Module 5 Test 6

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1.
1 point
What are the data bus cables terminated using?
2.
1 point
Why does ARINC data bus system send data to line replacement unit in series?
3.
1 point
What logic gate requires two positive voltage to operate?
4.
1 point
How do you prevent the High intensity Radiated Field entering a fibre optic cable?
5.
1 point
The flight management system operating program is altered in-flight by:
6.
1 point
In ARINC 429, the first 8 bits represents:
7.
1 point
How long is the flight management system operational program updated?
8.
1 point
How do you create a NOT-gate from NOR-gate or NAND-gate?
9.
1 point
What are the alerting modes of a flight management system alerting?
10.
1 point
How many accelerometers/gyros unit in basic inertial reference system?
11.
1 point
Who is responsible for software changes?
12.
1 point
On cathode ray tube display, the beam deflection control uses:
13.
1 point
How do you prevent the electromagnetic compatibility effects on fibre optics?
14.
1 point
On modern aircraft, when are the built in test equipment checks carried out?
15.
1 point
In Cathode ray tube, what counteracts the magnetic coil effect?
16.
1 point
What do the aircraft manufacturers do to protect against electro-static device service?
17.
1 point
Hexadecimal system is to base:
18.
1 point
What is the ARINC 429 language?
19.
1 point
The 3 accelerometers on stable platform are mounted:
20.
1 point
What is the deflection field if the electromagnetic deflection is used?
21.
1 point
What is the dot matrix or light emitting diode construction?
22.
1 point
In order to maintain HIRF protection, bonding checks between airframe and electrical components carrying voltages greater than 50 volts RMS or DC or main earth return should not exceed
23.
1 point
Aircraft heading is:
24.
1 point
When removing electronic circuit boards from line replacement unit, you should turn off the power and connect a low current path between:
25.
1 point
When considering High intensity radiated field, the manufacturer should ensure all unshielded cables are:
26.
1 point
To turn NOR-gate or NAND-gate into NOT-gate, what do you do?
27.
1 point
Electronic flight instrumental system input to the flight data recorder goes:
28.
1 point
Cross track, XTK is:
29.
1 point
Where is the parity bit installed in data word?
30.
1 point
Aircraft fibre optics commonly uses:
31.
1 point
What does the electro-static device service symbol mean on line replacement unit>
32.
1 point
For inertial reference system to pass the 'alignment system performance test':
33.
1 point
In engine indicating and crew alerting system, when is the maintenance mode available?
34.
1 point
When doing instrument landing system approach and you are below the beam, where is the bug?
35.
1 point
On digital flight computer controlled aircraft control surface positional inputs are converted:
36.
1 point
When is the maintenance format used?
37.
1 point
How is multiplication achieved in Arithmetic and logic unit?
38.
1 point
What is meaning about the ARINC 629 is a bi-directional data bus?
39.
1 point
If both inputs to NOR-gate are inverted, the output is:
40.
1 point
Central maintenance computer works to
41.
1 point
How many wires in ARINC 629 data bus?
42.
1 point
Gyro-compassing is the term used for:
43.
1 point
What logic gate does a parallel circuit represent?
44.
1 point
Command bars, what makes them move the correct amount?
45.
1 point
In flight director, how are small deviations corrected?
46.
1 point
On electronic flight display, the glide-slope indicator is below the center position. The aircraft should fly:
47.
1 point
What does the waveform created by electron beam in Cathode Rat Tube , look like prior to contact with the screen, if deflected by plates?
48.
1 point
What is the main disadvantage of a fibre-optic data bus?
49.
1 point
In flight director bars move up in slow increments, what controls their rate/speed?
50.
1 point
Using Inertial navigation system, the aircraft flies: