Chapter 3 Engines Flashcards

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1
Q

Most general aviation airplane engines are of the ___ opposed variety.

A

Horizontally

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2
Q

Horizontally opposed cylinder arrangements pack a lot of engine into a ___ amount of space. Less space used by the engine means less overall ___.

A

Small, Drag

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3
Q

Name the four cycles of an airplane engine:

A

Intake, compression, power, exhaust

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4
Q

While the piston is in its downward journey, the ___ valve opens, and a mixture of fuel and air rushes in.

A

Intake

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5
Q

The ___ cycle occurs when the intake valve closes and the piston rises.

A

Compression

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6
Q

Just before the cylinder hits the top of its return journey, the ___ ___ fire.

A

Spark Plugs

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7
Q

The burning mixture pushes the piston downward. This is the ___ stroke.

A

Power

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8
Q

One purpose of the dual ignition system on an aircraft engine is to provide for …

A

improved engine performance

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9
Q

Magnetos contain spinnable magnets, housed in metal cases. When the internal magnets are spun, they generate electricity for the ___ ___.

A

Spark Plugs

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10
Q

What’s particularly interesting about magnetos is that they are self-contained spark generators and require no outside source of electrical energy to work other than the ___ motion of the airplane engine.

A

Turning

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11
Q

What is the purpose of the magneto’s impulse coupling?

A

To provide extra spin energy for the magneto’s internal magnets

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12
Q

Normally, airplanes are operated with the magneto switch in the ___ position.

A

Both

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13
Q

Is it permissible to operate the engine on one magneto?

A

yes. If one magneto goes bad, it’s permissible to switch to a single magneto

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14
Q

In many cases we’re concerned not only with the RPM drop on each magneto, but with the ___ in RPM between each mag drop.

A

Difference

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15
Q

Selecting the right or left magneto ___ the other mag by grounding it to the air frame.

A

Deactivates

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16
Q

The mag is grounded to the air frame via a wire called the …

A

P-lead

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17
Q

Mechanics (and flight instructors) sometimes recommend doing a P-lead security check just before shutting down. With the engine idling, quickly turn the mag switch from ___ to off, then immediately back to ___ again.

A

both, both

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18
Q

Exhaust gases sometimes have an afterlife. They can be put to use spinning a ___ or indirectly heating the ___ or cabin.

A

Turbocharger, carburetor

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19
Q

The ___, ___ and ___ manifold (pipes connected to each cylinder) make up the induction system on carburetor equipped airplanes.

A

air filter, carburetor, intake

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20
Q

Airplane carburetors located underneath the engine are called ___ type carburetors because air and fuel must be drawn upward toward each cylinder.

A

Updraft

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21
Q

The operating principle of float-type carburetors is based on the…

A

difference in air pressure at the venturi throat and the air inlet

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22
Q

The ___ jet is that portion of the carburetor that allows the engine to run when the throttle is pulled full aft.

A

Idling

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23
Q

Why doesn’t the engine quit or falter when the throttle is opened abruptly?

A

The accelerator pump supplies a shot of fuel into the throat of the carburetor along with the inrushing air.

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24
Q

Assuming the airplane has an updraft carburetor with an accelerator pump, what happens when the engine isn’t running and the throttle is pumped?

A

Fuel may fall to the bottom of the carburetor and soak the air filter, creating an opportunity for an engine fire.

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25
Q

Fuel-air ratios of approximately ___ part(s) fuel to ___ parts of air are the most efficient for combustion

A

one, 13

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26
Q

Temperature drops of as much as ___ within the carburetor’s throat are not uncommon.

A

70 degrees

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27
Q

your carburetor is a fine ice maker. because of the considerable drop in temp caused by the atomization and evaporation of fuel, any ___ present can and will freeze

A

moisture

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28
Q

be prepared for carburetor ice to form at almost any outside air temp, though it’s most likely to occur between outside temps of ___

A

20 degree F to 70 degrees F

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29
Q

Impact ice occurs when ___ ___ is present and the outside air temp (OAT) is at or below freezing

A

visible moisture

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30
Q

When is it possible to have an air filter freeze over while nowhere near a cloud?

A

If the air is moist and temps are low, water can accumulate and the air filter’s membrane can freeze.

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31
Q

Another occasion where impact ice is likely is during ___

A

freezing rain

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32
Q

if your air filter ever becomes clogged by impact ice, you have a remedy at hand. It’s called the ___ control

A

Carb Heat

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33
Q

Fuel ice forms ___ of the main discharge nozzle.

A

Downstream

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34
Q

Which condition is most favorable for the development of carb icing?

