Aircraft Systems Flashcards

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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

A

detonation

24
Q

3238- Detonation may soccer at high power setting when

A

the fuel air mixture ignites instantaneously

25
Q

3238-1- Detonation occurs in a reciprocating aircraft engine when

A

The unburned charge in the cylinders explodes instead of burning instantly

26
Q

3240- The uncontrolled firing of the fuel/air charge in advance if normal spark ignition is known as

A

pre-ignition

27
Q

3242- What type of fuel can be substituted for an aircraft if the recommended octane is not available

A

The next highest octane aviation gas

28
Q

3243- Filling the fuel tanks after the last flight of the day is considered good operating procedure because this will

A

Prevent moisture condensation by eliminating airspace in the tanks

29
Q

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

A

fuel strainer drain and the fuel tank sumps

30
Q

2353- During preflight in cold weather, crankcase breather lines should receive special attention because they are susceptible to being clogged by

A

Ice from crankcase vapors that have condensed and subsequently frozen

31
Q

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

A

Lower nose slightly to increase airspeed

32
Q

3221- Excessively high engine temperatures will

A

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

33
Q

3221-1- Excessively high engine temperatures, either in the air or on the ground, will

A

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

34
Q

3222- If the engine oil temperature and cylinder head temperature gauges have exceeded their normal operating range, the pilot may have been operating with

A

too much power and with the mixture set too lean

35
Q

3241- Which would most likely cause the cylinder head temperature and engine oil temperature gauges to exceed their normal operating ranges

A

Using fuel that has a lower than specified fuel rating

36
Q

3244- For internal cooling, reciprocating engines are especially dependent on

A

The circulation of lubricating oil

37
Q

2354- Which is true regarding preheating an aircraft during cold weather operations

A

The cabin area as well as the engine should be preheated

38
Q

3245- An abnormally high engine oil temperature indication may be caused by

A

The oil level being too low

39
Q

3651- What action can a pilot take to aid in cooling an engine that is overheating during a climb

A

Reduce climb and increase airspeed

40
Q

3652- What is one procedure to aid in an engine that is overheating

A

Enrichen fuel mixture

41
Q

3711- The most important rule to remember in the event of a power failure after becoming airborne is

A

immediately establish proper gliding attitude and airspeed

42
Q

3653- How is engine operation controlled on an engine equipped with a constant speed propeller

A

The throttle controls power output as registered on the manifold pressure gauge and the propeller regulates RPM

43
Q

3654- What is an advantage of a constant speed propeller

A

Permits the pilot to select the blade angle for the most efficient performance

44
Q

3655- A precaution for the operation of an engine equipped with a constant-speed propeller is to

A

Avoid high manifold pressure settings with low RPM

45
Q

3207- In what flight condition is torque effect the greatest in a single engine airplane

A

low airspeed, high power, high angle of attack

46
Q

3208- The let turning tendency of an airplane caused by P-factor is the result of the

A

Propeller blade descending to the right, producing more thrust than the ascending blade on the left

47
Q

When does P-factor cause the airplane to turn to the left

A

When at high angles of attack.