Flight control balancing Flashcards

1
Q

Unbalanced control surfaces lead to what?

A

-Control surface fluttering
-Fatigue cracking of mounting structure
-Loss of the control surface itself or the whole wing/stabilizer structure

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2
Q

When should flight control limits be checked? List at least 3 reasons

A

-After paintings
-After repairs
-Loss of balance weight

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3
Q

Different aircraft configurations may have different control surface limits. T/F?

A

True

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4
Q

The moment of a flight control should be checked if it is being __________. Even if its being exchanged with a flight control from same type aircraft

A

Should be checked if it is being replaced

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5
Q

What is a hinge line?

A

A line that extends through the pivot point of the surface hinge

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6
Q

What is a balancing fixture?

A

A device that supports the control surface while allowing it to pivot around the hinge line

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7
Q

Overbalance is when the center of mass is what?

A

When the center of mass is ahead of the of the hinge line

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8
Q

Underbalance is when the center of mass is what?

A

When the center of mass is behind of the hinge line

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9
Q

Moment is defined as the measure of torque that does what?

A

Measure of torque that the control imbalance puts on the control surface

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10
Q

What is balance weight?

A

Material that is added to the front of the hinge line to bring the surface moment into limits

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11
Q

What is positive and negative stability?

A

Positive stability is defined as the tendency to return to equilibrium while negative stability is the tendency to continue in the displacement direction

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12
Q

What is meant by AERODYNAMIC BALANCE?

A

The surface area AHEAD of the hinge line to assist in pilot control

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13
Q

What is the formula for calculating moment?

A

(Xoz/ 16oz/lb) x distance between hinge line and trailing edge

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14
Q

Some manufactures refer to
overbalance as negative (-) moment, and others positive (+) moment. T/F?

A

True

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15
Q

Generally speaking, there are three methods of balancing, what are they?

A

Scale method
Trial weight method
Component method

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16
Q

Describe the scale method:

A

This method revolves around the use of a scale to weigh the amount of imbalance in level attitude

17
Q

Describe the trial method:

A

This one involves adding weight to either the leading or trailing edge of the control surface depending whether it is over balanced or underbalanced

18
Q

Describe the component method:

A

The use of a balance beam on a control surface in which a weight is added to the beam and slid around until the surface is balanced

19
Q

Most flight controls require weight in front of the hinge line to properly balance the surface. These are called what?

A

Counterweights

20
Q

Counterweights need to be very heavy and often have limited space to occupy. Hence, are often made from what?

A

Heavy high density material such as steel. depleted uranium, tungsten, lead. etc

21
Q

Control surfaces balance moments MUST fall within the manufacturer specifications to be considered airworthy. And if they don’t you can resolve these issues by doing what?

A

Adding counterweights (usually ahead of the hinge line
Removing counterweights (if the said surface is overbalanced

22
Q

Do control tabs need to be balanced?

A

Yes, some may require counterweights to prevent flutter

23
Q

When are ICCs required and what are the 4 main checks that are required?

A

Required after maintenance is performed that may have disturbed the flight controls. There must be a check for Correct assembly, safety devices, correct sense and range of travel