Weight And Balance Flashcards
Effects of adverse balance
Stability
Control
Negligible weight / CG change
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
Moment arm
Horizontal distance in inches from reference datum line to the CG
Basic empty weight
GAMA
Standard plus equipment
CG
Point aircraft would balance if suspended, mass center
In inches from datum line or percent of MAC
CG limits
Forward and aft points within CG must be located
CG range
Datum
Imaginary vertical plane or line from which all measurements of arm are taken
Established by manufacturer
Floor load limit
Max weight per sqr in/foot
Fuel load
Expendable part of the fuel
Ramp or taxi weight vs take off weight
Difference due to fuel burn during taxi
Max zero fuel weight - GAMA
Exclusive usable fuel
Moment
Weight of an item x arm
In pound-inches
Moment index
Divided by constant such as 100, 1000
Simplify weight and balance computation
Payload - GAMA
Weight of occupants, cargo, baggage
Standard empty weight - GAMA
Airframe, engines, fixed equipment, ballast, hydraulic fluid, unusable fuel, engine oil