Airplanes need two major things in order to fly.
They need some type of propulsion, usually one or more engine driven propellers or some type of jet engine. The thrust provided by the propeller or jet engine has to be enough to over come the drag caused by the air that impacts the aircraft during movement. Gliders use gravity to create the forward motion instead of an engine.
Airplanes also need some type of device that will create enough lift to overcome the weight of the aircraft.
A diagram showing the four forces on an aircraft in flight:
http://www.myaeromodelling.com/wp/wp-content/uploads/2008/01/aerodynamic-force.jpg
Many people are under the impression that Bernoulli's principle is responsible for the production of lift on an aircraft's wing. That is incorrect. A wing produces nearly all of its lift by being at an angle to the airflow. That angle is called the 'angle of attack'. With the front or leading edge of the wing higher than the back or trailing edge of the wing, the wing has a positive angle of attack.
Diagram showing different angles of attack:
http://www.discoverhover.org/infoinstructors/images/angleOfAttack.jpg
If the angle of attack is too high, the airflow will not be smooth (laminar) and the wing will stall, or quit producing lift. That is shown in the bottom view of that diagram.
If Bernoulli's principle were responsible for the production of lift, then airplanes wouldn't need a positive angle of incidence (the angle of the wing in relation to the fuselage centerline).
To learn how an airfoil really works, go here:
http://www.av8n.com/how/htm/airfoils.html
An airplane is controlled by deflecting control surfaces into the airstream. Most aircraft have three primary flight controls. One for pitch (nose up and nose down), one for roll (banking left and right) and one for yaw (turning left and right)
The names of the primary flight controls are:
For pitch.........elevator (usually on the tail)
For roll...........aileron (one on each wing)
For yaw..........rudder (one on each tail if the aircraft has two tails)
A diagram showing the primary flight controls:
http://www.allstar.fiu.edu/aero/images/pic5-5.gif
Some aircraft have secondary flight controls such as flaps, spoilers, speedbrakes and slats. Some aircraft have other secondary flight controls.
The flight controls are operated from the cockpit by the pilot, the copilot or the autopilot.