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DRA G INDEX=200 TOTAL FUEL FLOW LB/HR MIL VMIN MIL VMAX KTAS FUEL FLOW KTAS FUEL FLOW 22 24 26 28 30 32 34 36 38 40 44 48 EFFECT FACTOR TEMP +20C -20C ° ° KTAS GW- 1000 LB 180 210 * DRA G INDEX=250 MIL VMIN MIL VMAX KTAS FUEL FLOW KTAS FUEL FLOW 180 210 T.O. GR1F16CJ11 B430Change 3 Subsonic Cruise 16,000 Feet DATA BASIS FLIGHT TEST CONDITIONS: ENGINE F110GE129 STANDARD DAY TEMPERATURE (-17 ° C) NOTE: REFER TO SECTION V FOR AIRSPEED LIMITATIONS. ---- ---- ---- ---- 6264 6360 6462 6565 6668 6770 6995 7245 1.041 0.933 --- --- --- --- 182 193 203 214 224 234 256 278 1.039 0.964 3265 3824 4536 5380 1.147 0.878 2740 3098 3497 3936 4462 5093 5887 1.108 0.903 2516 2768 3048 3363 3715 4124 4573 5103 5663 6410 1.099 0.901 2542 2704 2897 3109 3368 3644 3967 4314 4693 5188 6277 1.083 0.926 2701 2824 2970 3127 3306 3499 3706 3966 4256 4560 5323 6281 1.067 0.953 2972 3069 3176 3298 3441 3594 3757 3938 4139 4355 4890 5573 1.043 0.974 3317 3397 3490 3592 3702 3821 3957 4107 4267 4437 4848 5312 1.029 0.989 3764 3834 3912 3997 4091 4193 4302 4418 4542 4684 5042 5444 1.007 1.006 4312 4371 4437 4509 4588 4673 4765 4865 4980 5115 5410 5766 0.997 1.014 4953 4998 5050 5112 5184 5272 5369 5473 5583 5703 5965 6255 0.985 1.031 5767 5813 5864 5920 5986 6064 6147 6236 6331 6432 6652 6902 0.975 1.035 6726 6759 6798 6843 6892 6945 7009 7083 7164 7252 7445 7657 0.970 1.046 7870 7894 7921 7952 7987 8026 8069 8118 8182 8260 8428 8613 0.957 1.102 10,440 10,455 10,473 10,494 10,518 10,549 10,584 10,623 10,665 10,710 10,854 11,026 0.834 1.162 11,245 11,243 11,240 11,238 11,235 11,231 11,226 11,222 11,217 11,211 11,196 11,178 0.896 0.991 575 575 575 574 574 574 574 573 573 573 572 571 1.021 0.964 MAX ENDURANCE 250 261 271 281 290 299 307 312 320 329 343 355 1.038 0.960 2507 2698 2897 3097 3298 3499 3701 3907 4130 4355 4823 5309 1.041 0.957 MAX RANGE 312 322 336 345 355 365 374 377 387 397 410 424 1.038 0.960 2794 2994 3228 3436 3650 3871 4093 4258 4508 4760 5271 5822 1.041 0.957 *TEMPERATURE DEVIATION FROM STANDARD DAY. --- VMIN LESS THAN 180 KTAS. ---- ---- ---- ---- 6271 6370 6472 6578 6682 6789 7019 7278 1.041 0.933 --- --- --- --- 183 194 204 215 225 236 258 281 1.039 0.964 3321 3883 4606 5470 1.145 0.879 2804 3165 3570 4011 4548 5185 6002 1.107 0.904 2593 2851 3132 3449 3807 4219 4683 5216 5778 6555 1.096 0.903 2649 2815 3006 3216 3477 3760 4085 4434 4834 5333 6451 1.080 0.927 2842 2970 3114 3270 3447 3639 3846 4115 4406 4711 5510 6470 1.064 0.957 3154 3252 3361 3483 3625 3776 3938 4124 4327 4548 5083 5806 1.039 0.978 3554 3635 3727 3827 3937 4054 4188 4340 4500 4685 5101 5570 1.023 0.994 4061 4130 4207 4290 4383 4484 4592 4708 4847 5010 5372 5770 1.002 1.009 4674 4732 4796 4867 4948 5047 5157 5277 5404 5539 5832 6184 0.992 1.025 5440 5493 5554 5629 5711 5799 5895 5997 6106 6225 6485 6768 0.979 1.033 6388 6432 6481 6536 6600 6677 6759 6849 6943 7044 7264 7513 0.972 1.036 7447 7479 7519 7563 7613 7668 7734 7811 7894 7982 8173 8385 0.965 1.054 8784 8804 8828 8856 8888 8924 8964 9009 9071 9149 9317 9502 0.948 1.119 11,091 11,090 11,090 11,089 11,087 11,085 11,083 11,081 11,078 11,075 11,060 11,043 0.901 0.986 566 566 566 566 566 565 565 565 565 565 564 563 1.012 0.963 MAX ENDURANCE 245 254 264 273 282 291 302 310 316 324 340 355 1.038 0.960 2591 2795 3003 3212 3422 3632 3846 4070 4301 4539 5033 5562 1.041 0.957 MAX RANGE 308 314 325 335 345 356 367 375 374 382 396 410 1.038 0.960 2916 3088 3307 3531 3761 4009 4261 4484 4633 4901 5453 6032 1.041 0.957 Figure B43.(Sheet 24) |