Page 188 - Aeronautical Engineer Data Book
P. 188
458 40 000 3270 1565 2079
M0.87 31 000 8970 M0.81 31 000 7060 5994 6787 8234 3701 0.0543 2 192 201
437 35 000 2275 2267 0.0483 348 075
469 9000 459 12 000 6195 0.052 2 075 325
456 26 000 2565 414 35 000 1716 1290 1290 1746 2282 0.0604 138 030
461 26 000 2391 401 35 000 1475 1085 1080 1467 1635 0.0981 75 600
410 37 000 1022 367 32 000 880 850 1390 1563 1791
459 37 000 424 37 000 1620 1982 2090
41 000 452 39 000 2186.84 2897 2927 0.0465 463 520
438 35 000 1375 1811.43 1788.04 0.0684 145 750
7050 8500 9000 2865.71 4144.91 0.0554 2 975 000
500 33 000 7300 475 39 000 5700 6371 7150 8089 2529.97 4242.69 0.0472 2 395 250
470 39 000 4210 6370 2269.21 3146.34 0.046 1 866 410
487 28 000 3550 450 37 000 2100 1955 2700 2602 2211.48 2590.29 0.0465 502 200
487 28 000 3200 448 37 000 2100 637 2700 3672 1962.27 2423.85 0.0443 405 000
Max cruise: Speed (kt) Altitude (ft) Fuel consumption (kg/h) Long range cruise: Speed (kt) Altitude (ft) Fuel consumption (kg/h) Range (nm): Max. payload Design range Max
