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 -11 -15 76 554 1108 212 203 71 536 1072 208 199 2000 -15 -19 72 519 1038 206 202 67 503 1006 202 199 4000 -19 -23 67 484 968 198 201 64 471 942 196 199 6000 -23 -27 64 453 906 192 200 61 440 880 190 198 8000 -27 -31 61 424 848 185 199 57 411 822 184 197 10,000 -31 -35 58 398 796 179 198 54 382 764 177 196 12,000 -35 -39 56 376 752 174 199 51 356 712 170 195 14,000 -39 -43 55 361 722 171 201 49 336 672 166 195 16,000 -43 -47 54 347 694 168 204 47 317 634 160 195 18,000 -47 -51 53 334 668 164 206 45 299 598 155 194 20,000 -51 -55 52 323 646 160 208 44 286 572 151 196 22,000 -54 -59 53 319 638 159 212 45 284 568 150 201 24,000 -58 -63 53 315 630 157 216 45 281 562 149 207 26,000 -62 -67 53 311 622 154 221 46 280 560 148 212 28,000 -66 -70 50 295 590 146 217 46 277 554 147 218 29,000 -68 -72 51 298 596 146 220 46 272 544 145 218 31,000 -71 -76 54 309 618 149 231 44 262 524 138 215 33,000 -76 -80 --- --- --- --- --- 45 268 536 138 224 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT05241 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 7-64.  Maximum Range Power at 1500 RPM - ISA -30°C (Sheet 1 of 2) 7-98