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MODULE 13 B2 MOCK TEST - 1B

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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

    Aramid yarn in fiber optical cable construction;

  2. Question 2 of 60
    2. Question
    1 points

    Which type of bonding material is used between moving parts or parts subjected to vibration

  3. Question 3 of 60
    3. Question
    1 points

    The primary purpose of a hydraulic actuating unit is transform

  4. Question 4 of 60
    4. Question
    1 points

    APU supplies the bleed air to the bleed manifold through the;-

  5. Question 5 of 60
    5. Question
    1 points

    The engine airliners typically have a pressure transmitter and which is mounted in pneumatic manifold of

  6. Question 6 of 60
    6. Question
    1 points

    Retractable gear aircraft generally use what colour light to indicate that the gear is down and locked

  7. Question 7 of 60
    7. Question
    1 points

    ——-fuel tank have commonly been located in the wing or fuselage or may be located in other location such as horizontal stabilizer

  8. Question 8 of 60
    8. Question
    1 points

    The main disadvantage of using short pitch winding in alternator is that-

  9. Question 9 of 60
    9. Question
    1 points

    What is the purpose of bleed air isolation valve purpose valve purpose and state;

  10. Question 10 of 60
    10. Question
    1 points

    The absence of green disk indicates

  11. Question 11 of 60
    11. Question
    1 points

    A vacuum is associated in lavatory waste system

  12. Question 12 of 60
    12. Question
    1 points

    What is the purpose of cross feed system

  13. Question 13 of 60
    13. Question
    1 points

    Shock wave forms at;-

  14. Question 14 of 60
    14. Question
    1 points

    Fuel supply systems, consists of

  15. Question 15 of 60
    15. Question
    1 points

    The purpose of landing gear safety switch is to;

  16. Question 16 of 60
    16. Question
    1 points

    Non intrusive ice detector is

  17. Question 17 of 60
    17. Question
    1 points

    Common type of portable extinguisher used in aircraft are

  18. Question 18 of 60
    18. Question
    1 points

    The difference between shut off valve used in oxygen system other system is that

  19. Question 19 of 60
    19. Question
    1 points

    Sources for high pressure pneumatic system inducts

  20. Question 20 of 60
    20. Question
    1 points

    Low pressure pneumatic system in case pressure regulator failure system is protected for-

  21. Question 21 of 60
    21. Question
    1 points

    Usual protection used on pilot and static probes is;

  22. Question 22 of 60
    22. Question
    1 points

    The oxygen cylinder is charged usually up to;

  23. Question 23 of 60
    23. Question
    1 points

    While refuelling the aircraft

  24. Question 24 of 60
    24. Question
    1 points

    Every fuel tank must be able withstand without fail

  25. Question 25 of 60
    25. Question
    1 points

    The airframe compartment for the bladder is structural ,and a fairly small opening is provided for the

  26. Question 26 of 60
    26. Question
    1 points

    The purpose of electrical bonding in aircraft is

  27. Question 27 of 60
    27. Question
    1 points

    Modern aircraft wheels are of ;-

  28. Question 28 of 60
    28. Question
    1 points

    In probe and drain heating system propeller boot a receives electric current from-

  29. Question 29 of 60
    29. Question
    1 points

    waste system flushing methods are;-

  30. Question 30 of 60
    30. Question
    1 points

    In aircraft hydraulic system which is the component converts fluid pressure into useful work by linear or reciprocating mechanical motion?

  31. Question 31 of 60
    31. Question
    1 points

    What is subsonic speed-

  32. Question 32 of 60
    32. Question
    1 points

    The ACM has a compressor on a common shaft-

  33. Question 33 of 60
    33. Question
    1 points

    An aircraft air conditioning package uses ram air to cool the bleed air is ;-

  34. Question 34 of 60
    34. Question
    1 points

    AUDIO INTERGRATING SYSTEM (AIS) provides;-

  35. Question 35 of 60
    35. Question
    1 points

    Mark the correct statement in case of demand flow system of oxygen supply regulator

  36. Question 36 of 60
    36. Question
    1 points

    Main ducal for cabin air supply where air temperature are above 200dig C are made of

  37. Question 37 of 60
    37. Question
    1 points

    The drag of those aircraft parts which do not distribute towards the lift is known as-

  38. Question 38 of 60
    38. Question
    1 points

    Choices most current statement regarding aircraft hydraulic system

  39. Question 39 of 60
    39. Question
    1 points

    In case of emergency situation where all methods of powering hydraulic system are lost, the system which is used to power any one hydraulic system;

  40. Question 40 of 60
    40. Question
    1 points

    Flight interphone

  41. Question 41 of 60
    41. Question
    1 points

    For controlling the probe heating system

  42. Question 42 of 60
    42. Question
    1 points

    the most aircraft wiper system fail to provide satisfactory vision in heavy rain due to –

  43. Question 43 of 60
    43. Question
    1 points

    YAW damper receives electrical deigns from-

  44. Question 44 of 60
    44. Question
    1 points

    In the longitudinal balance system, when the amount of trim is increased –

  45. Question 45 of 60
    45. Question
    1 points

    After a hydraulic accumulator has been installed and air chamber changed the main system hydraulic pressure gauge will not show a hydraulic pressure reading until

  46. Question 46 of 60
    46. Question
    1 points

    In the air conditioning system, the PACK valve is

  47. Question 47 of 60
    47. Question
    1 points

    Weather cracking of deicer boots rubber

  48. Question 48 of 60
    48. Question
    1 points

    In probe and drain heating system propeller boot received electric current from-

  49. Question 49 of 60
    49. Question
    1 points

    High volume ducting is used in distribution og medium pressure pneumatic system;-

  50. Question 50 of 60
    50. Question
    1 points

    In pneumatic vacuum system , to reduce the vacuum for the turn and bank indications

  51. Question 51 of 60
    51. Question
    1 points

    The localizer and glide slope beams are captured when the aircraft has descended to—– feet radio altitude

  52. Question 52 of 60
    52. Question
    1 points

    The various sources of air supply on a large transport category aircraft can be

  53. Question 53 of 60
    53. Question
    1 points

    A ram air turbine is installed in the aircraft to provide electrical power and hydraulic power –if

  54. Question 54 of 60
    54. Question
    1 points

    What happens of collective sticks is moved up

  55. Question 55 of 60
    55. Question
    1 points

    When windshield wiper switch is tuned the wiper motor

  56. Question 56 of 60
    56. Question
    1 points

    Hydraulic fuel must have following qualities;

  57. Question 57 of 60
    57. Question
    1 points

    In the air conditioning system , water separated used for-

  58. Question 58 of 60
    58. Question
    1 points

    A large aircraft is usually divided into zones with –

  59. Question 59 of 60
    59. Question
    1 points

    Examples of pressure sensing elements are;

  60. Question 60 of 60
    60. Question
    1 points

    Hydraulic system actuators are designed to use with hydraulic fluid, in emergency air-operation is permitted

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