Assembaly And Rigging Flashcards

1
Q

What are the three axes of an airplane

A

Longitudinal ( roll ) extends through the fuselage from nose to tail , lateral ( pitch ) extends crosswise from wingtip to wingtip, and vertical ( yaw ) passes through the center from top to bottom

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2
Q

What are the primary flight controls of an aircraft

A

Ailerons is roll axis ,elevator is pitch axis , and rudder is yaw

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3
Q

Name several secondary flight controls

A

Trim tab, balance tabs, anti-servo, servo tabs, wing flaps and spring tabs. They help the pilot in moving the controls with flying hands free

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4
Q

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

A

The auxiliary flight controls consist of the various high-lift devices used during low-speed flight such as leading and trailing edge flaps, slats, slots, spoilers, and speed brakes

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5
Q

What is a servo tab

A

A cockpit controlled adjustable tab attached to the trailing edge of a primary control surface. The tab moves opposite the direction of the control surface producing an aerodynamic force that moves the primary

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6
Q

What is a spring tab

A

It is an auxiliary control designed to help move the primary control at high speeds when forces become too high

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7
Q

What is a balance trim tab

A

It is an auxiliary control designed to create aerodynamic forces to assist in moving a control surface.

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8
Q

What are for most common types of high lift devices

A

Leading and trailing edge flaps, slats and slots

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9
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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10
Q

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

A

Cables, push-pull rods, and torque tools

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11
Q

What is a fairlead

A

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

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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 information is required before a cable rigging chart can be used

A

The ambient temperature and the cable size

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14
Q

What is the function of a cable tension regulator

A

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

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15
Q

Describe the function of a rotorcraft collective pitch control

A

Used to change the pitch of the main rotor blades therefore increases or decreases lift

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16
Q

Describe the function of a rotorcraft cyclic pitch control

A

The cyclic control tilts the main rotor disc by changing the pitch angle of each rotor blade during its cycle of rotation which causes the helicopter to move in the direction the rotor tilts

17
Q

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

A

The tail rotor

18
Q

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

A

By moving the foot pedal

19
Q

Why should control surfaces be locked when an aircraft is parked

A

To prevent damage from the wind

20
Q

What is the function of a vortex generator

A

Prevents separation from the surface of the wing

21
Q

What is the function of the ailerons on an airplane

A

Ailerons rotate the airplane about its longitudinal axis

22
Q

What is the function of a rudder

A

Rotates the airplane about its vertical axis

23
Q

How much is a fairlead allowed to deflect a control cable

A

3 degrees

24
Q

What are vortex generators

A

Small airfoils mounted on the upper surface of the wings. Designed to prevent airflow from separating from the upper surface of the wing

25
Q

What factor are used to determine the proper tension cable

A

Size of cable and outside temperature

26
Q

What reference publication should be used to rig aircraft included the control system

A

Refer to aircraft specifications, TCDS issued by FAA, and also the maintenance manual issued by manufacture