TM 1-1510-223-10 MAXIMUM CRUISE POWER 1700 RPM ISA -10°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 9 5 83 637 1274 219 217 83 636 1272 220 218 2000 6 1 83 618 1236 218 222 83 617 1234 219 224 4000 2 -3 83 601 1202 215 226 83 601 1202 217 228 6000 -2 -7 83 586 1172 213 230 83 585 1170 215 232 8000 -6 -11 83 573 1146 211 235 83 572 1144 213 237 10,000 -10 -15 83 562 1124 209 239 83 561 1122 211 241 12,000 -13 -19 83 551 1102 207 244 83 550 1100 208 246 14,000 -17 -23 83 541 1082 205 249 83 541 1082 207 252 16,000 -21 -27 83 533 1066 203 255 83 533 1066 205 257 18,000 -25 -31 81 514 1028 198 257 81 514 1028 200 260 20,000 -29 -35 77 490 980 192 257 77 490 980 194 261 22,000 -33 -39 73 461 922 184 256 73 461 922 187 260 24,000 -37 -43 68 432 864 176 254 68 433 866 180 258 26,000 -41 -47 63 402 804 168 250 63 403 806 172 256 28,000 -45 -50 58 373 746 158 245 58 374 748 163 252 29,000 -47 -52 55 358 716 153 242 56 359 718 159 250 31,000 -51 -56 50 330 660 142 233 51 332 664 149 244 33,000 -56 -60 45 301 602 127 218 46 304 608 139 236 35,000 -60 -64 --- --- --- --- --- 41 275 550 125 222 BT055935 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 747.  Maximum Cruise Power at 1700 RPM - ISA -10 °C (Sheet 1 of 2)  CA Change 2  7-63