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 85 596 1192 198 207 80 581 1162 196 205 2000 35 31 79 556 1112 191 206 76 545 1090 190 205 4000 31 27 75 520 1040 185 205 73 511 1022 185 205 6000 27 23 71 485 970 178 204 69 479 958 179 205 8000 23 19 67 454 908 171 203 65 446 892 172 203 10,000 19 15 63 424 848 165 201 62 417 834 166 203 12,000 15 11 60 398 796 158 200 59 392 784 161 203 14,000 11 7 58 382 764 153 200 55 368 736 153 200 16,000 7 3 59 376 752 152 205 51 345 690 146 198 18,000 3 -1 60 370 740 150 209 49 327 654 141 197 20,000 0 -5 60 364 728 148 213 50 321 642 139 201 22,000 -4 -9 59 356 712 144 215 51 320 640 138 207 24,000 -8 -13 --- --- --- --- --- 52 317 634 137 212 26,000 -12 -17 --- --- --- --- --- 51 310 620 133 214 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03593 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 7-98.  Maximum Range Power at 1500 RPM - ISA +20 °C (Sheet 1 of 2)   IR Change 2  7-151