TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA -10°C WEIGHT® 16,000 POUNDS 14,000 POUNDS PRESSURE ALTITUDE IOAT OAT 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 83 633 1266 230 228 83 632 1264 232 229 2000 6 1 83 614 1228 230 234 83 614 1228 231 235 4000 2 -3 83 598 1196 227 238 83 597 1194 229 240 6000 -1 -7 83 583 1166 225 242 83 583 1166 227 244 8000 -5 -11 83 570 1140 223 247 83 570 1140 224 249 10,000 -9 -15 83 559 1118 220 252 83 559 1118 222 254 12,000 -13 -19 83 548 1096 218 257 83 548 1096 220 259 14,000 -16 -23 83 539 1078 216 263 83 539 1078 218 265 16,000 -20 -27 83 531 1062 214 269 83 530 1060 216 271 18,000 -24 -31 82 515 1030 210 272 82 516 1032 212 275 20,000 -28 -35 78 491 982 204 272 78 491 982 206 276 22,000 -32 -39 73 463 926 196 271 74 463 926 199 275 24,000 -36 -43 69 434 868 188 269 69 435 870 192 274 26,000 -40 -47 64 405 810 179 266 64 406 812 183 272 28,000 -44 -50 59 375 750 169 261 59 376 752 174 268 29,000 -46 -52 56 361 722 164 257 57 362 724 170 266 31,000 -51 -56 51 332 664 152 248 52 334 668 160 260 33,000 -55 -60 46 304 608 138 235 47 307 614 149 252 35,000 -59 -64 - - - - - - - - - - - - - - - 42 279 558 136 239 BT05222 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 7-42.  Maximum Cruise Power at 1700 RPM - ISA -10°C (Sheet 1 of 2) 7-62