 33 28 66 424 848 185 233 60 405 810 176 227 14,000 29 24 65 403 806 180 234 58 380 760 170 227 16,000 25 20 60 378 756 166 230 56 362 724 166 229 18,000 21 16 55 349 698 156 224 55 344 688 166 231 20,000 17 12 50 323 646 145 216 --- --- --- --- --- 22,000 12 8 47 302 604 134 207 --- --- --- --- --- 24,000 8 4 42 280 560 115 185 --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05255 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 7-71.  Maximum Range Power at 1500 RPM - ISA +37°C (Sheet 1 of 2) 7-112