TM 1-1510-223-10 MAXIMUM RANGE POWER 1500 RPM ISA + 30°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 49 45 84 606 1212 204 216 82 600 1200 204 217 2000 45 41 82 82 1152 199 218 76 557 1114 196 215 4000 42 37 79 546 1092 195 219 71 519 1038 189 213 6000 37 33 74 509 1018 187 217 67 483 966 181 211 8000 34 29 70 478 956 181 217 63 450 900 175 210 10,000 30 25 67 450 900 175 217 60 421 842 169 210 12,000 26 21 65 423 846 169 217 57 395 790 164 210 14,000 22 17 62 400 800 164 217 55 370 740 158 209 16,000 17 13 --- --- --- --- --- 54 354 708 154 211 18,000 14 9 --- --- --- --- --- 54 347 694 152 215 20,000 --- --- --- --- --- --- --- --- --- --- --- --- 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559213 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 7-101.  Maximum Range Power at 1500 RPM - ISA +30 °C (Sheet 1 of 2)   CA Change 2  7-157