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 94 631 1262 228 233 94 631 1262 229 235 2000 26 21 94 612 1224 225 238 94 611 1222 227 232 4000 22 17 94 594 1188 223 242 94 594 1188 225 244 6000 19 13 94 579 1158 220 246 94 578 '1156 222 249 8000 15 9 94 566 1132 218 251 94 565 1130 220 253 10,000 11 5 89 534 1068 210 250 89 534 1068 213 253 12,000 7 1 85 506 1012 205 251 85 507 1014 207 254 14,000 3 -3 82 480 960 199 252 82 480 960 202 255 16,000 -1 -7 78 453 906 192 251 78 454 908 195 255 18,000 -5 -11 73 427 854 185 250 74 428 856 188 255 20,000 -9 -15 69 402 804 177 248 69 403 806 181 254 22,000 -13 -19 65 379 758 168 245 65 380 760 174 252 24,000 -17 -23 60 355 710 160 240 61 356 712 166 249 26,000 -21 -27 56 331 662 149 234 56 332 664 157 245 28,000 -26 -30 51 307 614 137 223 52 310 620 148 239 29,000 -28 -32 49 296 592 129 215 50 298 596 143 236 31,000 -32 -36 --- --- --- -- --- 46 277 554 131 226 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- 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-56.  Normal Cruise Power at 1500 RPM - ISA +10C (Sheet 1 of 2) 7A-86