TM 1-1510-224-10 MAXIMUM RANGE POWER 1500 RPM ISA 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 20 15 89 607 1214 224 226 87 600 1200 224 226 2000 16 11 84 571 1142 216 224 83 566 1132 217 225 4000 12 7 79 538 1076 210 224 78 533 1066 211 225 6000 8 3 76 506 1012 203 224 74 500 1000 204 225 8000 4 -1 72 477 954 197 224 70 468 936 198 224 10,000 0 -5 69 448 896 191 224 67 439 878 191 224 12,000 -4 -9 66 420 840 185 223 64 412 824 186 224 14,000 -8 -13 63 396 792 178 223 60 385 770 179 223 16,000 -12 -17 60 372 744 172 222 57 363 726 173 223 18,000 -16 -21 57 352 704 165 221 55 344 688 168 224 20,000 -20 -25 54 333 666 158 218 53 326 652 162 223 22,000 -24 -29 52 318 636 151 216 50 309 618 155 222 24,000 -28 -33 52 314 628 148 219 47 292 584 148 219 26,000 -32 -37 54 319 638 149 228 45 277 554 141 216 28,000 -35 -40 56 327 654 150 237 45 277 554 138 220 29,000 -38 -42 --- --- --- --- --- 46 279 558 138 224 31,000 -41 -46 --- --- --- --- --- 48 286 572 139 234 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05247 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 7-67.  Maximum Range Power at 1500 RPM - ISA (Sheet 1 of 2) 7-104