TM 1-1510-223-10 MAXIMUM CRUISE POWER 1700 RPM ISA 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 20 15 83 635 1270 221 223 83 635 1270 222 224 2000 16 11 83 620 1240 219 227 83 619 1238 220 228 4000 12 7 83 604 1208 217 232 83 604 1208 218 233 6000 8 3 83 588 1176 215 236 83 588 1176 216 237 8000 -5 -1 83 574 1148 212 241 83 574 1148 214 242 10,000 1 -5 83 561 1122 210 246 83 561 1122 212 247 12,000 -3 -9 83 549 1098 209 251 83 549 1098 210 253 14,000 -7 -13 83 541 1082 206 256 83 541 1082 208 258 16,000 -11 -17 79 511 1022 200 257 79 511 1022 202 259 18,000 -15 -21 75 482 964 194 257 75 482 964 196 260 20,000 -18 -25 71 457 914 188 258 71 457 914 190 261 22,000 -22 -29 67 432 864 182 258 67 432 864 184 261 24,000 -26 -33 63 406 812 175 257 63 407 814 178 261 26,000 -30 -37 59 381 762 168 256 59 381 762 171 260 28,000 -35 -40 54 355 710 160 253 55 355 710 164 258 29,000 -37 -42 52 341 682 156 252 52 342 684 160 257 31,000 -41 -46 48 316 632 148 247 48 317 634 152 254 33,000 -45 -50 43 291 582 138 241 44 292 584 144 250 35,000 -49 -54 39 265 530 128 233 39 267 534 135 244 BT055938 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/HRIENG, and true airspeed will be reduced approximately 20 knots. Figure 7-49.  Maximum Cruise Power at 1700 RPM - ISA (Sheet 2 of 2)   CA 7-68  Change 2