Ch 2B - Powerplant and Related Systems Flashcards

(54 cards)

1
Q

AC

A

Alternating Current - alternators produce

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2
Q

DC

A

Direct Current - alternator rectifier converts AC to DC

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3
Q

Turbine engine

A

Costly, powerful

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4
Q

Reciprocating engine

A

Converts fuel into mechanical energy within cylinders

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5
Q

Four-stroke operating cycle

A

intake of fuel/air mix, compression by the piston, ignition and expansion of the gas, venting of burned gas

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6
Q

Throttle control

A

Controls engine power by regulating the amount of fuel and air mixture that flows into the cylinders

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7
Q

Mixture control

A

Controls the fuel/air ratio

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8
Q

Intake port

A

Where outside air enters induction system

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9
Q

Carburetor

A

Mixes the incoming air with fuel and delivers it to the combustion chamber

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10
Q

Carburetor ice

A

Caused by fuel vaporization and decreasing air pressure in the venturi, more likely to occur below 21C(70F) and relative humidity above 80%, carburetor heat systems route air across heat source before entering carburetor

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11
Q

Supercharger

A

compresses incoming air using a pump driven by the engine

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12
Q

Constant speed propeller

A

adjusted in cockpit, manifold pressure gauge monitor engine output by displaying pressure in inches of mercury (Hg)

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13
Q

Constant speed propeller

A

adjusted in cockpit by propeller control, manifold pressure gauge monitor engine output by displaying pressure in inches of mercury (Hg) and propeller control sets engine RPM on the tachometer, low RPM and high manifold pressure causes engine stress

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14
Q

Fixed pitch propeller is displayed on

A

a tachometer in revolutions per minute (RPM)

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15
Q

Fuel injection

A

increases engine efficiency and eliminates carburetor ice

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16
Q

Turbocharger

A

pressurizes air using a mechanism driven by engine exhaust gases

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17
Q

Magneto

A

self-contained, supplies electrical current to the spark plugs

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18
Q

Detonation

A

uncontrolled explosive ignition of the fuel/air mixture within the cylinders combustion chamber

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19
Q

Preignition

A

uncontrolled combustion of fuel in advance of normal ignition

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20
Q

Fuel pump system

A

engine driven pump provides fuel under pressure from the fuel tanks

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21
Q

Fuel pressure gauge

A

useful in measuring fuel pump malfunctions

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22
Q

Vapor lock

A

occurs when high engine temperatures cause bubbles of fuel vapor to form in the fuel lines or fuel pump

23
Q

Gravity-feed system

A

fuel flows from fuel tanks to engine by gravity

24
Q

Fuel tanks

A

usually in wings, has vent to make pressure equal in and out

25
Fuel quantity gauges
use sensing unit to measure fuel, measured in gallons/pounds/metric units
26
Fuel selector valve
Left/Right/Both/(Off)
27
Fuel strainer
removes moisture and other sediments that settle at sump in bottom of the strainer
28
Fill fuel tanks at end of the day
prevents moisture from condensing in tanks
29
If fuel grade is not available
use next higher grade if approved by manufacturer, using a lower grade will cause engine to overheat
30
Dry sump system
oil is contained in a separate tank and circulated through the engine by pumps
31
wet sump system
all oil is carried in a sump that is part of the engine
32
oil used for
lubrication of internal parts and cooling
33
oil pressure gauge
indicates pressure in pound per square inch (PSI) or bars
34
oil temperature gauge
can take several minutes after starting to read increase in temp
35
High engine oil temp
caused by too low oil level
36
Immediately after starting the engine
adjust RPM and check engine instruments for proper indications
37
Cowl flap
creates a larger opening for air to exit the engine compartment
38
Excessive engine temperatures
can result in loss of power, high oil consumption, and engine damage
39
cylinder head temperature gauge
provides direct temp reading from one of the engine cylinders
40
Engine temp can be reduced by
enriching the mixture, reducing the rate of climb, increasing airspeed, or reducing power
41
If oil and cylinder head temp are above normal
you might be using too much power with an overly lean mixture
42
Fixed pitch propeller
blade angle is set for primary function of the airplane and cannot be adjusted
43
Climb propeller
propeller with low blade angle, provides best performance for takeoff and climb
44
Cruise propeller
propeller with high blade angle, optimized for high speed and altitude cruise
45
Alternator
produce AC current and then convert it to DC for use in the airplane
46
Ammeter
monitors electrical current in amperes, can measure current flowing to/from battery and/or loadmeter measures load on alternator
47
Master switch
controls entire electircal system except ignition system
48
Standby battery
disconnects from main bus and powers essential bus
49
When a mixture is leaned
fuel flow is decreased to compensate for decreased air density, can eliminate engine roughness during runup at high-elevation airports
50
During descents from high to low altitudes
you have to enrich the mixture control
51
First indication of carburetor ice in a fixed pitch propeller is
loss of RPM, caused by enriched mixture
52
Carburetor heat
decreases engine performance
53
If you suspect detonation on climbout
lower nose to increase airspeed and increase cooling airflow around the engine
54
How to reduce engine temps
enrich the mixture, reduce rate of climb, increase airspeed, or reduce power