TM 1-1510-223-10 MAXIMUM CRUISE POWER 1700 RPM ISA -10°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 9 5 83 614 1228 213 212 83 614 1228 214 213 2000 5 1 83 594 1188 213 218 83 594 1188 214 219 4000 2 -3 83 578 1156 211 222 83 578 1156 212 223 6000 -2 -7 83 564 1128 209 226 83 564 1128 210 227 8000 -6 -11 83 553 1106 207 231 83 552 1104 208 232 10,000 -10 -15 83 542 1084 205 235 83 542 1084 206 237 12,000 -13 -19 83 534 1068 203 240 83 533 1066 204 242 14,000 -17 -23 83 526 1052 201 245 83 526 1052 202 247 16,000 -21 -27 83 520 1040 199 251 83 520 1040 201 252 18,000 -25 -31 83 514 1028 197 256 83 514 1028 198 258 20,000 -29 -35 79 490 980 191 256 79 490 980 193 259 22,000 -33 -39 74 461 922 184 256 74 461 922 186 259 24,000 -37 -43 69 432 864 177 255 70 433 866 180 258 26,000 -41 -47 64 403 806 170 253 64 403 806 172 257 28,000 -45 -50 59 373 746 162 250 59 374 748 165 254 29,000 -47 -52 57 359 718 158 248 57 360 720 161 253 31,000 -51 -56 52 332 664 149 244 52 332 664 153 250 33,000 -55 -60 47 305 610 140 239 47 306 612 145 246 35,000 -59 -64 42 277 554 130 230 42 279 558 136 241 BT03282 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 7-46.  Maximum Cruise Power at 1700 RPM - ISA -10 °C (Sheet 2 of 2) IR 7-62  Change 2