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 -2 -5 80 567 1134 198 193 73 542 1084 192 188 2000 -6 -9 76 531 1062 191 192 70 510 1020 187 188 4000 -10 -13 72 497 994 185 191 66 478 956 182 188 6000 -14 -17 68 467 934 179 191 63 447 894 175 187 8000 -17 -21 65 440 880 174 191 60 419 838 170 187 10,000 -21 -25 63 415 830 169 191 56 391 782 164 186 12,000 -25 -29 61 394 788 164 192 54 368 736 159 186 14,000 -29 -33 59 377 754 160 193 52 350 700 154 186 16,000 -33 -37 58 362 724 156 194 51 333 666 150 187 18,000 -37 -41 57 351 702 153 197 50 320 640 146 189 20,000 -41 -45 57 343 686 150 200 49 309 618 143 191 22,000 -45 -49 57 339 678 149 205 49 303 606 141 194 24,000 -49 -53 56 329 658 144 205 49 298 596 139 198 26,000 -53 -57 52 311 622 135 200 49 295 590 138 203 28,000 -57 -60 --- --- --- --- --- 47 282 564 131 201 29,000 -59 -62 --- --- --- --- --- 45 274 548 127 198 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03585 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 7-90.  Maximum Range Power at 1500 RPM - ISA -20°C (Sheet 1 of 2)  IR Change 2  7-135