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 75 554 1108 201 192 71 538 1076 198 189 2000 -16 -19 71 518 1036 194 191 67 505 1010 192 188 4000 -20 -23 67 485 970 188 190 64 471 942 186 188 6000 -24 -27 64 455 910 182 190 60 440 880 180 187 8000 -28 -31 61 427 854 176 189 57 412 824 174 186 10,000 -32 -35 58 401 802 170 189 54 383 776 167 186 12,000 -35 -39 57 381 762 166 190 51 359 718 162 186 14,000 -39 -43 55 364 728 162 191 491 339 678 157 186 16,000 -43 -47 54 348 696 158 193 47 319 638 152 186 18,000 -47 -51 53 335 670 155 195 46 204 608 148 186 20,000 -51 -55 52 324 648 151 196 45 292 584 144 188 22,000 -53 -59 53 322 644 150 201 45 287 574 142 191 24,000 -59 -63 54 320 640 149 207 45 281 562 140 195 26,000 -62 -67 53 315 630 146 210 46 281 562 140 201 28,000 -65 -70 51 300 600 139 207 47 281 562 140 208 29,000 -68 -72 53 307 614 140 212 45 273 546 136 206 31,000 -72 -76 54 314 628 141 220 45 268 536 131 206 33,000 -76 -80 --- --- --- --- --- 47 276 552 132 215 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05592 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 7-89.  Maximum Range Power at 1500 RPM - ISA -30°C (Sheet 1 of 2)CA Change 2  7-133