Weight And Balance Flashcards

1
Q

Effects of adverse balance

A

Stability

Control

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2
Q

Negligible weight / CG change

A

1lbs or less for <5000lbs
2lbs or less for 5000-50000lbs
5lbs or less for 50000lbs+
CG change less than 0.05%.of mean aerodynamic chord (MAC) = average distance from leading edge to trailing edge

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3
Q

Moment arm

A

Horizontal distance in inches from reference datum line to the CG

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4
Q

Basic empty weight

A

GAMA

Standard plus equipment

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5
Q

CG

A

Point aircraft would balance if suspended, mass center

In inches from datum line or percent of MAC

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6
Q

CG limits

A

Forward and aft points within CG must be located

CG range

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7
Q

Datum

A

Imaginary vertical plane or line from which all measurements of arm are taken
Established by manufacturer

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8
Q

Floor load limit

A

Max weight per sqr in/foot

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9
Q

Fuel load

A

Expendable part of the fuel

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10
Q

Ramp or taxi weight vs take off weight

A

Difference due to fuel burn during taxi

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11
Q

Max zero fuel weight - GAMA

A

Exclusive usable fuel

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12
Q

Moment

A

Weight of an item x arm

In pound-inches

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13
Q

Moment index

A

Divided by constant such as 100, 1000

Simplify weight and balance computation

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14
Q

Payload - GAMA

A

Weight of occupants, cargo, baggage

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15
Q

Standard empty weight - GAMA

A

Airframe, engines, fixed equipment, ballast, hydraulic fluid, unusable fuel, engine oil

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16
Q

Standard weights

A

Use if actual weights are not available

17
Q

Station

A

Location in aircraft, distance in inches from datum

18
Q

Useful load

A

Pilot, co-pilot, passengers, baggage, usable fuel, drainable oil

19
Q

Determine load weight and CG

Computational method

A

List weight of aircraft, occupants, fuel (6lbs/gal), baggage
Weight x arm = Moment
Total weight and total moment
Total moment / total weight = CG

20
Q

Loaded weight and CG

Graph method

A

Graphs calculate moment

Find weight and draw line straight across until it intercepts with item, straight line down to read moment

21
Q

Other load weight and CG calculations

A

Table
With negative arm
With zero fuel,weight

22
Q

Calculate weight shift and CG
100lbs shifted from station 30 to 150
Moment increases total by 12000in-lbs

A

Moment at 150 = 100lb x 150in = 15000in-lb
Moment at 30 = 100lb x 30in = 12000in-lb
Moment change 15000-3000= 12000
Total moments = 616000 + 12000 = 628000
CG = 628000in-lb/8000lb (total weight) = 78.5in

23
Q

Calculate shift of CG

A

Weight shifted / total weight = ^CG / distance of weight shift
100 / 8000 = ^CG / 120
^CG = 1.5in
Previous CG + ^CG = new CG

24
Q

Add/Subtract ^CG

A

Shifting aft, add

Shifting forward, subtract