Primary Flight Controls Flashcards

1
Q

5 Types of Primary Flight Controls

A

Elevator- Pitch about the lateral Axis
Rudder- Yaw about the vertical Axis
Ailerons- Roll about the longitudinal axis
Roll Control Spoilers- Roll about the longitudinal axis
Flaperons- Roll about the longitudinal axis

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2
Q

What is a primary flight control

A

Primary control rotate an aircraft about its three axis- Creates a change in Flight Path or attitude

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3
Q

control in pitch is controlled by

A

Rearward movement of the control column causing upward movement of the elevator causing it to pitch up

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4
Q

Control in roll

A

Achieved by the ailerons or the roll control spoilers. Turning the wheel to the right causes the right aileron to move up and left to move down, therefore the aircraft rolls to the right

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5
Q

Control In Yaw

A

Rudder- Moving the right rudder pedal forward

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6
Q

Manual Flight Controls

A

Reversible as the pilot can feel the load on the control surface

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7
Q

Fully powered Controls

A

Hydraulically or electrically- Not reversible as the pilot cannot feel the loading on the control surface. A form of artificial feel will be required

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8
Q

Partially powered control

A

Hydraulic or electric- These are reversible as the pilot can feel the loading surface

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9
Q

Manual control System Explanation

A

A manual Control System consists of a series of cables, push rods and chains that connect the pilots control column or yoke to the control surface

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10
Q

What is a turnbuckle (Manual Flight Control)

A

It is important to have the correct tension in the control cables. if the tension is too low the cable will be loose, if the tension is too high the controls will be too stiff to move Cable tension is adjusted by means of turnbuckles.

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11
Q

Temperature compensator (Manual Flight Control)

A

Maintains the correct temp if pressure is changes

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12
Q

Pulley (Manual Flight Control)

A

Facilitates a change in direction for the cables

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13
Q

Fairleads (Manual Flight Control)

A

Provide a guide for control to pass through frames or bulkheads preventing damage to cable/ control rod due to chaffing against the aircraft structure

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14
Q

Primary & Secondary Control Stops (Manual Flight Control)

A

Fitted to limit the range of movement of the control surfaces

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15
Q

Control Locks (Manual Flight Control)

A

Prevent damage to control surfaces in the event of high wind

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