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1.When reviewing the logbook of an aircraft on a periodic inspection, you note that theATC transponder was tested 12 months ago. During the inspection you will be required to carry out: (A) no transponder maintenance as it Is only required to be tested every 24 months. (B) no transponder maintenance as it is only required to be tested every three years. (c)a transponder test using bench test equipment. (d) a transponder test using either bench or portable test equipment.

2.The Chief Engineer of a Part 145 maintenance organisation is considered a senior person in the organisation. To hold this position the person must be. (A)acceptable to the Director and should have had at least five years experience relevant to the position held. (B)acceptable to the Chief Executive and should have had at least four years experience relevant to the position held. (c) specified in the company exposition and should have had a minimum of two years experience relevant to the position held. (D) acceptable to the Director and should have had at least six years experience relevant to the position held.

3.You have been overseas for the last 13 months on a working holiday and not been associated with aviation. Priorto going overseas you were working for an aircraft maintenance firm as a LAME, On return from overseas in order lo exercise the privileges of your life time aircraft maintenance engineer licence you. (A)must pass the Airworthiness legislation wrilten examination again. (B) are not required to do anything as long as you are familiar with the respective aircraft or components. (c) must work for six months associated with aircraft maintenance prior to exercising the privileges. (d)must work forthree months associated with aircraft maintenance prior to exercising the privileges.

4.As a certifying engineer authorised under CA Rule Part 145, the maintenance organisation you work for is required to maintain records covering your. (a) experience, qualiflcations, training and current authorisations, and retain these records for five years after the work is released to service,. (B)experience, licence ratings, training and authorisations, and retain these records for two years after the work is released to service. (C) experience, licence ratings, company training and authorisations, and retain these records for 12 months after the work is released to service. (D) experience, licence ratings, training and company approvals, and retain these records for 6 months after the work is released to service.

5.After replacing an elevator trim tab due to damage, you are required to carry out a duplicate safety inspection. The extent of the duplicate inspection would cover: (A)all parts of the control system, including both the trim tab system and elevator system, to ensure freedom from defects. (B)all parts of the control system disturbed to ensure freedom from defects, and the complete system for correct operationand correct sense. (C) all parts of the control system disturbed for any possibility of fouling orjamming, and the complete system for correct locking. (D)all parts of the control system disturbed for correct locking, and the complete system for correct rigging.

6.There is a requirement to transfer one of the aircraft that you maintain from an annual inspection cycle to a progressive inspection cycle. The annual inspection on the aircraft was completed only three months ago, therefore to transfer the aircraft onto the progressive cycle: (A)no additional inspection is necessary as the aircraft has had an annual inspection within the last three months. (B)a complete inspection of the aircraft is required prior to starting the progressive cycle. (C)only a partial inspection of the aircraft is required, covering components and areas of the aircraft which will not be inspected during the next 12 months. (D) a complete inspection of the aircraft is required, but the detailed inspections in the progressive inspection programme can be deferred for up to 12 months.

7.As an appropriately rated LAME you have just completed the airframe content of a 100-hour inspection. The release to service statement you certify in the aircraft logbook should specify: (A) hat the work has been performed in accordance with current CA Rules and approved maintenance procedures. (B)the work performed on the airframe was carried out in accordance with all current CA Rules and in respect of that work the aircraft was fit for release to service. (C) all work carried out on the entire aircraft has been performed in accordance with current CA Rules and the entire aircraft is fit for release to service. (D)work performed is fit for release to service and the entire aircraft complies with all curront CA Rules.

8.An aviation maintenance specialist certificate AMS-4 issued by CAA for certifying maintenance on a large gas turbine engine would: (A)normally be valid for life. (B) automatically expire on the grant of the relevant rating. (C) be valid until the expiry date stated on the certificate. (D) be valid for a period of up lo 24 months.

9.After submitting a defect report to CAA for a cracked cylinder head, you are required to retain the damaged component for a period of: (A) 14 days. (B) 28 days. (C)30 days. (D) 90 days.

