TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA -30°C 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 -10 -15 83 627 1254 233 222 83 627 1254 234 223 2000 -14 -19 83 608 1216 232 228 83 608 1216 233 229 4000 -18 -23 83 590 1180 232 234 83 590 1180 233 235 6000 -22 -27 83 574 1148 230 238 83 574 1148 231 240 8000 -25 -31 83 562 1124 229 244 83 562 1124 230 245 10,000 -29 -35 83 553 1106 227 249 83 552 1104 228 250 12,000 -33 -39 83 542 1084 225 254 83 542 1084 226 256 14,000 -37 -43 83 533 1066 223 260 83 533 1066 224 261 16,000 -40 -47 83 526 1052 221 265 83 526 1052 223 267 18,000 -44 -51 83 519 1038 219 271 83 519 1038 221 273 20,000 -48 -55 83 513 1026 217 277 83 513 1026 219 279 22,000 -51 -59 83 509 1018 215 283 83 508 1016 217 285 24,000 -55 -63 80 488 976 210 285 80 489 978 212 288 26,000 -59 -67 74 456 912 202 284 75 457 914 204 287 28,000 -63 -70 67 416 832 192 279 68 418 836 195 283 29,000 -65 -72 64 395 790 186 276 64 397 794 189 281 31,000 -70 -76 57 356 712 175 269 57 358 716 179 275 33,000 -74 -80 50 320 640 163 261 51 323 646 168 268 35,000 -79 -84 43 282 564 149 249 44 286 572 156 259 BT0586816 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-40.  Maximum Cruise Power at 1700 RPM - ISA -30°C (Sheet 1 of 2) 7A-58