TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA -30°C WEIGHT® 16,000 POUNDS 14,000 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 -11 -15 83 628 1256 230 219 83 627 1254 232 221 2000 -14 -19 83 609 1218 229 225 83 608 1216 231 226 4000 -18 -23 83 591 1182 229 231 83 590 1180 231 233 6000 -22 -27 83 575 1150 227 235 83 575 1150 229 237 8000 -26 -31 83 563 1126 226 241 83 563 1126 228 243 10,000 -29 -35 83 553 1106 224 246 83 553 1106 225 247 12,000 -33 -39 83 543 1086 221 250 83 542 1084 223 252 14,000 -37 -43 83 534 1068 219 255 83 534 1068 221 258 16,000 -40 -47 83 527 1054 217 261 83 526 1052 219 263 18,000 -44 -51 83 520 1040 215 267 83 519 1038 218 269 20,000 -48 -55 83 514 1028 213 272 83 514 1028 215 275 22,000 -51 -59 83 510 1020 211 278 83 509 1018 213 281 24,000 -55 -63 79 486 972 204 278 80 487 974 207 282 26,000 -60 -67 73 452 904 195 275 74 454 908 199 280 28,000 -64 -70 66 410 820 184 268 67 413 826 188 274 29,000 -66 -72 62 389 778 177 263 63 392 784 182 271 31,000 -71 -76 55 348 696 163 252 56 353 706 170 262 33,000 -75 -80 48 312 624 147 237 49 315 630 156 251 35,000 -80 -84 40 272 544 122 207 42 279 558 141 235 BT0586815 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 2 of 2) 7A-59