1.

The design take-off gross weight of aircraft is given by _____

A. W0 = Wcrew + Wpayload + Wfuel – Wempty
B. W0 = Wcrew + Wpayload – Wfuel – Wempty
C. W0 = Wcrew + Wpayload + Wfuel * Wempty
D. W0 = Wcrew + Wpayload + Wfuel + Wempty
Answer» E.


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