TM 1-1510-223-10 MAXIMUM RANGE POWER 1500 RPM ISA +37°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 56 52 86 605 1210 197 212 76 573 1146 190 205 2000 52 48 82 570 1140 192 212 74 542 1084 186 206 4000 48 44 80 542 1084 188 214 73 517 1034 183 209 6000 44 40 77 512 1024 183 215 73 495 990 180 213 8000 40 36 74 482 964 177 215 70 467 934 175 213 10,000 36 32 71 455 910 171 215 66 437 874 169 212 12,000 32 28 --- --- --- --- --- 62 408 816 162 211 14,000 28 24 --- --- --- --- --- 59 386 772 157 211 16,000 --- --- --- --- --- --- --- --- --- --- --- --- 18,000 --- --- --- --- --- --- --- --- --- --- --- --- 20,000 --- --- --- --- --- --- --- --- --- --- --- --- 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03597 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 7-102.  Maximum Range Power at 1500 RPM - ISA +37 °C (Sheet 1 of 2)   IR Change 2  7-159