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 89 610 1220 201 213 79 580 1160 194 206 2000 45 41 86 579 1158 196 215 78 553 1106 191 209 4000 41 37 81 542 1084 189 214 74 518 1036 185 208 6000 37 33 76 506 1012 182 212 69 481 962 177 206 8000 33 29 72 474 948 175 211 64 449 898 170 205 10,000 29 25 69 447 894 170 210 61 418 836 163 203 12,000 25 21 66 423 846 164 211 57 390 780 157 202 14,000 21 17 64 401 802 159 211 55 366 732 151 201 16,000 18 13 63 389 778 156 213 54 354 708 148 204 18,000 13 9 --- --- --- --- --- 55 350 700 147 210 20,000 --- --- --- --- --- --- --- --- --- --- --- --- 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03595 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 7-100.  Maximum Range Power at 1500 RPM - ISA +30 °C (Sheet 1 of 2)  IR Change 2  7-155