Aircraft weight and balance concepts Flashcards

1
Q

Since weight and balance directly affects the efficiency and safety of an aircraft, a ____________weight and balance control system is used which allows the SMA to check weight limits before takeoff

A

standardized

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2
Q

In addition to checking weight, it is necessary to know that the aircraft is ____________ within the limits established by the manufacturer.

A

balanced

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3
Q

The _____________ _______of an aircraft can be determined by locating its center of gravity (CG)

A

balance point

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4
Q

An imaginary point where the aircraft would balance if freely suspended in air

A

center of gravity (CG)

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5
Q

The CG limits specify the __________ and ______ center of gravity locations within which an aircraft can safely operate.

A

forward

aft

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6
Q

The center of gravity and CG limits are usually specified in ___________ from a reference line in front of the aircraft.

A

inches

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7
Q

The reference point that represents an imaginary vertical plane from which all horizontal distances are measured, in inches, for balance purposes is called the _________ _______ _______ (______) .

A

Reference Datum Line (RDL)

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8
Q

The Reference Datum Line (RDL) is normally the first line drawn on the ________ ___________ and it is placed forward of the aircraft nose to ensure that all measurements used in the weight and balance computations are positive.

A

design sketches

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9
Q

The RDL for instructional purposes in this course is located ____ inches forward of the aircraft nose

A

30

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10
Q

The horizontal distance in inches from the reference datum line to the center of gravity for any object on the aircraft

A

arm

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11
Q

The weight of an item in pounds multiplied by the arm in inches. It is the torque the aircraft weight would produce relative to the reference datum line.

A

moment

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12
Q

The measurement unit for the moment is the:

A

inch-pound

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13
Q

Weight is a __________ which means it is a unit that has magnitude and direction

A

vector

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14
Q

The mass (magnitude) of an object multiplied by the value of gravity.

A

weight

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15
Q

Since gravity affects all the objects on an aircraft in the same way, weight is ____________ to an object’s mass which is measured in pounds.

A

proportional

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16
Q

An objects mass is measured in

A

pounds

17
Q

Represents an imaginary vertical plane from which all horizontal distances are measured, in inches, for balance purposes

A

Reference Datum Line (RDL)

18
Q

The reference datum line (RDL) is placed forward of the aircraft nose to ensure that all measurements used in the weight and balance computations are _________

A

positive

19
Q

Aircraft diagrams show the reference datum line as ___________ __________ _________

A

fuselage station zero

20
Q

A vertical plane, parallel to the RDL, identified by a number equal to its distance from the RDL, which identifies particular points in the airplane by telling you how far you are from the RDL

A

fuselage station

21
Q

The balance point of of an aircraft, or aircraft center of gravity arm (CGA), is found by dividing the _________ __________ (____) by the __________ __________ (_____) of the aircraft

A
total moment (TM)
total weight (TW)
22
Q

The result, or balance point of an aircraft, found by dividing the total moment (TM) by the total weight (TW) of the aircraft.

A

Aircraft Center of Gravity Arm (CGA) or Average Arm

23
Q

The distance in inches from the RDL to the center of gravity of the aircraft

A

Aircraft Center of Gravity Arm (CGA)

24
Q

The aircraft center of gravity arm (CGA) in an important part in planning the balance of the aircraft and needs to be more precise than the cargo numbers, for this reason it is rounded to __________________

A

the tenth of an inch

25
Q

The sum of the moments of all items making up the basic weight of the aircraft and recorded on DD form 365-3 (Chart C)

A

Basic Moment

26
Q

The weight of the aircraft as it is equipped to fly before adding crew, fuel and other items available to load. It may vary due to equipment and structural changes, and it is recorded on the DD form 365-3 (Chart C)

A

Basic Weight

27
Q

The average arm or CG of a compartment, fuel tank, piece of equipment, cargo, etc.

A

Centroid