TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA +10°C 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 30 25 83 637 1274 228 234 83 636 1272 230 235 2000 26 21 83 617 1234 226 238 83 616 1232 227 240 4000 23 17 83 599 1198 223 243 83 598 1196 225 244 6000 19 13 83 582 1164 221 247 83 582 1164 223 249 8000 15 9 83 569 1138 219 252 83 569 1138 221 254 10,000 11 5 83 561 1122 217 258 83 560 1120 219 260 12,000 7 1 81 537 1074 212 260 81 537 1074 215 263 14,000 4 -3 77 506 1012 205 260 77 506 1012 208 263 16,000 0 -7 73 476 952 198 259 73 477 954 201 263 18,000 -4 -11 69 448 896 191 258 69 449 898 194 263 20,000 -8 -15 65 424 848 184 257 65 424 848 188 262 22,000 -13 -19 61 399 798 176 255 61 400 800 180 261 24,000 -17 -23 57 375 750 168 252 57 375 750 173 259 26,000 -21 -27 53 351 702 159 247 53 352 704 165 256 28,000 -25 -30 49 328 656 149 241 50 330 660 156 253 29,000 -27 -32 47 317 634 143 237 48 318 636 152 250 31,000 -32 -36 43 293 586 128 222 44 296 592 142 243 33,000 -35 -40 - - - - - - - - - - - - - - - 40 272 544 129 231 35,000 -- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - BT05218 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 7-44.  Maximum Cruise Power at 1700 RPM - ISA +10°C (Sheet 1 of 2) 7-66