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Aircraft Weight and Balance Quiz

Total questions: 20

Worksheet time: 10mins

Name
Class
Date
1.

Who is responsible for documenting weight changes after an aircraft repair or alteration?

a)

The aircraft owner

b)

The aircraft manufacturer

c)

The FAA-certificated mechanic or repairman

d)

The pilot

2.

What does the suffix '-R' indicate in the equipment list?

a)

Optional equipment item

b)

Standard equipment item

c)

Required item or equipment for FAA certification

d)

Additional equipment item

3.

What must be completed to describe a major repair or alteration?

a)

A verbal report to the FAA

b)

A Repair Station record and/or FAA form 337

c)

A maintenance log entry

d)

A pilot's logbook entry

4.

What is the first step in weight and balance computation?

a)

Check the fuel load

b)

Make a chart listing all involved items

c)

Determine the new CG

d)

Calculate the moment index

5.

What is the loaded CG after alteration or repair in percent MAC?

a)

10.42 percent MAC

b)

25.98 percent MAC

c)

17.9 percent MAC

d)

36.4 percent MAC

6.

What does a positive arm indicate in weight and balance calculations?

a)

Weight of the equipment

b)

Distance aft of the datum

c)

Distance forward of the datum

d)

Moment index

7.

What must be done if the TCDS lists the EWCG range as 'None'?

a)

No further checks are needed

b)

A fore and aft check for adverse loading must be made

c)

The aircraft must be grounded

d)

The pilot must be notified

8.

What is the purpose of adverse-load CG checks?

a)

To determine the maximum payload

b)

To calculate fuel efficiency

c)

To verify no legal loading condition moves the CG outside allowable limits

d)

To ensure the aircraft is within weight limits

9.

What is indicated by an asterisk (*) in the weight and arm column?

a)

A standard item

b)

A required item

c)

A complete assembly installation

d)

An optional item

10.

What is the significance of the leading edge mean aerodynamic chord (LEMAC) in CG calculations?

a)

It determines the aircraft's speed

b)

It is used to calculate the CG in percent MAC

c)

It indicates the fuel capacity

d)

It shows the maximum payload

11.

What are the first steps performing a weight and balance check

a)
Inspect the exterior for damage.
b)

refuel to full levels and check tire pressure.

c)
Gather documentation and measure current weight and center of gravity.
d)
Review the flight plan and weather conditions.
12.

What are the first steps performing a weight and balance check

a)

Wash the aircraft

b)
Review the flight plan and weather conditions.
c)
Inspect the engine and perform a systems check.
d)

Remove all wing panels before jacking

13.

What is the purpose of a moment index in weight and balance calculations?

a)

To determine the aircraft's speed

b)

To calculate the center of gravity

c)

To measure fuel efficiency

d)

To assess the structural integrity

14.

What does the term 'datum' refer to in aircraft weight and balance?

a)

The point from which all horizontal distances are measured for balance purposes

b)

The maximum allowable weight of the aircraft

c)

The standard fuel capacity

d)

The location of the main landing gear

15.

How is the center of gravity (CG) location expressed in aircraft weight and balance?

a)

In terms of fuel consumption

b)

As a percentage of the mean aerodynamic chord (MAC)

c)

In pounds per square inch

d)

As a ratio of wing span

16.

What is the effect of a forward CG on aircraft performance?

a)

Increased fuel efficiency

b)

Decreased stall speed

c)

Increased stability but decreased performance

d)

Decreased stability and increased performance

17.

How does a change in the aircraft's weight affect the CG location?

a)

It has no effect on the CG location

b)

It shifts the CG forward

c)

It shifts the CG aft

d)

It can shift the CG either forward or aft

18.

What is the primary purpose of a weight and balance report?

a)

To ensure the aircraft's speed is optimal

b)

To verify the aircraft's structural integrity

c)

To confirm the aircraft is within safe operational limits

d)

To calculate the aircraft's fuel consumption

19.

________ causes the front wheels to have increased traction, allowing them to control directional control on wet snowy runways

Select one:

a)

Energy transformation

b)

Weight transfer

c)

Rotational force

d)

None of the above

20.

What subject dose this FAR cover FAA-H8083-1A

a)

Corrosion Control Handbook

b)

Jacking and Shoring

c)

Aircraft Weight and balance

d)

Aircraft Weight and balance adverse load checks