FAA-H-8083-25C · Source PDF page 245
Weight and Balance
Weight and Balance · PHAK page 10-1

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Chapter 10
Weight and Balance
Introduction
Compliance with the weight and balance limits of any aircraft
is critical to flight safety. Operating above the maximum
weight limitation compromises the structural integrity of
an aircraft and adversely affects its performance. Operation
with the center of gravity (CG) outside the approved limits
results in control difficulty.
Weight Control
As discussed in Chapter 5, Aerodynamics of Flight, weight
is the force with which gravity attracts a body toward the
center of the Earth. It is a product of the mass of a body and
the acceleration acting on the body. Weight is a major factor
in aircraft construction and operation and demands respect
from all pilots.
The force of gravity continuously attempts to pull an aircraft
down toward Earth. The force of lift is the only force that
counteracts weight and sustains an aircraft in flight. The
amount of lift produced by an airfoil is limited by the airfoil
design, angle of attack (AOA), airspeed, and air density. To
assure that the lift generated is sufficient to counteract weight,
loading an aircraft beyond the manufacturer’s recommended
weight must be avoided. If the weight is greater than the lift
generated, the aircraft may be incapable of flight.
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