Discussion
An aircraft has an operating empty weight of \( 45 \) t, payload of \( 20 \) t and fuel of \( 25 \) t. Its take-off weight is
Answer: B
Correct answer: 90 t
The take-off weight is the sum of the three:
\[ 45 + 20 + 25 = 90 \text{ t} \]Operating empty weight covers the structure, systems, engines and crew; payload is what is being carried for revenue; and fuel is the third component. This simple addition is the constraint that generates the payload-range diagram, since the total is capped.
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