TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA -30°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 -15 83 628 1256 234 223 83 628 1256 235 224 2000 -14 -19 83 609 1218 233 229 83 609 1218 234 230 4000 -18 -23 83 591 1182 233 235 83 591 1182 234 236 6000 -22 -27 83 576 1152 231 239 83 575 1150 232 240 8000 -25 -31 83 564 1128 230 245 83 564 1128 231 246 10,000 -29 -35 83 554 1108 228 250 83 554 1108 229 251 12,000 -33 -39 83 544 1088 226 255 83 544 1088 227 256 14,000 -36 -43 83 535 1070 224 261 83 535 1070 225 262 16,000 -40 -47 83 528 1056 222 266 83 527 1054 223 268 18,000 -44 -51 83 521 1042 220 272 83 520 1040 222 274 20,000 -47 -55 83 515 1030 218 278 83 514 1028 219 280 22,000 -51 -59 83 510 1020 216 284 83 510 1020 218 286 24,000 -55 -63 80 488 976 211 286 80 489 978 213 289 26,000 -59 -67 75 456 912 203 285 75 457 914 205 288 28,000 -63 -70 67 416 832 192 280 68 418 836 195 284 29,000 -65 -72 64 395 790 187 277 64 397 794 190 281 31,000 -70 -76 57 356 712 176 270 57 359 718 179 276 33,000 -74 -80 50 320 640 164 262 51 323 646 169 269 35,000 -79 -84 43 282 564 150 250 44 286 572 156 260 BT05209 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 7-40.  Maximum Cruise Power at 1700 RPM - ISA -30°C (Sheet 2 of 2) 7-59