TM 1-1510-224-10 MAXIMUM RANGE POWER 1500 RPM ISA -20°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 -1 -5 85 592 1184 222 216 76 561 1122 213 208 2000 -5 -9 80 553 1106 214 214 72 526 1052 207 207 4000 -9 -13 75 516 1032 206 213 68 492 984 200 206 6000 -13 -17 71 484 968 200 212 64 458 916 193 205 8000 -17 -21 67 454 908 193 211 61 427 854 186 204 10,000 -21 -25 64 427 854 187 211 57 399 798 180 203 12,000 -25 -29 62 401 802 181 211 54 373 746 174 203 14,000 -29 -33 60 381 762 176 212 52 352 704 169 203 16,000 -32 -37 58 364 728 172 213 51 334 668 164 204 18,000 -36 -41 57 350 700 168 215 49 319 638 160 206 20,000 -40 -45 55 337 674 164 216 48 307 614 157 208 22,000 -44 -49 55 329 658 161 220 48 300 600 155 212 24,000 -48 -53 54 322 644 157 223 48 292 584 152 215 26,000 -52 -57 52 306 612 150 219 48 287 574 149 219 28,000 -56 -60 51 301 602 145 220 46 278 556 145 220 29,000 -58 -62 52 307 614 146 226 45 271 542 131 218 31,000 -62 -66 --- --- --- --- --- 44 266 532 137 219 33,000 -65 -70 --- --- --- --- --- 47 277 554 139 231 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05243 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 7-65.  Maximum Range Power at 1500 RPM - ISA - 20°C (Sheet 1 of 2) 7-100