TM 1-1510-223-10 MAXIMUM RANGE POWER 1500 RPM ISA -20°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 -1 -5 82 584 1168 207 201 75 558 1116 200 196 2000 -5 -9 77 545 1090 199 200 71 524 1048 195 195 4000 -9 -13 73 510 1020 193 199 67 489 978 188 195 6000 -13 -17 69 479 958 187 199 63 457 914 182 194 8000 -17 -21 66 450 900 181 198 60 427 854 176 193 10,000 -21 -25 63 423 846 175 198 57 399 798 170 193 12,000 -25 -29 61 399 798 170 199 54 374 748 165 192 14,000 -29 -33 59 380 760 166 200 52 353 706 160 193 16,000 -33 -37 58 364 728 162 202 50 334 668 155 193 18,000 -37 -41 57 352 704 159 204 49 319 638 151 194 20,000 -41 -45 56 342 684 156 207 48 307 614 147 196 22,000 -44 -49 56 336 672 154 211 48 301 602 146 201 24,000 -48 -53 55 324 648 149 211 48 296 592 144 205 26,000 -53 -57 52 308 616 141 208 48 292 584 142 210 28,000 -56 -60 53 310 620 139 212 46 279 558 136 208 29,000 -58 -62 54 315 630 140 217 45 271 542 132 206 31,000 -62 -66 -- --- --- --- --- 46 275 550 131 211 33,000 -66 -70 -- --- --- --- --- 48 282 564 131 219 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT055923 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 7-91.  Maximum Range Power at 1500 RPM - ISA -20°C (Sheet 1 of 2)  CA Change 2  7-137