TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA 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 20 15 83 631 1262 233 234 83 631 1262 234 235 2000 16 11 83 616 1232 231 239 83 616 1232 232 240 4000 13 7 83 601 1202 228 243 83 601 1202 230 245 6000 9 3 83 585 1170 226 248 83 585 1170 227 250 8000 5 -1 83 571 1142 224 253 83 571 1142 225 255 10,000 1 -5 83 559 1118 222 259 83 558 1116 223 260 12,000 -2 -9 83 547 1094 220 265 83 547 1094 222 266 14,000 -6 -13 83 539 1078 218 270 83 539 1078 220 272 16,000 -10 -17 80 513 1026 213 272 80 513 1026 214 274 18,000 -14 -21 76 484 968 206 272 76 484 968 208 275 20,000 -18 -25 72 458 916 200 273 72 459 918 202 276 22,000 -22 -29 68 433 866 193 273 68 434 868 195 276 24,000 -26 -33 64 408 816 186 273 64 409 818 189 276 26,000 -30 -37 60 383 766 179 271 60 383 766 182 275 28,000 -34 -40 55 357 714 171 269 55 357 714 174 274 29,000 -36 -42 53 343 686 167 267 53 344 688 170 273 31,000 -40 -46 48 318 636 158 263 49 319 638 162 270 33,000 -44 -50 44 293 586 148 257 44 294 588 154 265 35,000 -49 -54 40 267 534 137 248 40 269 538 144 260 BT05221 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 7-43.  Maximum Cruise Power at 1700 RPM - ISA (Sheet 2 of 2) 7-65