Question Answer A Answer B
The amount of excess A) position of the CG. B) speed of the airplane.
load that can be imposed
on the wing of an airplane
depends upon the
Which basic flight A) Climbs. B) Turns.
maneuver increases the
load factor on an airplane
as compared to straight-
and-level flight?
During an approach to a A) stall at a higher B) have a tendency to
stall, an increased load airspeed. spin.
factor will cause the
airplane to
(Refer to figure 2.) If an A) 2,300 pounds B) 3,400 pounds.
airplane weighs 2,300
pounds, what approximate
weight would the airplane
structure be required to
(Refer to figure 2.) If an A) 1,200 pounds B) 3,100 pounds
airplane weighs 3,300
pounds, what approximate
weight would the airplane
structure be required to
(Refer to figure 2.) If an A) 4,500 pounds 6,750 pounds
airplane weighs 4,500
pounds, what approximate
weight would the airplane
structure be required to
Answer C Correct Answer Image FAA Question ID
C) abruptness at which B The amount of
the load is applied. excess load that can
be imposed on an
airplane’s wing is a
C) Stalls. B Level turns will
increase load factor
on an airplane
because lift must be
C) be more difficult to A increased to
During an approach
control. to a stall, increasing
the load factor will
cause the airplane to
C) 4,600 pounds. C stall at a higher
In Figure 2, the
column “Load
Factor n” is the
amount aircraft
C) 3,960 pounds C weight is multiplied
In Figure 2, the
column “Load
Factor n” is the
amount aircraft
7,200 pounds B weight is multiplied
In Figure 2, the
column “Load
Factor n” is the
amount aircraft
weight is multiplied