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WorksheetsAMT 126
Total questions: 20
Worksheet time: 7mins
Which kind of plane movement is being shown in this picture?
roll
pitch
yaw
Which kind of plane movement is being shown?
roll
pitch
yaw
Which part of the airplane controls the roll of an airplane?
ailerons
elevators
rudders
Which part of the plane controls the pitch of the plane?
ailerons
elevators
rudders
Which part of the plane is responsible for the yaw movement?
ailerons
elevators
rudder
What is the name of the green control surface?
Horizontal stabilizer
Aileron
Rudder
Elevators
The blue control surfaces are the Ailerons. They control:
Wind speed
Yaw
Roll
Pitch
Where the pilot and controls are:
Cockpit
Fuselage
Envelope
Vertical stabilizer
This part is responsible for an airplanes left and right stability. It is called a:
Horizontal stabilizer
Flaps
Diagonal Stabilizer
Vertical stabilizer
This part is responsible for an airplanes left and right stability. It is called a:
Horizontal stabilizer
Flaps
Diagonal Stabilizer
Vertical stabilizer
To cause this plane to pitch upward, the pilot probably:
Turned the ailerons down.
Moved the elevators up.
Moved the elevators down.
Moved the rudder up.
If you wanted to cause the plane to Yaw nose to left, you would turn the:
Elevator left
Horizontal stabilizer right
Rudder left
Rudder right
Everything that flies needs
wings
air
drag
Lift can be created by
greenhouse gasses
more speed - increase aircraft’s forward motion
reducing power
extending flaps and landing gear
Flight controls are operated by:
Cables, Drums and Pulleys
Flaps, Ailerons and Rudder
Cables, Pushrods and Bell cranks
Where are the geared servo tabs located?
Located on both ailerons and bottom of rudder
Located on left aileron, left elevator and top of rudder
Located on both ailerons and top of the rudder
Trim tabs are located on?
The rudder, both elevators, and the right aileron
The ailerons and elevators only
The rudder, left elevator and left aileron
The wing flaps are:
Actuated hydraulically by an actuator located in the cabin roof through a system of push-pull rods, levers and bell cranks
Actuated by an electric motor located on the left wing
Actuated hydraulically by actuators located at each flap segment
What is the purpose of the Flap/Elevator interconnect tab?
To help automatically trim the aircraft when flaps are selected
To minimize pitch change during Flap operations
Lessen force required to move the control surfaces
