Lesson 1 Flashcards

1
Q

is vital to maintain the safe and efficient operation of the aeroplane engines and their associated systems. It varies according to the type of engines fitted (e.g. piston, turboprop, or gas turbine), and in many cases the individual instruments are identical.

A

Instrumentation

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2
Q

A heat engine that uses one or more reciprocating pistons to convert pressure into a rotating motion.

A

PISTON ENGINES

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3
Q

It uses a piston that moves up and down inside the cylinder.

A

PISTON ENGINES

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4
Q

This is a measure of how much work is being done by the engine and is measured in revolutions per minute (rpm).

A

Engine Speed or (TACHOMETER)

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5
Q

This is a measure of the engine power of a supercharged engine (absolute pressure).

A

Induction Manifold Pressure, or Boost Pressure (MAP)

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6
Q

is usually given in inches of mercury (in Hg), and boost is normally measured in pounds per square inch (psi).

A

MAP or Manifold Air Pressure

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7
Q

more on suction

A

BOOST PRESSURE GAUGE

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8
Q

inside pressure

A

MAP or Manifold Air Pressure

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9
Q

Super charged engine is designed for an aircraft that flies up to [?] feet above sea level.

A

10, 000 feet

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10
Q

Acts on the output shaft of the engine and is proportional to the horsepower developed. It is occasionally used to provide information for power control.

A

Torque or Turning Moment

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11
Q

means the rotation of the shaft of the engine.

A

TORQUE

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12
Q

Helps in monitoring the condition of the reduction gears (set of gears that control the rotation of the propeller and the crankshaft).

A

TORQUE

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13
Q

This temperature is important because excessive temperatures can cause engine damage.

A

Cylinder Head Temperature

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14
Q

The temperature is measured in degrees Celsius.(°C).

A

Cylinder Head Temperature

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15
Q

When the pointer exceeds to the [?], it means the engine has a malfunction that causes overheating and can damage other components.

A

red line

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16
Q

Cylinder Head Temperature uses a [?] sensor then sends the signal to the instrument.

A

thermocouple

17
Q

Ensures adequate lubrication of the engine. In pressure terms it may be HIGH or LOW, whereas the temperature is usually in degrees Celsius (°C).

A

Lubricating Oil Pressure and Temperature

18
Q

is very important in engine operation for its purpose (cooling, lubrication and cleaning).

A

OIL

19
Q

Purpose of Oil

A

cooling
lubrication
cleaning

20
Q

When the temperature gauge is too high and the pressure is low it indicates [?] of the engine.

A

OVERHEATING

21
Q

Provides a measure of the economy of the engine, and is measured in pounds, kilograms or gallons/hour.

A

Fuel Flow

22
Q

indicates when there is a blockage or leakage on the fuel lines going to the engine.

A

FUEL FLOW

23
Q

When the fuel flow shows a higher indication than the normal amount it may show that there is a [?].

A

leakage

24
Q

Then when it drops it means there is something that [?] the fuel to flow on the engine.

A

blocking

25
Q

Shows if the aircraft alternator is charging during normal operation. If continuous discharge is shown during flight, it is prudent to land as soon as possible as it would suggest that the battery will shortly become too depleted to operate normal aircraft.

A

Ammeter

26
Q

Monitors the condition of the vacuum system which is driven from the engine.

A

Vacuum Gauge

27
Q

The [?] drives the gyros for the artificial horizon and heading indicator instruments.

A

vacuum system