Airplane Instruments, Engines, and Systems Flashcards

1
Q

In the Northern Hemisphere, a magnetic compass will normally indicate a turn toward the north if

A

an aircraft is accelerated while on an east or west heading

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

During flight, when are the indications of a magnetic compass accurate?

A

Only in straight and level unaccelerated flight

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Deviation in a magnetic compass is caused by

A

magnetic fields within the aircraft distorting the lines of magnetic force

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

In the Northern Hemisphere, if an aircraft is accelerated or decelerated, the magnetic compass will normally indicate…

A

correctly when on a north or south heading

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

In the Northern Hemisphere, a magnetic compass will normally indicate initially a turn toward the west if

A

a right turn is entered from a north heading

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

In the Northern Hemisphere, the magnetic compass will normally indicate a turn toward the south when

A

the aircraft is decelerated while on a west heading

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

In the Northern Hemisphere, a magnetic compass will normally indicate initially a turn toward the east if

A

a left turn is entered from a north heading

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

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?

A

the compass will initially indicate a turn to the right, but at a faster rate than is acutally occurring

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

The pitot system provides impact pressure for which instrument?

A

airspeed indicator

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Which instrument will become inoperative if the pitot tube becomes clogged?

A

airspeed

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

If the pitot tube and outside static vents become clogged, which instruments would be affected?

A

The altimeter, airspeed indicator, and the vertical speed indicator

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Which instruments will become inoperative if the static vents become clogged?

A

airspeed. altimeter, and vertical speed

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

What does the red line on an airspeed indicator represent?

A

never-exceed speed

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

What is an important airspeed limitation that is not color coded on airspeed indicators?

A

maneuvering speed

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

What is absolute altitude?

A

The vertical distance of the aircraft above the surface

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

What is true altitude?

A

The vertical distance of the aircraft above the sea level

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

What is density altitude?

A

The pressure altitude corrected for nonstandard temperature

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Under what condition is pressure altitude and density altitude the same value?

A

At standard temperature

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Under what condition is indicated altitude the same as true altitude?

A

When at sea level under standard conditions

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Under which condition will pressure altitude be equal to true altitude?

A

When standard atmospheric conditions exist

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

What is pressure altitude?

A

The altitude indicated when the baramotric pressure scale is set to 29.92

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

Altimeter setting iw the value to which the barometric pressure scale of the altimeter is set so the altimeter indicates…

A

true altitude at field elevation

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

If it is necessary to set the altimeter from 29.15 to 29.85, what change occurs?

A

700-foot increase in indicated altitude

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

If a pilot changes the altimeter setting from 30.11 to 29.96, what is the appropriate change in indication?

