TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA +10°C WEIGHT® 12,000 POUNDS 10,000 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 83 636 1272 231 237 83 635 1270 232 238 2000 26 21 83 616 1232 229 241 83 615 1230 230 242 4000 23 17 83 598 1196 227 246 83 598 1196 228 247 6000 19 13 83 582 1164 224 251 83 581 1162 226 252 8000 15 9 83 568 1136 223 256 83 568 1136 224 257 10,000 12 5 83 560 1120 221 262 83 560 1120 222 263 12,000 8 1 81 537 1074 216 265 81 538 1076 218 267 14,000 4 -3 77 507 1014 210 266 77 507 1014 212 268 16,000 0 -7 73 477 954 204 266 73 478 956 206 268 18,000 -4 -11 69 449 898 197 266 69 450 900 199 269 20,000 -8 -15 65 425 850 191 266 65 425 850 193 269 22,000 -12 -19 61 401 802 184 266 62 401 802 186 269 24,000 -16 -23 58 376 752 177 265 58 376 752 180 269 26,000 -20 -27 54 353 706 169 263 54 353 706 173 268 28,000 -24 -30 50 330 660 162 261 50 331 662 166 267 29,000 -26 -32 48 319 638 158 259 49 320 640 162 266 31,000 -30 -36 44 297 594 149 255 45 298 596 155 263 33,000 -35 -40 41 275 550 140 249 41 276 552 146 259 35,000 -39 -44 37 251 502 129 239 37 253 506 137 253 BT05219 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 2 of 2) 7-67