(6) CHAPTER 1-AIRCRAFT STRUCTURAL ASSEMBLY AND RIGGING

What is the function of the vortex generator

to delay or prevent separation of the boundary layer

What are the 3 axes of an airplane

longitudinal, lateral and vertical.

What are the three primary flight controls of an aircraft

ailerons , elevator and rudder

Name several secondary flight controls and describe their general purpose

balance tabs, anti-servo tabs, and spring tabs. their function is move the controls and trim the aircraft

Name several types of auxiliary flight controls and describe their general purpose

Leading and trailing edges flaps, slats slots are use as high-lift device at low speed

What is a servo trim tab

it is an auxiliary control designed to create aerodynamic force to assist in moving the control surfaces

What is a spring tab

it is an auxiliary control designed to move primary control at high-speed

What is a balance trim tab

it is an auxiliary control designed to create aerodynamic force to move control surface

What are the four most common types of high lift devices

leading and trailing edge flap ,slat and slots

Describe some of the tools used to check control surface travel

universal propeller protractor, special control surface protractor

Name three mechanical methods by which flight control systems may be actuated

cables, push-pull rod, and torque tube

What is a fairlead

it is a device to prevent cable from rubbing on the aircraft structure

What are the most likely places for a control cable to wear or break

over pulleys or trough fairlead

What information is required before a cable rigging chart can be used

the ambient temperature and size of the cable

What is the function of a cable tension regulator

It automatically adjust the cable tension to compensate for expansion and contraction in the aircraft structure

Describe the function of a rotorcraft collective pitch control

to change it is pitch angle by the same amount thus increasing or decreasing the lift produce by the rotor

Describe the function of a rotorcraft cyclic pitch control

to tilt the main rotor disc by changing the pitch angle of each rotor blade during cycle of rotation

What mechanism is most commonly used to compensate for the torque produced by the main rotor of a helicopter

the tail rotor

19.How is the amount of thrust produced by the tail rotor controlled

by moving the foot pedals

Why should control surfaces be locked when an aircraft is parked

to prevent damage from the wind