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 83 614 1228 211 206 83 613 1226 213 207 2000 -6 -9 83 594 1188 211 211 83 593 1186 212 213 4000 -9 -13 83 576 1152 209 215 83 575 1150 211 217 6000 -12 -17 83 561 1122 208 220 83 561 1122 209 222 8000 -16 -21 83 551 1102 206 225 83 550 1100 207 226 10,000 -20 -25 83 542 1084 203 229 83 541 1082 205 231 12,000 -24 -29 83 533 1066 201 234 83 533 1066 203 236 14,000 -27 -33 83 526 1052 199 238 83 525 1050 201 241 16,000 -31 -37 83 519 1038 197 243 83 519 1038 199 246 18,000 -35 -41 83 514 1028 195 248 83 514 1028 197 251 20,000 -39 -45 83 512 1024 193 253 83 511 1022 195 256 22,000 -43 -49 79 970 186 253 257 79 486 972 189 256 24,000 -47 -53 74 455 910 178 251 74 455 910 182 255 26,000 -51 -57 68 423 846 170 248 69 424 848 174 253 28,000 -55 -60 63 391 782 161 243 63 393 786 165 249 29,000 -59 -64 57 359 718 150 236 60 377 754 161 247 31,000 -62 -66 54 341 682 143 230 54 344 638 150 240 33,000 -66 -70 47 305 610 127 213 48 309 618 138 229 35,000 -70 -74- --- --- --- --- --- 41 273 546 122 212 BT03279 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 7-44.  Maximum Cruise Power at 1700 RPM - ISA -20 °C (Sheet 1 of 2)  IR Change 2  7-57