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 10 5 93 622 1244 229 226 89 609 1218 226 224 2000 6 1 87 582 1164 221 225 83 566 1132 226 224 4000 2 -3 82 545 1090 213 224 77 526 1052 209 222 6000 -2 -7 77 509 1018 206 223 72 490 980 202 218 8000 -6 -11 73 478 956 199 222 68 457 914 194 217 10,000 -10 -15 70 449 898 193 221 64 427 854 188 216 12,000 -14 -19 67 422 844 187 221 61 399 798 182 215 14,000 -18 -23 64 400 800 181 222 58 376 752 176 216 16,000 -22 -27 62 379 758 176 222 56 356 712 171 216 18,000 -26 -31 60 362 724 171 223 54 337 674 165 216 20,000 -30 -35 58 347 694 165 223 52 324 648 161 218 22,000 -34 -39 55 331 662 158 222 51 313 626 158 220 24,000 -38 -43 52 314 628 150 218 50 301 602 153 222 26,000 -42 -47 51 307 614 145 218 47 287 574 146 220 28,000 -46 -50 54 318 636 148 229 44 271 542 148 215 29,000 -47 -52 56 324 648 149 235 45 272 544 137 217 31,000 -52 -56 --- --- --- --- --- 47 281 562 139 227 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0587111 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-66.  Maximum Range Power at 1500 RPM - ISA -10°C (Sheet 1 of 2) 7A-102