TM 1-1510-224-10 NORMAL CRUISE POWER 1500 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 30 25 83 592 1184 216 221 82 588 1176 217 222 2000 26 21 79 555 1110 209 221 78 553 1106 211 222 4000 22 17 75 522 1044 203 221 74 517 1034 204 222 6000 18 13 71 489 978 196 220 71 486 972 198 223 8000 14 9 68 461 922 190 220 67 457 914 192 222 10,000 10 5 64 432 864 182 217 63 427 854 184 220 12,000 6 1 61 405 810 175 217 60 401 802 178 220 14,000 2 -3 59 383 766 170 217 57 377 754 173 220 16,000 -2 -7 56 360 720 163 215 55 355 710 167 220 18,000 -6 -11 54 344 688 158 215 52 332 664 160 218 20,000 -10 -15 54 336 672 155 218 49 314 628 153 216 22,000 -14 -19 55 334 668 153 223 47 299 598 147 215 24,000 -18 -23 56 336 672 153 230 46 291 582 143 217 26,000 -22 -27 --- --- --- --- --- 47 291 582 142 222 28,000 -26 -30 --- --- --- --- --- 49 294 588 142 230 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT058717 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately 10%,  fuel  flow  will  decrease  approximately  5%,  and  true  airspeed  will  be  reduced by approximately 10 knots. Figure 7A-68.  Maximum Range Power at 1500 RPM - ISA +10°C (Sheet 1 of 2) 7A-106