TM 1-1510-223-10 MAXIMUM RANGE POWER 1500 RPM ISA 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 19 15 92 607 1214 208 210 87 591 1182 205 207 2000 15 11 87 573 1146 201 209 83 560 1120 199 207 4000 11 7 83 542 1084 195 209 80 530 1060 194 208 6000 7 3 79 510 1020 189 209 76 499 998 189 208 8000 3 -1 75 480 960 183 208 71 467 934 182 207 10,000 -1 -5 71 452 904 177 208 68 438 876 176 207 12,000 -5 -9 68 424 848 171 207 64 411 822 170 207 14,000 -9 -13 64 400 800 164 206 61 387 774 164 206 16,000 -13 -17 61 378 756 158 205 59 366 732 159 206 18,000 -17 -21 57 355 710 151 202 56 349 698 154 207 20,000 -21 -25 55 339 678 144 201 53 330 660 148 205 22,000 -25 -29 53 323 646 137 198 51 314 628 142 204 24,000 -39 -43 --- --- --- --- --- 48 295 590 134 200 26,000 -33 -37 --- --- --- --- --- 46 285 570 128 198 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 - --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03589 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 7-94.  Maximum Range Power at 1500 RPM - ISA (Sheet 1 of 2)   IR Change 2  7-143