TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA +20°C WEIGHT® 16,000 POUNDS 14,000 POUNDS PRESSURE ALTITUDE IFAT FAT TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS FEET °C °C PERCENT LBS/HR LBS/HR KTS KTS PERCENT LBS/HR LBS/HR KTS KTS 0 40 35 83 639 1278 226 235 83 638 1276 227 237 2000 36 31 83 618 1236 223 239 83 617 1234 225 241 4000 33 27 83 599 1198 221 244 83 598 1196 223 246 6000 29 23 83 583 1166 219 249 83 582 1164 220 251 8000 25 19 81 560 1120 214 252 81 560 1120 217 254 10,000 21 15 78 531 1062 209 253 78 531 1062 211 255 12,000 17 11 74 500 1000 202 253 75 500 1000 205 256 14,000 13 7 69 468 936 194 251 70 469 938 197 254 16,000 9 3 65 439 878 186 249 65 440 880 190 253 18,000 5 -1 62 413 826 179 247 62 414 828 183 253 20,000 1 -5 58 387 774 171 244 58 388 776 176 251 22,000 -3 -9 54 364 728 163 241 54 365 730 168 249 24,000 -7 -13 50 341 682 153 236 51 342 684 160 246 26,000 -12 -17 47 319 638 143 229 47 321 642 152 242 28,000 -16 -20 43 299 598 131 218 44 302 604 143 238 29,000 -17 -22 38 266 532 135 233 43 292 584 139 234 31,000 -22 -26 35 248 496 125 225 39 271 542 126 223 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT058685 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately 12%,  fuel  flow  will  decrease  approximately  8%,  and  true  airspeed  will  be  reduced by approximately 15 knots. Figure 7A-45.  Maximum Cruise Power at 1700 RPM - ISA +20°C (Sheet 1 of 2) 7A-68