A

Altimeter will indicate 150 feet lower

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
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
26
If a flight is made from an area of high pressure into an area of lower pressure without the altimeter setting being adjusted, the altimeter will indicate...
higher than the actual altitude above sea level
27
Which condition would caue the altimeter t indicate a lower altitude than true altitude?
Air temperature warmer than standard
28
Under what condition will true altitude be lower than indicated altitude?
In colder than standard air temperature
29
How do variations in temperature affect the altimeter?
Pressure levels are raised on warm days and the indicated altitude is lower than true altitude
30
What is a benefit of flying with a glass cockpit?
Situational awareness is increased
31
What steps must be taken when flying with glass cockpits to ensure safe flight?
Regularly scan both inside and outside, use all appropriate checklists, and cross check with other forms of information
32
An abnormally high engine oil temperature indication may be caused by...
the oil level being too low
33
Excessively high engine temperatures will...
cause loss of power, excessive oil consumption, and possible permanent internal engine damage
34
Excessively high engine temperatures either in the air or on teh ground will
cause loss of power, excessive oil consumption, and possible permanentt internal engine damage
35
For internal cooling, air cooled engines are especially dependent on
the circulation of lubricating oil
36
If the engine oil temperature and cylinder head temperature gauges ahve eceeded their normal operating range, the pilot may have been operating with
too much power and with the mixture set too lean
37
What action can a pilot take to aid in cooling an engine that is overheating during a climb?
reduce rate of climb and increase airspeed
38
what is one procedure to aid in cooling an engine that is overheating?
enrich the fuel mixture
39
How is engine operation controlled on an engine equipped with a constant-speed propeller?
The throttle controls power output as registered on the manifold pressure gauge and the propeller control regulates engine RPM
40
A precaution for the operation of an engine equipped with a constant speed propeller is to
avoid high manifold pressure settings with low RPM
41
What is an advantage of a constant-speed propeller?
Permits the pilot to select the blade angle for the most efficient performance
42
One purpose of the dual ignition system on an aircraft engine is to provide for
improved engine performance
43
If the ignition switch ground wire becomes disconnected, the magneto
may continue to fire
44
With regard to carburetor ice, float type carburetor systems in comparison to fuel injection systems are generally considered to be
more susceptible to icing
45
Which condition is most favorable to the development of carburetor icing?
Temperatures between 20F and 70F and high humidity
46
The possibility of carburetor icing exists even when the ambient air temperature is as
high as 70F and the relative humidity is high
47
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
48
The operating principle of float-type carburetors is based on the
difference in air pressure at the venturi throat and the air inlet
49
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
50
Generally speaking, the use of carburetor ehat tends to
decrease engine performance
51
Applying carburetor heat will
enrich the fuel/air mixture
52
What change occurs in teh fuel/air mixture when carburetor heat is applied?
The fuel/air mixture becomes leaner
53
During the run-up at a high-elevation airport, a pilot notes a slight engine roughness that is not affected by the magneto check but grows worse during the carburetor heat check. Under these circumstances, what would be the most logical initial action?
Check the results obtained with a leaner setting of the mixture
54
The basic purpose of adjusting the fuel/air mixture at altitude is to
decrease the fuel flow in order to compensate for decreased air density
55
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?
The fuel/air mixture may become excessively lean
56
Detonation occurs in a reciprocating aircraft when
the unburned charge in the cylinders explodes instead of burning normally
57
Detonation may occur at high-power settings when
the fuel mixture ignites instantaneously instead of burning progressively and evenly
58
If a pilot suspects that the engine (with a fixed pitch propeller) is detonating during climb-out after takeoff, the intitial corrective action to take would be to
lower the nose slightly to increase airspeed
59
If the grade of fuel used in an aircraft engine is lower than specified for the engine, it will most likely cause
detonation
60
The uncontrolled firing of the fuel/air charge in advance of normal spark ignition is known as
pre-ignition
61
What type fuel can be substitued for an aircraft if the recommended octane is not available?
the next higher octane aviation gas
62
Filling the fuel tanks after the last flight of the day is considered a good operating procedure because this will...
prevent moisture condensation by eliminating airspace in the tanks
63
To properly purge water from the fuel system of an aircraft equipped with fuel tank sumps and a fuel strainer quick drain, it is necessary to drain fuel from the
fuel strainer drain and the fuel tank sumps
64
On aircraft equipped with fuel pumps, when is the auxiliary electric driven pump used?
in the event engine-driven fuel pump fails
65
Which would most likely cause the cylinder head temperature and engine oil temperature gauges to exceed their normal operating ranges?
using fuel that has a lower than specified fuel rating
66
What should be the first action after starting an aircraft engine?
adjust for proper RPM and check for desired indications on the engine gauges
67
Should it become necessary to handprop an airplane engine, it is extremely important that a competent pilot
be at the controls in the cockpit
68
An electrical system failure (battery and alternator) occurs during flight. In this situation, you would
experience avionics equipment failure
69
A positive indication on an ammeter
shows the rate of charge on the battery
70
To keep a battery charged, the alternator voltage output should be
higher than the battery voltage
71
Which of the following is a true statement concerning electrical systems?
lights and radios use the electrical system for power