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 56 52 76 582 1164 205 220 77 582 1164 208 223 2000 53 48 74 551 1102 201 222 75 551 1102 203 225- 4000 49 44 72 521 1042 196 223 72 521 1042 199 226 6000 45 40 70 492 984 191 224 70 492 984 194 228 8000 41 36 67 465 930 186 225 67 465 930 189 229 10,000 37 32 65 439 878 180 226 65 439 878 184 230 12,000 33 28 63 415 830 175 226 63 416 832 179 232 14,000 29 24 61 392 784 169 226 61 393 786 174 232 16,000 25 20 57 367 734 161 223 57 367 734 167 231 18,000 21 16 52 338 676 150 216 53 339 678 158 226 20,000 16 12 47 309 618 137 204 48 311 622 147 219 22,000 13 8 --- --- --- --- --- 44 290 580 138 212 24,000 8 4 --- --- --- --- --- 40 270 540 126 202 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05869 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-59.  Normal Cruise Power at 1500 RPM - ISA +370C (Sheet 1 of 2) 7A-92