 
			 
			MCQOPTIONS
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				| 1. | A fuselage is configure to have length L. What will be the approximated internal volume (V)? | 
| A. | V = 3.4*(S<sub>top</sub>*A<sub>side</sub>/4L) | 
| B. | V = 3.4/4L | 
| C. | V = 3.4*(S<sub>top</sub>*A<sub>side</sub>/4) | 
| D. | V = 0.4*(S<sub>top</sub>*A<sub>side</sub>/L) | 
| Answer» B. V = 3.4/4L | |