TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA WEIGHT® 16,000 POUNDS 14,000 POUNDS PRESSURE ALTITUDE IOAT OAT 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 83 632 1264 230 231 83 632 1264 231 233 2000 16 11 83 617 1234 228 236 83 617 1234 229 238 4000 12 7 83 602 1204 225 240 83 601 1202 227 242 6000 9 3 83 586 1172 223 245 83 586 1172 225 247 8000 5 -1 83 572 1144 221 250 83 572 1144 222 252 10,000 1 -5 83 559 1118 218 255 83 559 1118 220 257 12,000 -3 -9 83 548 1096 217 260 83 547 1094 219 263 14,000 -6 -13 83 540 1080 215 266 83 539 1078 217 268 16,000 -10 -17 80 512 1024 208 266 80 513 1026 211 269 18,000 -14 -21 75 483 966 201 266 76 483 966 204 269 20,000 -18 -25 71 458 916 194 266 72 458 916 197 270 22,000 -22 -29 67 432 864 187 264 68 433 866 190 269 24,000 -26 -33 63 407 814 179 262 64 408 816 183 268 26,000 -30 -37 59 381 762 170 259 59 382 764 175 266 28,000 -35 -40 54 354 708 160 253 55 356 712 166 262 29,000 -37 -42 52 341 682 155 249 53 342 684 162 259 31,000 -41 -46 47 314 628 142 239 48 316 632 151 253 33,000 -45 -50 - - - - - - - - - - - - - - - 43 291 582 140 243 35,000 -50 -54 - - - - - - - - - - - - - - - 39 265 530 125 228 BT05220 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 7-43.  Maximum Cruise Power at 1700 RPM - ISA (Sheet 1 of 2) 7-64