MOD 14 WEIGHT AND BALANCE Flashcards

1
Q

Aircraft performance how is affected by weight:

A
More weight = longer take-off
More weight = lower climb rate
More weight = slower cruise 
More weight = longer landing
More weight = More stress and strain on aircraft!
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2
Q

Large aircraft must be reweighed every _____ years

A

5 years -CARS 625 Appendix C

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3
Q

when Small aircraft are re-weighed ?

A

only if it affects weight and Centre of Gravity position

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4
Q

Who is responsible for the accuracy of the aircraft’s weight and balance?

A

CARS 724.32
“the air operator will establish and be responsible for the accuracy of the aeroplane basic empty weight and centre of gravity…”

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5
Q

what is Basic empty weight

A

Weight of aircraft with optional or special equipment
Fixed ballast
Unusable fuel
Full operating fluids

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6
Q

what is Max. Take off Weight

A

Maximum approved weight for the start of the takeoff roll.

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7
Q

what is Max. Landing Weight

A

Maximum allowable weight at which an aircraft can be landed.

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8
Q

what is Useful load

A

Difference between Max. take off weight and basic empty weight

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9
Q

what is Equipment List

A

A list of equipment that does not form part of the aircraft type design

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10
Q

When is a weight and balance amendment required?

A

As per CARS 571 Appendix C “ following a modification or a major repair that involves a change to the empty weight or centre of gravity of an aircraft…”

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11
Q

what is Fulcrum or datum

A
  • Vertical plane from which all horizontal measurement are taken with the aircraft in a level flight attitude.
  • Sits perpendicular to the longitudinal axis
  • Location varies with aircraft
  • Forward of datum is regarded as a negative number
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12
Q

Datum information can be located in the

A
  • AMM (Aircraft maintenance Manual)
  • POH (Pilot’s operating handbook)
  • Type Certificate Data Sheet
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13
Q

what is Centre of Gravity

A
  • Point along an aircraft’s longitudinal axis which the weight is considered to be concentrated
  • Nose-heavy and tail-heavy moments are exactly equal in magnitude
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14
Q

Centre of Gravity – Out of Limits what happens when CG is too far forward ?

A
  • Nose heavy
  • Longer takeoff distance
  • Higher stalling speeds
  • Extreme nose heavy the elevator or Stabilator will be insufficient to lift the nose.
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15
Q

Centre of Gravity – Out of Limits what happens when CG is too far Aft ?

A
  • Tail heavy
  • Unstable in pitch
  • Elevator or Stabilator becomes ineffective in a stall or spin recovery
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16
Q

what is moment

A

Product of weight multiplied by its arm

17
Q

what is Arm

A
  • Horizontal distance from the datum

- The number will be negative forward of the datum and negative aft of the datum

18
Q

Centre of Gravity formula

A

CG = Total moment
_________
Total Weight

19
Q

what happens with an overloaded aircraft

A
  • aircraft must accelerate to a higher speed to generate sufficient lift
  • needs more run way to attain higher speed
  • reduces climb performance
  • its service ceilings are decrease
  • aircraft become unstable and difficult to fly
20
Q

what is MAC ?

A

Mean Aerodynamic Chord is the chord drawn trough the the center of the wing plan area