MODULE 08 MOCK TEST - 1
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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 pointsDensity is defined as
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Question 2 of 20
2. Question
1 pointsTemperature at sea level is
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Question 3 of 20
3. Question
1 pointsWhich of the following flight operation is not depends on density
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Question 4 of 20
4. Question
1 pointsCoefficient of viscosity is defined as
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Question 5 of 20
5. Question
1 pointsDuring turn the outer wing offers more
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Question 6 of 20
6. Question
1 pointsWhen engine failure occurs and lift is forward of the weight then
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Question 7 of 20
7. Question
1 pointsAccording to ISA at sea level temperature, pressure, density is
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Question 8 of 20
8. Question
1 pointsMTCS-about stability
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Question 9 of 20
9. Question
1 pointsRudder gives which stability
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Question 10 of 20
10. Question
1 pointsHigher weight in gliding flight is not affected not by
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Question 11 of 20
11. Question
1 pointsIf aspect ratio is higher than induced drag is
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Question 12 of 20
12. Question
1 pointsIf induced drag is reduced
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Question 13 of 20
13. Question
1 pointsMTCS-higher Reynolds number
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Question 14 of 20
14. Question
1 pointsOn a delta wing aircraft lift
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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 pointsIn the case of aircraft nose drop thrust line is placed———-and drag line is———
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Question 17 of 20
17. Question
1 pointsDuring turn stalling angle
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Question 18 of 20
18. Question
1 pointsWhich of the following gives stall warning to pilot
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Question 19 of 20
19. Question
1 pointsLongitudinal stability is highly affected due to
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Question 20 of 20
20. Question
1 pointsSpeed of sound at mean sea level
