What is the boundary layer in relation to an aircraft?
airflow closest to the surface of the aircraft.
What are the three types of commonly used flight control systems?
The cable system is the most widely used because deflections of the structure to which it is attached do not affect its operation.
What is used in large metal aircraft to keep control cable tension within acceptable limits?
A cable tension regulator.
This device ensures that control cables maintain proper tension for effective operation.
What is a fairlead?
cable guide
How much cable deflection is acceptable due to a fairlead?
3°
This limit helps maintain the integrity and functionality of the control cables.
Where does failure of control cables occur most frequently?
pulleys and through fairleads.
Which flight control surfaces are considered the primary group?
These controls are essential for the basic maneuverability of the aircraft.
Which flight controls are considered the secondary group?
Secondary controls assist but do not independently cause rotation of the aircraft.
Which flight controls are in the auxiliary group?
These devices are considered high lift devices for slow speed flight.
How do wing flaps affect landing speed and approach angle of an aircraft?
decreased speed without decreasing lift.
What is a balance tab?
It is an auxiliary control with fixed linkage
What is a trim tab?
It is an auxiliary control attached to the trailing edge
What is the purpose of the collective pitch control in a helicopter?
change pitch of the main rotor blades.
Why is it important for the blades of a helicopter rotor system to be tracked?
To reduce vertical vibrations.
What is the most efficient way to check a helicopter rotor for dynamic balance?
balance computer.
What unit on a helicopter is used to compensate for torque created by the main rotor?
The tail rotor.
The tail rotor counteracts the torque effect, allowing for controlled flight.
What control operates the helicopter tail rotor?
The anti-torque pedals.
What are the three axes of an aircraft?
Each axis corresponds to specific control surfaces: ailerons for roll, elevators for pitch, and rudder for yaw.
What precaution should be taken regarding the position of the bolt when installing an aircraft bolt?
top installed vertically, and forward installed horizontally.
How is the propeller torque corrected for during assembly and rigging in some single engine aircraft?
The leading edge is offset to the longitudinal
What reference publications should be used to rig aircraft, including the control system?
What are vortex generators?
low-aspect-ratio airfoils
What is a servo tab?
A cockpit control attached to the trailing edge
What factors are used to determine the proper cable tension?
These factors ensure the cable operates effectively under varying conditions.