Module -10 Final Practice Exam (Aviation Legislation 40 Questions 50 Mints)

 

Module - 10 (Aviation Legislation)

Final Practice Exam Test

  

 

1. Which is true about the privileges of Category C certifying staff ?
   1.   They can supervise trainee examinations
   2.   They can sign line maintenance tasks
   3.   They can certify base maintenance release
2. A Part-145 approval covers?
   1.   the major part of the organisation
   2.   base maintenance
   3.   only line maintenance
3. Which document defines the privileges and limitations of licence holders ?
   1.   Part-66
   2.   Part-147
   3.   Part-145
4. An Airworthiness Review Certificate (ARC) may be extended by ?
   1.   The aircraft manufacturer
   2.   CAMO approved under Part-M Subpart G
   3.   Any approved maintenance organization
5. Which Part specifies requirements for the certification of design organizations ?
   1.   Part-145
   2.   Part-M Subpart G
   3.   Part-21 Subpart J
6. The continuing airworthiness of aircraft components is managed under ?
   1.   Part-66
   2.   Part-147
   3.   Part-M
7. Who issues Airworthiness Directives in the European system ?
   1.   The operator
   2.   EASA
   3.   The manufacturer
8. Which Subpart of Part-M deals with Airworthiness Review ?
   1.   Subpart F
   2.   Subpart G
   3.   Subpart I
9. An EASA Form 1 is invalid if ?
   1.   It was issued by a non-approved organization
   2.   The item has expired shelf life
   3.   The form is handwritten
10. Which Part defines procedures for changes to type design ?
    1.   Part-M
    2.   Part-145
    3.   Part-21
11. In Germany, aircraft registration begins with ?
    1.   D-
    2.   I-
    3.   F-
12. An aircraft logbook records ?
    1.   Passenger details
    2.   Crew training
    3.   Flight and maintenance data
13. The validity of an ARC (Aircraft Review Certificate) is ?
    
    
    1.   2 years
    2.   1 year
    3.   3 years
14. JAR OPS subpart J covers ?
    1.   Instruments and equipment
    2.   Mass and balance
    3.   Maintenance
15. The CAMO is responsible for ?
    1.   Continuing airworthiness management
    2.   Air traffic control
    3.   Aircraft production
16. MOE stands for ?
    
    1.   Manual of Engineering
    2.   Maintenance Operation Equipment
    3.   Maintenance Organization Exposition
17. Which document must always be carried on board ?
    1.   Maintenance logbook
    2.   Certificate of Airworthiness
    3.   Pilot’s licence
18. The term “airworthiness” means ?
    
    1.   Fit for flight and safe operation
    2.   Approved by EASA
    3.   Designed in Europe
19. Part-66 refers to ?
    1.   Air operations
    2.   Continuing airworthiness
    3.   Aircraft maintenance licences
20. An aircraft Radio License has to be renewed ?
    
    1.   only on change of aircraft ownership
    2.   every five years
    3.   every three years
21. JAA was replaced by ?
    
    1.   IATA
    2.   ICAO
    3.   EASA
22. Which organization regulates civil aviation in Europe ?
    1.   FAA
    2.   EASA
    3.   IATA
23. Which Annex deals with personnel licensing ?
    
    1.   Annex 7
    2.   Annex 6
    3.   Annex 1
24. Which Annex of ICAO deals with airworthiness ?
    
    1.   Annex 9
    2.   Annex 8
    3.   Annex 7
25. The headquarters of ICAO is in ?
    
    1.   London
    2.   Brussels
    3.   Montreal
26. ICAO stands for ?
    1.   International Civil Aviation Organization
    2.   International Control of Air Operations
    3.   International Company of Aircraft Operators
27. Which document identifies aircraft nationality and registration ?
    1.   ARC
    2.   C of R
    3.   C of A
28. The main objective of ICAO is to ?
    1.   Set international aviation safety standards
    2.   Approve European aviation organizations
    3.   Train maintenance engineers
29. Who produces and prints maintenance schedules ?
    1.   CAA for Air Operators Certificate Organizations
    2.   CAA and approved by the manufacturer
    3.   The Part-M approved organisation
30. Details of placards and markings on aircraft will be found in ?
    1.   Operations Manual
    2.   ATA Chapter 11 of the AMM
    3.   Approved Maintenance Manual
31. CAP 360 relates to ?
    
