General: Weight & Balance πŸ”Š Flashcards

1
Q

What is the datum and its purpose when making weight and balance computations?

A

It is an imaginary vertical line or plane from which all measurements are taken both forward and after to determine the relative location of items in the aircraft

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2
Q

What items concerning weight and balance can be found in the type certificate data sheet?

A

Datum, CG limits, unusable fuel and oil, baggage capacity, seat locations, fuel capacity, leveling means, engine horsepower, weight maximum *DCUBS FLEW

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3
Q

What is the purpose of weight and balance control?

A

Safety and efficiency in flight

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4
Q

When computing weight and balance, what is the moment and how is it obtained?

A

Moment is a force which tends to rotate the aircraft about one of its axes. It’s obtained by multiplying the weight of an item in pounds by the distance of the item from the datum. It is expressed in inch pounds

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5
Q

How would a negative moment be obtained forward of the datum?

A

By adding weight

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6
Q

What is the arm of an item and how is it obtained?

A

It’s the distance in inches and item is located either forward or after the datum, it’s obtained by actually measuring or from weight and balance records

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7
Q

What is tare weight and how is it handled when making weight and balance calculations?

A

Tare is the weight of extra equipment used for weighing aircraft such as chalks, jacks and chains. It must be subtracted from the scale readings in order to obtain the empty way of the aircraft.

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8
Q

What is meant by minimum fuel and how is a calculated for weight and balance?

A

Amount of fuel needed for an extreme condition check to see if the center of gravity will be out of limits in that situation. For reciprocating engine airplanes, the calculation is maximum except takeoff horsepower divided by two. METOΓ·2

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9
Q

What is meant by residual fuel?

A

Fuel remaining in the tanks, sumps, lines, and engine after fuel exhaustion also known as unusable. It is part of the aircraft empty weight

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10
Q

What is meant by center of gravity range?

A

Distance in inches from the most forward acceptable center of gravity to the most rearward

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11
Q

What is an aircraft loading graph?

A

A method for determining load distribution so the aircraft remains with an operating CG

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12
Q

How would you determine the empty weight and empty weight CG of an aircraft if all weight and balance records are missing?

A

Re-weigh the aircraft and calculate new weight and balance records

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13
Q

What is the difference between fixed wing and rotary wing aircraft CG ranges?

A

CG location and helicopters are much more critical than fixing aircraft, some helicopters CG range will be less than 3 inches

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14
Q

When weighing an aircraft to determine the empty weight CG, what must you do regarding the fixed equipment which is normally carried in the aircraft?

A

All operational equipment must be included in the aircraft’s empty weight.

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15
Q

Why do some manufacturers specify an empty CG even though the aircraft is not operated at this empty weight?

A

When the empty weight CG falls within the empty weight CG range, it’s unnecessary to perform a weight and balance check if standard loading and seating arrangements are used

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16
Q

Why must the aircraft category be considered when computing weight and balance?

A

Some aircraft are certified in both normal and utility categories, meaning a different maximum allowable gross weight depending on which category the aircraft will be operating in that day

17
Q

Where is the center of gravity located in relation to the aerodynamic center of lift for most airplanes?

A

In front of the center of lift

18
Q

What are two common ways of representing the CG of an aircraft?

A

Inches from the datum or percent of mean aerodynamic chord (% of MAC)

19
Q

Is there a federal regulation that requires the regular re-weighing of private aircraft?

A

No

20
Q

Where must a record of the most recent empty weight and center of gravity be kept?

A

It should be maintained in the aircraft, flight manual or weight and balance records (FAR 23.1583)

21
Q

What should be done regarding aircraft fuel when performing a weight and balance when draining is not an option?

A

When weighing with full fuel tanks, the exact weight per gallon should be verified with a hydrometer. The weight of usable fuel must be mathematically subtracted in the weight and balance calculations.

22
Q

How should aircraft fuel be drained for weight and balance?

A

Level the aircraft per the TCDS then drain the fuel supply until empty, only leaving the unusable fuel in the system

23
Q

What is ballast?

A

It can be lead bars, metal plates, shot bags, sandbags, or other items of weight which are placed in the aircraft to attain a desired CG location.

24
Q

If the forward CG limit of an aircraft is exceeded after installing several items in the engine compartment, how could the limit be returned to limits without removing or changing any of the newly installed equipment?

A

By adding a ballast weight in the rear of the aircraft

25
Q

What are the placard requirements for ballast?

A

Ballast location must have a placard stating any limitations on contents that are necessary under the loading requirements

26
Q

What is recommended for marking a permanent ballast?

A

In red paint mark β€œpermanent ballast do not remove”

27
Q

How should an aircraft be leveled for weighing during a weight and balance?

A

Leveled per the requirements of the aircraft specification or type certificate data sheet

28
Q

Name one common method of leveling an aircraft during weight and balance.

A

You may use a built-in leveling scale and a plum bob

29
Q

Describe a plumb bob and its use.

A

It’s a heavy object in the shape of a cone that is used to determine a spot directly below the point the tool is hanging from

30
Q

How can you determine if a part will affect the CG without weighing the aircraft?

A

By basic weight and balance computations if weight imbalance records are up to date.