TM 1-1510-224-10 MAXIMUM RANGE POWER 1500 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 78 582 1164 213 225 74 567 1134 210 222 2000 46 41 71 537 1074 203 222 68 524 1048 201 219 4000 42 37 67 501 1002 196 221 64 489 978 194 219 6000 38 33 62 464 928 189 219 59 454 908 187 218 8000 34 29 58 431 862 182 218 56 423 846 181 217 10,000 30 25 55 401 802 175 217 53 393 786 175 217 12,000 26 21 52 373 746 169 217 51 367 734 170 218 14,000 22 17 49 347 694 163 216 48 342 684 165 218 16,000 18 13 47 326 652 157 215 45 317 634 157 216 18,000 14 9 45 313 626 152 216 41 296 592 150 213 20,000 10 5 45 301 602 149 219 38 275 550 143 211 22,000 6 1 44 289 578 145 221 37 260 520 138 211 24,000 2 -3 43 279 558 142 224 36 247 494 134 212 26,000 -2 -7 43 271 542 139 227 34 236 472 130 213 28,000 -6 -10 --- --- --- --- --- 34 228 456 126 215 29,000 -8 -12 --- --- --- --- --- 34 224 448 124 216 31,000 -12 -16 --- --- --- --- --- 32 209 418 118 214 33,000 -16 -20 --- --- --- --- --- 32 207 414 116 218 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05254 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 2 of 2) 7-111