BASIC TERMINOLOGIES And WEIGHT N BALANCE Flashcards

1
Q

An imaginary point where aircrafts weight is concentrated.

A

Center of Gravity (CG)

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2
Q

An imaginary vertical plane from which all horizontal distances are
measured.

A

Reference Datum

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3
Q

It includes the weight of the standard airplane, optional equipment,
unusable fuel, including all operational fluids including full engine oil.

A

Basic empty weight

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4
Q

It is the small amount of fuel in the tanks that cannot be used inflight and
fuel drained on the ground.

A

Unusable fuel

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5
Q

The weight of an aircraft before takeoff.

A

Ramp weight

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6
Q

The ramp weight less the fuel burned during engine start, run up and taxi.

A

Takeoff weight

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7
Q

The takeoff weight less the fuel burned en-route.

A

Landing weight

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8
Q

The weight of usable fuel, flight crew, passengers and baggage.

A

Useful load

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9
Q

The weight of passengers, baggage and cargo.

A

Payload

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10
Q

The maximum weight allowed for ground operation.

A

Maximum ramp weight

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11
Q

The maximum weight before takeoff.

A

Maximum takeoff weight

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12
Q

The maximum weight before landing.

A

Maximum landing weight

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13
Q

The fuel available in flight.

A

Usable fuel

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14
Q

The Distance from reference datum.

A

Arm

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15
Q

The measurement of the tendency of the weight to cause rotation of fulcrum.
Length multiplied by weight.

A

Moment

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16
Q

It is the force generated by the gravitational pull
of the earth on the total load of the aircraft.

A

Weight

17
Q

Disadvantages of an overweight aircraft

A

■ Longer Takeoff and Landing Roll
■ Higher Takeoff Speed
■ Poor Climb Performance
■ Lower Cruising Level
■ Reduced Cruising Speed
■ Less Maneuverability
■ Reduced Range and Endurance
■ Higher Stalling Speed

18
Q

One (1) Gallon of AVGAS: __ lbs

A

6 lbs

19
Q

One (1) Gallon of oil: __ lbs

A

7.5 lbs

20
Q

A point at which the entire weight of the aircraft is
assumed to be concentrated, and where the
counterclockwise turning moments are balanced
by the clockwise turning moments.

A

CENTER OF GRAVITY (CG)

21
Q

A point at which an airplane would balance if
suspended.

A

CENTER OF GRAVITY (CG)

22
Q

Effects of CG Too far forward

A

■ Lack of elevator authority (specially during flare)
■ Higher angle of attack
■ Drag will increase

23
Q

Effects of CG to far after

A

■ Unstable airplane
■ Very difficult to recover from a stall

24
Q

Distance from the datum

A

Arm

25
Q

Is the measurement of the tendency of the weight
to cause rotation of the fulcrum.

A

MOMENT