TM 1-1510-224-10 MAXIMUM RANGE POWER 1500 RPM ISA -10°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 10 5 93 621 1242 229 226 89 608 1216 227 224 2000 6 1 87 581 1162 221 225 83 565 1130 218 222 4000 2 -3 82 543 1086 213 224 77 525 1050 209 220 6000 -2 -7 77 507 1014 206 222 72 488 976 202 218 8000 -6 -11 73 476 952 199 222 67 455 910 194 217 10,000 -10 -15 69 447 894 193 221 63 425 850 188 216 12,000 -14 -19 66 420 840 187 221 60 397 794 181 215 14,000 -18 -23 63 397 794 181 222 58 374 748 176 216 16,000 -22 -27 61 377 754 176 222 55 353 706 171 216 18,000 -26 -31 59 360 720 171 223 53 335 670 165 216 20,000 -30 -35 57 345 690 165 223 52 321 642 161 218 22,000 -34 -39 55 331 662 159 223 51 310 620 157 220 24,000 -38 -43 52 314 628 152 220 49 299 598 153 222 26,000 -42 -47 50 301 602 144 217 47 286 572 147 221 28,000 -46 -50 53 312 624 146 227 44 269 538 138 215 29,000 -47 -52 55 319 638 148 234 44 267 534 136 216 31,000 -52 -56 --- --- --- --- --- 46 276 552 138 226 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- BT05245 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 7-66.  Maximum Range Power at 1500 RPM - ISA - 10°C (Sheet 1 of 2) 7-102