    1.   EASA aircraft only
    2.   Crop spraying aircraft only
    3.   Public Transport aircraft
32. A service bulletin contains ?
    1.   A list of maintenance tasks to be carried out on a particular aircraft
    2.   Information concerning the airworthiness of aircraft and are distributed by the CAA
    3.   A detailed description of a problem and corrective action to be taken
33. The telecommunications log book is considered to be part of the ?
    1.   Radio Licence
    2.   Public Address Licence
    3.   Radio approved document
34. The period of validity of a Certificate of Fitness for Flight under 'A' Conditions is ?
    1.   1 flight
    2.   7 days
    3.   5 days
35. The excess ILS deviation light is coloured ?
    1.   Red and flashing
    2.   Amber and flashing
    3.   Amber and continuous
36. Category 2 auto-land with a decision height of 100 ft has a visual line up approach limit of ?
    1.   400 meters
    2.   300 meters
    3.   500 meters
37. CAA Additional Airworthiness Directives are printed on ?
    1.   Blue Papers
    2.   White Papers
    3.   Yellow Papers
38. A Noise Certificate is a requirement of ?
    1.   IR Part-M
    2.   JAR OPS
    3.   IR Part-21
39. The aircraft owner's Name Plate must be fixed ?
    1.   On the instrument panel
    2.   Near the main entrance of the aircraft
    3.   On the rear fuselage
40. Which of the following does not require a Noise Certificate ?
    1.   A small business jet aircraft
    2.   A fixed wing aircraft under 2730 kg
    3.   A helicopter under 5700 kg

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Module 10 Aviation Legislation100 important sentences (EASA Part-66 Module 10)

