III.2.2
Design wing area and Definition:
Airbus Industries (Wing middle as square)
| C601 | [m] | |
| Inner chord | 17 | |
| Chord kink 1 | 12 | |
| Chord kink 2 | 7 | |
| Outer chord | 4 | |
| Width at fuselage | 2 * 3.1 | |
| Interval of span 1 | 2 * 8.9 | |
| Interval of span 2 | 2 * 16 | |
| Interval of span 3 | 2 * 8.15 | |
| Area in fuselage | 105.4 | [m2] |
| Inner area | 258.1 | |
| Middle area | 304 | |
| Outer area | 89.7 | |
| Sum: area | 757.15 | |
| Chord in fuselage | 17 | [m] |
| Inner M.A.C. | 14.6 | |
| Middle M.A.C. | 9.7 | |
| Outer M.A.C. | 5.6 | |
| M.A.C. | 11.5 |