Untitled Deck Flashcards

(37 cards)

1
Q

Why is having good systems knowledge essential for pilots?

A

To troubleshoot effectively in the event of a system malfunction or failure. The stakes are high when things break in an aircraft.

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2
Q

What are your aircraft’s primary flight controls?

A
  • Ailerons
  • Rudder
  • Elevator
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3
Q

What are your aircraft’s secondary flight controls?

A
  • Flaps
  • Trim
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4
Q

How are the yoke and rudder pedals linked to their associated flight control surfaces?

A

Through cables, pulleys, bellcranks, and pushrods.

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5
Q

When you turn the yoke to the left, which direction does each aileron move?

A
  • Left aileron up
  • Right aileron down
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6
Q

Aerodynamically, how does rolling the plane to the left occur?

A

The right aileron drops, increasing its wing’s camber and airflow speed, increasing lift, while the left aileron goes up, decreasing camber and lift.

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7
Q

Around what axis does the aircraft roll?

A

Longitudinal.

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8
Q

What type of ailerons does your plane have?

A

Differential and frise.

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9
Q

What is the purpose of differential ailerons?

A

To counteract adverse yaw.

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10
Q

How do differential ailerons counteract adverse yaw?

A

The left aileron sticks up higher than the right’s downward deflection, creating additional drag to help yaw in the direction of the turn.

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11
Q

What is the frise feature of the ailerons?

A

It allows airflow beneath the wing to join and re-energize airflow on the top surface of the aileron, increasing its effectiveness.

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12
Q

What type of horizontal tail surface does your plane have?

A

Elevator (attached to the back of the fixed horizontal stabilizer).

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13
Q

How is a stabilator different from an elevator?

A

A stabilator is a single slab that pivots from a central hinge point.

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14
Q

When you pull the yoke back, which direction does the trailing edge of the elevator deflect?

A

Up.

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15
Q

Aerodynamically, how does the elevator cause the plane to pitch up?

A

The upward deflection pushes the tail down and raises the nose. It also increases camber on the bottom of the horizontal tail surface.

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16
Q

Around what axis does the aircraft pitch?

17
Q

When you step on the left rudder pedal, which direction does the trailing edge of the rudder deflect?

18
Q

What effect does the left deflection of the rudder have on the plane’s orientation?

A

The plane yaws to the left.

19
Q

What primary function does the rudder serve?

A

To counteract adverse yaw and unwanted yaw tendencies.

20
Q

What other functions does the rudder serve?

A
  • Create more parasite drag during forward slips
  • Maintain longitudinal alignment during crosswind landings
  • Help maintain directional control after engine failures
  • Turn the aircraft if ailerons malfunction
21
Q

Around what axis does the rudder cause the plane to yaw?

22
Q

What is the purpose of balance weights on primary flight controls?

A

To decrease control surface flutter at higher airspeeds and reduce pilot control forces.

23
Q

At slow airspeeds, would you expect your flight controls to be more or less effective?

A

Less effective due to reduced airflow over the control surfaces.

24
Q

What effect will trimming the plane nose down have on the trim tab?

A

The trailing edge of the trim tab will deflect upward.

25
How does an upward trim tab help maintain a nose-down pitch attitude?
The airflow over the horizontal tail surface tends to force the trailing edge of the elevator down.
26
What is the primary purpose of trim?
To relieve control pressure.
27
Does the 172 have a servo or anti-servo trim tab?
Servo.
28
What is the difference between a servo and anti-servo trim tab?
Servo tabs deflect in the opposite direction of the elevator's movement to increase control sensitivity; anti-servo tabs decrease control sensitivity.
29
Does the rudder have trim?
Yes, it has a ground-adjustable trim tab.
30
Can pilots adjust the rudder trim?
Yes, pilots can adjust it, but maintenance typically handles adjustments.
31
What kind of flaps does the aircraft have?
Electrically operated, single-slot type flaps.
32
Where is the flaps motor located?
In the right wing, a couple of feet outboard of the cabin.
33
What are some purposes of flaps?
* Produce more lift for lower landing speed * Produce greater drag for steeper descent angle * Reduce the length of the landing roll
34
Which flap settings primarily produce lift and which increase drag?
The first 1-15 degrees of flaps primarily produce lift; beyond 15 degrees generates large increases in drag.
35
How does the slot in the slotted flap aid in producing lift?
* Ducts high energy air to the flap's upper surface * Accelerates the upper surface boundary layer * Delays airflow separation
36
What is the bent metal in the aircraft's control surfaces called?
Corrugation.
37
Why is the metal in the control surfaces designed with corrugation?
It increases the structural strength of the metal.