TM 1-1510-224-10 NORMAL CRUISE POWER 1500 RPM ISA -30°C WEIGHT® 16,000 POUNDS 14,000 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 20 15 89 607 1214 223 225 88 602 1204 224 226 2000 16 11 84 572 1144 216 224 82 566 1132 216 224 4000 12 7 80 539 1078 209 224 78 534 1068 210 225 6000 8 3 76 507 1014 203 223 74 500 1000 204 224 8000 4 -1 72 477 954 197 224 71 469 938 197 224 10,000 0 -5 69 448 896 190 223 67 441 882 192 224 12,000 -4 -9 66 422 844 184 223 64 412 824 185 223 14,000 -8 -13 63 396 792 178 222 61 387 774 179 223 16,000 -12 -17 60 373 746 171 221 58 365 730 173 224 18,000 -16 -21 57 353 706 165 220 55 344 688 167 223 20,000 -20 -25 54 334 668 157 217 53 327 654 161 223 22,000 -24 -29 52 320 640 151 216 50 310 620 154 221 24,000 -28 -33 53 319 638 149 221 47 292 584 147 217 26,000 -32 -37 55 325 650 150 229 45 279 558 140 215 28,000 -36 -40 --- --- --- --- --- 46 281 562 139 221 29,000 -38 -42 --- --- --- --- --- 47 284 568 139 225 31,000 -41 -46 --- --- --- --- --- 49 291 582 140 235 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT058719 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 7A-67.  Maximum Range Power at 1500 RPM - ISA (Sheet 1 of 2) 7A-104