10.After fitting new mainplanes to an aircraft which is used on International flights, registration markings will be painted: (A) on the lower surface of the right-hand wing structure with the tops of the letters towards the trailing edge. (B) on the upper surface of the left-hand wing structure with the tops of the letters towards the leading edge. (C) on the upper surface of the right-hand wing structure with the letters equidistant from the leading and trailing edges. (D) on the lower surface of the left-hand wing structure with the tops of the letters towards the leading edge.

11. Which of the following documents must be carried on an aircraft?. (A) Flight manual, airworthiness certificate, technical log and type acceptance certificate. (B) Technical log, flight manual, certificate of registration and airworthiness certificate. (C) Aircraft logbooks, flight manual, certificate of registration and airworthiness certificate. (D)Radio station approval, certificate of registration, flight manual and weight and balance certificate.

12. To determine that a PNG registered aircraft has the correct flight manual, reference should be made to the;. (A)aircraft logbook. (B) technical log. (C) airworthiness certificate. (D) type certificate.

13. A minimum equipment list {MEL) for an aircraft contains equipment that may be partially or fully inoperative and the MEL would normally be approved by: (A) the aircraft operato. (B) an aircraft design organisation. (C) a Part 145 organisation. (D) the manufacturer of the aircraft.

14.Which one of the following activities must be performed as part of a maintenance review?. (A)Aircraft re-weigh. (B) Check that the flight manual is the current version for the aircraft. (C) Compass compensation. (D) Periodic inspection.

15. To gain a company authorisation to certify the release to service of an aircraft after maintenance was performed in PNG, you must have: (A) an AME licence in an appropriate category and with appropriate ratings issued under Part 66. (B) only a basic licence in the appropriate category. (C) a qualification that is at least equal to that required by Part 66 for the grant of a basic AME licence without a rating. (D) 36 months of practical aviation related experience appropriate to the authorisation sought.

16. When the Director issues an Airworthiness Directive, he must specify: (A) the aircraft hours at which AD compliance must be carried out. (B) who is responsible for AD compliance. (C) the date by which each aircraft operator must comply. (D)allowable latitudes for compliance.

17.Under which one of the following circumstances would a person be permitted to perform and certify maintenance on an aircraft?. (A)Hold a current aircraft maintenance organisation certificate that is used within a Part 43 organisatio. (B) Hold a current Part 66 licence and appropriate rating that is used within a Part 145 organisatio. (C) Hold an appropriate Part 145 maintenance specialist certificate that Is used within a Part 135 organisation. (D)Hold a current Part 61 licence and appropriate rating that Is used within a Part 43 organisation.

18. A Part 66 aircraft maintenance engineer licence may be issued In one or more of the following categories?. (A)Aeroplane, rotorcraft, powerplant, avionics. (B) Airframe, powerplant. (C) Mechanical, avionics, lighter than air. (D) Mechanical, electrical, instrument, radio.

19- In order to certify the release-to-service of a repair to a Cessna 206 flight control, tho engineer would be required to hold a;. (A) chanical General (Aeroplanes) Piston Engine Powered rating. (B) Mechanical General (Powerplant) rating. (C) Specific Type Rating. (D) Mechanical General (Aeroplanes) Turbine Engine Powered rating.

20. Which one of the following criteria would an air operator be required to specify in a maintenance programme for their aircraft?. (A) The training requirements for certifying personnel. (B) Procedures for the calibration of special tost equipment. (C) Procedures for the issue of the airworthiness certificate. (D) Instructions for exceeding an inspection interval.

21. The party responsible for ensuring that allapplicable ADs relating to an aircraft or its components are [ complied with is the: (A) Civil Aviation Authority. (B) designated maintenance organisation. (C)operator of that aircraft. (D) Pilot-in-Command of the aircraft operation.

22. When transferring details of maintenance from a technical log to the aircraft logbook, the statement of release-to-service on the technical log: (A ) IS eferenced In the logbook. (B) reissued in the logbook. (C) deleted off the technical log. (D) taken for granted in the logbook.

