MODULE 15 B1 MOCK TEST - 2
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Information
- Number of Multiple choice Questions – 92
- Passing Marks – 69
- Time allowed – 115 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
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- 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 92
1. Question
1 pointsAn oil inlet temperature indicator frequently provided to show temperature of oil
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Question 2 of 92
2. Question
1 pointsThe ability of an engine to run smoothly and give desired performance at all speed from idling to full power output
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Question 3 of 92
3. Question
1 pointsThe thrust of gas turbine engine
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Question 4 of 92
4. Question
1 pointsMTCS ( why we use synthetic oil)
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Question 5 of 92
5. Question
1 pointsIn turboshaft engine output is measured in
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Question 6 of 92
6. Question
1 pointsLoss in centrifugal compressor, due to
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Question 7 of 92
7. Question
1 pointsThree main cause of vapor lock
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Question 8 of 92
8. Question
1 pointsLow volatile fuel
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Question 9 of 92
9. Question
1 pointsDisadvantage of divided type intake
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Question 10 of 92
10. Question
1 pointsThe thrust of engine calculated by
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Question 11 of 92
11. Question
1 pointsThermal efficiency is depend on
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Question 12 of 92
12. Question
1 pointsThe type of inlet duct use in gas turbine engine
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Question 13 of 92
13. Question
1 pointsEngine installation with cable hoist
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Question 14 of 92
14. Question
1 pointsCompressor washing
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Question 15 of 92
15. Question
1 pointsWhich bearing use in very high heat resistance
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Question 16 of 92
16. Question
1 pointsMaterial of Jet Pipe
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Question 17 of 92
17. Question
1 pointsSpecific gravity of fuel is measured by
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Question 18 of 92
18. Question
1 pointsIn compressor clearance between rotor and case is maintained by
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Question 19 of 92
19. Question
1 pointsAir enter into the Can type combustion chamber by
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Question 20 of 92
20. Question
1 pointsAdvantage of Can-annular combustion chamber
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Question 21 of 92
21. Question
1 pointsMTCS
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Question 22 of 92
22. Question
1 pointsInstalled engine represerved
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Question 23 of 92
23. Question
1 pointsMTCS ( engine mount inspection)
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Question 24 of 92
24. Question
1 pointsIndication of the compressor stall
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Question 25 of 92
25. Question
1 pointsTransistor ignition excitor unit consist of
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Question 26 of 92
26. Question
1 pointsAt which position fuel injected in the combustion chamber
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Question 27 of 92
27. Question
1 pointsMost critical factor of the gas turbine engine
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Question 28 of 92
28. Question
1 pointsIn turboprop engine SHP taken from
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Question 29 of 92
29. Question
1 pointsThe air use for cooling, anti icing pressurising taken from
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Question 30 of 92
30. Question
1 pointsCorrosion preventive compound are
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Question 31 of 92
31. Question
1 pointsStall is prevented by
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Question 32 of 92
32. Question
1 pointsWhich starter is used once
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Question 33 of 92
33. Question
1 pointsEngine cowling
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Question 34 of 92
34. Question
1 pointsWhich is not function of centrifugal switch
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Question 35 of 92
35. Question
1 pointsAn engine normally be sufficiently coal to shut engine has been operated above approx 85%rpm for exceeding 1 min time for cooling
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Question 36 of 92
36. Question
1 pointsFunction of centrifugal switch in APU
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Question 37 of 92
37. Question
1 pointsMTCS
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Question 38 of 92
38. Question
1 pointsFunction of the APU
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Question 39 of 92
39. Question
1 pointsBall bearing takes load
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Question 40 of 92
40. Question
1 pointsVariable geometry duct is called
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Question 41 of 92
41. Question
1 pointsWhich type of fire detectors use in the engine
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Question 42 of 92
42. Question
1 pointsDrive allow engine to drive rotor but prevent from driving engine called?
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Question 43 of 92
43. Question
1 pointsGrowth of Blade term applied to?
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Question 44 of 92
44. Question
1 pointsEngine Vibration throughout RPM range, but indicated amplitude reduces as RPM is reduced cause maybe?
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Question 45 of 92
45. Question
1 pointsDisadvantages of Water Injection System?
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Question 46 of 92
46. Question
1 pointsMost Helicopter use of Short shaft system to deliver power to transmission & have?
