Term
| One of the main functions of flaps during approach and landing is to |
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Definition
| increase the angle of descent without increasing the airspeed. |
|
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Term
| (Refer to figure 23.) Which is a split flap? |
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Definition
|
|
Term
| Which type of flap creates the greatest change in pitching moment? |
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Definition
|
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Term
| (Refer to figure 23.) Which is a slotted flap? |
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Definition
|
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Term
| (Refer to figure 23 below) Which is a fowler flap? |
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Definition
|
|
Term
| What is one purpose of wing flaps? |
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Definition
| To enable the pilot to make steeper approaches to a landing without increasing the airspeed. |
|
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Term
| A purpose of flight spoilers is to |
|
Definition
| reduce lift without increasing airspeed. |
|
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Term
| The purpose of a servo tab is to |
|
Definition
| reduce control forces by deflecting in the proper direction to move a primary flight control. |
|
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Term
| Which direction from the primary control surface does a servo tab move? |
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Definition
|
|
Term
| Which type of flap creates the least change in pitching moment? |
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Definition
|
|
Term
| Which direction from the primary control surface does an antiservo tab move? |
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Definition
|
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Term
| A purpose of leading edge slats on high performance wings is to |
|
Definition
| direct air from the high-pressure area under the leading edge along the top of the wing. |
|
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Term
| A purpose of leading edge slats on high performance wings is to |
|
Definition
| increase lift at relative slow speeds. |
|
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Term
| How is engine operation controlled on an engine equipped with a constant-speed propeller? |
|
Definition
| The throttle controls power output as registered on the manifold pressure gauge and the propeller control regulates engine RPM. |
|
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Term
| A precaution for the operation of an engine equipped with a constant-speed propeller is to |
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Definition
| avoid high manifold pressure settings with low RPM. |
|
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Term
| Which statement best describes the operating principle of a constant-speed propeller? |
|
Definition
| The propeller control regulates the engine RPM, and in turn, the propeller RPM. |
|
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Term
| The primary purpose of an oil-to-fuel heat exchanger is to |
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Definition
|
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Term
| Should it become necessary to hand prop an airplane engine, it is extremely important that a competent pilot |
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Definition
| be at the controls in the cockpit. |
|
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Term
| Which location has the highest gas volume in a turbine engine? |
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Definition
|
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Term
| The speed (RPM or percent) of the low pressure compressor of a dual compressor engine is referred to as |
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Definition
|
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Term
| If the engine oil temperature and cylinder head temperature gauges have exceeded their normal operating range, the pilot may have been operating with |
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Definition
| too much power and with the mixture set too lean. |
|
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Term
| Detonation can be caused by |
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Definition
| using a lower grade of fuel than recommended. |
|
