Aircraft Systems Part 1/2 Flashcards

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1
Q

Name 10 aircraft systems

A
Engine
Propeller
Induction
Ignition
Fuel
Lubrication
Cooling
Electrical
Landing Gear
Environmental Control
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2
Q

Most small aircraft are designed with what kind of engine?

A

Reciprocating engine (pistons move back and forth)

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3
Q

Name the two primary reciprocating engine designs (not types)

A
  • Spark ignition

- Compression ignition

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4
Q

Name the most popular reciprocating engine used on smaller aircraft

A

Opposed-Type engine (can be spark or compression ignition)

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5
Q

Most common engine type used in general aviation

A

Spark 4 stroke engine

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6
Q

Continuous operation of the engine depends on what auxiliary systems

A
  • Induction
  • Ignition
  • Fuel
  • Oil
  • Cooling
  • Exhaust
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7
Q

A propeller is a:

A

Rotating Airfoil

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8
Q

The amount of thrust a propeller produces depends on:

A
  • Shape of the airfoil
  • Angle of attack of the propeller blade
  • Revolutions per minute
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9
Q

Why is a propeller twisted?

A

To produce uniform lift. There is a difference in speed through out the blade.

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10
Q

Name two types of propellers

A

Fixed pitch vs adjustable pitch propellers

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11
Q

Name two types of fixed pitch propellers & describe them

A

Climb (less drag, higher rpm, more horsepower, decreased performance for cruising flight)

cruise propellers (more drag, less rpm, less horsepower, increased efficiency in cruising flight)

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12
Q

Name the indicator of engine power & how is it calibrated?

A

Tachometer - calibrated in hundreds of rpm

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13
Q

What does a tachometer indicate

A

engine power via engine and propeller rpm

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14
Q

What is the green arch on a tachometer?

A

maximum continuous operating rpm

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15
Q

How is rpm regulated?

A

Throttle - controls the fuel/airflow through the engine

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16
Q

What does engine power output depend on?

A

Air density (decreases as altitude increases)

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17
Q

What does a decrease in air density result in? When?

A

Decreased power output of the engine. As you increase in altitude

18
Q

How to you maintain the same rpm as you gain altitude?

A

Position of throttle must be changed

19
Q

Describe a constant-speed propeller

A
  • Pitch automatically varied during flight by a governor
  • Constant rpm despite varying air loads
  • Most common type of adjustable pitch propeller
  • more efficient
20
Q

Two controls for adjustable propeller aircraft:

A
  • Throttle (controls power output)

- Propeller control (regulates engine RPM)

21
Q

On an aircraft with a constant speed propeller, power output is controlled by:

A

The throttle and indicated by a manifold pressure gauge

22
Q

What does a manifold pressure gauge measure?

A

Measures absolute pressure of fuel-air inside intake manifold

23
Q

What does an induction system do?

A

Brings in air from the outside, mixes it with fuel and delivers the fuel-air mixture to the cylinder where the combustion occurs

24
Q

Name two types of induction systems

A

Carburetor system & fuel injection system

25
Q

What are two types of carburetor systems

A
Float type (most common)
Pressure type (uses fuel pump)
26
Q

Name disadvantages of float type carburetors

A
  • Disrupted by abrupt maneuvers
  • Low pressure fuel discharge causes incomplete vaporization & inhibits injection systems
  • icing tendency
27
Q

When does carbon buildup occur?

A

As altitude increases, air density decreases. Since density of fuel remains the same, it creates a progressively richer mixture that can result in engine roughness & loss of power. Rich mixture lowers the temp inside the cylinder, inhibiting complete combustion of the fuel.

28
Q

During descent, mixture must be:

A

enriched to avoid an excessively lean mixture

29
Q

Overly lean mixture can cause:

A

Detonation & rough engine operation, overheating, loss of power, damage engine

30
Q

Best way to maintain proper mixture

A

Monitor engine temperature. An exhaust gas temperature gauge can aid proper mixture.

31
Q

What is carb ice caused by?

A

A sharp decrease in temp in the carb, due to vaporization of the fuel and the low pressure at the Venturi

32
Q

Ice is most likely to occur when temperature & humidity is:

A

Below 70degF or 21degC & relative humidity is above 80%

33
Q

First indication of icing in an aircraft with a fixed pitch propeller

A

Decrease in engine RPM

34
Q

First indication of icing in an aircraft with a constant speed propeller

A

Drop in manifold pressure but no reduction in rpm

35
Q

Ice is particularly dangerous during:

A

low power descents where engine temp is low & ice may build unnoticed until power is increased

36
Q

Carb heat causes a decrease in engine power, why?

A

Heated air is less dense than outside air that had been entering the engine, thus the mixture is enriched

37
Q

Name 6 basic components of a fuel injection system

A
  1. Engine driven fuel pump
  2. Fuel/air control unit
  3. Fuel manifold valve
  4. Fuel distributor
  5. Discharge nozzles
  6. Auxiliary fuel pump
  7. Fuel pressure/flow indicators
38
Q

What is impact icing?

A

Ice forms on exterior of the aircraft & blocks openings such as air intake

39
Q

Name advantages of fuel injection

A
  • Reduction in evaporative icing
  • Better fuel flow
  • Faster throttle response
  • Precise control of mixture
  • Better fuel distribution
  • Easier cold weather starts
40
Q

Disadvantages of fuel injection

A
  • Difficulty in starting hot engines
  • Vapor lock during ground ops on hot days
  • Problems restarting of fuel-starved engine