TM 1-1510-224-10 NORMAL CRUISE POWER 1500 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 50 45 86 606 1212 220 233 86 607 1214 221 234 2000 46 41 83 577 1154 216 235 84 577 1154 217 237 4000 42 37 81 548 1096 211 237 81 548 1096 212 239 6000 38 33 78 519 1038 206 238 78 1038 1038 208 240 8000 34 29 75 491 982 201 240 75 491 982 203 242 10,000 31 25 72 463 926 195 241 72 463 926 197 244 12,000 27 21 70 438 876 191 243 70 439 878 193 246 14,000 23 17 67 415 830 186 244 67 416 832 188 248 16,000 19 13 63 389 778 179 244 63 390 780 182 247 18,000 15 9 58 361 722 170 240 58 361 722 173 244 20,000 11 5 53 334 668 162 216 54 335 670 166 242 22,000 7 1 50 313 626 155 234 50 314 628 159 241 24,000 2 -3 46 293 586 147 231 47 293 586 152 239 26,000 -2 -7 44 275 550 140 228 44 276 552 146 238 28,000 -6 -10 41 261 522 133 225 42 262 524 140' 237 29,000 -8 -12 40 253 506 129 223 41 254 508 137 237 31,000 -12 -16 37 236 472 118 214 38 238 476 130 233 33,000 -16 -20 --- --- --- --- --- 34 219 438 120 225 35,000 -20 -24 --- --- --- --- --- 31 199 398 109 213 8T058094 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-58.  Normal Cruise Power at 1500 RPM - ISA +30°C (Sheet 2 of 2) 7A-91