Powerplant Review Flashcards

1
Q

The general requirements for an aircraft engine include efficiency, reliability, and a low weight-to-horsepower ratio. It also must?
A. have a short time between overhauls, easy access for maintenance, and a wide range of power output at various speeds and altitudes.
B. have good fuel economy, high durability, and be capable of sustained high power output.
C. be compact, efficient, and have a narrow range of power output at a specific speed.

A

B. have good fuel economy, high durability, and be capable of sustained high power output.

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2
Q

The heat engine used predominantly in aviation is the?
A. Radial engine.
B. O-type engine.
C. V-type engine.

A

B. O-type engine

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3
Q

The crankcase of an aircraft engine?
A. houses the valve operating mechanism and the engine cylinders.
B. is lightweight and primarily used as a reservoir for the engine oil.
C. is the foundation of the engine containing crankshaft bearings and cylinder pads

A

C. is the foundation of the engine containing crankshaft bearings and cylinder pads

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4
Q

The cylinders of an aircraft engine are mounted on cylinder pads that are machined onto the crankcase. The common method of attachment of the cylinders to the crankcase is?
A. by studs mounted in threaded holes in the crankcase.
B. by bolts into locking helicoils mounted in the crankcase.
C. by heating the crankcase and cooling the cylinder for an interference fit

A

A. by studs mounted in threaded holes in the crankcase

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5
Q

The crankpin is?
A. used to ensure the crankshaft does not shift in the crankcase.
B. a solid, heavy journal to withstand crankshaft shock loads.
C. hardened by nitriding and is hollow to reduce weight.

A

C. hardened by nitriding and is hollow to reduce weight.

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6
Q

Which statement is correct about radial engine crankshafts?
A. Moveable counterweights serve to reduce the torsional vibrations in an aircraft reciprocating engine.
B. Moveable counterweights serve to reduce the dynamic vibrations in an aircraft reciprocating engine.
C. Moveable counterweights are designed to resonate at the natural frequency of the crankshaft.

A

B. Moveable counterweights serve to reduce the dynamic vibrations in an aircraft reciprocating engine.

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7
Q

What is an advantage of using metallic sodium filled exhaust valves in aircraft reciprocating engines?
A. increased strength and resistance to cracking.
B. reduced valve operating temperature.
C. greater resistance to deterioration at high valve temperature.

A

B. reduced valve operating temperature.

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8
Q

The horsepower developed in the cylinders of a reciprocating engine is known as the?
A. shaft horsepower.
B. indicated horsepower.
C. brake horsepower.

A

B. indicated horsepower.

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9
Q

What are the two functional elements of the centrifugal flow compressor?
A. turbine and compressor
B. bucket and expander
C. impeller and diffuser

A

C. impeller and diffuser

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10
Q

What is the primary advantage of an axial-flow compressor over a centrifugal flow compressor?
A. high frontal area
B. less expensive
C. greater pressure ratio

A

C. greater pressure ratio

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11
Q

On a carburetor without an automatic mixture control, as you ascend to altitude, the mixture will
A. be enriched.
B. be leaned.
C. is not affected.

A

A. be enriched.

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12
Q

Fuel is discharged for idling speeds on a float-type carburetor?
A. from the idle discharge nozzle.
B. in the venturi.
C. through the idle discharge air bleed.

A

A. from the idle discharge nozzle.

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13
Q

The continuous-flow fuel injection system injects fuel into the intake port during which stroke?
A. intake stroke
B. intake and compression stroke
C. all strokes

A

C. all strokes

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14
Q

When a new carburetor is installed on an engine?
A. warm up the engine and adjust the float level.
B. do not adjust the idle mixture setting; this was accomplished on the flow bench.
C. and the engine is warmed up to normal operating temperature, adjust the idle mixture and then the idle speed.

A

C. and the engine is warmed up to normal operating temperature, adjust the idle mixture and then the idle speed.

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15
Q

It is necessary to control acceleration and deceleration rates in turbine engines in order to?
A. prevent blowout or die-out.
B. prevent over-temperature.
C. prevent friction between turbine wheels and the case due to expansion and contraction.

A

A. prevent blowout or die-out.

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16
Q

In a supervisory electronic engine control EEC, any fault in the EEC that adversely affects engine operation?
A. causes redundant back-up systems to take over and continue normal operation.
B. usually degrades performance to the extent that continued operation can cause damage to the engine.
C. causes an immediate reversion to control by the hydromechanical fuel control unit.

A

C. causes an immediate reversion to control by the hydromechanical fuel control unit.

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17
Q

When trimming a turbine engine, the fuel control is adjusted to?
A. produce as much power as the engine is capable of producing.
B. set idle RPM and maximum speed or EPR.
C. allow the engine to produce maximum RPM without regard to power output.