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Term
| On aircraft equipped with fuel pumps, when is the auxiliary electric driven pump used? |
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Definition
| In the event engine-driven fuel pump fails. |
|
|
Term
| What is one procedure to aid in cooling an engine that is overheating? |
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Definition
|
|
Term
| It is important to monitor the EGT when starting the engines to prevent |
|
Definition
| hot section burnout or metal distortion. |
|
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Term
| (Refer to figure 7 below) The internal engine temperature will be the lowest at which location? |
|
Definition
|
|
Term
| Which engine instrument is most likely to show an elevated reading if the turbine wheel is damaged? |
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Definition
|
|
Term
| (Refer to figure 7 below) The internal engine pressure will be the lowest at which location? |
|
Definition
|
|
Term
| The speed (RPM or percent) of the high pressure compressor of a dual compressor engine is referred to as |
|
Definition
|
|
Term
| What is an advantage of a constant-speed propeller? |
|
Definition
| Permits the pilot to select the blade angle for the most efficient performance. |
|
|
Term
| The pilot controls the air/fuel ratio with the |
|
Definition
|
|
Term
| What effect does high density altitude, as compared to low density altitude, have on propeller efficiency and why? |
|
Definition
| Efficiency is reduced because the propeller exerts less force at high density altitudes than at low density altitudes. |
|
|
Term
| Excessively high engine temperatures will |
|
Definition
| cause loss of power, excessive oil consumption, and possible permanent internal engine damage. |
|
|
Term
| For internal cooling, reciprocating aircraft engines are especially dependent on |
|
Definition
| the circulation of lubricating oil. |
|
|
Term
| Before shutdown, while at idle, the ignition key is momentarily turned OFF. The engine continues to run with no interruption; this |
|
Definition
| should not normally happen. Indicates a magneto not grounding in OFF position. |
|
|
Term
| Which difference does engine pressure ratio measure? |
|
Definition
| Uncorrected compressor inlet pressure and turbine discharge pressure. |
|
|
Term
| The mixture control can be adjusted, which |
|
Definition
| prevents the fuel/air combination from becoming too rich at higher altitudes. |
|
|
Term
| One purpose of the dual ignition system on an aircraft engine is to provide for |
|
Definition
| improved engine performance. |
|
|
Term
| (Refer to figure 7 below) The internal engine pressure will be the highest at which location? |
|
Definition
|
|
Term
| Which location has the highest gas pressure in a turbine engine? |
|
Definition
|
|
Term
| An abnormally high engine oil temperature indication may be caused by |
|
Definition
| operating with an excessively rich mixture. |
|
|
Term
| Which would most likely cause the cylinder head temperature and engine oil temperature gauges to exceed their normal operating ranges? |
|
Definition
| Using fuel that has a lower-than-specified fuel rating. |
|
|
Term
| What type fuel can be substituted for an aircraft if the recommended octane is not available? |
|
Definition
| The next higher octane aviation gas |
|
|
Term
| Detonation occurs in a reciprocating aircraft engine when |
|
Definition
| the unburned charge in the cylinders explodes instead of burning normally. |
|
|
Term
| An abnormally high engine oil temperature indication may be caused by |
|
Definition
| operating with an excessively rich mixture. |
|
|
Term
| Applying carburetor heat will |
|
Definition
| enrich the fuel/air mixture. |
|
|
Term
| If the grade of fuel used in an aircraft engine is lower than specified for the engine, it will most likely cause |
|
Definition
| lower cylinder head temperatures. |
|
|
Term
| Generally speaking, the use of carburetor heat tends to |
|
Definition
| decrease engine performance. |
|
|
Term
| Which indicator is used to determine if conditions are conducive to formation of ice in jet fuel? |
|
Definition
|
|
Term
| The uncontrolled firing of the fuel/air charge in advance of normal spark ignition is known as |
|
Definition
|
|
Term
| Unless adjusted, the fuel/air mixture becomes richer with an increase in altitude because the amount of fuel |
|
Definition
| remains constant while the density of air decreases. |
|
|
Term
| Which condition is most favorable to the development of carburetor icing? |
|
Definition
