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 83 615 1230 211 209 83 615 1230 212 210 2000 5 1 83 595 1190 210 215 83 595 1190 212 216 4000 1 -3 83 579 1158 208 219 83 579 1158 210 220 6000 -2 -7 83 565 1130 206 223 83 565 1130 208 224 8000 -6 -11 83 553 1106 204 277 83 553 1106 206 229 10,000 -10 -15 83 543 1086 202 231 83 543 1086 203 234 12,000 -14 -19 83 534 1068 200 236 83 534 1068 201 238 14,000 -17 -23 83 527 1054 197 241 83 527 1054 199 243 16,000 -21 -27 83 521 1042 195 246 83 520 1040 197 249 18,000 -25 -31 83 513 1026 193 250 83 514 1028 195 253 20,000 -29 -35 79 489 978 186 250 79 489 978 189 254 22,000 -33 -39 74 460 920 179 249 74 461 922 182 253 24,000 -37 -43 69 431 862 171 246 69 432 864 174 251 26,000 -41 -47 64 401 802 162 242 64 402 804 166 248 28,000 -45 -50 58 371 742 153 237 59 373 746 158 244 29,000 -47 -52 56 357 714 148 233 54 344 688 149 239 31,000 -52 -56 51 329 658 136 224 51 330 660 144 236 33,000 -36 -40 --- --- --- --- --- 46 303 606 133 227 35,000 -60 -64- --- --- --- --- --- 41 273 546 119 212 BT03281 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 1 of 2)  IR Change 2  7-61