TM 1-1510-223-10 MAXIMUM RANGE POWER 1500 RPM ISA 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 19 15 88 607 1214 212 214 86 598 1196 211 213 2000 15 11 83 573 1146 205 213 81 565 1130 205 213 4000 11 7 79 539 1078 198 212 77 531 1062 198 213 6000 7 3 75 508 1016 192 212 73 499 998 192 212 8000 3 -1 72 478 956 187 122 70 469 938 187 213 10,000 -10 -5 68 449 898 180 212 67 441 882 181 213 12,000 -5 -9 65 422 844 175 121 63 413 826 175 213 14,000 -9 -13 62 395 790 168 210 60 386 772 169 212 16,000 -13 -17 59 374 748 162 210 58 365 730 164 212 18,000 -17 -21 56 352 704 155 208 55 346 692 159 212 20,000 -21 -25 54 335 670 149 207 52 327 654 152 211 22,000 -25 -29 52 321 642 143 205 50 311 622 146 210 24,000 -28 -33 53 322 644 142 211 47 292 584 139 207 26,000 -32 -37 55 326 652 141 217 45 281 562 133 205 28,000 -36 -40 56 330 660 141 224 47 285 570 132 212 29,000 -38 -42 --- --- --- --- ---- 47 286 572 132 215 31,000 -42 -46 --- --- --- --- --- 49 290 580 131 222 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT055927 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 7-95.  Maximum Range Power at 1500 RPM - ISA (Sleet 1 of 2)   CA Change 2  7-145