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 78 607 1214 200 214 78 607 1214 201 216 2000 52 48 76 577 1154 195 216 76 577 1154 197 218 4000 48 44 74 548 1096 191 218 74 548 1096 193 220 6000 45 40 71 521 1042 186 219 72 521 1042 189 222 8000 41 36 69 493 986 181 220 69 494 988 184 223 10,000 37 32 66 465 930 175 220 66 466 932 178 224 12,000 33 28 62 434 868 168 218 62 434 868 172 222 14,000 29 24 58 405 810 161 216 58 405 810 165 221 16,000 24 20 53 376 752 152 211 54 377 754 157 218 18,000 20 16 49 346 692 142 205 49 348 696 148 213 20,000 16 12 44 320 640 131 196 45 322 644 139 208 22,000 12 8 --- --- --- --- --- 42 302 604 131 203 24,000 8 4 --- --- --- --- --- 39 282 564 121 195 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03291 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/HRIENG, and true airspeed will be reduced approximately 20 knots. Figure 7-56.  Maximum Cruise Power at 1700 RPM - ISA +37 °C (Sheet 1 of 2)  IR Change 2  7-81