A

Temps between 20 degrees F and 70 degrees F and High humidity

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35
Q

Fuel ice can occur at outside air temps as high as ___ and at humidities as low as ___

A

85°F and 50% Humidity

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36
Q

Throttle ice forms on the ___ side of the throttle valve.It is more likely to occur when the throttle is in a ___ position.

A

rear, partially closed

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37
Q

Pulling the carb heat lever allows heated air to enter the carburetor, raising the air temp within its throat as much as ___

A

90°F

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38
Q

If an aircraft is equipped with a fixed pitch propeller and a float-type carburetor, the first indication of carb ice would most likely be ___

A

Loss of RPM

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39
Q

The presence of carb ice in an aircraft equipped with a fixed pitch propeller can be verified by applying car heat and noting…

A

a further decrease in RPM and then a gradual increase in RPM

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40
Q

Generally speaking, the use of carb heat tends to

A

decrease engine performance

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41
Q

Applying carb heat will

A

enrich the fuel/air mixture

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42
Q

What change occurs in the fuel/air mixture when carb heat is applied?

A

The fuel/air mixture becomes richer

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43
Q

A carburetor air temp gauge allows you to identify the ___ temp range where carburetor ice is most likely to occur.

A

Critical

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44
Q

All engines ___ have the same carb icing potential

A

DO NOT

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45
Q

Pulling out (toward you) on the mixture control ___ the amount of fuel for a given amount of air entering the engine

A

decreases

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46
Q

with an increase in altitude the air becomes thinner and doesn’t ___ as much for a given volume

A

Weigh

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47
Q

The basic purpose of adjusting the fuel/air mixture at altitude is to…

A

decrease the fuel flow in order to compensate for decreased air density.

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48
Q

Most engine manufacturers recommend leaning the mixture whenever you’re operating at or below ___ of the engine’s maximum power output.

A

75%

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49
Q

How might you estimate that you’re operating at power levels greater than 75% in a non-turbocharged engine?

A

If the airplane is operating with full throttle at less than 5,000 feet MSL

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50
Q

Remember, failure to lean appropriately means you’ll use up ___ portion of fuel unnecessarily

A

an extra

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51
Q

Airplanes with fixed pitch propellers (propellers having one pitch that can’t be changed in flight) and float-type carburetors can be leaned by reference to the ___

A

Tachometer

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52
Q

While leaning with reference to the tachometer, the RPM peaks. this means that you are at the fuel-air ratio that produces maximum ___ for a given air density and throttle setting.

A

power

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53
Q

A mixture that is too rich causes engine ___

A

roughness

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54
Q

A fouled spark plus in flight can sometimes be detected by ___

A

an increase in EGT

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55
Q

An excessively rich mixture contributes to ___,___,___, and ___.

A

A rough running engine, high fuel consumption, less range, smaller fuel reserves

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56
Q

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?

A

Check the results obtained with a leaner setting of the mixture

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57
Q

The biggest danger with an excessively lean mixture is that it ___

A

burns hot

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58
Q

What is one procedure to aid in cooling an engine that is overheating?

A

Enrichen the fuel mixture

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59
Q

High cylinder head temps also lead to something known as ___

A

detonation

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60
Q

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?

A

The fuel/air mixture may become excessively lean.

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61
Q

For best power (most usable power per unit of air), enrich the mixture until the temperature ___. (check your POH to ensure the proper procedure for your aircraft.)

A

Decreases 125°F from peak EGT

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62
Q

Water is the most frequent contaminant found in fuel. Water, weighing approximately ___ pounds per gallon, ___ ___ than fuel, which weighs approximately ___ pounds per gallon

A

8, is heavier, 6

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63
Q

If it’s present, water rests on the ___ of the fuel tanks, where it’s often the first thing to go to the engine.

A

Bottom

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64
Q

Filling the fuel tanks after the last flight of the day is considered a good operating procedure because this will…

A

prevent moisture condensation by eliminating airspace in the tanks

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65
Q

Fuel tanks have sump drains found at the ___ part of the tank. The sumps should be drained after every ___

A

lowest, refueling

66
Q

Different grades of aviation fuel (called AVGAS) are dyed for easy identification. Red colored fuel is of the ___ octane variety (very hard to find nowadays). ___ Fuel is of the 100LL or low lead variety and is one of the most common aviation fuels in use today. ___ fuel is 100 octane and is also very hard to find.

A

80, blue, green

67
Q

What type fuel can be substituted for an aircraft if the recommended octane is not available?

