TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA -10°C WEIGHT® 12,000 POUNDS 10,000 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 83 632 1264 233 231 83 631 1262 234 232 2000 6 1 83 613 1226 233 237 83 613 1226 234 238 4000 2 -3 83 597 1194 230 241 83 597 1194 231 242 6000 -1 -7 83 582 1164 228 246 83 582 1164 229 247 8000 -5 -11 83 570 1140 226 251 83 569 1138 227 252 10,000 -9 -15 83 559 1118 224 256 83 558 1116 225 257 12,000 -12 -19 83 548 1096 222 261 83 548 1096 223 263 14,000 -16 -23 83 538 1076 220 267 83 538 1076 221 269 16,000 -20 -27 83 530 1060 218 273 83 530 1060 220 275 18,000 -24 -31 82 516 1032 215 277 82 516 1032 216 279 20,000 -27 -35 78 492 984 209 278 78 492 984 210 281 22,000 -31 -39 74 464 928 202 278 74 464 928 204 281 24,000 -35 -43 69 436 872 195 278 69 436 872 197 281 26,000 -39 -47 64 407 814 187 276 65 407 814 189 280 28,000 -44 -50 59 377 754 178 274 60 378 756 182 278 29,000 -46 -52 57 363 726 174 272 57 364 728 178 277 31,000 -50 -56 52 336 672 165 268 53 337 674 169 274 33,000 -54 -60 48 309 618 156 263 48 311 622 161 271 35,000 -58 -64 43 282 564 145 255 43 284 568 152 265 BT05223 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 2 of 2) 7-63