1-13.
What airfoil maintains directional
1-20.
When the control stick of an
1-14.
1-15.
1-16.
1-17.
1-18.
1-19.
stability in an aircraft?
The rudder
2.
The elevators
3.
The vertical stabilizer
4.
The horizontal stabilizer
Which of the following is a primary
flight control?
Rudder
2.
Spoiler
3.
Trim tab
4.
Wing flap
To roll an aircraft clockwise, you
must cause which of the following
changes in flight control
positions?
1.
Raise the left aileron and
lower the right one
2.
Lower the left aileron and
raise the right one
3.
Raise the elevators and move
the rudder(s) to the left
4.
Lower the elevators and move
the rudder(s) to the right
The pilot of a fighter type
aircraft has underestimated his
altitude and must climb steeply to
get over a mountain.
Which of the
following actions should he take?
1.
Pull back on the yoke
2.
Push the yoke forward
3.
Push the stick forward
4.
Pull back on the stick
Which of the following systems
would assist the pilot of a high-
speed aircraft in moving the
control surfaces?
1.
A torsion link
2.
A compound link
3.
A manual-boost system
4.
A power-operated system
Longitudinal control systems
control movement of the aircraft
about which of the following axes?
1.
Lateral only
2.
Vertical only
3.
Longitudinal only
4.
Lateral, vertical, and
longitudinal
A load-feel bungee in a lateral
control system is NOT used for
which of the following purposes?
1.
Artificial feel
2.
Control stick centering
3.
Interconnects aileron systems
4.
Automatic aileron trim control
1-21.
1-22.
1-23.
1-24.
1-25.
aircraft equipped with a flaperon
system is moved to the left, the
left and right flaperons will be in
which of the following positions?
1.
Left down, right up
2.
Left up, right flush
3.
Left down, right flush
4.
Left flush, right down
An aircraft is equipped with a
spoiler/deflector system.
When the
spoilers are set at 60 degrees,
which of the following angles of
deflection can NOT be achieved with
the deflectors?
The actuator of the slab type
horizontal stabilizer can operate
in which of the following modes?
1.
Manual or series only
2.
Manual or parallel only
3.
Manual, series, or parallel
4.
Manual, series, or conductive
The yawing motion of an aircraft is
controlled by what flight
control(s) ?
1.
Ailerons
2.
Elevators
3.
Rudder(s)
4.
Trim tabs
On the F-14 aircraft, variable-
geometry wings are used for what
purpose?
1.
To increase performance at all
speeds
2.
To increase the length of the
wing
3.
To change the angle of attack
4.
To fold the wings
The mechanical mode of the F-14
wing sweep is used for which of the
following purposes?
1.
Normal landings
2.
Normal takeoffs
3.
Emergencies
4.
Formation flying
1.
1.
2