| Temperature between 20 and 70 °F and high humidity. |
|
|
Term
| The purpose of a fuel temperature indicator is to |
|
Definition
| determine if fuel temperatures are conducive to ice crystal formation. |
|
|
Term
| While cruising at 9,500 feet MSL, the fuel/air mixture is properly adjusted. What will occur if a descent to 4,500 feet MSL is made without readjusting the mixture? |
|
Definition
| The fuel/air mixture may become excessively lean. |
|
|
Term
| Filling the fuel tanks after the last flight of the day is considered a good operating procedure because this will |
|
Definition
| prevent moisture condensation by eliminating airspace in the tanks. |
|
|
Term
| For internal cooling, reciprocating aircraft engines are especially dependent on |
|
Definition
| the circulation of lubricating oil. |
|
|
Term
| The basic purpose of adjusting the fuel/air mixture at altitude is to |
|
Definition
| decrease the fuel flow in order to compensate for decreased air density. |
|
|
Term
| The pitot system provides impact pressure for which instrument? |
|
Definition
|
|
Term
| What is absolute altitude? |
|
Definition
| The vertical distance of the aircraft above the surface |
|
|
Term
| (Refer to figure 4 below) What is the caution range of the airplane? |
|
Definition
|
|
Term
| (Refer to figure 4 below) What is the maximum structural cruising speed? |
|
Definition
|
|
Term
| Altimeter setting is the value to which the barometric pressure scale of the altimeter is set so the altimeter indicates |
|
Definition
| true altitude at field elevation. |
|
|
Term
| During flight, when are the indications of a magnetic compass accurate? |
|
Definition
| Only in straight-and-level unaccelerated flight |
|
|
Term
| What is pressure altitude? |
|
Definition
| The altitude indicated when the barometric pressure scale is set to 29.92 |
|
|
Term
| (Refer to figure 4 below) Which color identifies the never-exceed speed? |
|
Definition
|
|
Term
| (Refer to figure 4 below) What is the maximum flaps-extended speed? |
|
Definition
|
|
Term
| What is an operational difference between the turn coordinator and the turn-and-slip indicator? The turn coordinator |
|
Definition
| indicates roll rate, rate of turn, and coordination; the turn-and-slip indicator indicates rate of turn and coordination |
|
|
Term
| What does the red line on an airspeed indicator represent? |
|
Definition
|
|
Term
| What is density altitude? |
|
Definition
| The pressure altitude corrected for nonstandard temperature |
|
|
Term
| Why should flight speeds above VNE be avoided? |
|
Definition
| Design limit load factors may be exceeded, if gusts are encountered |
|
|
Term
| To determine pressure altitude prior to takeoff, the altimeter should be set to |
|
Definition
| 29.92" Hg and the altimeter indication noted. |
|
|
Term
| (Refer to figure 7 below) How should a pilot determine the direction of bank from an attitude indicator such as the one illustrated? |
|
Definition
| By the relationship of the miniature airplane (C) to the deflected horizon bar (B) |
|
|
Term
| (Refer to figure 4 below) What is the full flap operating range for the airplane? |
|
Definition
|
|
Term
| (Refer to figure 4 below) Which color identifies the power-off stalling speed with wing flaps and landing gear in the landing configuration? |
|
Definition
| Lower limit of the white arc |
|
|
Term
| (Refer to figure 7 below) The proper adjustment to make on the attitude indicator during level flight is to align the |
|
Definition
| miniature airplane to the horizon bar. |
|
|
Term
| Which instrument(s) will become inoperative if the static vents become clogged? |
|
Definition
| Airspeed, altimeter, and vertical speed. |
|
|
Term
| Deviation in a magnetic compass is caused by the |
|
Definition
| magnetic fields within the aircraft distorting the lines of magnetic force. |
|
|
Term
| (Refer to figure 5 below) A turn coordinator provides an indication of the |
|
Definition
| movement of the aircraft about the yaw and roll axis. |
|
|
Term
| (Refer to figure 3 below) Altimeter 1 indicates |
|
Definition
|
|
Term
| Calibrated airspeed is best described as indicated airspeed corrected for |
|
Definition
| installation and instrument error. |
|
|
Term
| True airspeed is best described as calibrated airspeed corrected for |
|
Definition
| altitude and non-standard temperature. |
|
|
Term
|
Definition
| The vertical distance of the aircraft above sea level. |
|
|
Term
| What is an advantage of an electric turn coordinator if the airplane has a vacuum system for other gyroscopic instruments? |
|
Definition
| It is a backup in case of vacuum system failure |
