ACI 2 (Mod 1&2 - Finals) Flashcards

1
Q

Systematic troubleshooting approach according to Airbus

A
  • Identify the source of vibration
  • Use onboard sensors and maintenance data for diagnosis
  • Analyze vibration patterns
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2
Q

Corrective actions according to Airbus

A
  • Component inspections
  • Adjusting and replacing affected parts
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3
Q

When performing aircraft maintenance it’s important to always verify
the

A

OEM’s recommendation for sensor and mount installation

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4
Q

Who will specify when maintenance should be conducted

A

Manufacturer

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5
Q

Who issued directives that relate to engine safety

A

FAA

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6
Q

Measures acceleration forces, commonly used for engine and airframe monitoring

A

Accelerometers

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7
Q

Measures the velocity of an object or fluid using various methods

A

Velocimeters

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8
Q

2 methods/approach used in velocimeters

A
  • Doppler effect
  • Laser velocimetry
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9
Q

In digital vibration monitoring systems where do sensors send data

A

Central processing unit

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10
Q

Vibration levels are shown on digital displays, often integrated into the cockpit’s ____

A

Multi-function display

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11
Q

is a vibration analysis and balancing tool that rapidly and accurately acquires and analyzes aircraft and engine vibration data.

A

Honeywell Chadwick-Helmuth’s Vibrex™ 2000 Plus (V2K+)

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12
Q

are critical for monitoring and managing the levels of various fluids essential to an aircraft’s operation.

A

Fluid quantity system

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13
Q

Types of fluids monitored

A
  • Fuel
  • Oil
  • Hydraulic fluid
  • Water
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14
Q

The most critical fluid, requiring precise measurement to ensure sufficient supply for the entire flight.

A

Fuel

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15
Q

Used for engine lubrication and cooling.

A

Oil

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16
Q

Powers various aircraft systems, including landing gear, brakes, and flight controls.

A

Hydraulic fluid

17
Q

Used in lavatory systems and potable water supply.

A

Water

18
Q
  • Used primarily for fuel measurement
  • Consist of two conductive plates separated by a dielectric material (fuel).
  • The capacitance changes with the fluid level, altering the electrical signal proportional to the fuel quantity.
A

Capacitance probes

19
Q

What principle does a gyroscope use

A

conservation of angular momentum

19
Q
  • Common in oil and hydraulic systems.
  • Use a float mechanism connected to a variable resistor.
  • As the fluid level changes, the float moves, adjusting the resistance and changing the signal sent to the indicator.
A

Resistive sensors

19
Q
  • Use sound waves to measure fluid levels.
  • Transmit ultrasonic pulses and measure the time it takes for the echoes to return.
  • Suitable for various fluid types, including fuel and water.
A

Ultrasonic sensors

20
Q

a device with a spinning disc or wheel mechanism that harnesses the principle of conservation of angular momentum

A

gyroscope

21
Q

the tendency for the spin of a system to remain constant unless subjected to external torque.

A

principle of conservation of angular momentum

22
Q

Instruments that is considered to be a gyro instrument

A
  • Turn indicator
  • Heading indicator
  • Attitude indicator
23
Q

also known as the turn and slip indicator is a variant that are essentially two aircraft flight instruments in one device.

A

Turn indicator

24
Q

What does the turn indicator indicate

A
  • rate of turn
  • skid or slip
25
Q

also known as the directional gyro, or DG displays the aircraft’s heading incompass points, and with respect to magnetic north when set with a compass.

A

Heading indicator

26
Q

also known as anartificial horizon shows the aircraft’s relation to the horizon.

A

Attitude indicator

27
Q

Two things that an attitude indicator is able to display

A
  • roll
  • pitch
28
Q

use tiny vibrating structures to measure angular velocity.

A

Micro-Electro-Mechanical Systems gyroscopes

29
Q

Use light traveling through optical fibers to detect rotation.

A

Fiber Optic Gyroscopes (FOGs)

30
Q

Utilize laser beams in a ring-shaped cavity to measure rotational motion.

A

Ring Laser Gyroscopes (RLGs)

31
Q

focuses on providing three-dimensional orientation by processing data from gyroscopes, accelerometers, and sometimes magnetometers. It gives precise attitude (pitch, roll, and yaw) and heading information to the PFD.

A

Attitude and Heading Reference System (AHRS)

32
Q

Advantages of Digital Gyroscopic Instruments

A
  • High precision in measuring rotational movement
  • Less prone to mechanical wear and tear
  • Easily integrated with other digital avionics systems
  • Lower maintenance requirements compared to traditional mechanical gyroscopes