TM 1-1510-224-10 NORMAL CRUISE POWER 1500 RPM ISA +10°C WEIGHT® 16,000 POUNDS 14,000 POUNDS PRESSURE ALTITUDE IOAT OAT 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 94 633 1266 229 234 94 632 1264 230 236 2000 26 21 94 613 1226 226 238 94 613 1226 228 240 4000 23 17 94 596 1192 224 243 94 595 1190 226 245 6000 19 13 94 580 1160 221 248 94 580 1160 223 250 8000 15 9 94 567 1134 219 252 94 567 1134 221 254 10,000 11 5 89 534 1068 211 251 89 534 1068 214 254 12,000 7 1 85 506 1012 205 252 85 507 1014 208 255 14,000 3 -3 82 480 960 199 253 82 481 962 202 256 16,000 -1 -7 78 454 908 193 252 78 454 908 196 256 18,000 -5 -11 73 427 854 185 251 74 428 856 189 256 20,000 -9 -15 69 403 806 178 249 69 403 806 182 255 22,000 -13 -19 65 379 758 169 246 65 380 760 174 253 24,000 -17 -23 60 355 710 161 242 61 356 712 167 250 26,000 -21 -27 56 331 662 151 235 56 333 666 158 246 28,000 -26 -30 51 308 616 139 226 52 310 620 149 241 29,000 -28 -32 49 296 592 131 218 50 299 598 144 238 31,000 -32 -36 --- --- --- --- --- 46 277 554 133 228 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05226 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 7-56.  Normal Cruise Power at 1500 RPM - ISA +10°C (Sheet 1 of 2) 7-86