TM 1-1510-223-10 MAXIMUM RANGE POWER 1500 RPM ISA -30°C WEIGHT® 16,000 POUNDS 14,000 POUNDS TORQUE FUEL TOTAL TORQUE FUEL TOTAL PRESSURE PER FLOW FUEL PER FLOW FUEL ALTITUDE IFAT FAT ENGINE PER FLOW IAS TAS ENGINE PER FLOW IAS TAS ENGINE ENGINE FEET °C °C PERCENT LBS/HR LBS/HR KTS KTS PERCENT   LBS/HR    LBS/HR KTS KTS 0 -12 -15 76 548 1096 196 188 73 537 1074 195 187 2000 -16 -19 72 512 1024 189 187 70 504 1008 189 187 4000 -20 -23 68 480 960 183 186 66 472 944 184 186 6000 -24 -27 64 448 896 177 185 62 439 878 177 185 8000 -28 -31 61 421 842 171 184 59 411 822 171 184 10,000 -32 -35 58 395 790 165 183 55 382 764 164 182 12,000 -36 -39 56 374 748 160 183 53 359 718 159 182 14,000 -40 -43 56 361 722 157 185 50 336 672 152 180 16,000 -43 -47 55 348 696 153 187 48 321 642 148 181 18,000 -47 -51 54 337 674 150 189 46 304 608 143 181 20,000 -51 -55 53 327 654 146 191 45 293 586 139 182 22,000 -55 -59 54 324 648 145 195 46 290 580 138 187 24,000 -59 -63 54 324 648 144 200 46 287 574 136 190 26,000 -63 -67 54 319 638 141 203 47 285 570 135 195 28,000 -65 -70 --- --- --- --- --- 48 284 568 135 201 29,000 -69 -72 --- --- --- --- --- 46 275 550 130 198 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03583 NOTE During operations with ice vanes extended, torque will decrease approximately 10 percentage   points   (E.      G.,   64%   -   10   percentage   points   =   54%),   fuel   flow   will decrease   approximately   20   LBS/HR/ENG,   and   true   airspeed   will   be   reduced approximately 10 knots. Figure 7-88.  Maximum Range Power at 1500 RPM - ISA -30°C (Sheet 1 of 2)  IR Change 2  7-131