AMT 220 ENGINE INSTRUMENTS SYSTEM Flashcards

1
Q

System continuously monitors and controls ignition timing, fuel injection timing, and fuel-to-air ratio mixture

A

Full Authority Digital Engine Control

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2
Q

does not require magnetos and eliminates the need for manual fuel/air mixture control.

A

FADEC equipped engine

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3
Q

Is a type of electronic control unit that controls a series of actuators on an internal combustion engine to ensure optimal engine performance.

A

Two Electronic Control Units (ECUs)

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4
Q

Panel is a system to alert operators of alarm conditions in the plant.In one common alarm sequence, the light in a window will flash and a bell or horn will sound to attract the operator’s attention when the alarm condition is detected.

A

Health Status Annunciator (HSA)

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5
Q

By receiving multiple input variables of the current flight condition including air density, throttle lever position, engine temperatures, engine pressures, and many other parameters.

A

FADEC Sensor set

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6
Q

-Are used mainly on select high-performance aircraft that have anti-skid braking systems.

A

Speed Sensor Assembly (SSA)

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7
Q

The dual-purpose is to compare the speed of one wheel to the other wheels and to measure the speed of the wheel after a touchdown in order to activate the anti-skid system.

A

Speed Sensor Assembly (SSA)

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8
Q

Comparing one wheel rotational speed to another wheel helps to identify a skid condition.

A

Speed Sensor Assembly (SSA)

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8
Q

It is also good to have an hour meter/tachometer so you will know if your engine is running at peak output and when maintenance is required.

A

Cylinder Head Temperature (CHT)

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8
Q
  • Is an essential tool used to monitor the running temperature and health of a (2) stroke engine.
A

Cylinder Head Temperature (CHT)

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9
Q

-Is a measurement of the temperature of the exhaust gases at the exhaust manifold.

A

Exhaust Gas Temperature (EGT)

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10
Q

As the temperature of the exhaust gas varies with the ratio of fuel to air entering the cylinders, it can be used as a basis for regulating the fuel/air mixture entering the engine.

A

Exhaust Gas Temperature (EGT)

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11
Q

-Sensor is a key sensor because it senses engine load.

A

Manifold Air Pressure (MAP)

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12
Q

generates a signal that is proportional to the amount of vacuum in the intake manifold.

A

Manifold Air Pressure (MAP): sensor

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13
Q

then uses this information to adjust ignition timing and fuel enrichment.

A

Manifold Air Pressure (MAP): engine computer

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14
Q
  • Sensor is usually mounted in the intake manifold so the tip will be exposed to air entering the engine.
A

Manifold Air Temperature (MAT)

15
Q

-Senses the amount of fuel in the fuel rail by reading the internal pressure of the rail.

A

Fuel Pressure Sensors

16
Q

-Controls the mass flow-rate of air (in fuel-injected engines) or air/fuel mixture (in carburetted engines) delivered to the cylinders.

A

Throttle Position Sensor

17
Q

Consist of high voltage harness and spark plugs

A

FADEC Ignition System

18
Q

Number of plugs per cylinder

A

2

19
Q

Employs a waste spark ignition system-plugs fire once on compression and once on exhaust

A

FADEC Ignition System

19
Q

fires top and bottom spark plugs for cylinders 1 & 2

A

ECU#1

20
Q

fires top and bottom spark plugs for cylinders 3 & 4

A

ECU#2

21
Q

fires top and bottom spark plugs for cylinders 3 & 4

A

ECU#2

22
Q

14v 60amp alternator and 12v 25Ah Lead Acid type battery (located aft baggage compartment)

A

Primary Power Supply

23
Q

12v 7Ah Lead Acid type battery

A

Secondary Power Source

24
Q

Have separate set of breakers and the power supply circuits are separated

A

PPS and SPS

25
Q

will illuminate HAS with PPWR FAIL or EBAT FAIL to alert pilot of possible power supply loss

A

Battery condition monitor