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287 - ATPL Question Bank in English - In a swept-wing aeroplane without corrective devices, assume shock-induced separation develops symmetrically first near the wing roots and shifts the wing centre of pressure aft. A possible consequence is:

Question 287 - Principles of Flight - ATPL - Airline Transport Pilot Licence

Engine unbalance and buffeting.
An increase in speed and a tendency to pitch up.
Buffeting of the aeroplane and a tendency to pitch up.
Buffeting of the aeroplane and a tendency to pitch down.

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