 ✈️ 100 Important Sentences – Aviation Legislation

1. EASA ensures safety in European civil aviation operations.

2. ICAO sets international standards for air safety.

3. Part-66 defines aircraft maintenance engineer licensing.

4. Part-145 governs approved aircraft maintenance organizations.

5. Part-M ensures continuing airworthiness of aircraft.

6. Part-21 covers design and production approvals.

7. Aircraft must have a valid airworthiness certificate.

8. Pilots require licences under ICAO Annex One.

9. Annex Eight relates to aircraft airworthiness certification.

10. EASA replaced JAA as European aviation authority.

11. The FAA regulates aviation safety within America.

12. ICAO headquarters are located in Montreal, Canada.

13. Every aircraft must display a registration mark.

14. Certificate of Airworthiness proves aircraft is airworthy.

15. Maintenance release certifies safe aircraft after maintenance.

16. Airworthiness Review Certificate remains valid for one year.

17. Operator ensures aircraft’s continuing airworthiness and safety.

18. Type Certificate issued for specific aircraft models.

19. Airworthiness Directives ensure mandatory safety compliance worldwide.

20. Maintenance Organization Exposition describes approved procedures clearly.

21. EASA Form 1 certifies release to service.

22. CAMO manages aircraft’s continuing airworthiness requirements daily.

23. Operator is responsible for safe flight operations.

24. Aircraft logbooks record maintenance and operational history.

25. Maintenance records must be retained for inspection purposes.

26. Each maintenance organization needs competent certifying staff.

27. Human factors training is mandatory under Part-145.

28. Quality system ensures maintenance organization’s regulatory compliance.

29. Safety management system reduces operational safety risks.

30. Approved data must be used for maintenance.

31. Part-66 licence categories define maintenance privileges precisely.

32. Category B1 engineers handle mechanical aircraft systems.

33. Category B2 engineers maintain avionic aircraft systems.

34. Category C certifies base maintenance release authority.

35. Part-147 covers training organization approval and standards.

36. Training organizations must follow approved EASA syllabi.

37. Examination questions must meet required knowledge levels.

38. Certificates of recognition issued after approved training.

39. Licence validity depends on competence and currency.

40. Civil Aviation Authority issues licences and approvals.

41. Aircraft maintenance must meet manufacturer’s approved data.

42. Unserviceable components must be clearly identified immediately.

43. All defects must be rectified before release.

44. Technical log records aircraft flight and maintenance details.

45. Maintenance intervals defined by approved maintenance program.

46. Certificate of Release to Service authorizes aircraft operation.

47. Non-certifying staff work under certifying staff supervision.

48. Maintenance planning ensures compliance with required schedules.

49. Air operator’s certificate required for commercial operations.

50. Continuing airworthiness ensures safe aircraft operational life.

51. EASA regulates civil aviation across European countries.

52. Competent authority audits approved organizations for compliance.

53. Licence holder must maintain recent maintenance experience.

54. Safety oversight prevents aviation system rule violations.

55. National aviation authorities cooperate under EASA framework.

56. Part-145 approval valid only within EASA states.

57. Organizations outside Europe require EASA foreign approval.

58. Part-21 governs design, production, and airworthiness certification.

59. Design organizations issue minor change approvals independently.

60. Production organizations issue authorized release certificates accordingly.

61. Airworthiness directives correct unsafe aircraft conditions promptly.

62. Mandatory inspections prevent recurrence of safety issues.

63. Aircraft type design ensures performance and structural safety.

64. Environmental certification includes aircraft noise and emissions.

65. Aircraft registration identifies nationality and ownership legally.

66. Registered owner responsible for aircraft airworthiness status.

67. Aircraft documents must be kept on board.

68. Certificate of registration proves aircraft legal ownership.

69. Certificate of insurance required for aircraft operation.

70. Flight manual provides operational limitations and procedures.

71. Maintenance data includes drawings, manuals, and bulletins.

72. Service bulletins issued by manufacturer for improvements.

73. Operators may adopt manufacturer’s recommended maintenance programs.

74. Maintenance tasks categorized as line or base maintenance.

75. Line maintenance includes daily and transit checks.

76. Base maintenance involves detailed structural aircraft inspection.

77. Independent inspection required after critical maintenance tasks.

78. Competence assessments ensure engineers perform tasks correctly.

79. Human error minimized through proper training procedures.

80. Fatigue management critical for maintenance staff performance.

81. Safety culture promotes reporting of maintenance errors.

82. Part-M Subpart G defines CAMO requirements clearly.

83. Subpart I of Part-M covers Airworthiness Review.

84. ARC may be extended by approved organizations.

85. Aircraft without ARC cannot be legally operated.

86. Technical records provide history of aircraft maintenance actions.

87. Data accuracy vital for regulatory and operational safety.

88. Maintenance schedule deviations require authority’s prior approval.

89. Pilot reports may identify aircraft technical discrepancies.

90. Deferred defects must be controlled and rectified.

91. Airworthiness Review staff require appropriate authorization levels.

92. Non-EASA aircraft must meet equivalent safety standards.

93. Maintenance tools must be calibrated and controlled properly.

94. Safety equipment must meet certified operational requirements.

95. Personnel must understand relevant national aviation regulations.

96. Quality audits evaluate compliance with approved procedures.

97. Part-66 exams test knowledge of aviation legislation.

98. Engineering ethics promote integrity and professional responsibility.

99. Record falsification results in severe legal penalties.

100. Continuous learning ensures competence in aviation legislation.

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Module 11 – Aircraft Structures & Systems 100 sentences cover Aircraft structures and systems topics.

