TM 1-1510-223-10 NORMAL CRUISE POWER 1500 RPM ISA -10°C WEIGHT® 12,000 POUNDS 10,000 POUNDS TORQUE FUEL TOTAL TORQUE FUEL TOTAL PRESSURE PER FLOW FUEL PER FLOW FUEL ALTITUDE IFAT FAT ENGINE PER FLOW IAS TAS ENGINE PER FLOW IAS TAS ENGINE ENGINE FEET °C °C PERCENT LBS/HR LBS/HR KTS KTS PERCENT   LBS/HR    LBS/HR KTS KTS 0 9 5 94 630 1260 222 220 94 630 1260 223 221 2000 6 1 94 613 1226 221 225 94 612 1224 222 226 4000 2 -3 94 596 1192 219 229 94 596 1192 220 231 6000 -2 -7 94 582 1164 216 234 94 582 1164 218 235 8000 -6 -11 94 570 1140 214 238 94 569 1138 215 240 10,000 -9 -15 94 559 1118 212 243 94 559 1118 213 244 12,000 -13 -19 94 549 1098 210 248 94 548 1096 211 249 14,000 -17 -23 94 540 1080 207 253 94 539 1078 209 254 16,000 -21 -27 91 516 1032 202 255 91 516 1032 204 256 18,000 -25 -31 86 487 974 196 255 87 487 974 198 257 20,000 -29 -35 83 464 928 191 256 83 465 930 193 259 22,000 -33 -39 78 439 878 184 256 78 439 878 187 259 24,000 -37 -43 73 413 826 178 255 74 414 828 180 259 26,000 -41 -47 68 385 770 170 253 68 386 772 173 257 28,000 -45 -50 62 355 710 161 249 62 356 712 165 254 29,000 -47 -52 59 340 680 157 247 60 341 682 161 253 31,000 -51 -56 54 314 628 148 243 54 315 630 153 249 33,000 -55 -60 49 290 580 139 237 50 291 582 145 246 35,000 -59 -64 45 266 532 129 230 45 267 534 136 241 BT055916 NOTE During operations with ice vanes extended, torque will decrease approximately 10 percentage points (E.G. 64% - 10 percentage points = 54%), fuel flow will decrease approximately 35 LBS/HR/ENG, and true airspeed will be reduced approximately 20 knots. Figure 7-70.  Normal Cruise Power at 1500 RPM - ISA -10 °C (Sheet 2 of 2)   CA Change 2  7-103