A

The next higher octane aviation gas

68
Q

As the fuel pump sucks from the tank, air must replace the departing fuel or a ___ forms

A

Vacuum

69
Q

Boost pumps are often used during ___ to pressurized the fuel system. This helps purge air trapped within the fuel lines. After the engine starts, the electric boost pump is ___ to see if the ___ pump is operational and is pressurizing the system.

A

Engine start, turned off, mechanical

70
Q

On aircraft equipped with fuel pumps, the practice of running a fuel tank dry before switching tanks is considered unwise because…

A

the engine-driven fuel pump or electric fuel boost pump may draw air into the fuel system and cause vapor lock.

71
Q

The primer usually squirts fuel in the ___ portions of the induction system, ___ the carburetor completely.

A

Upper, bypassing

72
Q

The regulations require fuel gauges to be accurate in only two conditions: when the tank is ___ and then it’s ___

A

Full, empty (no usable fuel on board)

73
Q

Remember Rod Machado’s fuel axiom No. 13: If you smell fuel on take off, go back and land. You probably left the cap off your ___

A

Tank

74
Q

If an airplane’s oil cap is left off or comes loose during flight, oil may be ___ ___ the engine

A

expelled from

75
Q

For internal cooling, reciprocating aircraft engines are especially dependent on …

A

the circulation of lubricating oil

76
Q

What should be the first action after starting an aircraft engine?

A

Adjust for proper RPM and check for desired indications on the engine gauges

77
Q

Engines are generally preheated in extreme cold. Lycoming, for example, recommends the engine be preheated at temps below ___ to prevent engine damage during startup. Continental says ___.

A

10°F, 20°F

78
Q

An abnormally high engine oil temp indication may be caused by…

A

the oil level being too low

79
Q

Excessively high engine temps will…

A

cause loss of power, excessive oil consumption, and possible permanent internal engine damage

80
Q

If the engine oil temp and cylinder head temp gauges have exceeded their normal operating range, the pilot may have been operating with…

A

too much power and the with the mixture set too lean

81
Q

What action can a pilot take to aid in cooling an engine that is overheating during a climb?

A

Reduce rate of clime and increase airspeed

82
Q

Inside most airplane engines is something known as an ___. This valve provides an alternate path for the flow of oil if the pressure within the system becomes dangerously ___

A

Oil pressure relief valve, high

83
Q

Most modern airplane engines are ___ cooled. Water cooling may be more efficient, but it would mean carrying considerably more ___

A

Air, weight

84
Q

In order to avoid shock-cooling a high performance engine during a cruise descent, make small power changes. A good rule of thumb is to make no more than a ___ RPM per minute reduction in engine speed on small engines and no more than ___ of manifold pressure per minute on high performance airplanes. Always leave enough power on so as not to cool the cylinder head temps below allowable limits.

A

100, 1 inch

85
Q

Keep in mind that engine cooling is least effective at ___ power settings and ___ airspeeds, where a limited amount of air enters the engine cowling.

A

high, low

86
Q

Keeping the ___ flaps closed helps maintain engine temps during the descent.

A

Cowl

87
Q

During a descent, your job is to maintain stable cylinder head temps (CHT) and oil tmeps. On some airplanes, ___ entensoin or even ___ extension at high speeds can be used in lieu of large power reductions to start a descent (check your POH)

A

gear, partial flap

88
Q

In an airplane with a fixed pitch prop, one lever, the ___ controls both power and propeller blade RPM.

A

Throttle

89
Q

As you move up into higher performance airplanes you encounter constant speed (controllable pitch) propellers. Airplanes with these propellers usually have both a ___ and a/an ___ control, so you manage engine power and propeller RPM separately.

A

throttle, propeller

90
Q

What is an advantage of a constant speed propeller?

A

It permits the pilot to select the blade angle for the most efficient performance

91
Q

On airplanes with constant speed propellers, movement of the ___ determines the amount of fuel and air reaching the cylinders.

A

throttle

92
Q

Simply stated, the ___ determines how much power the engine can develop.