|
|
Term
| (Refer to figure 3 below) Altimeter 3 indicates |
|
Definition
|
|
Term
| Which instrument will become inoperative if the pitot tube becomes clogged? |
|
Definition
|
|
Term
| (Refer to figure 6 below) To receive accurate indications during flight from a heading indicator, the instrument must be |
|
Definition
| periodically realigned with the magnetic compass as the gyro precesses. |
|
|
Term
| (Refer to figure 3 below) Which altimeter(s) indicate(s) more than 10,000 feet? |
|
Definition
|
|
Term
| If it is necessary to set the altimeter from 29.15 to 29.85, what change occurs? |
|
Definition
| 700-foot increase in indicated altitude |
|
|
Term
| (Refer to figure 4 below) The maximum speed at which the airplane can be operated in smooth air is |
|
Definition
|
|
Term
| (Refer to figure 4 below) Which color identifies the power-off stalling speed in a specified configuration? |
|
Definition
| Lower limit of the green arc. |
|
|
Term
| What is an important airspeed limitation that is not color coded on airspeed indicators? |
|
Definition
|
|
Term
| (Refer to figure 4 below) Which color identifies the normal flap operating range? |
|
Definition
|
|
Term
| (Refer to figure 3 below) Altimeter 2 indicates |
|
Definition
|
|
Term
| If the pitot tube and outside static vents become clogged, which instruments would be affected? |
|
Definition
| The altimeter, airspeed indicator, and vertical speed indicator |
|
|
Term
| An in-flight condition necessary for structural icing to form is |
|
Definition
|
|
Term
| To which position should the oxygen regulator be set when symptoms of hypoxia or hyperventilation are experienced? |
|
Definition
|
|
Term
| Which best describes cabin differential pressure? |
|
Definition
| The difference between ambient and internal air pressure |
|
|
Term
| Which components make up the basic air-cycle cooling system? |
|
Definition
| A source of compressed air, heat exchangers, and a turbine |
|
|
Term
| What is used primarily as a propellant for installed fire extinguishing systems? |
|
Definition
|
|
Term
| The air-cycle cooling system produces cold air by |
|
Definition
| passing air through an expansion turbine and extracting heat energy. |
|
|
Term
| Why must oxygen not be permitted to come in contact with oil, grease, or solvents? |
|
Definition
| Oxygen contact with petroleum products can cause spontaneous fires or explosions. |
|
|
Term
| What is the nominal voltage rating of a fully charged lead-acid battery containing six cells? |
|
Definition
|
|
Term
| What color identifies MIL-H-5606 or BRACO 882 Hydraulic Fluids? |
|
Definition
|
|
Term
| A disadvantage of Skydrol hydraulic fluid is that |
|
Definition
| it can irritate the skin painfully. |
|
|
Term
| What type of gas is released by a lead-acid battery during charging? |
|
Definition
| Oxygen and explosive hydrogen |
|
|
Term
| A turbojet aircraft is equipped with heated inlet ducts and airfoil leading edges. When is this type of anti-icing system usually activated during flight? |
|
Definition
| Whenever icing conditions are first encountered or are expected to occur |
|
|
Term
| What type of gas may be used to service hydraulic accumulators? |
|
Definition
|
|
Term
| The purpose of a hydraulic accumulator is to |
|
Definition
| store hydraulic fluid under pressure. |
|
|
Term
| What component of a pressurization system prevents the cabin altitude from becoming higher than the airplane altitude? |
|
Definition
| Negative pressure relief valve. |
|
|
Term
| An electrical system failure (battery and alternator) occurs during flight. In this situation, you would |
|
Definition
| experience avionics equipment failure. |
|
|
Term
| What is one danger of any oxygen leak? |
|
Definition
| Any ignition source may ignite highly explosive oxygen which over a period of time saturates the surroundings in poorly vented areas |
|
|
Term
| What is the voltage of two lead-acid 12 volt batteries connected in series? |
|
Definition
|
|
Term
| Which component of an air-cycle cooling system undergoes a pressure and temperature drop of air during operation? |
|
Definition
|
|
Term
| Which position should be selected on the diluter-demand oxygen regulator if there is smoke in the cockpit? |
|
Definition
|
|
Term
| Concerning the advantages of an aircraft generator or alternator, select the true statement. |
|
Definition
| An alternator provides more electrical power at lower engine RPM than a generator. |
|
|
Term
| Why is engine anti-ice not normally activated below an ambient temperature of +5 °F? |
|
Definition
| The air is too dry to form ice. |
|
|