TM 1-1510-223-10 MAXIMUM CRUISE POWER 1700 RPM ISA -20°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 -1 -5 83 633 1266 219 213 83 633 1266 220 214 2000 -5 -9 83 613 1226 218 218 83 613 1226 219 220 4000 -8 -13 83 596 1192 217 224 83 596 1192 219 225 6000 -12 -17 83 583 1166 215 228 83 583 1166 217 230 8000 -16 -21 83 571 1142 213 232 83 571 1142 215 234 10,000 -20 -25 83 561 1122 211 237 83 560 1120 212 239 12,000 -23 -29 83 550 1100 209 242 83 549 1098 210 244 14,000 -27 -33 83 540 1080 207 247 83 540 1080 208 249 16,000 -31 -37 83 532 1064 205 252 83 531 1062 206 254 18,000 -35 -41 83 525 1050 202 257 83 525 1050 204 260 20,000 -38 -45 82 516 1032 199 261 83 517 1034 201 264 22,000 -42 -49 78 486 972 192 260 78 487 974 195 264 24,000 -46 -53 73 456 912 184 259 73 457 914 188 263 26,000 -50 -57 68 425 850 176 256 68 426 852 180 261 28,000 -55 -60 62 393 786 166 251 63 395 790 171 257 29,000 -57 -62 59 377 754 161 248 60 379 758 166 255 31,000 -61 -66 53 344 688 149 239 54 346 692 156 248 33,000 -66 -70 47 307 614 134 223 48 311 622 144 238 35,000 -70 -74- --- --- --- --- --- 41 275 550 128 221 BT055933 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 7-45.  Maximum Cruise Power at 1700 RPM - ISA -20 °C (Sheet 1 of 2)  CA Change 2  7-59