TM 1-1510-223-10 MAXIMUM CRUISE POWER 1700 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 83 632 1264 220 210 83 631 1262 221 211 2000 -15 -19 83 613 1226 219 215 83 612 1224 220 216 4000 -18 -23 83 595 1190 218 220 83 594 1188 220 222 6000 -22 -27 83 579 1158 217 226 83 578 1156 219 227 8000 -26 -31 83 568 1136 215 230 83 567 1134 217 232 10,000 -30 -35 83 558 1116 213 234 83 557 1114 215 236 12,000 -34 -39 83 547 1094 211 239 83 547 1094 212 241 14,000 -37 -43 83 538 1076 209 244 83 538 1076 210 246 16,000 -41 -47 83 531 1062 206 249 83 530 1060 208 251 18,000 -45 -51 83 525 1050 204 254 83 524 1048 206 256 20,000 -48 -55 83 519 1038 202 259 83 519 1038 205 262 22,000 -52 -59 83 511 1022 199 264 83 512 1024 202 267 24,000 -56 -63 78 482 964 192 263 78 483 966 195 267 26,000 -60 -67 72 446 892 183 259 72 448 896 187 264 28,000 -65 -70 64 403 806 171 252 65 406 812 176 258 29,000 -67 -72 60 382 764 165 247 61 385 770 170 254 31,000 -71 -76 54 344 688 152 237 54 346 692 159 246 33,000 -76 -80 47 308 616 137 222 48 311 622 146 236 35,000 -81 -84 40 268 536 111 190 41 275 550 131 221 BT05593 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 7-43.  Maximum Cruise Power at 1700 RPM - ISA -300C (Sheet 1 of 2)   CA Change 2  7-55