7.16 Aircraft Weight and Balance Flashcards

1
Q

What Alter the position of CG?

A

Passengers , fuel , cargo and equipment

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2
Q

What will incorrect loading affect?

A

the aircraft rate of climb , maneuverability , ceiling , speed and fuel

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3
Q

If CG were too far forward what will happen?

A

It would result in a nose-heavy condition

which could be potentially dangerous on take-off and landing

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4
Q

If CG were too far aft what will happen?

A

It would result in the tail-heavy condition which will increase the tendency of the aircraft to stall and make landing more difficult

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5
Q

The unit of measurement for mass and balance are normally dictated by who?

A

The aircraft Manufacturer and can be either Metric or Imperial terms

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6
Q

What is the mathod of calculating the CG position based on?

A

The principle of Turning Moments

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7
Q

Principle of Turning Moments

A

The moment of a force about a point is the product of the force and the perpendicular distance from the point to the line of action of the force.

Are expressed in lbs , Ft , Nm

Must be specified; Clockwise(+) anti-Clockwise(-) positive or negative

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8
Q

describe a Datum?

A

Is an imaginary vertical plane from which horizontal measurments are taken

no fixed rule

the manufacturer will normally specify the nose of the aircraft

could be at the front main bulkhead or even forward of the aircraft nose

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9
Q

descrive an Arm?

A

The horizontal distance from an item or piece of equipment to the datum

usually measured in inches or millimeters

may preceded by a (+) aft of the datum
                         or a (-) fwd of the datum
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10
Q

describe Moment?

A

The product of a force multiplied by the distance about which the force acts

in case of mass and balance
the force is the mass kg/lb and the distance is the arm m/in

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11
Q

describe CG?

A

The point about which all of the mass of the aircraft or object is concentrated

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12
Q

describe CG limits?

A

normal operation: the CG should be between the Forward and Aft limits as specified by the manufacturer

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13
Q

describe Dry Operating Mass?

A

the total mass of the aeroplane , ready for a specific type of operation , excluding all usable fuel and traffic load

includes crew and crew baggage , catring and removable passenger service equipment , portable water and lavatory chemicals

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14
Q

descibe Maximum Zero Fuel Mass?

A

the maximum permissible mass of an aircraft with no usable fuel

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15
Q

describe Maximum Structural Take-Off Mass (MTOM)?

A

the maximum permissible total aeroplane mass at the start of the take-off run

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16
Q

describe Maximum Structural Landing Mass?

A

the maximum permissible total aeroplane mass upon landing under normal circumstances

17
Q

describe Traffic Load?

A

Includes the total mass of passengers , baggage and cargo , including any none-revenue load

18
Q

describe Basic Equipment?

A

Is the inconsumable fluids such as coolant , hydraulic fluids , and equipments which are common to all roles for which the operator intends to use the aeroplane

19
Q

describe Basic Weight?

A

Is the weight of the aircraft and all its basic equipment and that of the declared quantity of unusable fuel and unusable oil

tubine engine : not exceeding 12500 lb 5700 kg it may also include the weight of usable oil

20
Q

What is the Main Purpose of monitoring the mass and balance of aircraft?

A

To maintain safety

and achieve efficiency in flight