Air Legislation
1. State of registry means
(a) country responsible for design of aircraft
(b) country on whose register the aircraft is entered
(c) country where the owners are based
2. Contacting state means
(a) country that leases aircraft on contract
(b) any state that is party tot e convention on international civil aviation
(c) country where federal aviation regulation apply
3. Certificate of release to service of aircrafts is raised when
(a) after a mandatory modification is completed
(b) after a mandatory airworthiness directive is accomplished
(c) after all the inspections are carried out on the aircraft an made ready for flight
4. Aircraft technical log sheer will not record the following information
(a) times when aircraft took off and landed
(b) particulars of defects encountered during flight
(c) reference number of the certificate of airworthiness
5. A type certificate is issued to aircraft by
(a) manufacturer of aircraft
(b) state of design
(c) state of registry
6. A certificate of airworthiness is issued to aircraft by
(a) state of design
(b) state of registry
(c) state of the operator
7. An aircraft weight schedule will be preserved for a period of
(a) 2 years
(b) until next overhaul
(c) period of 6 months after the next aircraft weighing occasion
8. Aircraft log book will be preserved for a period of
(a) 2 years from date of last entry
(b) 2 years from date when aircraft is destroyed or permanently withdrawn from service
(c) until aircraft is destroyed
9. For item below is not mandatory to keep a log book
(a) aircraft
(b) fuel pump
(c) engine
(d) variable pitch propeller
10. Master Minimum Equipment List (MMEL) is prepared by
(a) manufacturer
(b) operator
(c) state of registry
11. Minimum Equipment List (MEL) is approved by
(a) state of design
(b) state of registry
(c) manufacturer
12. ……… defects can be deferred in accordance with
(a) MEL
(b) release to service certificate
(c) chief engineer’s instructions
13. The maximum validity period of a certificate of airworthiness prior to renewal is
(a) 6 months
(b) 12 moths
(c) 24 moths
14. During refueling of aircraft bending and …….. are to take place to prevent
(a) fuel spillage
(b) build up of static electrically
(c) accumulation of fuel vapour
15. During towing of aircraft the person seated in the captain’s seat in the cockpit must be aware of
(a) aircraft flying controls
(b) aircraft starting procedures
(c) application of aircraft brakes
16. During night marshalling the following equipment is to be used
(a) marshalling bats
(b) illuminate wands
(c) hand signals
17. Aircraft Maintenance Engineer (AME) to release aircraft to service for flight should have
(a) rating endorsement on type of aircraft
(b) C category rating
(c) X category rating
18. An Approved Maintenance Organization will have its quality control functions and procedures listed in the
(a) maintenance control manual
(b) approved maintenance schedule
(c) manufacture’s maintenance manual for the aircraft
19. The regulatory authority will ensure compliance of mandatory requirement by the issue of
(a) service bulletin
(b) service information letter
(c) airworthiness directive
20. Mandatory service bulletins are issued by
(a) state of registry
(b) state of the operator
(c) manufacturer with approval of state of design
21. A serious accident is defined as
(a) passenger suffer death
(b) aircraft forced lading
(c) aircraft aborted take off
22. Certificate of maintenance is
(a) a certificate issued by the director general of civil aviation stating that the aircraft is maintained in an airworthiness condition
(b) a document signed by an appropriated licenced engineer stating that the aircraft has been maintained in accordance with the approved maintenance schedule
(c) a certificate signed by an appropriately licenced engineer stating that the aircraft is airworthy when released for service