23. Which one of the following criteria would be considered a "basic essential" of a Part 145 internal quality assurance system?. (A) Procedures for the performance of periodic inspections. (B) The aircraft maintenance programme. (C) An internal audit programme. (D )Part 66 licensing procedures for certifyingstaff.

24.First aid kits, when required to be carried on aircraft, shall be inspected: (A) within the preceding six months. (B)only when used by the crew or a component of the kit has reached its expiry date. (C) within the preceding 12 months. (D) within the preceding 24 months.

25 An inspection called up under the provisions of a maintenance programme would be defined as a: (A) periodic inspection. (B) special inspection. (C) required inspection. (D) routine inspection.

26. To gain sufficient experience for a type rating to be issued, application may be made forthe Director to grant. (A) AMS-I Certificat. (B)AMS-2 Certificat. (C) AMS-4 Certificat. (D) AMS-5 Certificate.

27.After completing a periodic inspection on a Continental O 470 engine, prior to certifying the release to service of the inspection you shall. (A) conduct a flight test to determine that the engine meets performance specifications. (B) conduct a ground run to ensure that the engine starts. (C)conduct a performance ground run, only for the purpose of checking for fluid leaks. (D) conduct a performance ground run to ensure that the engine meets the manufacturer specified parameters,.

28 While carrying out a periodic inspectlon you note that the DR compass was last calibrated 15 months ago. This would: (A) require that the compass is re-calibrate. (B) require that the compass is re-calibrated if the aircraft is used on air transport operations. (C) not require that the compass be re-calibrated unless specifically stated otherwise in the operators maintenance programme. (D) not require that the compass be re-calibrated unless specifically stated otherwise in the aircraft's flight manual.

29.A finite life component that has reached the end of Its service life should be: (A) returned to the manufacturer for refurbishment or overhaul. (B) mutilated to such an extent that it could never be returned to service or passed off to another operator as a serviceable component. (C) held as an emergency replacement item to alleviate an AOG situation. (D) held in stores In case the manufacturer gives It a life extension.

30 An Installed piston engine that has been placed in long term storage should: (A) be turned weekly in order to redistribute the protective coating on the cylinder walls. (B) be re-sprayed monthly with a cylinder wall inhibiting compound. (C) hot oil primed every three months. (D) not be turned.

31. When updating the aircraft logbook for a Cessna 172 aircraft, you note that the last maintenance carried out on the emergency location transmitter was a bench test 12 months ago. You would therefore be required to: (A) carry out the required tests and inspections. (B) take no further action as ELTs are only checked every 24 months. (C) conduct an operational check only which includes checking the battery condition and expiry. (D) replace the ELT battery as it must be replaced every 12 months.

32. When a component is released from stores for installation on an aircraft, the accompanying documentation must show that the component. (A) is new or has been overhauled. (B) has been inspected by the holder of an Inspection Authorisation. (C) conforms to the acceptable standards. (D) was supplied by the holder of the component's type certificate.

33.For the issue of an airworthiness certificate in the standard category, the applicant must show that: (A) any repairs carried out to the aircraft conform to design changes approved for the type. (B) all manufacturer's service bulletins have been embodied. (C) all defects have been properly recorded and rectified. (D) the aircraft has been test flown within the last 60 days.

34. The Part 145 certificate displayed in the company's entrance area specifies a C4 rating. This rating authorises the company for maintenance of aircraft: (A) engines and propellers as defined in the organisation's expositio. (B) instrument equipment as defined in the organisation's exposition. (C) components as defined in the organisation's exposition. (D) radio equipment as defined in the organisation's exposition.

35 As an appropriately rated licensed aircraft maintenance engineer operating in a small maintenance firm, you are required to certify maintenance on an aircraft used for air operations. The maintenance tasks may be performed by. (A) an unsupervised tradesperson. (B) an unrated or unauthorised aircraft maintenance engineer without your direct supervision. (C)an unsupervised pilot licence holder who has a flight crew rating forthe aircraf. (D) any competent person under your direct supervisio.

