TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA WEIGHT® 16,000 POUNDS 14,000 POUNDS PRESSURE ALTITUDE IFAT FAT TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS FEET °C °C PERCENT LBS/HR LBS/HR KTS KTS PERCENT LBS/HR LBS/HR KTS KTS 0 20 15 83 631 1262 229 230 83 630 1260 230 232 2000 16 11 83 616 1232 227 235 83 615 1230 229 237 4000 12 7 83 601 1202 224 239 83 600 1200 226 241 6000 9 3 83 585 1170 222 244 83 584 1168 224 246 8000 5 -1 83 571 1142 220 249 83 570 1140 222 251 10,000 1 -5 83 558 1116 218 254 83 557 1114 219 256 12,000 -3 -9 83 546 1092 216 259 83 545 1090 218 262 14,000 -6 -13 83 538 1076 214 265 83 538 1076 216 267 16,000 -10 -17 80 512 1024 207 266 80 513 1026 210 269 18,000 -14 -21 75 483 966 200 265 75 483 966 203 269 20,000 -18 -25 71 458 916 193 265 72 458 916 197 269 22,000 -22 -29 67 432 864 186 263 68 433 866 190 268 24,000 -26 -33 63 407 814 178 261 64 407 814 182 267 26,000 -30 -37 59 381 762 169 257 59 382 764 174 265 28,000 -35 -40 54 354 708 159 251 55 356 712 165 261 29,000 -37 -42 52 341 682 154 247 52 342 684 161 258 31,000 -41 -46 47 314 628 141 236 48 316 632 150 251 33,000 -45 -50 --- --- --- --- --- 43 291 582 139 241 35,000 -50 -54 --- --- --- --- --- 39 264 528 123 224 BT058689 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately 12%,  fuel  flow  will  decrease  approximately  8%,  and  true  airspeed  will  be  reduced by approximately 15 knots. Figure 7A-43.  Maximum Cruise Power at 1700 RPM - ISA (Sheet 1 of 2) 7A-64