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 39 35 81 596 1192 202 211 78 584 1168 201 210 2000 35 31 76 556 1112 195 210 74 546 1092 194 209 4000 31 27 72 520 1040 188 209 70 510 11020 188 209 6000 27 23 69 488 976 183 209 66 477 954 182 208 8000 23 19 65 455 910 176 207 63 445 890 176 208 10,000 19 15 62 425 850 169 206 59 413 826 169 206 12,000 15 11 60 402 804 164 207 56 388 776 163 206 14,000 11 7 59 387 774 160 208 53 365 730 157 205 16,000 7 3 59 376 752 157 212 51 347 694 152 205 18,000 4 -1 58 366 732 154 215 49 329 658 146 205 20,000 0 -5 58 357 714 151 218 50 321 642 144 209 22,000 -4 -9 --- --- --- --- --- 50 315 630 142 213 24,000 -8 -13 --- --- --- --- --- 50 309 618 140 217 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559211 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 7-99.  Maximum Range Power at 1500 RPM - ISA +20 °C (Sheet 1 of 2)   CA Change 2  7-153