36An additional Cessna 206 aeroplane has recently been imported into PNG by an operatorfor whom you carry out maintenance. In order for this aircraft to enter air operations the owner would. (A) require the CAA to issue a Type Certificate. (B) require the CAA to issue a Type Acceptance Certificate. (C) not require the CAA to undertake any type certification action. (D) require the CAA to Issue a restricted category Type Acceptance Certificate.

376 When performing a duplicate inspection of a control system, the person certifying the second inspection. (A)is only required to check correct assembly and locking. (B) is only required to determine that the control is not binding in the area that was disturbed. (C) must check and certify the freedom of movement of all control systems on the aircraft. (D) must check that the system is free from defects, operates correctly and in the correct sense.

38. The reporting of a defect incident to CM should be: (A) on form CA005 and within 7 days of the incident. (B) on form CA2129 and within 10 days of the incident. (C)on form CA8130 and within 14 days of the incident. (D) on form CA005 and within 10 days of the incident.

39. A new form CAA 2129 would be raised: (A) at the completion of a maintenance review. (B) at the initial Issue of an airworthiness certificate. (C)every four years. (D) when a type acceptance certificate is issued.

40,If an aircraft is registered in Canada: (A)it may also be registered in PNG. (B) it may not fly in PNG. (C) it may not fly in PNG without PNG nationality markings.it may not fly in PNG without PNG nationality markings. (D) it cannot also be registered in PNG.

41 For an aircraft engaged in air operations, who is responsible for airworthiness?. (A) The air operator certificate holder. (B) The Part 145 maintenance organisation. (C) The maintenance controller. (D) The CAA.

42The maximum time a technical log may remain in use is: (A) 12 calendar months or until the entire log is full. (B) 100-hours of aircraft operation or until the entire log is full.00-hours of aircraft operation or until the entire log is full. (C) 6 calendar months or until any part of the log is full. (D) 12 calendar months or until any part of the log is full.

43 A conformity inspectionfollowing a major repairwould normally be certified: (A) in the appropriate logbook. (B) on form CA005. (C) on form CA2129. (D) on form CA337.

44.The MCTOW for an aircraft means: (A) maximum certified take-off weight. (B) maximum controlled take-off weight. (C) minimum certified take-off weight. (D) maximum certificated take-off weight.

45. Which one of the following occurrences should be reported to CAA as a defect incident?. ( A) Wing tip damage caused by a towing accident. (B) Cracked undercarriage torque link found during an NDT inspection called up in an AD. (C) Oil leaking from a quill seal in a helicopter transmission. (D)Clutch slippage caused by glazing of the clutch shoes in a helicopter drive train.

45.In order to exercise the privileges of a licence the holder must have had a visual acuity test by a qualified person within the last: (A) 5 years. (B) 5 years if under 40 years of age and 2 years thereafter. (C) 10 years. (D) 2 years when over 50 years of age.

47. The identification plate for an aircraft should be attached to the: (A) instrument panel. (B) fuselage at tho base of the fin. (C) underside of the left-hand wing root. (D) aircraft structure at the main point of entrance.

48. An emergency AD is promulgated by the Director and forwarded to the: (A) holder of the certificate of registration within 7 days. (B)operator within 28 days. (C) operator as soon as practicable. (D)older of the certificate of registration as soon as practicable.

49. An amateur built aircraft would normally operate under a: (A) restricted category airworthiness certificate. ( B) special category - experimental airworthiness certificate. (C)special flight permit. (D) special category - PNC airworthiness certificate.

50. An export airworthiness certificate: (A) does not authorise the operation of an aircraft. (B) is used for a de-registered aircraft to permit it to fly to an overseas destination. (C) is issued only for parts or products manufactured in PNG and exported. (D) can be used as a replacement for a standard category airworthiness certificate.