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 75 581 1162 194 208 76 581 1162 196 211 2000 52 48 73 550 1100 190 210 73 551 1102 192 213 4000 48 44 71 520 1040 185 211 71 520 1040 188 214 6000 44 40 69 491 982 180 212 69 491 982 183 216 8000 40 36 66 464 928 175 213 67 464 928 179 217 10,000 36 32 64 438 876 170 214 64 438 876 174 218 12,000 33 28 --- --- --- --- --- 62 415 830 169 219 14,000 29 24 --- --- --- --- --- 58 385 770 162 217 16,000 --- --- --- --- --- --- --- --- --- --- --- --- 18,000 --- --- --- --- --- --- --- --- --- --- --- --- 20,000 --- --- --- --- --- --- --- --- --- --- --- --- 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559215 NOTE During operations with ice vanes extended, torque will decrease approximately 10 percentage   points   (E.G.,   64%   -   10   percentage   points   =   54%0),   fuel   flow   will decrease   approximately   20   LBS/HR/ENG,   and   true   airspeed   will   be   reduced approximately 10 knots. Figure 7-103.  Maximum Range Power at 1500 RPM - ISA +37 °C (Sheet 1 of 2)   CA Change 2  7-161