DO NOT MOVE ON TO THE NEXT PAGE WITHOUT ATTEMPTING THIS QUESTION! At landing c...
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DO NOT MOVE ON TO THE NEXT PAGE WITHOUT ATTEMPTING THIS QUESTION!
At landing conditions, the following specifications apply:
- Landing field length = TOFL / 1.5 (TOFL as before)
- Landing CLmax = 2.3
- Weight at landing = MLW (using usual correlation with range = 5169 nm)
- Landing constant 'B' = 0.72
- Ambient density = 0.956 ISA sea-level value
Q3 Calculate, to the nearest 10 Pa, the maximum wing loading (MTOW/Sref, in Pa) which will still satisfy the LFL constraint.
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