10-10.
An aircraft lateral control system
incorporates a load-feel bungee in
the aileron system for which of
the following purposes?
1.
To provide artificial feel
only
2.
To provide a centering device
only
3.
To provide artificial feel and
a centering device only
4.
To provide artificial feel, a
centering device, and
effortless control stick
movement
IN ANSWERING QUESTION 10-11, REFER TO
FIGURE 9-10 IN THE TEXTBOOK.
10-11.
The aircraft flaperon control
system has a total of how many
actuators?
Five
Two
Three
Seven
10-12.
Flaperon autopilot actuators are
capable of operating in which of
the following modes?
Manual only
Manual or series only
Manual, series, or parallel
only
Manual, series, parallel, or
independent
10-13.
When the flaperon autopilot
actuator is operating in the
series mode, the AFCS can be
overridden by the pilot applying
what minimum amount of force to
the control stick?
25 lb
20 lb
15 lb
10 lb
10-14.
The combination aileron and
spoiler/deflector system is used
to enhance what in-flight
capability of the aircraft?
1.
Increased pitch control in
rapid descents
2.
Increased climb rate about the
lateral axis
3.
Increased yaw control during
high-speed turns
4.
Increased roll rate about the
longitudinal axis
10-15.
On a combination aileron and
spoiler/deflector system, what is
the maximum deflection of (a) the
spoiler and (b) the deflector?
1.
(a) 30°
(b) 15°
2.
(a) 40°
(b) 20°
3.
(a) 50°
(b) 25°
4.
(a) 60°
(b) 30°
10-16.
In a spoiler control system,
spoiler action is provided by all
EXCEPT which of the following
components?
The pitch computer
The spoiler actuators
The mechanical interlock
The roll command transducer
10-17.
In a rudder control system, the
pedal position transmitter and the
rudder surface transmitter
function only under which of the
following conditions?
1.
When the automatic flight
control system is disengaged
2.
When the automatic flight
control system is engaged
3.
When the nosewheel steering
system is disengaged
4.
When the nosewheel steering
system is engaged
10-18.
The servo cylinders used in an
electronic flight control system
are controlled by what means?
Mechanical linkage
Electrically controlled cables
Electrical impulses from
computers
Hydraulic impulses from
electronic data centers
10-19.
The backup flight control system
reservoir has what total capacity?
0.84 quart
0.97 quart
1.31 quarts
1.75 quarts
10-20.
The three-position backup system
hydraulic test switch located in
the cockpit is spring-loaded to
what position?
ON
OFF
FLIGHT
COMBINED
49
