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MODULE 13 B2 MOCK TEST - 1A

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Information

  • Number of Multiple choice Questions – 60
  • Β Passing Marks – 45
  • Time allowedΒ  – 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 TESTΒ  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 aΒ  nominal average timeΒ  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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  1. Answered
  2. Review
  1. Question 1 of 60
    1. Question
    1 points

    Measures undertaken to prevent corrosion around and under lavatories and galleys are

  2. Question 2 of 60
    2. Question
    1 points

    Chemical rain prellent should not be discharged onto dry windshield because

  3. Question 3 of 60
    3. Question
    1 points

    Air conditioning packs shutdown in the event of

  4. Question 4 of 60
    4. Question
    1 points

    When the collective pitch lever is operated the pitch of each blade of the main rolour of helicopter is-:

  5. Question 5 of 60
    5. Question
    1 points

    Shimmy damping

  6. Question 6 of 60
    6. Question
    1 points

    In hydraulic system, Hydraulic power landing gear extension and retraction flight
    control,auto flight the operational logic for these advances system controlled by :-

  7. Question 7 of 60
    7. Question
    1 points

    In probe thermal electric anti ice -:

  8. Question 8 of 60
    8. Question
    1 points

    When pressure is increased of boiling point Of liquid –

  9. Question 9 of 60
    9. Question
    1 points

    Thermocouple type fire warning system :-

  10. Question 10 of 60
    10. Question
    1 points

    Pressure accumulators

  11. Question 11 of 60
    11. Question
    1 points

    The control valves adjust, regulate or limit the amount of pressure In
    aircraft hydraulic system is termed

  12. Question 12 of 60
    12. Question
    1 points

    Mark the correct statement in case pneumatic system

  13. Question 13 of 60
    13. Question
    1 points

    The characteristic of manifold cross feed fuel system Used in large transport aircraft are

  14. Question 14 of 60
    14. Question
    1 points

    DC motor in wiper system drives a converter which changes the output of the motor is-:

  15. Question 15 of 60
    15. Question
    1 points

    A negative pressure relief valve in included On pressurized aircraft to ensure

  16. Question 16 of 60
    16. Question
    1 points

    Airspeed indicator may also have An additional White arc to indicate-

  17. Question 17 of 60
    17. Question
    1 points

    Auto brake deactivated when-:

  18. Question 18 of 60
    18. Question
    1 points

    A rain repellent System permit application of chemical repellent-:

  19. Question 19 of 60
    19. Question
    1 points

    The internal resistance of field which tends to prevent it from prevent is called following

  20. Question 20 of 60
    20. Question
    1 points

    Control of the Stearing

  21. Question 21 of 60
    21. Question
    1 points

    Which of the following portable fire extinguisher unusable in cabin or cockpit

  22. Question 22 of 60
    22. Question
    1 points

    High lift divice in group of flight control surface comprising of:-

  23. Question 23 of 60
    23. Question
    1 points

    An X on an isolation valve symbol of the APU shut off valve symbol shows

  24. Question 24 of 60
    24. Question
    1 points

    Choose most correct statement sensing element resistance of the continue loop system various:-

  25. Question 25 of 60
    25. Question
    1 points

    Venting should be installed such that

  26. Question 26 of 60
    26. Question
    1 points

    Each fuel tank must have

  27. Question 27 of 60
    27. Question
    1 points

    A crosstalk bus allows;

  28. Question 28 of 60
    28. Question
    1 points

    Which indication used as primary means of monitoring fuel delivery to the engine

  29. Question 29 of 60
    29. Question
    1 points

    In case of power transfer unit (PTUS)-

  30. Question 30 of 60
    30. Question
    1 points

    Most fuel boost pumps are;-

  31. Question 31 of 60
    31. Question
    1 points

    The used of load sensore insteed of proemty switches for air ground searching

  32. Question 32 of 60
    32. Question
    1 points

    Fiber optic cable

  33. Question 33 of 60
    33. Question
    1 points

    The insulation material used for wires and cables must conform to a no of rigid requirement such as-

  34. Question 34 of 60
    34. Question
    1 points

    Wings ribs are

  35. Question 35 of 60
    35. Question
    1 points

    swash plat assembly transmit;-

  36. Question 36 of 60
    36. Question
    1 points

    tyres pressure should not be measured until they have been amc weight at least-

  37. Question 37 of 60
    37. Question
    1 points

    This switch is kept in position to open or close depending on compression of main landing gear strut

  38. Question 38 of 60
    38. Question
    1 points

    Following details must be required for high pressure storage cylinders;-

  39. Question 39 of 60
    39. Question
    1 points

    No of bleed ports on compressor stages of turbofan engines are;-

  40. Question 40 of 60
    40. Question
    1 points

    Where is the collective sticks located –

  41. Question 41 of 60
    41. Question
    1 points

    The function of squat switch is to;-

  42. Question 42 of 60
    42. Question
    1 points

    Fuel tanks in large aircrafts have baffies to prevent free –movement of fuel n flight to

  43. Question 43 of 60
    43. Question
    1 points

    Following are structural components of an aircraft

  44. Question 44 of 60
    44. Question
    1 points

    Electrical bonding is

  45. Question 45 of 60
    45. Question
    1 points

    What is critical match number?

  46. Question 46 of 60
    46. Question
    1 points

    In POWERED STEWERING system nose wheel is turned by

  47. Question 47 of 60
    47. Question
    1 points

    Which component absorbs the shock of landing and cushions the roughness of takeoff,rollout and taxi operation

  48. Question 48 of 60
    48. Question
    1 points

    Carbon fibre breakes can withstand temperature ———-than the steel components breakes ;-

  49. Question 49 of 60
    49. Question
    1 points

    The moment produced for given control surface deflection depends on-

  50. Question 50 of 60
    50. Question
    1 points

    When landing gears (all three)up and locked

  51. Question 51 of 60
    51. Question
    1 points

    This is to provide pneumatic power for engine start engine conditioning-

  52. Question 52 of 60
    52. Question
    1 points

    An active hydraulic system layout consists of;-

  53. Question 53 of 60
    53. Question
    1 points

    The filter used in aircraft hydraulic system is for the purpose of

  54. Question 54 of 60
    54. Question
    1 points

    Engine bleed air temperature typically various form

  55. Question 55 of 60
    55. Question
    1 points

    Bleed air distribution system, high volume ducting is used for –

  56. Question 56 of 60
    56. Question
    1 points

    What is called empennage?

  57. Question 57 of 60
    57. Question
    1 points

    If computerized C .G on ground system switches to fault mode

  58. Question 58 of 60
    58. Question
    1 points

    In case of portable fire extinguisher, halon extinguisher is used for

  59. Question 59 of 60
    59. Question
    1 points

    An accumulator;-

  60. Question 60 of 60
    60. Question
    1 points

    Shielding drainage and surface treatment with ice phobic materials is called

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