TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA WEIGHT® 12,000 POUNDS 10,000 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 20 15 83 630 1260 232 233 83 630 1260 233 234 2000 16 11 83 615 1230 230 238 83 615 1230 231 239 4000 13 7 83 600 1200 228 243 83 599 1198 229 244 6000 9 3 83 584 1168 225 247 83 584 1168 227 249 8000 5 -1 83 570 1140 223 252 83 569 1138 224 254 10,000 1 -5 83 557 1114 221 258 83 557 1114 223 259 12,000 -2 -9 83 545 1090 219 263 83 545 1090 221 265 14,000 -6 -13 83 537 1074 218 269 83 537 1074 219 271 16,000 -10 -17 80 513 1026 212 271 80 513 1026 214 273 18,000 -14 -21 76 483 966 205 272 76 484 968 207 274 20,000 -18 -25 72 458 916 199 272 72 459 918 201 275 22,000 -22 -29 68 433 866 193 272 68 434 868 195 275 24,000 -26 -33 64 408 816 186 272 64 409 818 188 275 26,000 -30 -37 60 383 766 178 270 60 383 766 181 275 28,000 -34 -40 55 356 712 170 268 55 357 714 174 273 29,000 -36 -42 53 343 686 166 266 53 344 688 170 272 31,000 -40 -46 48 318 636 157 261 49 319 638 162 269 33,000 -44 -50 44 292 584 147 255 44 294 588 153 265 35,000 -49 -54 39 267 534 136 246 40 268 536 144 259 BT0586810 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-43.  Maximum Cruise Power at 1700 RPM - ISA (Sheet 2 of 2) 7A-65