Systems Flashcards

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0
Q

What does the carburetor do?

A

The carburetor vaporizes liquid fuel into small particles and then mixes it with air. It measures the airflow and meters fuel accordingly.

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1
Q

What are 4 strokes that must occur in each cylinder of a typical 4 stroke engine in order for it to produce full power?

A

Intake - Fuel mixture is drawn into cylinder by downward stroke
Compression - Mixture is compressed by the upward stroke
Power - Spark ignites mixture forcing piston downward and producing power
Exhaust - Burned gases are pushed out of the cylinder by an upward stroke

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2
Q

How does Carb Heat work?

A

A Carb Heat valve controlled by the pilot allows unfiltered heated air from a shroud located around an exhaust riser or muffler to be directed to the induction air manifold prior to the carburetor.

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3
Q

What does the throttle do?

A

The throttle controls the amount of fuel/air charge entering the cylinders .

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4
Q

What does the mixture control do?

A

The mixture regulates the fuel-to-air ratio.

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5
Q

What is the purpose of a fuel tank vent?

A

Allows air to enter the fuel tank as fuel is consumed, preventing the formation of a vacuum inside the fuel tank

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6
Q

What color of dye does 80, 100, 100LL, and JetA have?

A

80 - Red
100 - Green
100LL - Blue
JetA - colorless

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7
Q

What is the purpose of a primer?

A

Engine Start. The primer draws fuel from the fuel strainer and injects it directly into the cylinder intake ports.

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8
Q

What are two kinds of oil?

A

Mineral - (non detergent oil) contains no additives. Usually used after an engine overhaul or when an aircraft engine is new… for engine break in purposes

Ashless dispersant - Mineral Oil with additives. Contains anti-wear properties along with multi-viscosity. Picks up contamination and carbon particles and keeps them suspended so that buildups and sludge do not form in the engine

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9
Q

What causes Carb Icing and what are the first indications?

A

Carb icing occurs when the vaporization of fuel, combined with the expansion of air as it passes through the carburetor, causes a sudden cooling of the mixture. The temperature of the air passing through the carburetor may drop as much as 60degrees F within a second. Water vapor is squeezed out by this cooling, and if the temperature is 32deg F or less, you will build up ice. The first indication is a loss of RPMs

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10
Q

How do you know when carburetor icing is gone?

A

After applying carb heat, you will see a loss in engine RPM, followed by a rise with engine roughness possible. When you turn carb ht off, your rpm should rise to the normal levels

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11
Q

What conditions are favorable for carburetor icing?

A

When temperatures are below 70 degrees (21C) and the relative humidity is above 80%.

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12
Q

What is detonation?

A

An uncontrolled, explosive ignition of the fuel/air mixture within the cylinder’s combustion chamber. Usually characterized by high CHTs and most likely to occur at high power settings

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13
Q

What are some common causes of detonation?

A

Using a fuel grade lower than specified by the aircraft manufacturer
Operating at high power settings with an excessively lean mixture
Operating with extremely high manifold pressure in conjunction with low RPM
Extended ground operations or steep climbs where cylinder cooling is reduced

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14
Q

What should you do if detonation is suspected?

A

reduce temperature and pressure of the fuel air charge

Reduce power, reduce climb rate, enrich the fuel/air mixture, open cowl flaps

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15
Q

What is pre-ignition?

A

When the fuel/air mixture ignites prior to the engine’s normal ignition event resulting in reduced engine power and high operating temperatures

16
Q

What should you do if you suspect pre-ignition?

A

Reduce Power, reduce the climb rate, enrich the fuel/air mixture, and open cowl flaps if available

17
Q

What instruments operate off the pitot/static system?

A

Altimeter, VSI, and ASI

18
Q

What is a limitation of the VSI?

A

6-9 second lag

19
Q

How does the Airspeed indicator work?

A

Measures the difference between impact pressure from the pitot head and undisturbed pressure from the static port. The difference is registered onn the face of the instrument

20
Q

What are different types of aircraft speeds?

A

IAS - Indicated - what you read from your ASI
CAS - Calibrated - airspeed indicator reading corrected for position and instrument errors.
EAS - Equivalent - reading corrected for position and instrument errors, and for adiabatic compressible flow for the particular altitude.
TAS - True - the speed of the airplane in relation to the air mass in which it is flying

21
Q

What are your gyroscopic instruments?

A
  • Turn Coordinator
  • Heading Indicator
  • Attitude Indicator
22
Q

What are 2 fundamental properties of a gyroscope?

A

1) Rigidity in space - a gyroscope remains in a fixed position in the plane in which it is spinning
2) Precession - The tilting of a gyro in response to a deflective force which occurs 90 degrees later in the direction of rotation

23
Q

What are some errors associated with the compass?

A

Oscillation Error - Erratic movement of the compass card caused by turbulence or rough control technique
Deviation Error - Due to electrical and magnetic disturbances in the aircraft
Variation Error - Angular difference between true and magnetic north; reference isogonic lines of variation
Dip Errors:
Northerly Turning Error - The compass leads in the south half of a turn, and lags in the north half of a turn
UNOS
Undershoot
North
Overshoot
South
Acceleration Errors - On E or W hdgs, while acceleration, the mag compass shows a turn to the north, and turn to S when decelerating
ANDS
Accelerate
North
Decelerate
South

24
Q

What does “High Oil Pressure” mean?

A

High Oil Pressure could lead to…

  • seals/oil lines could blow
  • loss of oil
  • Problem could be caused by pump
25
Q

What does “High Oil Temp” indicate?

A
  • Engine is hot
  • wears faster
  • could be loss of oil
  • possibly pump failure
26
Q

What is the significance of Va (Maneuvering Speed)?

A

Hitting turbulence (or an updraft) increases the angle of attack, thus increasing load factor. While flying below Va, the aircraft will stall before it breaks. Va increases with weight because the Angle of Attack is higher with added weight, thus increasing stall speed. An aircraft can over-stress the wings before stalling if flying above Va.