TM 1-1510-224-10 NORMAL CRUISE POWER 1500 RPM ISA -30°C WEIGHT® 12,000 POUNDS 10,000 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 0 -5 94 622 1244 234 228 94 622 1244 235 229 2000 -4 -9 94 604 1208 233 232 94 603 1206 234 233 4000 -8 -13 94 586 1172 231 237 94 586 1172 232 238 6000 -11 -17 94 573 1146 230 243 94 573 1146 231 244 8000 -15 -21 94 562 1124 227 247 94 562 1124 229 249 10,000 -19 -25 94 552 1104 225 252 94 552 1104 227 254 12,000 -23 -29 94 542 1084 223 257 94 542 1084 225 259 14,000 -26 -33 94 533 1066 221 263 94 533 1066 222 264 16,000 -30 -37 94 526 1052 218 268 94 525 1050 220 270 18,000 -34 -41 94 518 1036 216 273 94 518 1036 217 275 20,000 -38 -45 90 496 992 210 275 90 496 992 212 277 22,000 -42 -49 85 468 936 204 275 85 468 936 206 278 24,000 -46 -53 80 440 880 197 275 80 441 882 199 278 26,000 -50 -57 74 409 818 189 273 74 410 820 191 276 28,000 -54 -60 68 377 754 179 269 68 378 756 183 273 29,000 -56 -62 65 361 722 175 267 65 362 724 178 272 31,000 -60 -66 59 331 662 165 262 59 333 666 169 268 33,000 -64 -70 53 303 606 155 255 54 306 612 160 263 35,000 -69 -74 47 274 548 143 246 48 277 554 150 257 8T0588614 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-53.  Normal Cruise Power at 1500 RPM - ISA -200C (Sheet 2 of 2) 7A-81