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 30 25 83 592 1184 216 222 82 588 1176 217 223 2000 26 21 79 555 1110 210 221 78 552 1104 211 223 4000 22 17 75 522 1044 203 221 74 517 1034 205 223 6000 18 13 72 490 980 197 221 71 486 972 199 223 8000 14 9 67 459 918 190 220 67 457 914 192 222 10,000 10 5 63 431 862 182 218 63 427 854 185 221 12,000 6 1 60 404 808 176 217 60 402 804 179 221 14,000 2 -3 58 383 766 171 218 57 377 754 174 221 16,000 -2 -7 56 359 718 164 216 54 354 708 167 220 18,000 -6 -11 54 343 686 159 216 52 332 664 160 219 20,000 -10 -15 53 332 664 154 218 49 313 626 154 217 22,000 -14 -19 54 330 660 153 223 47 297 594 147 215 24,000 -18 -23 55 331 662 152 229 46 287 574 142 216 26,000 -22 -27 --- --- --- --- --- 46 287 574 141 221 28,000 -26 -30 --- --- --- --- --- 48 289 578 141 229 29,000 -27 -32 --- --- --- --- --- 49 292 584 141 233 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05249 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 7-68.  Maximum Range Power at 1500 RPM - ISA +10°C (Sheet 1 of 2) 7-106