Flight Controls Flashcards
What is the propose of an aileron balance cable?
It ties the ailerons together in such a way that when one aileron deflects downward, the other one is pulled upward.
What is the most common construction configuration of flexible control cables?
7 by 19.
What materials are used to manufacture flexible control cables?
carbon steel coated with tin or zinc, or corrosion-resistant steel.
What is the definition of a critical fatigue area of a control cable?
Any working length of a cable where the cable runs over, under, or around a pully, sleeve, or through a fairlead; or any section where the cable is flexed, rubbed, or worked in any manner; or any point within 1 foot of a swaged-on fitting.
How are the ends of two control cables normally connected together?
With swaged, threaded terminals on the ends of each cable, connected with a turnbuckle.
How much is a fairlead allowed to deflect a control cable?
No more than 3°.
Why are the control cables of large airplanes normally equipped with automatic tension regulators?
The large amount of aluminum in the aircraft structure contracts so much as its temperature drops in flight that the control cables could become dangerously loose. The automatic tension regulators keep the cable tension constant as the dimensions of the aircraft change.
When rigging control cables, there are stops at the control surfaces that limit travel and stops at the control input. Which stops should the system contact first?
The stops at the control surface.
How are length adjustments made on a flight control push-pull rod?
One or both ends of the push-pull rod have threaded rod ends.
What is the purpose of a torque tube in a flight control system?
To convert a linear motion to an angular or twisting motion.
What component in a flight control system is often used to change motion by 90 degrees?
A bellcrank.
What is the function of the rudder on an airplane?
The rudder rotates the airplane about its vertical axis.
What is an aerodynamically balanced control surface?
A surface with part of its area ahead of the hinge line. When the surface is deflected, the portion ahead of the hinge aids the movement.
In what publication could you find correct control surface movement for a particular airplane?
In the TCDS for the airplane.
Why is it important than control surfaces be statically balanced?
An out-of-balance control surface can cause severe flutter.