A

throttle

93
Q

Movement of the propeller control changes the propeller’s…

A

pitch

94
Q

On an airplane with a constant speed propeller, the ___ determines engine power while the ___ determines how efficiently that power is used

A

throttle, propeller’s pitch

95
Q

Forward movement of the propeller control causes both havlves of the propeller to rotate about their axes and attack the wind at a ___ angle

A

smaller

96
Q

Pulling the propeller control rearward causes the propeller to attack the wind at a ___ angle of attack

A

larger

97
Q

On an airplane with a constant speed propeller, the ___ tells you how fast the propeller spins (its RPM), and the manifold pressure gauge gives you an approximate measure of engine ___

A

tachometer, power

98
Q

Opening the throttle slightly causes an increase in ___ pressure. More air and fuel are drawn inside the engine, and power ___. Eventually, as the throttle is fully opened, the pressure downstream of the throttle valve approaches that of the ___

A

Manifold, increases, atmostphere

99
Q

Under normal conditions ( assuming a non-turbocharged engine), the engine’s manifold pressure can’t rise above ___ pressure

A

atmospheric

100
Q

As a non-turbocharged airplane climbs, you’ll notice the manifold pressure gauge shows ___ even though the throttle is fulled opened

A

a decrease

101
Q

Why have a propeller that can change its pitch in flight in the first place?

A

Airplanes with controllable pitch propellers can select the optimum angle of attack for climb and cruise.

102
Q

Engine power is dependent on RPM. For an engine to develop its maximum power, it must be operated at its ___ allowable RPM. At any lower RPM the engine develops only a fraction of its total horsepower. That’s why on takeoff we want the propeller set to its ___ pitch (highest RPM) position.

A

Highest, Lowest

103
Q

During cruise flight, is it necessary to always fly with maximum power and maximum RPM?

A

NO!!

104
Q

Controllable pitch propellers on GA airplanes are of the constant speed variety. Once the RPM is established, changes in manifold pressure (by moving the throttle) ___ affect engine speed.

A

won’t

105
Q

When you want to increase both the manifold pressure and RPM, change the ___ first, then increase the ___.

A

RPM, manifold pressure

106
Q

A precaution for the operation of an engine equipped with a constant speed propeller is to…

A

avoid high manifold pressure setting with low RPM

107
Q

Follow the same philosophy when decreasing manifold pressure and RPM. Pull the ___ back first, followed by the ___.

A

Throttle, propeller contorl

108
Q

Be aware that the propeller governor starts working only when the engine is operating above a specific ___ and not below

A

RPM

109
Q

Detonation occurs in a reciprocating aircraft engine when…

A

the unburned charge in the cylinders explodes instead of burning normally

110
Q

Which would most likely cause the cylinder head temp and engine oil temp gauges to exceed their normal operating ranges?

A

Using fuel that has a lower-than-specified fuel rating

111
Q

If a pilot suspects that an airplane engine with a fixed-pitch propeller is detonating during climbout after takeoff, the initial corrective action to take would be to …

A

lower the nose slightly to increase airspeed

112
Q

If the grade of fuel used ina n aircraft engine is lower than specified for the engine, it will most likely cause…

A

detonation

113
Q

The uncontrolled firing of the fuel/air charge in advance of normal spark ignition is known as …

A

preignition

114
Q

Preignition causes peak pressures within the cylinder to occur before the beginning of the ___ cycle.

A

power

115
Q

Fuel injection is a process in which fuel is directly ___ and ___ to each cylinder without the use of a carburetor.

A

metered, distributed

116
Q

The FCU (fuel control unit) regulates botht he volume of the ___ entering the engine and the quantity of ___ delivered to the FMU (fuel manifold unit).

A

air, fuel

117
Q

You can’t get carb ice in a fuel injection system for one very important reason: there is ___

A

no carburetor associated with this system

118
Q

With regard to carb ice, float-type caruretor systems in comparison to fuel injection systems are generally considered to be …

A

more susceptible to icing

119
Q

A major advantage of fuel injection is…

A

improved control of fuel-air ratio

120
Q

A major disadvantage of Fuel Injection is

A

contamination of dirt and water can more easily affect fuel injected engines due to the small orifices of injector nozzles.

121
Q

Airplanes with turbochargers are able to produce___ power at high altitudes

A

sea level

122
Q

Turbocharging compresses air into the intake manifold by utilizing the normally unused ___ exiting the engine.

A

exhaust gases

123
Q

The ___ valve closes (either automatically or manually, depending on your airplane) allowing more ___ to flow over the turbine. This spins the ___, allowing compressed air to be pumped into the induction system.

A

Wastegate, exhaust, compressor

124
Q

Pressurizing an airplane allows you to fly at very high altitudes while remaining in a cabin environment with near ___ pressures. This is accomplished by directing ___ air from the ___ (or from an auxiliary compressor) into the cabin.

A

Sea-level, compressed, turbocharger

125
Q

Temps drop as much as ___ within the carburetor’s throat are not uncommon.

A

70 degrees

126
Q

Your carburetor is a fine ice maker. Because of the considerable drop in temp caused by the atomization and evaporation of fuel, any ___ present can and will freeze.