 1. Aircraft Structures

1. Fuselage provides strength, rigidity, and safe enclosure for crew, passengers, and cargo.

2. Semi-monocoque fuselage construction uses frames, stringers, bulkheads, and skin for strength.

3. Wing structure contains spars, ribs, and stringers to maintain aerodynamic shape.

4. Empennage includes horizontal stabilizer, vertical stabilizer, rudder, and elevator.

5. Primary flight controls are ailerons, elevator, and rudder for maneuvering.

6. Secondary flight controls include flaps, slats, spoilers, and trim tabs.

7. Landing gear absorbs landing loads, provides taxi support, and ground clearance.

8. Hydraulic actuators extend and retract landing gear during operation.

9. Aircraft doors use locking mechanisms to withstand cabin pressurization loads.

10. Composite materials reduce weight, improve corrosion resistance, and increase strength.

2. Hydraulic Systems

11. Hydraulic system uses pressurized fluid to transmit force and motion.

12. Pascal’s law states pressure applied to fluid is transmitted equally.

13. Hydraulic reservoirs store fluid, maintain pressure, and remove air bubbles.

14. Hydraulic pumps convert mechanical energy into fluid power pressure.

15. Filters remove contaminants, dirt, and particles from hydraulic system.

16. Hydraulic accumulators store pressure, absorb shocks, and damp pulsations.

17. Actuators convert hydraulic pressure into mechanical linear or rotary motion.

18. Pressure relief valves prevent over-pressurization and system damage.

19. Hydraulic lines are color-coded and labeled for maintenance safety.

20. Skydrol hydraulic fluid is fire resistant but corrosive to skin.

3. Pneumatic Systems

21. Pneumatic systems use compressed air for brakes, engine starting, and de-icing.

22. Sources of pneumatic power include engine bleed air and APU.

23. Pressure regulators maintain required pneumatic pressure during operation.

24. Moisture separators remove water vapor to avoid icing problems.

25. Pneumatic accumulators stabilize system pressure fluctuations effectively.

26. Over-pressure relief valves protect pneumatic system against excessive pressure.

27. Pneumatic system operates wing anti-ice boots using compressed air.

28. Engine cross-bleed valve controls pneumatic supply between engines.

29. Pneumatic leak detection uses overheat sensing loops along ducts.

30. Pneumatic manifolds distribute bleed air to multiple aircraft systems.

4. Landing Gear Systems

31. Retractable landing gear reduces drag and improves aerodynamic performance.

32. Nose gear provides steering control during taxiing and take-off.

33. Main gear supports aircraft weight during landing and ground operations.

34. Oleo strut absorbs landing shocks using hydraulic oil and nitrogen.

35. Landing gear doors reduce drag and protect retracted gear.

36. Anti-skid system prevents wheel lock-up and reduces tire wear.

37. Brake units are multi-disc or carbon disc assemblies for stopping.

38. Emergency extension system uses free-fall, pneumatic, or manual methods.

39. Proximity sensors provide landing gear position indication to cockpit.

40. Tire pressure must be checked regularly for safety and performance.

5. Electrical Systems

41. Aircraft electrical system provides power to avionics, lights, and instruments.

42. Direct Current (DC) is supplied by batteries and DC generators.

43. Alternating Current (AC) is supplied by alternators and inverters.

44. Transformer rectifier units convert AC power into regulated DC.

45. Circuit breakers protect wiring and components from overcurrent.

46. Bus bars distribute electrical power to aircraft subsystems.

47. Static inverters convert DC battery power into AC emergency power.

48. Ground power unit supplies external electrical power during maintenance.

49. Auxiliary Power Unit provides electrical and pneumatic power on ground.

50. Emergency power is supplied by battery when generators fail.

6. Avionics Systems

51. Pitot-static system measures airspeed, altitude, and vertical speed.

52. Altimeter displays aircraft altitude above mean sea level.

53. Airspeed indicator uses dynamic and static pressure difference.

54. Vertical speed indicator shows climb or descent rate.

55. Attitude indicator provides artificial horizon using gyroscopes.

56. Heading indicator gives aircraft directional reference during flight.

57. Radio altimeter measures height above ground using radio waves.

58. Flight Management System integrates navigation, performance, and guidance.

59. GPS provides global navigation signals using satellites.

60. Autopilot reduces pilot workload by automatically controlling flight path.

7. Fuel Systems

61. Fuel tanks store fuel inside wings, fuselage, or stabilizers.

62. Boost pumps deliver pressurized fuel to engines and APU.

63. Cross-feed valves allow fuel transfer between tanks during flight.

64. Fuel control unit meters correct amount of fuel to engine.

65. Fuel jettison system allows safe fuel dumping during emergencies.

66. Fuel filters remove water, contaminants, and particles from fuel.

67. Fuel quantity is measured by capacitance probes inside tanks.

68. Vent system prevents vacuum formation inside fuel tanks.

69. Fuel heaters prevent ice formation inside fuel lines.

70. Gravity feed ensures emergency fuel supply if pumps fail.

8. Environmental Systems

71. Pressurization system maintains cabin altitude and passenger comfort.

72. Outflow valve regulates cabin pressure by controlling air discharge.

73. Safety valve prevents excessive over-pressurization or negative pressure.

74. Air conditioning packs provide conditioned air using bleed air.

75. Mixing unit blends hot bleed air with cold conditioned air.

76. Recirculation fans reduce bleed air demand and save fuel.

77. Cabin temperature is controlled automatically or manually by pilots.

78. Oxygen system supplies crew and passengers during depressurization.

79. Chemical oxygen generators supply passenger masks during emergencies.

80. Portable oxygen bottles are available for crew mobility.

9. Fire Protection Systems

81. Fire detection uses continuous-loop, spot, and flame detectors.

82. Smoke detectors are installed in cargo compartments and lavatories.

83. Fire bottles contain Halon extinguishing agent under pressure.

84. Squibs rupture fire bottles for agent discharge when activated.

85. Engine fire handle closes fuel, hydraulic, and bleed air valves.

86. APU fire extinguishing system is independent from engine system.

87. Cargo fire suppression system uses multiple Halon bottles sequentially.

88. Fire warning indications are displayed on cockpit annunciator panels.

89. Built-in test equipment checks fire detection circuits automatically.

90. Cabin crew training includes fire drill and extinguisher operation.

10. Ice and Rain Protection

91. Pneumatic boots break ice by inflation and deflation cycles.

92. Thermal anti-ice uses hot engine bleed air on wings.

93. Windshield heat prevents ice formation and removes fogging.

94. Pitot probes use electrical heating for anti-ice protection.

95. Propeller de-icing uses electrical heating elements on blades.

96. Rain removal is achieved by windshield wipers and chemical rain repellent.

97. Thermal ice protection prevents engine inlet icing.

98. Electrical anti-ice systems protect static ports and sensors.

99. Ice detectors provide warning of ice accumulation to crew.

100. Integrated system combines pneumatic, thermal, and electrical anti-ice methods.

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