MODULE 08 MOCK TEST - 3
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Information
- Number of Multiple choice Questions – 20
- Passing Marks – 15
- Time allowed – 25 Minutes
- All mock test includes multiple choice questions.
- Each questions must have more than two alternative answers and having one correct answer and candidate gets a nominal average time of 75 seconds per question.
- According to CAR 66 the passing mark is 75%
- Note- We designed mock test 80% similar to DGCA exam, The only slight change is that in this we show the result immediately at the end of the test and also show which answer you got right ,which we don’t get to see in DGCA exam and also we didn’t set the holding period of 15sec like DGCA
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- Short notes
- DGCA previous question (Including latest)
- Practice question
- Mock test as well as will get the correct guidance to clear the respective module
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- Answered
- Review
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Question 1 of 20
1. Question
1 pointsAmount of water vapour present in air
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Question 2 of 20
2. Question
1 pointsLongitudinal instability is due to the
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Question 3 of 20
3. Question
1 pointsAs AOA increases
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Question 4 of 20
4. Question
1 pointsLift of an aircraft produced more due to
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Question 5 of 20
5. Question
1 pointsStick free condition
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Question 6 of 20
6. Question
1 pointsInduced drag is
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Question 7 of 20
7. Question
1 pointsIAS includes
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Question 8 of 20
8. Question
1 pointsThe weight of an aircraft is acting at which point
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Question 9 of 20
9. Question
1 pointsLateral stability about which axis
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Question 10 of 20
10. Question
1 pointsAt high speed induced drag is
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Question 11 of 20
11. Question
1 pointsLateral stability is maintained by
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Question 12 of 20
12. Question
1 pointsDuring climb which of the following curve should be consider ?
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Question 13 of 20
13. Question
1 pointsCo-efficient of viscosity
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Question 14 of 20
14. Question
1 pointsWhat is the mean sea level pressure
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Question 15 of 20
15. Question
1 pointsSpeed of sound at sea level
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Question 16 of 20
16. Question
1 pointsIn steeper turn rudder position is taken by
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Question 17 of 20
17. Question
1 pointsIf Cp of an aircraft is behind Cg ,what happened to the nose
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Question 18 of 20
18. Question
1 pointsDuring climbing
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Question 19 of 20
19. Question
1 pointsLateral stability can be reduced by
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Question 20 of 20
20. Question
1 pointsAngle between main plane and tail plane is known as
