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Question 1
10 / 20pts
Describe static strength in terms of loads and
load factors.
Question 2
15 / 20pts
Describe rigidity requirements in terms of
aerolastic problems, including aileron reversal, divergence, flutter, and
vibrations.
Question 3
0 / 20pts
What factors should be taken into account when
considering “service life”?
Question 4
18 / 20pts
What are the primary types of fuselage
construction?
Question 5
15 / 20pts
Describe the different types of flight control
surfaces and the influence of load and load limits.