review Flashcards

1
Q

The nondestructive inspection method most often used for parts
made of iron or iron alloys is magnetic particle inspection. Magnetic
particle inspection is useful for detecting cracks, splits, seams, and
voids that form when a metal ruptures.

A

Magnetic Particle Inspection

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2
Q

-Once an engine part is clean, it must be inspected closely for
damage. The first type of inspection that is usually done is a thorough
visual inspection aided by a magnifying glass, flashlight, and, if
necessary, a borescope. Visual inspections are done to detect many
different visible surface defects in parts.

A

Visual Inspection

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3
Q

Starts with our technicians applying a special liquid to the inspection
surface, which a process called capillary action then draws into any
surface breaking discontinuities.

A

Liquid Penetrant Inspection

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4
Q

Combines electricity and magnetism to create a magnetic field on the
conductive metal surface

A

Eddy Current Inspection

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5
Q

Methods use sound waves to find defects and measure thickness.

A

Ultrasonic Inspection

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6
Q

A non-destructive testing (NDT) method which uses either x-rays or
gamma rays to examine the internal structure of manufactured
components identifying any flaws or defects.

A

Radiography

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7
Q

A partial separation of material
usually caused by vibration,
overloading, internal stresses,
defective assembly, or fatigue.

A

CRACKS

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8
Q

The presence of small voids,
bubbles, or air pockets within a
material. These voids can occur
during the manufacturing process,
especially in composite materials
like carbon fiber reinforced
polymers (CFRP) or fiberglass,
which are widely used in modern
aircraft construction.

A

POROSITY

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9
Q

These are overlapping layers of material,
often metal, where one part of a sheet
is folded or overlapped onto another. In
aircraft structures, are common in
areas like the skin of the fuselage or
wing

A

LAPS

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10
Q

These are the joints where two edges of
materials meet or are fastened together, often
with rivets, welds, or adhesives.

A

SEAMS

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11
Q

-Aircraft can have various plastic components,
including interior panels, fairings, or nonstructural parts made from materials like acrylic,
polycarbonate, or composite plastics.

A

PLASTICS

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12
Q

Aircraft can have various plastic components,
including interior panels, fairings, or nonstructural parts made from materials like acrylic,
polycarbonate, or composite plastics.

A

PLASTICS

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13
Q

materials in aircraft can be found
in high-temperature applications, such as
thermal barriers in engines or insulating
components

A

CERAMIC

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14
Q

aircraft can include cockpit
windows, instrument covers, or
lighting elements

A

GLASS

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15
Q

An engine part is found to be structurally sound, it must be measured
to verify that it is within the manufacturer’s tolerances. This check is
referred to as a dimensional inspection and requires the use of
several precision measuring instruments such as

A

micrometer
calipers, telescoping gauges, and dial indicators.

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16
Q

extremely precise measuring
tools for external measurements, most notably
thickness, though they can be used for
measuring small external diameters.

A

Micrometer Caliper

17
Q

indirect measuring
devices used to measure the internal
diameter of a bore, hole, groove, slot, etc.

A

Telescoping Gauge

18
Q

Used for precise comparisons or
measurements of workpiece surfaces,
machine, equipment, part tolerances,
alignment of your machine’s
components, or the general deviation
of any object from an expected
standard.

A

Dial Indicator

19
Q

After all of the parts have been inspected and repaired as necessary,
the engine is ready to be reassembled.

A

Reassembly

20
Q

After an engine has been repaired, overhauled, or replaced, it must be
prepared for installation.

A

Installation & Testing

21
Q

Once an engine is completely installed on an aircraft or test stand,
you can prepare the engine for a test run.

A

Ground Test Preparation

22
Q

To prevent engine bearing failure during the initial start, you should.

A

Pre-oiling

23
Q

Before you attempt to start a newly installed engine, the fuel system
should be bled to purge any air bub bles from the fuel lines and
pumps and to help flush any preservative oil from the fuel system.

A

Fuel System Bleeding

24
Q

If an aircraft has cowl flaps, they must be rigged to accurately
regulate the passage of cooling air through the engine compartment.

A

Cowl Flap Rigging

25
Q

After the initial ground run and flight test, an engine must receive final
adjustments and a thorough visual inspection.

A

Post-run Check and Adjustment

26
Q

An engine’s crankshaft rpm is displayed by a
that is calibrated in hundreds of
rpm. is a primary engine
instrument used extensively by a pilot to
monitor engine condition and verify that
the engine is developing the appropriate
rpm and power output for a given throttle
setting.

A

Tachometer/ Crankshaft Speed

27
Q

gauge
measures the absolute pressure of the
fuel/air mixture within the intake manifold.

A

Manifold Pressure

28
Q

The engine temperature can have a
dramatic impact on engine performance.
Therefore, most reciprocating engine
powered aircraft are equipped with a
cylinder head temperature (CHT) gauge
that allows a pilot to monitor engine
temperatures.

A

Cylinder Head Temperature

29
Q

is
measured at the carburetor entrance
by a temperature sensing bulb in the
ram air intake duct.

A

Carburetor Air Temperature

30
Q

allows a
pilot to monitor the temperature of
the oil entering the engine. This is
important because oil circulation
cools the engine as it lubricates the
moving parts

A

Oil Temperature

31
Q

The engine lubrication system
supplies oil under pressure to the
moving parts of the engine. To allow
a pilot to monitor the effectiveness
of a given lubrication system, all
aircraft engines are equipped with an
oil pressure gauge that is calibrated
in pounds per square inch.

A

Oil Pressure

32
Q

displays the pressure of fuel supplied to
the carburetor or fuel control unit. Most fuel
pressure instruments display fuel pressure in
pounds per square inch (psi), and provide
indications to the pilot that the engine is
receiving the fuel needed for a given power
setting

A

Fuel Pressure

33
Q

measures the rate of
fuel an engine burns in gallons per hour or
pounds per hour. This provides the most
accurate indication of an engine’s fuel
consumption.

A

Fuel Flow Indicator

34
Q

Another performance monitoring instrument
often used in reciprocating engine
installations. the
temperature of the exhaust at some point
past the exhaust port

A

Exhaust Gas Temperature