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 10 5 94 626 1252 231 228 94 625 1250 233 230 2000 6 1 94 608 1216 229 233 94 608 1216 231 235 4000 2 -3 94 592 1184 227 238 94 592 1184 229 239 6000 -1 -7 94 578 1156 224 242 94 577 1154 226 244 8000 -5 -11 94 566 1132 222 246 94 565 1130 224 248 10,000 -9 -15 94 555 1110 220 251 94 555 1110 222 253 12,000 -13 -19 94 545 1090 217 256 94 545 1090 219 258 14,000 -16 -23 94 536 1072 215 261 94 536 1072 217 263 16,000 -20 -27 92 517 1034 210 263 92 518 1036 212 266 18,000 -24 -31 87 488 976 203 263 87 488 976 206 266 20,000 -28 -35 83 465 930 196 263 83 465 930 200 267 22,000 -32 -39 78 440 880 189 262 79 440 880 193 267 24,000 -36 -43 74 414 828 181 260 74 415 830 185 266 26,000 -40 -47 68 385 770 172 255 69 387 774 177 263 28,000 -45 -50 62 354 708 160 248 63 356 712 167 257 29,000 -47 -52 59 339 678 154 243 60 341 682 162 254 31,000 -51 -56 53 312 624 141 232 54 314 628 151 247 33,000 -55 -60 --- --- --- --- --- 49 290 580 140 238 35,000 -60 -64 --- --- --- --- --- 44 266 532 126 223 BT0586911 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-54.  Normal Cruise Power at 1500 RPM - ISA -10°C (Sheet 1 of 2) 7A-82