MODULE 13 B2 MOCK TEST - 1C
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Information
- Number of Multiple choice Questions – 60
- Passing Marks – 45
- Time allowed – 75 Minutes
- MODULE 13 MOCK TEST – 1A – QUESTION 1 TO 60
- MODULE 13 MOCK TEST – 1B – QUESTION 61 TO 120
- MODULE 13 MOCK TEST – 1C – QUESTION 121 TO 180
- MOCK TEST 1A + MOCK TEST 1B + MOCK TEST 1C = 180 QUESTIONS
- 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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- Answered
- Review
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Question 1 of 60
1. Question
1 pointsMark the correct statement
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Question 2 of 60
2. Question
1 pointsMark the correct statement in regard to low fuel pressure warning light
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Question 3 of 60
3. Question
1 pointsPrecaution to be take while refueling the aircraft
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Question 4 of 60
4. Question
1 pointsWhy ground card preferred as source of air bleed over APU bleed
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Question 5 of 60
5. Question
1 pointsIn hydraulic system these valves control the speed and/ or direction of fluid flow-
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Question 6 of 60
6. Question
1 pointsWhile using an external sources of air for the tasting of the a/c deicing boots system if the vacuum operated instruments show any deflection , it indicates;-
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Question 7 of 60
7. Question
1 pointsEngine inlet cowl anti icing system of a large aircraft fitted with turbine engine, uses
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Question 8 of 60
8. Question
1 pointsMark the correct statement ;
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Question 9 of 60
9. Question
1 pointsWhen windshield wiper switch is tuned off the wiper motor is
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Question 10 of 60
10. Question
1 pointsIn hydraulic system, microns type fitter element have the periodically– according to applicable instruction-
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Question 11 of 60
11. Question
1 pointsA typical micron type filter element
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Question 12 of 60
12. Question
1 pointsTires should be stored in time jack which hold them
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Question 13 of 60
13. Question
1 pointsWhich components absorbs the shock of landing and cushions the roughness of takeoff .allowed and taxi operation
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Question 14 of 60
14. Question
1 pointsThe pressure source for power brakes is.
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Question 15 of 60
15. Question
1 pointsThe fuel supply system, this must the open in allow any flow
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Question 16 of 60
16. Question
1 pointsAircraft tires accept a variety of —— dependable in wide range of operating conditions
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Question 17 of 60
17. Question
1 pointsEach tank must have an expression space of not less than
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Question 18 of 60
18. Question
1 pointsA gyro horizon of artificial horizon includes the pitch and bank altitude of aircraft relative to the
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Question 19 of 60
19. Question
1 pointsMTCS-
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Question 20 of 60
20. Question
1 pointsIt is at tank in which an adeguate supply of liquid for system is stored
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Question 21 of 60
21. Question
1 pointsThe outer bond edge which fits against the wheel stage is known as
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Question 22 of 60
22. Question
1 pointsThe use of load sensor and proximity stitches
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Question 23 of 60
23. Question
1 pointsThe hydraulic system , it hydraulic system parameter are out of normal range system control large circuits recognise the operation made from normal to-
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Question 24 of 60
24. Question
1 pointsDeicer boots’-
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Question 25 of 60
25. Question
1 pointsFuel system components must be bonded and grounded in order to-
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Question 26 of 60
26. Question
1 pointsIn IFE system ,the airbus ALNA , airline network architecture is a type of
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Question 27 of 60
27. Question
1 pointsIn aircraft hydraulic system the compound which stores supply of fuel for system operation
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Question 28 of 60
28. Question
1 points——-provide flood lighting of included instrument and one positioned on, panel to illuminate small adjacent over
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Question 29 of 60
29. Question
1 pointsData base in light system management system, contains.
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Question 30 of 60
30. Question
1 pointsA flight control system which depends on electric signals transmit the pilot action from flight deck through a computer to various flight control is
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Question 31 of 60
31. Question
1 pointsWindshield wiper system consist of
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Question 32 of 60
32. Question
1 pointsAn accumulation
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Question 33 of 60
33. Question
1 pointsWhile refuling the aircraft
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Question 34 of 60
34. Question
1 pointsCharacteristic of synthetic based hydraulic liquid is-
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Question 35 of 60
35. Question
1 pointsWater system flushing method are
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Question 36 of 60
36. Question
1 pointsThis is used to provide pneumatic power for engine start , engine , wing descending and airconditioning
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Question 37 of 60
37. Question
1 pointsMark the correct statement case of normal extension and retraction of landing gear system
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Question 38 of 60
38. Question
1 pointsAndroid switch built in system dilution as a function of altitude and provided unilated oxygen an positive pressure above.
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Question 39 of 60
39. Question
1 pointsIn hydraulic system that has reservoir pressurised with turbine engine compression bleed-air which unit reduces the air pressure between the engine & reservoir
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Question 40 of 60
40. Question
1 pointsCowl anti long system gets bleed air from-
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Question 41 of 60
41. Question
1 pointsIsolation valve used in
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Question 42 of 60
42. Question
1 pointsMTCS
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Question 43 of 60
43. Question
1 pointsMTCS high pressure system
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Question 44 of 60
44. Question
1 pointsMTCS Spoiler
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Question 45 of 60
45. Question
1 pointsWith the increase in speed of aircraft
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Question 46 of 60
46. Question
1 pointsMTCS Rigging of fuselage
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Question 47 of 60
47. Question
1 pointsCabin emergency equipment
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Question 48 of 60
48. Question
1 pointsOxygen cylinder
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Question 49 of 60
49. Question
1 pointsMTCS vertical stabiliser
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Question 50 of 60
50. Question
1 pointsConventional landing-gear configuration consists of
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Question 51 of 60
51. Question
1 pointsFire detection system
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Question 52 of 60
52. Question
1 pointsLight aircraft are design to operate at max cabin differential pressure of about
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Question 53 of 60
53. Question
1 pointsSpecifications for emergency equipment requirements
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Question 54 of 60
54. Question
1 pointsWing sweepback
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Question 55 of 60
55. Question
1 pointsLight aircraft uses
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Question 56 of 60
56. Question
1 pointsMineral based fluid MIL-0-83282.
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Question 57 of 60
57. Question
1 pointsEssential lights are
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Question 58 of 60
58. Question
1 pointsIMA advantage
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Question 59 of 60
59. Question
1 pointsType of failure of having no effect
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Question 60 of 60
60. Question
1 pointsDry powder mostly not used for other than metal because