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Question 47 of 92
47. Question
1 pointsIgnition system, Spark ignitions are generally located in?
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Question 48 of 92
48. Question
1 pointsFenwel Spot detector?
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Question 49 of 92
49. Question
1 pointsBeta Range of throttle quadrant, blade angle governed by?
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Question 50 of 92
50. Question
1 pointsTo dissipate residual charge on trigger capacitor?
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Question 51 of 92
51. Question
1 pointsMTCS about Carbon Seal
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Question 52 of 92
52. Question
1 pointsMajor difference among Pressure Relief System, full flow and total loss?
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Question 53 of 92
53. Question
1 pointsForward stage of compressor deliver more air and it can be effectively handle by rear stage of compressor?
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Question 54 of 92
54. Question
1 pointsEEC of APU monitor?
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Question 55 of 92
55. Question
1 pointsAdding water at Compressor Inlet?
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Question 56 of 92
56. Question
1 pointsHumidity Indicator on staved engine is inspected
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Question 57 of 92
57. Question
1 pointsProlong contact with turbine oil with the skin?
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Question 58 of 92
58. Question
1 pointsConvection cooling or Film cooling used to cool?
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Question 59 of 92
59. Question
1 pointsWater injection is designed to function at?
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Question 60 of 92
60. Question
1 pointsMTCS
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Question 61 of 92
61. Question
1 pointsInterconnector tube used in type of combustor?
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Question 62 of 92
62. Question
1 pointsAmount of thrust depend on?
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Question 63 of 92
63. Question
1 pointsIn Pressure Relief Valve system, Oil flow rate at high speed?
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Question 64 of 92
64. Question
1 pointsIntake of GTE designed to?
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Question 65 of 92
65. Question
1 points2/3rd of energy extracted by?
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Question 66 of 92
66. Question
1 pointsPurpose of cross feed valve in fuel system?
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Question 67 of 92
67. Question
1 pointsExhaust duct is strengthened by?
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Question 68 of 92
68. Question
1 pointsJet Engine thermal efficiencies is limited by ability of?
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Question 69 of 92
69. Question
1 pointsHighest Temperature in GTE?
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Question 70 of 92
70. Question
1 pointsCentrally Inner cone of Exhaust?
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Question 71 of 92
71. Question
1 pointsTemperature of Exhaust monitors to prevent?
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Question 72 of 92
72. Question
1 pointsWhen bleed air is ducted into vane and exit through porous material?
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Question 73 of 92
73. Question
1 pointsBearing used on speed approach 45000RPM?
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Question 74 of 92
74. Question
1 pointsFADEC contain 2 channel A&B
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Question 75 of 92
75. Question
1 pointsAviation fuel must have?
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Question 76 of 92
76. Question
1 pointsAPU load compressor provides?
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Question 77 of 92
77. Question
1 pointsMarking on combustion chamber should be done with?
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Question 78 of 92
78. Question
1 pointsTail Cone?
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Question 79 of 92
79. Question
1 pointsWhich type of duct used in high speed, single engine aircraft in which the pilot sit lower in fuselage and close to the nose?
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Question 80 of 92
80. Question
1 pointsEngine starting electric circuit?
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Question 81 of 92
81. Question
1 pointsMachined surface of rotor of GTE?
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Question 82 of 92
82. Question
1 pointsCan Annular contains forward face ?
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Question 83 of 92
83. Question
1 pointsThrust produced by turbojet
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Question 84 of 92
84. Question
1 pointsTurboprop
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Question 85 of 92
85. Question
1 pointsIn thrust augmentation, after burner produces thrust?
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Question 86 of 92
86. Question
1 pointsBearing used which is surround by thin film of oil to reduce
vibration? -
Question 87 of 92
87. Question
1 pointsCooling air is taken by
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Question 88 of 92
88. Question
1 pointsCentrifugal compressor MTCS
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Question 89 of 92
89. Question
1 pointsSupersonic airpass through Normal shockwave?
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Question 90 of 92
90. Question
1 pointsCross feed valve function?
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Question 91 of 92
91. Question
1 pointsThe primary one task inlet duct during flight operation which covert kinetic energy into?
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Question 92 of 92
92. Question
1 pointsAmount of air passing depends on three factors?