MODULE 08 MOCK TEST - 2
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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
ALL THE BEST
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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 pointsInduced drag is a part of
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Question 2 of 20
2. Question
1 pointsAngle of attack
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Question 3 of 20
3. Question
1 pointsNACA 0009 airfoil is having
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Question 4 of 20
4. Question
1 pointsThe longitudinal stability is depend upon
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Question 5 of 20
5. Question
1 pointsPerformance capability of jet engine with propeller is depends on
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Question 6 of 20
6. Question
1 pointsThe temperature variation near earth surface
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Question 7 of 20
7. Question
1 pointsViscosity coefficient
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Question 8 of 20
8. Question
1 pointsFor steeper turn
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Question 9 of 20
9. Question
1 pointsIf pitching moment about fuselage disturbed then which stability is affected
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Question 10 of 20
10. Question
1 pointsIf there is oscillation in a A/C with respect to time then it is
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Question 11 of 20
11. Question
1 pointsWhat are the flow properties considered in ISA
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Question 12 of 20
12. Question
1 pointsFactors of drag primarily depends on
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Question 13 of 20
13. Question
1 pointsMTCS- about stability..
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Question 14 of 20
14. Question
1 pointsIf induced drag is reduced ( minimum ) ………
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Question 15 of 20
15. Question
1 pointsDuring flat turn……
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Question 16 of 20
16. Question
1 pointsOn Delta wing aircraft lift ….
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Question 17 of 20
17. Question
1 pointsLongitudinal stability is highly affected due to …….
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Question 18 of 20
18. Question
1 pointsIf aspect ratio is higher than, induced drag is
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Question 19 of 20
19. Question
1 pointsLaw applicable for equilibrium flight is
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Question 20 of 20
20. Question
1 pointsWhen an aircraft is in damping oscillation at a period of time
