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Originally Posted by dinopoker
How do you fly a plane?
I could write a book to answer this and, in fact, several have been written. To go into a lot of detail would almost surely result in tl;dr.
It's all about learning the relation between power and use of flight controls and knowing how they interact. Try telling someone how to drive a car without actually demonstrating it in a car and you can start to realize what a futile effort it is for me to try to
tell you how to fly a plane.
We can discuss aerodynamic principles and flying techniques, but I can't tell you how much to pull back on the yoke for takeoff any more than you could tell a new driver how far to turn the steering wheel to negotiate a turn.
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What is a bank, pitch, or yaw, or whatever?
These I can answer.
Bank is movement around the longitudinal axis of the plane (an imaginary line extending from the nose to the tail of the plane). The ailerons (small control surfaces on the aft outboard part of each wing) are used to cause a bank. Move the control wheel (or stick in some aircraft) to the right and the right aileron moves upward into the slipstream causing the right wing to move downward, and the left aileron moves down causing that wing to move upward.
Pitch is movement around the lateral axis (line from wingtip to wingtip). Pull the wheel back and the elevator (control surface on the back of the horizontal stabilizer) will move up in the slipstream, forcing the tail down and the nose up. This will cause a climb. Additional power will be required if a constant airspeed is desired during the climb.
Yaw is movement around the vertical axis (a vertical line through the airplane's Center of Gravity). Push the right rudder pedal and the rudder (control surface on the back of the vertical stabilizer) moves to the right into the slipstream, forcing the tail to the left and the nose of the airplane pivots around the C.G. to the right.
Whatever is that annoying thing that my niece says when she can't formulate a coherent reply.
Flaps are not a required flight control surface, but sure are nice to have. They are located on the inboard aft portion of the wings and are selected to various positions depending on the airplane. On the 767 we can select 1, 5, 15, 25 or 30 degrees of flaps. They reduce the stall speed of the plane and also give a lower pitch attitude for a given airspeed. Thus we can fly our approach at a slower airspeed, which translates into less runway used to get stopped and less wear on the brakes. Of course there is a trade off since flaps add drag, so more power is required for a given airspeed. If we have a flap failure and have to land with flaps up, we might have an approach speed of 170 kts or so (about 195 mph) vs the normal range of 130 to 140 kts.
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How many control thingamajigs are there on a plane?
218 (unless I misunderstand the question)
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What keeps the plane in the air?
An airplane accelerates when thrust > drag.
It maintains a steady speed when thrust = drag.
It climbs when lift>gravity.
It cruises level when lift=gravity.
The wing produces lift by its shape and its affect on the airflow over it. I'll leave it as an exercise to the student to Wikipedia "Bernoulli Effect".
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What's the deal with all those gauges? I mean are they really all important or are some of them like a secret LOL?
Cool huh? They all have a meaning, but the importance varies all the way from "Who cares?" to "Holy S***, we'll need that to live!"
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Also, what is the deal with a flat spin? Why is it supposedly easy for a plane to get into one, and why is it so hard for a pilot to stop? Or is that even true?
Different airplanes will have different flying characteristics and vastly different spin characteristics. Some planes can be spun easily and the spin is docile and easy to recover from (just let go of things!). Others are not certified to spin and have warning placards to that effect; i.e. you can enter the spin, but you may not be able to recover.
A flat spin is just a way to describe a spin where the plane's pitch attitude is near level vs nose down as in a traditional spin. My old Grumman Yankee was placarded against spins. This was because the fuel tank was a simple tube extending along the lateral axis (see definition above). In a spin the fuel would tend to "dumbbell" out to the wingtips producing a flat spin and after about 3 turns it would be unrecoverable.
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What are the other basic danger that inexperienced pilots have to watch out for?
Don't fly to Martha's Vinyard on a moonless night unless you are instrument rated.
Last edited by W0X0F; 06-18-2014 at 06:52 PM.