TM 1-1510-223-10 NORMAL CRUISE POWER 1500 RPM ISA -30°C WEIGHT® 16,000 POUNDS 14,000 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 -11 -15 94 625 1250 222 212 94 625 1250 224 214 2000 -15 -19 94 607 1214 220 216 94 607 1214 222 218 4000 -18 -23 94 590 1180 218 220 94 590 1180 220 222 6000 -22 -27 94 575 1150 216 225 94 574 1148 218 226 8000 -26 -31 94 564 1128 215 230 94 563 1126 217 232 10,000 -30 -35 94 554 1108 213 234 94 554 1108 214 236 12,000 -34 -39 94 545 1090 210 239 94 544 1088 212 241 14,000 -37 -43 94 536 1072 208 243 94 536 1072 210 245 16,000 -41 -47 94 530 1060 206 248 94 529 1058 208 250 18,000 -45 -51 94 524 1048 203 253 94 524 1048 205 255 20,000 -49 -55 94 515 1030 200 257 94 515 1030 203 260 22,000 -53 -59 89 487 974 193 256 89 488 976 196 260 24,000 -57 -63 83 458 916 186 255 84 460 920 189 259 26,000 -61 -67 77 426 852 177 252 78 427 854 181 257 28,000 -65 -70 69 386 772 166 244 70 388 776 171 251 29,000 -67 -72 65 365 730 159 239 66 367 734 165 247 31,000 -72 -76 57 327 654 146 227 58 330 660 153 238 33,000 -76 -80 50 294 588 130 212 52 298 596 141 228 35,000 -80 -84 --- --- --- --- --- 45 266 532 126 213 BT05591 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 LBSIHR/ENG, and true airspeed will be reduced approximately 20 knots. Figure 7-66.  Normal Cruise Power at 1500 RPM - ISA -30 °C (Sheet 1 of 2)   CA 7-94  Change 2