23. What is the period of validity of a certificate of maintenance?
(a) Twenty four hors or one journey
(b) Thirty days or three hundred hours whichever is the earliest
(c) A period of time in days or flying hours whichever is the earliest
24. Under what conditions will certificate of maintenance becomes invalid?
(a) By expiration of the C of A
(b) By expiration of the period of validity of C of M
(c) By expiration of the period of validity or by invalidation of C of A
25. Minor modification to an aircraft
(a) should be done according to manufacturers recommendations and under the supervision of the chief inspector of the airline
(b) should be done according to the recommendation of the chief inspector and under the supervision of an Licenced aircraft maintenance engineer
(c) should be done under the supervision of an appropriately Licences aircraft maintenance engineer and the approval of the DCA
26. A certificates of maintenance is valid
(a) for the flight that it is issued
(b) for the twenty four hours
(c) for flying hours or days lapsed time whichever comes first
27. If a control system is disturbed at an outstation airfield
(a) the system should be double checked by an A M E only
(b) no double check required, the single check by the A M E being sufficient to return to base
(c) the double check may be carried out by the flight engineer or the captain
28. Who authorizes amendments to the maintenance schedule
(a) quality control manager
(b) production planning manager
(c) D C A
29. During duplicate inspection second inspection must be carried out
(a) independently
(b) independently and certified by a qualified person
(c) simultaneously and certified by a qualified person
30. After repairs of airframe or engines a licenced Aircraft Maintenance Engineer has the privilege of certifying it as:
(a) Serviceable
(b) Airworthy
(c) Proper functioning
31. Federal Aviation Administration (FAA) issues Airworthiness Directives;
(a) Only for American built aircraft.
(b) For passenger aircraft.
(c) Only for Aircraft which hold type certificate issued by that
Administration (FAA)
32. An approved certificate certifies that:
(a) Materials, Parts, conform to required standard.
(b) Materials, Parts, come from an approved source.
(c) Items are serviceable on delivery.
33. A certificate of design is raised:
(a) By the C.A.A.
(B) By the Operator.
(c) By the Manufacturer.
34. An approved store:
(a) Is required by every approved organization.
(b) Must contain quarantine and bonded store.
(c) Is the responsibility of Quality Assurance Department.
35. Technical logs are raised in:
(a) Duplicate.
(b) Triplicate.
(c) Only if aircraft is to land away from home.
36. The Aircraft Tech log is originated by the:
(a) Civil Aviation Authority.
(b) Operator of Aircraft.
(c) Manufacturer of Aircraft.
37. A concession is granted when time expires according to:
(a) Number of flying hours or calendar dates.
(b) Calendar dates only.
(c) Number of flying hours only.
38. If a Aircraft is grounded due to time of a component, a concession can be granted if:
(a) Provided with the condition and the part number of component.
(b) Provided with the history and the condition of the component.
(c) Provided with the history and the part number of the component.
39. Limitations of an aircraft would be found:
(a) In the certificate of Maintenance of Registration.
(b) In the certificate of compliance.
(c) In the certificate of Airworthiness or in the Flight Manual.
40. A signature for the work carried out for the embodiment of a modification is made;
(a) In the Certificate of Maintenance.
(b) In the Civil Modification Record.
(c) On a Certificate of Compliance.
41. On completion of a Modification full details are entered in the:
(a) Certificate of Registration.
(b) Appropriate Log Book.
(c) Certificate of fitness for flight.
42. The Maintenance Schedule
(a) And the Maintenance Manual must both be approved by DCA
(b) And the Maintenance Manual do not need DCA approval.
(c) Must be approved, the Maintenance Manual need not be DCA approved.
43. Equipment which has been proved to conform to specification is kept in a:
(a) quarantine store
(b) bonded store
(c) receipt and dispatch store.
44. Limitations of an aircraft would be found:
(a) in the certificate of Maintenance or Registration
(b) in the certificate of compliance
(c) in the certificate of Airworthiness or in the flight manual.
45. A signature for the work carried out for the embodiment of a modification is made:
(a) in the certificate of maintenance
(b) in the civil modification record
(c) on a certificate of compliance.
46. A technical log is a:
(a) complete technical history of the aircraft/engine
(b) day to day technical history of the aircraft
(c) book containing limitating limitations, information and procedures necessary for the safe operation of the aircraft.
47. On completion of a modification full details are entered in the:
(a) certificate of registration
(b) appropriate log book
(c) certificate of fitness for flight.
48. The manufacturers document for notifying operators of technical recommendations is the:
(a) Airworthiness notice
(b) Service Bulletin
(c) Modification Leaflet
49. The period of validity of the certificate of maintenance is found in the:
(a) maintenance manual
(b) type certificate
(c) maintenance schedule
50. The period of validity of a certificate of maintenance:
(a) expires after a specified number in flying hours or a period of time whichever may be earlier
(b) expires only after a specified number of flying hours
(c) expires only after a specified number of days.
