Avionics System Integration MCQs

Welcome to our comprehensive collection of Multiple Choice Questions (MCQs) on Avionics System Integration, a fundamental topic in the field of avionics engineering. Whether you're preparing for competitive exams, honing your problem-solving skills, or simply looking to enhance your abilities in this field, our Avionics System Integration MCQs are designed to help you grasp the core concepts and excel in solving problems.

In this section, you'll find a wide range of Avionics System Integration mcq questions that explore various aspects of Avionics System Integration problems. Each MCQ is crafted to challenge your understanding of Avionics System Integration principles, enabling you to refine your problem-solving techniques. Whether you're a student aiming to ace avionics engineering tests, a job seeker preparing for interviews, or someone simply interested in sharpening their skills, our Avionics System Integration MCQs are your pathway to success in mastering this essential avionics engineering topic.

Note: Each of the following question comes with multiple answer choices. Select the most appropriate option and test your understanding of Avionics System Integration. You can click on an option to test your knowledge before viewing the solution for a MCQ. Happy learning!

So, are you ready to put your Avionics System Integration knowledge to the test? Let's get started with our carefully curated MCQs!

Avionics System Integration MCQs | Page 1 of 11

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Q1.
What should be the value of R2 to have an attenuation of 0.5, if R1=200 ฮฉ?

a.

100 ฮฉ

b.

300 ฮฉ

c.

200 ฮฉ

d.

500 ฮฉ

Discuss
Answer: (c).200 ฮฉ
Q2.
What is the type of filter shown in the figure?

a.

Low pass filter

b.

High pass filter

c.

Band pass filter

d.

All pass filter

Discuss
Answer: (a).Low pass filter
Q3.
What is the type of filter shown in the figure?

a.

Low pass filter

b.

High pass filter

c.

Band pass filter

d.

All pass filter

Discuss
Answer: (a).Low pass filter
Q4.
Which of the following is false with respect to AIRNIC?

a.

Define system and equipment specification

b.

Non-profit organization

c.

Run by civil airlines with industry and establishment representation

d.

Used only in America

Discuss
Answer: (d).Used only in America
Q5.
What is the fastest mode of data communication between components in aircraft?

a.

Coaxial cable

b.

Twisted pair cable

c.

Fiber optic cable

d.

Radio communication

Discuss
Answer: (c).Fiber optic cable
Q6.
In an aircraft, serial data transfer is achieved by _________

a.

Time division Multiplexing

b.

Code Division Multiplexing

c.

Frequency Division Multiplexing

d.

Pulse Modulation

Discuss
Answer: (a).Time division Multiplexing
Q7.
What type of avionic architecture consist of a number of an interconnected but functionally independent subsystem with some degree of central computer of overall operating modes.

a.

IMA architecture

b.

Federated architecture

c.

Disjoint architecture

d.

Distributed architecture

Discuss
Answer: (b).Federated architecture
Q8.
How are Data bus in avionics architecture broadly divided into?

a.

High speed and low speed data bus

b.

AIRNIC and MIL standard data bus

c.

Electrical and Optical data bus

d.

Main and interconnecting data bus

Discuss
Answer: (c).Electrical and Optical data bus
Q9.
The type of Ethernet data bus adapted for airborne applications is _______

a.

Airborne Simplex Ethernet

b.

Airborne Duplex Ethernet

c.

Multiplexed Ethernet

d.

Avionics Full Duplex Switched Ethernet

Discuss
Answer: (d).Avionics Full Duplex Switched Ethernet
Q10.
What type of cable does MIL STD 1553 use?

a.

Coaxial cable

b.

Single twisted pair cable with shielding

c.

Single twisted pair cable without shielding

d.

Fiber optic cable

Discuss
Answer: (b).Single twisted pair cable with shielding
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