TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA +30°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 50 45 82 635 1270 223 236 82 635 1270 225 238 2000 46 41 80 606 1212 218 238 80 606 1212 220 240 4000 42 37 77 577 1154 214 240 77 577 1154 216 242 6000 39 33 75 548 1096 209 242 75 548 1096 211 244 8000 35 29 72 520 1040 203 243 73 520 1040 206 246 10,000 31 25 70 493 986 198 244 70 493 986 201 247 12,000 27 21 66 462 924 191 244 66 463 926 194 247 14,000 23 17 63 433 866 184 243 63 434 868 188 247 16,000 19 13 58 403 806 176 239 58 404 808 180 245 18,000 14 9 53 373 746 165 233 53 374 748 170 240 20,000 10 5 49 347 694 156 228 50 348 696 162 237 22,000 6 1 46 327 654 147 224 47 328 656 155 235 24,000 2 -3 43 307 614 137 216 44 308 616 147 231 26,000 -2 -7 - - - - - - - - - - - - - - - 41 290 580 139 227 28,000 -6 -10 - - - - - - - - - - - - - - - 39 273 546 129 220 29,000 -8 -12 - - - - - - - - - - - - - - - 37 264 528 124 215 31,000 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 33,000 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 35,000 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - BT05214 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 7-46.  Maximum Cruise Power at 1700 RPM - ISA +30°C (Sheet 1 of 2) 7-70