TM 1-1510-223-10 MAXIMUM CRUISE POWER 1700 RPM ISA -30°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 -11 -15 83 631 1262 222 212 83 631 1262 223 213 2000 -15 -19 83 612 1224 221 217 83 612 1224 222 218 4000 -18 -23 83 594 1188 221 223 83 594 1188 222 224 6000 -22 -27 83 578 1156 219 228 83 578 1156 220 229 8000 -26 -31 83 567 1134 218 233 83 566 1132 219 234 10,000 -30 -35 83 557 1114 216 238 83 557 1114 217 239 12,000 -33 -39 83 546 1092 214 242 83 546 1092 215 244 14,000 -37 -43 83 537 1074 212 247 83 537 1074 213 249 16,000 -41 -47 83 530 1060 210 253 83 530 1060 211 254 18,000 -45 -51 83 524 1048 208 258 83 523 1046 210 260 20,000 -48 -55 83 518 1036 206 264 83 518 1036 208 266 22,000 -52 -59 83 512 1024 204 269 83 513 1026 206 271 24,000 -56 -63 79 484 968 197 270 79 484 968 199 272 26,000 -60 -67 73 449 898 189 268 73 450 900 192 271 28,000 -64 -70 65 408 816 179 263 66 410 820 182 266 29,000 -66 -72 62 387 774 174 260 62 389 778 177 264 31,000 -70 -76 55 349 698 163 253 55 351 702 167 258 33,000 -75 -80 48 314 628 152 245 49 316 632 157 252 35,000 -79 -84 42 279 558 140 234 43 281 562 145 243 BT055932 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 2 of 2)   CA 7-56  Change 2