A

B. set idle RPM and maximum speed or EPR.

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18
Q

Hot spots can burn a hole in the combustion section liner on a turbine engine.
This is caused by?

A. a misaligned fuel nozzle resulting in a flame that is not centered in the flame area.
В. insufficient fuel flow to the fuel nozzles.
C. excessive fuel flow to the fuel nozzle which cannot be fully combusted.

A

A. a misaligned fuel nozzle resulting in a flame that is not centered in the flame area.

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19
Q

The use of carburetor heat when it is not needed causes?
A. a very lean mixture.
B. excessive increase in manifold pressure.
C. a decrease in power and possible detonation.

A

C. a decrease in power and possible detonation.

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20
Q

Ground boosted engine manifold pressure is generally considered to be any manifold pressure above?
A. 14.7 inches Hg.
B. 50 inches Hg.
C. 30 inches Hg.

A

C. 30 inches Hg.

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21
Q

An indication of unregulated power changes that result in continuous drift of manifold pressure indication on a turbocharged aircraft engine is known as?
A. overshoot.
B, waste gate fluctuation.
C. bootstrapping.

A

C. bootstrapping.

22
Q

The purpose of the engine inlet on a turbine engine is to?
A. provide a well-mixed volume of air to the inlet of the compressor.
B. provide a uniform and steady airflow to avoid compressor stall.
C. reduce the speed of the incoming air and direct it at the correct angle toward the compressor blades.

A

B. provide a uniform and steady airflow to avoid compressor stall.

23
Q

All of the following are recommended markers for reciprocating engine exhaust systems except?
A. Indian ink.
B. lead pencil.
C. white chalk.

A

B. lead pencil.

24
Q

The purpose of cascade vanes in a thrust reversing system is to?
A. form a solid blocking door in the jet exhaust path.
B. turn the exhaust gases forward just after exiting the exhaust nozzle.
C. turn to a forward direction the fan airstream.

A

C. turn to a forward direction the fan airstream.

25
Q

Which components make up the magnetic system of a magneto?
A. pole shoes, the pole shoe extensions, and the primary coil
B. primary and Secondary coils
C. rotating magnet, the pole shoes, the pole shoe extensions, and the coil core.

A

C. rotating magnet, the pole shoes, the pole shoe extensions, and the coil core.

26
Q

What is the approximate position of the rotating magnet in a high-tension magneto when the points first close?
A. full register
B. neutral
C. a few degrees after neutral

A

A. full register

27
Q

What is the relationship between the distributor and crankshaft speed of aircraft reciprocating engines?
A. The distributor turns at one-half crankshaft speed.
B. The distributor turns at one and one half crankshaft speed.
C. The crankshaft turns at one-half distributor speed.

A

A. The distributor turns at one-half crankshaft speed.

28
Q

How does the high tension ignition shielding tend to reduce radio interference?
A. Prevents ignition flashover at high altitudes.
B. Reduces voltage drop in the transmission of high-tension current.
C. Receives and grounds high frequency waves coming from the magneto and high-tension ignition leads.

A

C. Receives and grounds high frequency waves coming from the magneto and high-tension ignition leads.

29
Q

When the switch is off in a magneto ignition system, the primary circuit is?
A. grounded.
B. opened.
C. shorted.

A

A. grounded.

30
Q

What is the purpose of an impulse coupling with a magneto?
A. to absorb impulse vibrations between the magneto and the engine.
B. to compensate for backlash in the magneto and the engine gears.
C. to produce a momentary high rotational speed of the magneto.

A

C. to produce a momentary high rotational speed of the magneto.

31
Q

When internally timing a magneto, the breaker points begin to open when?
A. the piston has just past TDC at the end of the compression stroke.
B. the magnet poles are a few degrees beyond the neutral position.
C. the magnet poles are fully aligned with the pole shoes.

A

B. the magnet poles are a few degrees beyond the neutral position.

32
Q

If the ignition switch is moved from BOTH to either LEFT or RIGHT during an engine ground check, normal operation is usually indicated by a?
A. large drop in RPM.
B. momentary interruption of both ignition systems.
C. slight drop in RPM.

A

C. slight drop in RPM.

33
Q

Generally, starter brushes should be replaced when they are approximately?
A. one-half their original length.
B. one-third their original length.
C. two-thirds their original length.

A

A. one-half their original length.

34
Q

Which of the following factors helps determine the proper grade of oil to use in a particular engine?
A. adequate lubrication in various attitudes of flight
B. positive introduction of oil to the bearings
C. operating speeds of bearings

A

C. operating speeds of bearings

35
Q

The type of oil pump most commonly used on turbine powered engines are classified as?
A. positive displacement.
B. variable displacement.
C. constant speed.

