TM 1-1510-223-10 MAXIMUM RANGE POWER 1500 RPM ISA -10°C WEIGHT® 12,000 POUNDS 10,000 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 8 5 64 517 1034 183 182 54 477 954 171 171 2000 4 1 66 500 1000 183 187 53 454 908 169 173 4000 0 -3 64 475 950 180 190 53 435 870 168 177 6000 -4 -7 62 448 896 175 190 53 417 834 167 181 8000 -7 -11 59 420 840 170 191 52 394 788 163 183 10,000 -11 -15 56 392 784 164 190 50 370 740 159 184 12,000 -15 -19 53 366 732 158 189 47 346 692 154 184 14,000 -19 -23 50 344 688 153 189 45 323 646 148 183 16,000 -23 -27 48 324 648 148 189 42 301 602 143 183 18,000 -27 -31 46 306 612 143 189 40 281 562 137 181 20,000 -31 -35 44 293 586 139 190 38 265 530 132 181 22,000 -35 -39 44 284 568 136 193 37 255 510 129 183 24,000 -39 -43 44 276 552 134 196 37 247 494 127 186 26,000 -43 -47 44 271 542 133 201 36 239 478 124 189 28,000 -47 -50 42 262 524 129 202 36 232 464 122 192 29,000 -49 -52 41 255 510 125 201 35 228 456 121 194 31,000 -53 -56 39 241 482 118 196 35 223 446 119 197 33,000 -57 -60 --- --- --- --- --- 34 217 434 115 199 35,000 -61 -64 --- --- --- --- --- 32 205 410 108 195 BT03588 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 7-92.  Maximum Range Power at 1500 RPM - ISA -10°C (Sheet 2 of 2)  IR 7-140  Change 2