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This study guide provides a comprehensive overview of fundamental aviation principles and flight mechanics, covering topics such as wing flaps, flight controls, stability, and aircraft instruments. It presents a series of questions and answers related to these concepts, offering a valuable resource for aspiring pilots preparing for their written exam.
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What is one purpose of wing flaps? - ✔✔To enable the pilot to make steeper approaches to a landing without increasing the airspeed. One of the main functions of flaps during approach and landing is to: - ✔✔Increase the angle of descent without increasing the airspeed. What is the purpose of the rudder on an airplane? - ✔✔To control yaw. Which is not a primary flight control surface? A. Flaps B. Stabilator C Ailerons - ✔✔A. Flaps
The elevator controls movement around which axis? - ✔✔Lateral. Which statement is true concerning primary flight controls? A. The effectiveness of each control surface increases with speed because there is more flow over them B. Only when all three primary flight controls move in sequence do the airflow and pressure distribution change over and around the airfoil. C. Primary flight controls include ailerons, rudder, elevator, and trim systems - ✔✔A. The effectiveness of each control surface increases with speed because there is more flow over them. Which of the following is true concerning flaps? A. Flaps are attached to the leading edge of the wing and are used to increase wing lift. B. Flaps allow an increase in the angle of descent without increasing airspeed.
What is the relationship of lift, drag, thrust, and weight when the airplane is in straight-and-level flight? - ✔✔Lift equals weight. Thrust equals drag. Which statement relates to Bernoulli's principle? - ✔✔Air traveling faster over the curve upper surface of an airfoil causes lower pressure on the top surface. The term "angle of attack" is defined as the angle... - ✔✔between the wing chord line and the relative wind. Angle of attack is defined as the chord line of an airfoil and the... - ✔✔Direction of the relative wind. The angle of attack at which an airplane wing stalls will... - ✔✔Remain the same regardless of gross weight.
As altitude increases, the indicated airspeed at which a given airplane stalls in a particular configuration will... - ✔✔Remain the same regardless of altitude. In what flight condition must an aircraft be placed in order to spin? - ✔✔Stalled. During a spin to the left, which wing(s) is/are stalled? - ✔✔Both wings are stalled. How will frost on the wings of an airplane affect takeoff performance? - ✔✔Frost will disrupt the smooth flow of air over the wing, adversely affecting its lifting capability. Why is frost considered hazardous to flight? - ✔✔Frost spoils the smooth flow of air over the wings, thereby decreasing lifting capability.
What force makes an airplane turn? - ✔✔The horizontal component of lift. An airplane said to be inherently stable will... - ✔✔require less effort to control. What determines the longitudinal stability of an airplane? - ✔✔The location of the CG with respect to the center of lift. Changes in the center of pressure of a wing affect the aircraft's... - ✔✔Aerodynamic balance and controllability. An airplane has been loaded in such a manner that the CG is located aft of the aft CG limit. One undesirable flight characteristic a pilot might experience with this airplane would be... - ✔✔Difficulty in recovering from a stalled condition.
What causes an airplane (except a T-tail) to pitch nosedown when power is reduced and controls are not adjusted? - ✔✔The downwash on the elevators from the propeller slipstream is reduced and the elevator effectiveness is reduced Loading an airplane to the most aft CG will cause the airplane to be... - ✔✔Less stable at all speeds. In what flight condition is torque effect the greatest in a single-engine airplane? - ✔✔Low airspeed, high power, high angle of attack. The left turning tendency of an airplane caused by P-factor is the result of the... - ✔✔Propeller blade descending on the right, producing more thrust than the ascending blade on the left. When does P-factor cause the airplane to yaw to the left? - ✔✔When at high angles of attack.
