TM 1-1510-223-10 MAXIMUM CRUISE POWER 1700 RPM ISA 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 19 15 83 636 1272 218 220 83 635 1270 219 221 2000 16 11 83 621 1242 216 224 83 620 1240 217 226 4000 12 7 83 605 1210 214 228 83 605 1210 215 230 6000 8 3 83 589 1178 211 233 83 589 1178 213 235 8000 4 -1 83 575 1150 209 237 83 574 1148 211 239 10,000 1 -5 83 562 1124 207 242 83 561 1122 209 244 12,000 -3 -9 83 550 1100 205 247 83 550 1100 207 249 14,000 -7 -13 83 540 1080 202 252 83 540 1080 205 254 16,000 -11 -17 79 510 1020 196 252 79 510 1020 198 255 18,000 -15 -21 75 481 962 189 251 75 482 964 192 255 20,000 -19 -25 71 456 912 183 251 71 456 912 186 255 22,000 -23 -29 67 431 862 175 249 67 431 862 179 254 24,000 -27 -33 63 405 810 168 247 63 406 812 172 253 26,000 -31 -37 58 379 758 159 244 59 380 760 164 251 28,000 -35 -40 54 352 704 150 238 54 354 708 156 247 29,000 -37 -42 51 339 678 144 234 52 340 680 151 244 31,000 -42 -46 47 312 624 132 222 47 314 628 142 238 33,000 -47 -50 42 285 570 113 200 43 289 578 130 228 35,000 -50 -54 --- --- --- --- --- 38 263 526 115 211 BT055937 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 7-49.  Maximum Cruise Power at 1700 RPM - ISA (Sheet 1 of 2)   CA Change 2  7-67