AVN 2100 Airplane Basics Flashcards
(38 cards)
What are the 5 basic parts of an aircraft?
Powerplant, Wind, Fuselage, Empennage, Landing Gear
What are fuselage structure types?
Truss, Monocoque, Semi-monocoque
What are the 2 types of truss construction?
Open truss and closed truss
What is the difference between open truss and closed truss?
Open truss the struts and wire bracing are visible, closed truss the structure is covered with fabric or metal to streamline the airplane
When the skin is designed to be the only load carrying structure it is a _______ design.
Monocoque
Load carrying skin with an additional substructure for added strength is a ______ design
Semi-monocoque
Monocoque designs use ________ to support almost all the load
Stressed skin
Though very strong, a problem with stressed skin is that:
It will collapse easily if dented
The empennage consists of the:
Vertical stabilizer and horizontal stabilizer
Where is the rudder located?
On the vertical stabilizer
What is a stabilator?
A one piece stabilizer/elevator
What does the vertical stabilizer do?
Helps maintain a straight path through the air
What does the horizontal stabilizer do?
Provides stability and balance by producing a tail down force
What does the rudder do?
Moves the nose left and right (yaw)
How is the rudder controlled?
Foot pedals
Pushing the rudder pedal to the right will move the rudder _____, moving the tail to the ____ and the nose to the ______
Right, left, right
What is the elevator used for?
To pitch the nose up and down
Wings are designed to have ____
The maximum lifting capability possible
Where are the ailerons located?
The trailing edge of the wing, from the midpoint of the wing to the wingtips
Turning the control column to the left, the left aileron is deflected ____ and the right aileron is deflected _____
Up, down
In most small aircraft, flaps are ______ controlled
Electrically
Flaps are:
Lift altering devices used for takeoff and landing
Flaps extend from the _____ to the _____ of the wings
Root, midpoint
If the third gear is under the tail, the plane has a ______ configuration
Conventional