121 Flashcards

1
Q
  • are used to assist or to modify the effect of the primary flight
    controls.
A

Secondary Flight Controls

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2
Q

secondary flight controls includes

A

Flaps
Spoilers
Slats
Tabs

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3
Q

are most widely used method for modifying lift.

A

Flaps

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4
Q

Most —– are on the trailing edge of the wing inboard of the ailerons,
but some are located on the wings leading edge.

A

Flaps

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4
Q

are hinged surfaces located ahead of the flaps.

A

Spoilers

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5
Q

if the flap is increased the drag is increased also in the slats

A

true

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5
Q

Making your wings more versatile

A

Flaps

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6
Q

types of flaps

A

Plain flaps
split flaps
slotted flaps
fowler flaps
triple slotted flaps
leading edge flaps
kruger flaps

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6
Q

A higher
coefficient of lift is produced as a result of angle of attack
and speed, so by deploying ——– an aircraft can fly at slower
speeds, or take off and land in shorter distances.

A

Slats

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6
Q

They are used in conjunction with the
ailerons to assist in roll control.

A

Spoilers

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6
Q

are aerodynamic surfaces on the leading edge of the wings
of fixed-wing aircraft which, when deployed, allow the
wing to operate at a higher angle of attack.

A

Slats

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7
Q

small auxiliary devices on the trailing edge of various
primary control surfaces

A

Tabs

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7
Q

are
used to produce aerodynamic forces to trim the aircraft or
to aid the pilot in moving the controls.

A

Tabs

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7
Q

Control Yaw

A

Vertical Stabilizer

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8
Q

Change Pitch
(Up-Down)

A

Elevatror

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8
Q

Change Yaw
(Side-to-Side)

9
Q

Change Roll
(Rotate Body)

9
Q

Change Lift and Drag

10
Q

Change Lift and Drag
(Rotate Body)

11
Q

Change Lift

12
Q

Hold Things Together (Carry Payload - Fuel)

13
Q

Generate Thrust

A

Jet Engine

13
Q

Command and Control

14
Q

Generate Lift

15
Q

Control Pitch

A

Horizontal Stabilizer