Aircraft Systems Flashcards

(47 cards)

1
Q

3357- Should it. became necessary to hand prop an airplane engine, it is extremely important that a competent pilot

A

Be at the controls of the airplane

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2
Q

3356- What should be the first action after starting an airplane engine

A

Adjust for proper RPM and check desired indications on engine gauges

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3
Q

3651-1- What is one purpose for using reciprocating engines

A

The are relatively simple and easy to operate

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4
Q

3223- One purpose of the duel ignition system on an aircraft engine is to provide for

A

Improved engine performance

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5
Q

3223-1- An electrical system failure occurs during flight. In this situation, you would

A

Experience avionics equipment failure

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6
Q

3223-2- If the. ground wire between the magneto and the ignition system gets disconnected, the most noticeable result would be that the engine

A

Cannot be shut down by turning the. switch into the off position

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7
Q

2242- One purpose of the duel ignition system on a two cycle engine is to provide for

A

System redundancy in the ignition system

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8
Q

2238- An electrical system failure occurs in a magneto equipped aircraft during flight. In this situation you would

A

Experience avionics equipment failure

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9
Q

2364- Concerning the advantages of an aircraft generator or alternator, select the true statement

A

An alternator provides more electrical power at lower RPM than a generator

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10
Q

3225- The operating principal of float type carburetors is based on the

A

difference in air pressure between the Venturi throat and the air inlet

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11
Q

3226- The basic purpose of adjusting the fuel/air mixture at altitude is to

A

decrease fuel flow to compensate for decreased air density

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12
Q

3228- While cruising at 9,500MSL, the fuel air mixture properly adjusted. What will occur if a decent to 4,500MSL is made without readjusting the mixture

A

The fuel/air mixture may become excessively lean

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13
Q

3227- During the run up at high elevation airport, a pilot notices a slight 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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14
Q

3231- If an airplane is equipped with a fixed pitch propellor and a float type carburetor, the first indication of carb ice would be

A

loss of RPM

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15
Q

3229- Which condition is most favorable to carburetor icing

A

temp between 20-70F with high humidity

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16
Q

3230- Carburetor icing can occur with an OAT as high as

A

20C and high relative humidity

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17
Q

3232- Applying carburetor heat will

A

enrich the fuel/air mixture

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18
Q

3233- What change occurs in the fuel/air mixture when carburetor heat is applied

A

The fuel/air mixture is enriched

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19
Q

3234- Generally speaking, the use of carburetor heat tends to

A

decrease engine performance

20
Q

3236- With regard to carburetor ice, float type carburetors in comparison to fuel injection systems are generally considered to be

A

more susceptible to icing

21
Q

3241- Which condition is most favorable to carb ice

A

Temp between 20-70F

22
Q

3224- On aircraft equipped with fuel pumps, when is the aux fuel pump used

A

In the even the engine driven fuel pump fails

23
Q

3237- If the ride of fuel used in an aircraft engine is lower then specified for the engine, it will mostly likely cause

24
Q

3238- Detonation may soccer at high power setting when

A

the fuel air mixture ignites instantaneously

25
3238-1- Detonation occurs in a reciprocating aircraft engine when
The unburned charge in the cylinders explodes instead of burning instantly
26
3240- The uncontrolled firing of the fuel/air charge in advance if normal spark ignition is known as
pre-ignition
27
3242- What type of fuel can be substituted for an aircraft if the recommended octane is not available
The next highest octane aviation gas
28
3243- Filling the fuel tanks after the last flight of the day is considered good operating procedure because this will
Prevent moisture condensation by eliminating airspace in the tanks
29
3243-1- To properly purge water from the fuel system of an aircraft equipped with tank sumps and a fuel strainer quick drain, it is necessary to drain the fuel from
fuel strainer drain and the fuel tank sumps
30
2353- During preflight in cold weather, crankcase breather lines should receive special attention because they are susceptible to being clogged by
Ice from crankcase vapors that have condensed and subsequently frozen
31
3239- If the pilot suspects that the engine (with a fixed pitched propeller) is detonating during climb out after takeoff, the initial corrective action would be to
Lower nose slightly to increase airspeed
32
3221- Excessively high engine temperatures will
Cause loss of power, excessive oil consumption, and possible permanent internal engine damage
33
3221-1- Excessively high engine temperatures, either in the air or on the ground, will
Cause loss of power, excessive oil consumption, and possible permanent internal engine damage
34
3222- If the engine oil temperature and cylinder head temperature gauges have exceeded their normal operating range, the pilot may have been operating with
too much power and with the mixture set too lean
35
3241- 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
36
3244- For internal cooling, reciprocating engines are especially dependent on
The circulation of lubricating oil
37
2354- Which is true regarding preheating an aircraft during cold weather operations
The cabin area as well as the engine should be preheated
38
3245- An abnormally high engine oil temperature indication may be caused by
The oil level being too low
39
3651- What action can a pilot take to aid in cooling an engine that is overheating during a climb
Reduce climb and increase airspeed
40
3652- What is one procedure to aid in an engine that is overheating
Enrichen fuel mixture
41
3711- The most important rule to remember in the event of a power failure after becoming airborne is
immediately establish proper gliding attitude and airspeed
42
3653- 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 regulates RPM
43
3654- What is an advantage of a constant speed propeller
Permits the pilot to select the blade angle for the most efficient performance
44
3655- A precaution for the operation of an engine equipped with a constant-speed propeller is to
Avoid high manifold pressure settings with low RPM
45
3207- In what flight condition is torque effect the greatest in a single engine airplane
low airspeed, high power, high angle of attack
46
3208- The let turning tendency of an airplane caused by P-factor is the result of the
Propeller blade descending to the right, producing more thrust than the ascending blade on the left
47
When does P-factor cause the airplane to turn to the left
When at high angles of attack.