TM 1-1510-223-10 MAXIMUM CRUISE POWER 1700 RPM ISA +37°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 56 52 78 607 1214 203 218 78 607 1214 204 219 2000 53 48 76 577 1154 199 220 76 577 1154 201 222 4000 49 44 74 548 1096 195 222 74 548 1096 197 224 6000 45 40 72 521 1042 191 224 72 521 1042 192 226 8000 41 36 69 494 988 186 226 69 494 988 188 228 10,000 37 32 66 466 932 181 227 66 466 932 183 229 12,000 33 28 62 435 870 175 226 62 435 870 177 229 14,000 29 24 58 406 812 168 225 59 406 812 171 228 16,000 25 20 54 377 754 161 223 54 378 756 164 227 18,000 21 16 50 349 698 153 219 50 349 698 156 224 20,000 17 12 46 323 646 145 216 46 324 648 149 222 22,000 13 8 42 303 606 138 213 43 303 606 142 220 24,000 9 4 39 283 566 130 209 39 283 566 135 217 26,000 4 0 37 266 532 123 205 37 267 534 129 215 28,000 0 -3 35 252 504 116 202 35 253 506 124 215 29,000 -2 -5 34 245 490 112 200 34 247 494 121 215 31,000 -5 -9 --- --- --- --- --- 32 231 462 114 211 33,000 -10 -13 --- --- --- --- --- 29 213 426 105 203 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03292 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 7-56.  Maximum Cruise Power at 1700 RPM - ISA +37 °C (Sheet 2 of 2)  IR 7-82  Change 2