TM 1-1510-224-10 MAXIMUM RANGE POWER 1500 RPM ISA +30°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 50 45 89 615 1230 224 233 87 601 1202 222 231 2000 46 41 88 577 1154 217 233 77 557 1114 208 227 4000 42 37 81 542 1084 211 233 72 520 1040 200 225 6000 38 33 74 405 1010 197 229 67 482 964 192 223 8000 34 29 70 473 946 190 228 63 449 898 185 222 10,000 30 25 67 444 888 184 227 60 418 836 178 220 12,000 26 21 64 416 832 177 226 57 390 780 172 220 14,000 22 17 61 394 788 172 227 54 365 730 165 219 16,000 18 13 61 381 762 168 230 53 349 698 161 221 18,000 14 9 --- --- --- --- --- 53 341 682 159 225 20,000 --- --- --- --- --- --- --- --- --- --- --- --- 22,000 --- --- --- --- --- --- --- --- --- --- --- --- 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05253 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately 10%,  fuel  flow  will  decrease  approximately  5%,  and  true  airspeed  will  be  reduced by approximately 10 knots. Figure 7-70.  Maximum Range Power at 1500 RPM - ISA +30°C (Sheet 1 of 2) 7-110