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