Page 179 - Aeronautical Engineer Data Book

43 545 84 200 195 043 58 965 190 423 35 830 31 975 17 100 19 958 61 680 25 200 55 566 17 350 58 000 11 108 9302 5515 6295 14 690 12 220 18 999 30 343 13

222 000 51 635 31 450 29 735 164 875 170 390 0.467 0.141 0.423 0.647 195 620 65.6 5.64 5.64 11.63 437.3 61.2 8.35 8.56 0.22

178 000 48 150 33 160 28 025 113 125 129 850 0.479 0.178 0.412 0.701 141 500 62.47 5.64 5.64 11.08 363.1 58 7.26 9.26 0.251

165 142 36 400 – 24 035 85 765 120 200 0.523 0.158 0.478 0.77 139 090 57.77 5.64 5.64 10.24 363.1 58 7.26 9.26 0.251

71 500 22 780 19 060 17 670 23 330 48 000 0.539 0.256 0.21 0.826 23 700 44.51 4.14 3.95 11.27 122.4 33.91 4.29 9.39 0.24

60 500 19 190 13 500 14 250 17 940 41 310 0.562 0.261 0.256 0.878 23 860 37.57 4.14 3.95 9.51 122.4 33.91 4.29 9.39 0.24

Zero-fuel Max. payload Max. fuel payload Design payload Design fuel load Operational empty Weight ratios: Ops empty/Max. T/O Max. payload/Max. T/O Max. fuel/Max. T/O Max. landing/