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 94 613 1226 215 205 94 613 1226 216 207 2000 -15 -19 94 595 1190 213 209 94 594 1188 214 211 4000 -19 -23 94 578 1156 211 213 94 578 1156 212 215 6000 -23 -27 94 563 1126 209 217 94 563 1126 210 219 8000 -26 -31 94 551 1102 207 222 94 550 1100 208 223 10,000 -30 -35 94 543 1086 205 226 94 542 1084 207 228 12,000 -34 -39 94 535 1070 203 230 94 535 1070 205 232 14,000 -38 -43 94 529 1058 201 235 94 528 1056 203 237 16,000 -41 -47 94 524 1048 198 239 94 523 1046 200 242 18,000 -45 -51 94 520 1040 196 244 94 519 1038 198 246 20,000 -49 -55 94 517 1034 193 248 94 516 1032 196 251 22,000 -53 -59 90 492 984 187 248 90 493 986 190 252 24,000 -57 -63 84 463 926 180 247 85 464 928 183 251 26,000 -61 -67 78 429 858 171 243 78 430 860 175 248 28,000 -65 -70 70 389 778 160 236 70 391 782 165 242 29,000 -68 -72 65 367 734 153 230 66 370 740 159 238 31,000 -72 -76 57 329 658 139 218 58 332 664 147 230 33,000 -76 -80 --- --- --- --- --- 52 300 600 135 219 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03621 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 7-65.  Normal Cruise Power at 1500 RPM - ISA -30 °C (Sheet 1 of 2)   IR 7-92  Change 2