TM 1-1510-223-10 MAXIMUM CRUISE POWER 1700 RPM ISA + 37°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 56 52 72 606 1212 200 215 72 606 1212 202 217 2000 52 48 71 576 1152 197 218 71 576 1152 199 220 4000 49 44 69 548 1096 193 220 69 548 1096 195 222 6000 45 40 67 521 1042 188 222 67 521 1042 191 225 8000 41 36 65 494 988 184 223 65 494 988 186 226 10,000 37 32 62 466 932 178 223 63 466 932 181 227 12,000 33 28 59 434 868 171 222 59 435 870 175 226 14,000 29 24 56 405 810 164 220 56 406 812 168 225 16,000 25 20 52 376 752 156 216 52 377 754 161 223 18,000 20 16 47 347 694 146 210 48 349 698 152 219 20,000 16 12 44 321 642 135 202 44 323 646 143 214 22,000 12 8 40 300 600 123 192 41 302 604 135 209 24,000 8 4 --- --- --- --- --- 38 282 564 125 202 26,000 4 0 --- --- --- --- --- 36 265 530 115 194 28,000 0 3 --- --- --- --- --- 33 250 500 103 181 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559315 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 7-57.  Maximum Cruise Power at 1700 RPM - ISA +37 °C (Sheet 1 of 2)    CA Change 2  7-83