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 29 25 80 573 1146 199 204 63 515 1030 181 187 2000 25 21 78 544 1088 195 207 64 495 990 181 192 4000 21 17 75 512 1024 191 208 65 478 956 181 197 6000 17 13 71 479 958 184 207 65 458 916 179 201 8000 13 9 67 449 898 178 207 62 432 864 174 202 10,000 9 5 64 425 850 173 207 60 411 822 170 204 12,000 5 1 61 400 800 167 207 56 383 766 164 203 14,000 1 -3 58 375 750 162 207 53 357 714 158 202 16,000 -3 -7 54 352 704 156 206 50 334 668 152 202 18,000 -7 -11 51 330 660 150 205 47 314 628 147 202 20,000 -11 -15 49 312 624 144 204 45 296 592 143 202 22,000 -15 -19 45 292 584 137 202 43 281 562 138 203 24,000 -19 -23 42 274 548 130 199 40 263 526 132 201 26,000 -23 -27 40 257 514 123 195 38 248 496 126 200 28,000 -27 -30 40 253 506 119 197 36 235 470 121 199 29,000 -29 -32 --- --- --- --- --- 35 226 452 117 196 31,000 -33 -36 --- --- --- --- --- 33 216 432 111 195 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03592 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 7-96.  Maximum Range Power at 1500 RPM - ISA +10 °C (Sheet 2 of 2)   IR 7-148  Change 2