TM 1-1510-223-10 MAXIMUM CRUISE POWER 1700 RPM ISA +20°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 39 35 83 623 1246 207 217 83 623 1246 209 218 2000 36 31 83 602 1204 205 221 83 601 1202 207 222 4000 32 27 83 582 1164 203 225 83 582 1164 205 227 6000 28 23 83 566 1132 201 229 83 565 1130 203 232 8000 24 19 83 553 1106 199 234 83 553 1106 201 236 10,000 20 15 81 528 1056 194 236 81 528 1056 196 238 12,000 16 11 76 497 994 188 235 76 497 994 190 238 14,000 12 7 71 465 930 179 232 71 466 932 182 236 16,000 8 3 66 436 872 172 230 66 437 874 175 235 18,000 4 -1 62 410 820 164 228 62 411 822 168 234 20,000 0 -5 58 384 768 156 225 58 385 770 161 231 22,000 -4 -9 54 361 722 148 221 55 362 724 154 229 24,000 -8 -13 50 338 676 139 216 51 339 678 146 226 26,000 -12 -17 47 317 634 129 209 47 319 638 138 222 28,000 -16 -20 --- --- --- --- --- 44 299 598 130 217 29,000 -18 -22 --- --- --- --- --- 42 289 578 125 213 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03287 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 7-52.  Maximum Cruise Power at 1700 RPM - ISA +20 °C (Sheet 1 of 2)  IR Change 2  7-73