Aircraft Structural Assembly and Rigging Flashcards

1
Q

What is the function of a Vortex Generator?

A

Designed to delay or prevent the separation of the boundary layer.

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2
Q

What are the 3 axes of an airplane?

A

Longitudinal, Lateral, and Vertical

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3
Q

What are the three primary flight controls of an aircraft?

A

Elevator, Aileron and Rudder

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4
Q

What are the secondary flight controls? Describe their general purpose.

A

Various high lift devices used during low speed flight. Leading and trailing edge flaps, slats, slots, and speed brakes.

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5
Q

Name several types of Auxiliary Flight controls and describe their purpose.

A

Various types of trim tabs, such as balance tabs, anti servo tabs, and servo tabs. Their function is to assist the pilot in moving the flight controls and to trim the aircraft to fly hands off.

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6
Q

What is a servo trim tab?

A

An auxiliary control positioned by the movement of a cockpit control, designed to create aerodynamic forces to assist the pilot in moving the control surface.

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7
Q

What is a spring tab?

A

It is an auxiliary control designed to aid in movement of a primary control at high speeds when control forces become too high.

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8
Q

What is a balance tab?

A

It is an auxiliary control designed to create aerodynamic forces to assist in moving a control surface. The tab is positioned by a control rod connected to the fixed surface on the same side as the horn on the tab.

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9
Q

What are the four most common high lift devices?

A

Leading and trailing edge flaps, slats, and slots.

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10
Q

Describe some of the tools used to check control surface travel.

A

A universal propeller protractor or special control surface protractor.

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11
Q

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

A

Cables, push-pull rods, and torque tubes.

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12
Q

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

A

Where the cables pass over pulleys or through fairleads.

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13
Q

What is a fairlead?

A

A device to prevent a cable from rubbing on the aircraft structure.

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14
Q

What information is required before a cable rigging chat can be used?

A

The ambient temperature and the cable size.

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15
Q

What is the function of a cable tension regulator?

A

To automatically adjusts the cable tension to compensate for expansion and contraction of the aircraft structure.

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16
Q

Describe the function of a rotorcraft collective pitch control.

A

The collective control causes each rotor blade to change its pitch angle by the same amount, thus increase or decreasing the lift produces by the rotor.

17
Q

Describe the function of a rotorcraft cyclic pitch control.

A

Tilts the main rotor disc by changing the pitch angles of each rotor blade during its cycle of rotation, which causes the helicopter to move in the direction the rotor tilts.

18
Q

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

A

The tail / anti-torque rotor

19
Q

How is the amount of thrust produced by the tail rotor controlled?

A

By actuating the foot pedals.

20
Q

Why should control surface be locked when an aircraft is parked?

A

To prevent damage from the wind.