Weight and balance Flashcards

1
Q

Aircraft performance affected by weight?

A
  • longer take-off
  • longer climb of rate
  • slower cruise
  • longer landing
  • more stress and strain on aircraft
  • or more fuel if want to keep the speed
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2
Q

What happen if balance too forward (nose heavy)

A
  • aircraft may not rotate

- longitudinal control … too stable

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3
Q

What happen if balance too far aft

A
  • aircraft may over-control in pitch

- reduced longitudinal stability (hard to control)

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4
Q

why we care about weight and balance

A

because is illegal to fly an aircraft that is not within limits (air worthiness)

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5
Q

Who is responsible to provide empty weight and center of gravity?

A

AME

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6
Q

what is empty weight

A

weight of the aircraft and its balance point without fuel , pax, baggage and crew

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7
Q

loaded weight and balance report

A

the actual weight of the aircraft and its balance poiny in flight (pilots responsibility)

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8
Q

where to find empty weight and balance report in cars

A

chapter 571 of Airworthiness manual

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9
Q

whos responsable for have the record of weight and balance updated

A

owner

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10
Q

when do we need to do a new weight and balance report

A

after modification or mayor repair that involves a change on the empty weight or center of gravity
AWM 571 App C

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11
Q

what weight and balances includes

A

all items required by the basis of the aircraft type certification , and all additional items of installed equipment
AWM 571 App C

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12
Q

empty weight is determine by ?

A

-weighting the plane by scales or load cell min of 3
-Manufacturers can use standard weight with any
optional equipment mathematically added
-AME can calculate the empty weight by using the weight of the equippment added or removed

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13
Q

center of gravity

A

the point along the an AC logitudinal axis where the weight is considered concentrated

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14
Q

what info we need for to calculate C off G

A
  • datum
  • leveling info if weighing
  • Arm
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15
Q

what is Datum

A

imaginary vertical plane from which all are taken and manufactures determine that

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16
Q

where to find Datum

A

Pilot operating pilot, type certificate data cheet, amm

17
Q

how you level an aircraft for weighing

A

follow AMM,POH or Type certificated

18
Q

why we level an aircraft

A

because depends is is nose or tail heavy the CG will appear move forward or aft

19
Q

what is weight

A

mass of an object

20
Q

what is datum

A

arbitrary ref point

21
Q

what is arm

A

distance that the weight is away from ref point ( C or G

22
Q

what is moment

A

weight multiply by arm

23
Q

(moment) divided by (weight)

A

balance point (C G)

24
Q

if adding floats where can i find how to do it

A

AMM and Suplemental type certificade (STC)

25
Q

what is ammendment

A

when we calculate new wheight and balance due too adding (Floats or skiis)

26
Q

how you marked the old amendment

A

(Superseded) along with date and signature

27
Q

what is an Addendum

A

different configuration within a weight and balance report

28
Q

reasons to perform desimetry of check

A
  • any major structural repair
  • heavy landing
  • extreme turbulance
  • overspeeding
  • loose or sheared fasteners
  • wrinkling or buckling of structural plating
29
Q

symmetry geometrical planes

A

longitudinal and lateral

30
Q

types of NDT testing

A
  • liquid penetrant testing
  • electromagnetic testing
  • magnetic particle testing
  • ultrasound
  • eddy current
31
Q

NDT testing has a discontinuity that is ?

A

relevant or irrelevant

32
Q

where the engine should be positioned in its 4 stroke cycle for Magneto test

A

compression stroke number 1 cylinder 25 degree BTDC

33
Q

causes for leaks in the cylinder fro a pressure testing

A
  • Cylinder exhaust valve is not seating properly (air from the exhaust pipe)
  • Intake valve leaking (if you here air out of the carburetor heat box)
  • piston rings are defective(if hear air out of dipstick)
  • cylinder crack or defective