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 40 35 83 643 1286 215 224 83 643 1286 216 226 2000 36 31 83 622 1244 213 228 83 622 1244 214 230 4000 32 27 83 603 1206 210 233 83 603 1206 212 235 6000 28 23 83 587 1174 208 237 83 586 1172 210 239 8000 24 19 80 558 1116 203 239 81 558 1116 205 241 10,000 21 15 77 528 1056 197 240 77 529 1058 200 242 12,000 17 11 73 498 996 191 240 74 498 996 194 243 14,000 12 7 69 466 932 183 238 69 466 932 186 241 16,000 8 3 64 437 874 176 236 65 438 876 179 240 18,000 4 -1 61 411 822 169 234 61 412 824 173 240 20,000 0 -5 57 385 770 161 232 57 386 772 166 240 22,000 -4 -9 53 362 724 153 228 54 363 726 159 238 24,000 -8 -13 50 339 678 144 223 50 340 680 151 236 26,000 -12 -17 46 318 636 134 216 47 319 638 143 229 28,000 -17 -20 43 298 596 123 206 44 300 600 135 224 29,000 -19 -22 41 287 574 113 195 42 290 580 130 221 31,000 -22 -26 --- --- --- --- --- 38 270 540 118 210 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000- --- --- --- --- --- --- --- --- --- --- --- --- BT0559311 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 7-53.  Maximum Cruise Power at 1700 RPM - ISA +20 °C (Sheet 1 of 2)  CA Change 2  7-75