TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA -10°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 10 5 83 631 1262 229 227 83 631 1262 231 229 2000 6 1 83 613 1226 229 233 83 612 1224 231 235 4000 2 -3 83 596 1192 226 237 83 596 1192 228 239 6000 -2 -7 83 582 1164 224 242 83 581 1162 226 243 8000 -5 -11 83 569 1138 222 246 83 568 1136 224 248 10,000 -9 -15 83 558 1116 219 251 83 557 1114 221 253 12,000 -13 -19 83 547 1094 217 256 83 546 1092 219 258 14,000 -16 -23 83 537 1074 215 262 83 537 1074 217 264 16,000 -20 -27 83 529 1058 213 267 83 529 1058 215 270 18,000 -24 -31 82 515 1030 209 271 82 516 1032 212 274 20,000 -28 -35 78 491 982 203 271 78 491 982 206 275 22,000 -32 -39 73 463 926 195 270 74 463 926 198 274 24,000 -36 -43 69 434 868 187 268 69 435 870 191 273 26,000 -40 -47 64 405 810 178 265 64 406 812 183 271 28,000 -44 -50 59 375 750 168 259 59 376 752 174 267 29,000 -46 -52 56 360 720 163 256 57 362 724 169 265 31,000 -51 -56 51 332 664 151 247 52 334 668 159 259 33,000 -55 -60 46 304 608 136 232 47 307 614 148 250 35,000 -59 -64 --- --- --- --- --- 42 278 556 134 237 BT0586811 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-42.  Maximum Cruise Power at 1700 RPM - ISA -10°C (Sheet 1 of 2) 7A-62