A

A. positive displacement.

36
Q

During ground operation of an engine, the cowl flaps should be in what position?
A. fully closed
B. fully open
C. opened according to ambient conditions

A

B. fully open

37
Q

The actual distance a propeller moves forward through the air during one revolution is known as the?
A. effective pitch.
B. geometric pitch
C. relative pitch.

A

A. effective pitch.

38
Q

How does the aerodynamic twisting force affect operating propeller blades?
A. It tends to turn the blades to a high blade angle.
B. It tends to bend the blades forward.
C. It tends to turn the blades to a low blade angle.

A

A. It tends to turn the blades to a high blade angle.

39
Q

How do small feathering propellers prevent feathering when the engine is shut down?
A. Latches lock the propeller in low pitch to prevent excess load on the engine at start-up.
B. Oil pressure is held against the pitch change mechanism.
C. Aerodynamic twisting moment prevents feathering.

A

A. Latches lock the propeller in low pitch to prevent excess load on the engine at start-up.

40
Q

When the centrifugal force acting on the propeller governor flyweights overcomes the tension on the speeder spring, a propeller is in what speed condition?
A. on speed
B. under-speed
C. over-speed

A

C. over-speed

41
Q

Constant speed non-feathering McCauley, Hartzell, and other propellers of similar design without counterweights increase pitch angle using?
A. oil pressure.
B. spring pressure.
C. centrifugal twisting moment.

A

A. oil pressure.

42
Q

When lubricating a Hartzell propeller blade with grease, to prevent damage to the blade seals, the service manual may recommend on some models?
A. to pump grease into both zerk fittings for the blade simultaneously.
B. remove the seals prior to greasing and reinstall them afterwards.
C. remove one of the two zerk fittings for the blade and grease the blade through the remaining fitting.

A

C. remove one of the two zerk fittings for the blade and grease the blade through the remaining fitting.

43
Q

A ground incident that results in propeller sudden stoppage may require a crankshaft run-out inspection. What publication would be used to obtain crankshaft run-out tolerance?
A. current manufacturer’s maintenance instructions
B. type certificate data sheet
C. AC43.13-1A Acceptable Methods, Techniques, and Practices Aircraft Inspection and Repair

A

A. current manufacturer’s maintenance instructions

44
Q

A QECA (quick-engine-change-assembly) is?
A. used mostly for unscheduled, unexpected engine changes.
B. used whenever the most efficient and expeditious replacement of an aircraft engine is relied upon.
C. must be pre-approved by the administrator or an airframe and powerplant mechanic with inspection authorization.

A

B. used whenever the most efficient and expeditious replacement of an aircraft engine is relied upon.

45
Q

When mounting a replacement engine, always?
A. install AN bolts of the correct diameter and length while the weight of the engine is still on the engine hoist.
B. secure the engine first with starter bolts, remove the engine hoist and replace the starter bolts with the manufacturer’s specified bolts.
C. Install the manufacturer specified bolts and torque to the manufacturer recommended value.

A

C. Install the manufacturer specified bolts and torque to the manufacturer recommended value.

46
Q

Which of the following fire detection systems measure temperature rise compared to a reference temperature?
A. thermocouple
B. thermal switch
C. lindberg continuous element

A

A. thermocouple

47
Q

What is the principle of operation of the continuous loop fire detection system sensor?
A. fuse material which melts at high temperatures
B. core resistance material which prevents current flow at normal temperatures
C. a bimetallic thermo-switch which closes when heated to a high temperature

A

B. core resistance material which prevents current flow at normal temperatures

48
Q

Which of the following is the safest fire-extinguishing agent to use from a standpoint of toxicity and corrosion hazards?
A. dibromodiflouromethane (Halon 1202)
B. bromochlorodiflouromethane (Halon 1211)
C. bromotriflouromethane (Halon 1301)

A

C. bromotriflouromethane (Halon 1301)

49
Q

In a fixed fire-extinguishing system, there are two small lines running from the system and exiting overboard. The line exit ports are covered with a blowout type indicator disc. Which of the following statements is true?
A. When the red indicator is missing, it indicates the fire- extinguishing system has been normally discharged
B. When the yellow indicator disc is missing, it indicates the fire-extinguishing system has been normally discharged.
C. When the green indicator disc is missing, it indicates the fire-extinguishing system has had a thermal discharge.

A

B. When the yellow indicator disc is missing, it indicates the fire-extinguishing system has been normally discharged.

50
Q

During overhaul, reciprocating engine exhaust valves are checked for stretch?
A. with a suitable inside spring caliper.
B. using a manufacturer’s contour or radius gauge or by the stem diameter just behind the head.
C. by placing on a surface plate and measuring its length with a height gauge.

A

B. using a manufacturer’s contour or radius gauge or by the stem diameter just behind the head.