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 29 25 83 618 1236 212 218 83 618 1236 213 219 2000 26 21 83 598 1196 210 222 83 598 1196 211 223 4000 23 17 83 580 1160 208 226 83 580 1160 209 227 6000 18 13 83 564 1128 206 231 83 564 1128 207 232 8000 14 9 83 552 1104 204 236 83 552 1104 205 237 10,000 11 5 83 545 1090 202 241 83 544 1088 203 242 12,000 7 1 83 534 1068 200 246 83 534 1068 201 247 14,000 3 -3 79 503 1006 193 246 79 503 1006 195 248 16,000 -1 -7 74 474 948 187 245 74 474 948 189 248 18,000 -5 -11 70 446 892 181 245 70 447 894 183 248 20,000 -9 -15 66 422 844 174 245 66 422 844 177 248 22,000 -13 -19 62 398 796 168 244 62 398 796 170 248 24,000 -17 -23 58 373 746 161 243 58 374 748 164 247 26,000 -21 -27 54 350 708 154 241 54 351 702 157 246 28,000 -25 -30 50 328 656 147 238 50 329 658 151 244 29,000 -27 -32 48 317 634 143 237 48 318 636 147 243 31,000 -31 -36 44 294 588 135 232 45 295 590 140 241 33,000 -36 -40 40 272 544 125 225 41 273 546 132 237 35,000 -39 -44 36 248 496 114 215 37 250 500 123 230 BT03286 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 7-50.  Maximum Cruise Power at 1700 RPM - ISA +10 °C (Sheet 2 of 2)   IR 7-70  Change 2