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405 - ATPL - Control surface flutter can be avoided by: 1. a high torsional stiffness of the structure. 2. a low torsional stiffness of the structure. 3. locating a balancing mass in front of the control hinge. 4. locating a balancing mass behind the control hinge. The combination that regroups all of the correct statements is:

Question 405 - Aircraft General Knowledge - Airframe, Systems, Powerplant - ATPL - Airline Transport Pilot license

2, 4.
1, 4.
1, 3.
2, 3.

Training tests and timed exam simulations ATPL - Airline Transport Pilot license