Deviation in a magnetic compass is caused by the... - ✔✔Magnetic fields within the aircraft distorting the lines of magnetic force. In the Northern Hemisphere, if an aircraft is accelerated or decelerated, the magnetic compass will normally indicate... - ✔✔Correctly when on a north or south heading. In the Northern Hemisphere, a magnetic compass will normally indicate initially a turn toward the west if... - ✔✔A right turn is entered from a north heading. In the Northern Hemisphere, a magnetic compass will normally indicate a turn toward the south when... - ✔✔The aircraft is decelerated while on a west heading.
In the Northern Hemisphere, a magnetic compass will normally indicate initially a turn toward the east if... - ✔✔A left turn is entered from a north heading. What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from a south heading in the Northern Hemisphere?
What is density altitude? - ✔✔The pressure altitude corrected for nonstandard temperature. Under what conditions is pressure altitude and density altitude the same value? - ✔✔At standard temperature. Under what condition is indicated altitude the same as true altitude? - ✔✔When at sea level under standard conditions. Under what condition will pressure altitude be equal to true altitude? - ✔✔When standard atmospheric conditions exist. What is pressure altitude? - ✔✔The altitude indicated when the barometric pressure scale is set to 29.92.
Altimeter setting is the value to which the barometric pressure scale of the altimeter is set so the altimeter indicates... - ✔✔True altitude at field elevation. If it is necessary to set the altimeter from 29.15 to 29.85 what change occurs? - ✔✔700 foot increase in indicated altitude. (The altimeter-indicated altitude moves in the same direction as the altimeter setting and changes about 1,000 ft. for every change of 1" Hg.) If a pilot changes the altimeter setting from 30.11 to 29.96 what is the approximate change in indication? - ✔✔Altimeter will indicate 150 feet lower. If a flight is made from an area of low pressure into an area of high pressure without the altimeter setting being adjusted, the altimeter will indicate... - ✔✔Lower than the actual altitude above sea level.
How do variations in temperature affect the altimeter? - ✔✔Pressure levels are raised on warm days and the indicated altitude is lower than the true altitude. What is a benefit of flying with a glass cockpit? - ✔✔Situational awareness is increased. What steps must be taken when flying with glass cockpits to ensure safe flight? - ✔✔Regularly scan both inside and outside, use all appropriate checklist, and cross-check with other forms of information. An abnormally high engine oil temperature indication may be caused by... - ✔✔The oil level being too low. Excessively high engine temperatures will... - ✔✔Cause loss of power, excessive oil consumption, & possible permanent internal engine damage.
Excessively high engine temperatures, either in the air or on the ground, will... - ✔✔Cause loss of power, excessive oil consumption, & possible permanent internal engine damage. For internal cooling, air cooled engines are especially dependent on... - ✔✔The circulation of lubricating oil. If the engine oil temperature and cylinder head temperature gauges have exceeded their normal operating range, the pilot may have been operating with...
If the ignition switch ground wire becomes disconnected, the magneto... - ✔✔May continue to fire. With regard to carburetor ice, float-type carburetor systems in comparison to fuel injection systems are generally considered to be... - ✔✔More susceptible to icing. Which condition is most favorable to the development of carburetor icing? - ✔✔Temperature between 20ºF and 70ºF and high humidity. The possibility of carburetor icing exist even when the ambient air temperature is as... - ✔✔High as 70ºF and the relative humidity is high. If an aircraft is equipped with a fixed-pitch propeller and a float-type carburetor, the first indication of carburetor ice would most likely be... - ✔✔Loss of RPM.
The operating principle of float-type carburetors is based on the... - ✔✔Difference in air pressure at the venturi throat and the air inlet. The presence of carburetor ice in an aircraft equipped with a fixed-pitch propeller can be verified by applying carburetor heat and noting... - ✔✔A decrease in RPM and then a gradual increase in RPM. Generally speaking, the use of carburetor heat tends to... - ✔✔Decrease engine performance. Applying carburetor heat will... - ✔✔Enrich the fuel/air mixture. What change occurs in the fuel/air mixture when the carburetor heat is applied? - ✔✔The fuel/air mixture becomes richer.