A

Moisture

127
Q

Be prepared for carburetor ice to form at almost any outside air temp, though it’s most likely to occur between outside temps of ___.

A

20 degrees to 70 degrees.

128
Q

Impact ice occurs when ___ ___ is present and. The tide air temp (OAT) is at or below freezing

A

Visible moisture

129
Q

When is it possible to have an air filter freeze o

Ver while nowhere near a cloud?

A

If the air is moist and temps are low, water can accumulate on the air filter’s membrane and freeze.

130
Q

Another occasion where impact ice is likely is during ___.

A

Freezing rain

131
Q

If your air filter ever becomes clogged by impact ice, you have a remedy at hand. It’s called the ___ control.

A

Carb heat

132
Q

Fuel ice forms ___ of the main discharge nozzle.

A

Downstream

133
Q

Which condition is post favorable for the development of carb icing?

A

Temps between 29 degrees and 70 degrees and high humidity

134
Q

Fuel ice can occur at outside air temps as high as ___ and at humidities as low as ___.

A

85 degrees F, 50%

135
Q

Throttle ice forms on the ___ side if

The throttle valve. It is more likely to occur when the throttle is in a ___ position.

A

Rear, partially open

136
Q

Pulling the carburetor heat lever allows heated air to enter the carburetor, raising the air temperature within it’s throat as much as ___

A

90 degrees

137
Q

If an aircraft is equipped with a fixed pitch propeller and a float-type carburetor, the first indication of carburetor ice wo uld most likely be ___

A

Loss of RPM

138
Q

THe presence of carb ice in an aircraft equipped with a fixed pitch propeller can be verified by applying carb heat and noting ___

A

A further decrease in RPM and then a gradual increase in RPM

139
Q

Generally speaking, the use of carb heat tends to …

A

Decrease engine performance

140
Q

Applying carb heat will …

A

Enrich the fuel/air mixture

141
Q

What change occurs in the fuel/air mixture when carb heat is applied?

A

The fuel/air mixture becomes richer

142
Q

A carburetor air temperature gauge allows you to identify the ___ temperature range where carb ice is most likely to occur.

A

Critical

143
Q

All engines ___ have the same carb icing potential.

A

Do not

144
Q

Pulling out (toward you) on the mixture control ___ the amount of fuel given amount of air entering the engine.

A

Decreases

145
Q

With an increase in altitude the air becomes t hinder and doesn’t ___ as much for a given volume.

A

Weigh

146
Q

The basic purpose of adjusting the fuel/air moisture at altitude is to …

A

Decrease the fuel flow in order to compensate for decreased air density

147
Q

Most engine manufacturers recommend leaning the mixture whenever you’re operating at or below ___ of the engine’s maximum power output (check your POH to be sure)

A

75%

148
Q

How might you estimate that you’re operating at power levels greater than 75% in a non-turbocharged engine?

A

If the airplane is operating with full throttle at less than 5000 feet MSL.

149
Q

Remember, failure to lean appropriately means you’ll use up ___ portion of fuel unnecessarily.

A

An extra

150
Q

Airplanes with fixed pitch propellers (propellers having one pitch that can’t be changed in flight) and float-type carburetor a can be leaned by reference to the …

A

Tachometer

151
Q

While leaning with reference to the tachometer, the RPM peaks. This means that you are at the fuel-air ratio that produces maximum ___ for a given air density and throttle setting.

A

Power

152
Q

A mixture that is too rich causes engine …

A

Roughness

153
Q

A fouled spark plug in flight can sometimes be detected by …

A

An increase in Exhaust Gas Temp (EGT)

154
Q

An excessively rich mixture contributes to ___,___,___and ___.

A

A rough running engine, high fuel consumption, less range, smaller fuel reserves

155
Q

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?

A

Check the results obtained with a leaner setting of the mixture.

156
Q

The biggest danger with an excessively lean mixture is that it …

A

Burns hot

157
Q

Want is one procedure to aid in cooling an engine that is overheating?

A

Enriched the fuel mixture

158
Q

High cylinder head temperatures also lead to something known as …

A

Detonation

159
Q

Wile 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?

A

The fuel/air intrude may become excessively lean.

160
Q

For best power (most useable power per unit of air), enrich the mixture until the temp ___. (Check your POH to ensure the proper procedure for your aircraft.)

A

Decreases 125 degrees F from peak EGT

161
Q

Water is the most frequent contaminant found in fuel. Water, weighing approximately ___ pounds per gallon, ___ than fuel which weighs approximately ___ pounds per gallon.

A

8, is heavier, 6