1.

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

A. W<sub>0</sub> = W<sub>crew</sub> + W<sub>payload</sub> + W<sub>fuel</sub> W<sub>empty</sub>
B. W<sub>0</sub> = W<sub>crew</sub> + W<sub>payload</sub> W<sub>fuel</sub> W<sub>empty</sub>
C. W<sub>0</sub> = W<sub>crew</sub> + W<sub>payload</sub> + W<sub>fuel</sub> * W<sub>empty</sub>
D. W<sub>0</sub> = W<sub>crew</sub> + W<sub>payload</sub> + W<sub>fuel</sub> + W<sub>empty</sub>
Answer» E.


Discussion

No Comment Found

Related MCQs