DAVID 3

1. 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: acceptable to the Director and should have had at least five years experience relevant to the position held. acceptable to the Chief Executive and should have had at least four years experience relevant to the position held. specified in the company exposition and should have had a minimum of two years experience relevant to the position hold. acceptable to the Director and should have had at least six years experience relevant to the position held.

When calculating "Time in Service" for a flight, what must be recorded?. The total time from the moment the aircraft first moves under its own power for the purposes of taking-off until the moment it comes to rest at the end of the flight. The elapsed time from the aircraft leaving the surface until touching ii again on landing. The total time from when the powerplants are started until they are shut-down. Time from when the aircraft moves on a take-off roll to the time it stops after landing.

The Part 145 certificate displayed in the company's entrance area specifies a C4 rating. This rating authorises the company for maintenance of alrcraft: engines and propellers as defined in the organisation's exposition. Instrument equipment as defined in the organisation's exposition. components as defined in the organisation's exposition. radio equipment as defined in the organisation's exposition.

4. When checking the airworthiness certificate for an aircraft that you are maintaining you observe that the certificate has been granted for both the standard and restricted categories. This would mean that the aircraft. meets the certification requirements for each category when in the configuration for each category. meets the requirement of the standard category, and because this is the highest category it can be automatically certificated for the restricted category. can be internally equipped for dispensing substances on agricultural operations and still be used for air transport operations in this configuration. can never be used on air operations.

5. You have held an AME Licence in category avionics for six years. Since changing employment you have been working mainly in the hangar servicing light aircraft in all trades. To gain the mechanical category on your licence what experience would you be required to show?. A minimum of three year. A minimum of two years. A minimum of one year. A minimum of six months.

6.The CAA will publish an airworthiness directive: within 28 days of its issue by the Directo. within 14 days of its issue by the Director. as soon as practicable by the fastest means possible. within 90 days of its issue by the Director.

7.The responsibility for ensuring that an aircraft is maintained in an airworthy condition rests with the: CAA. operator. maintenance organisation. maintenance controller.

8 Tho completed form used to certify a conformity inspection is normally distributed as follows. One copy to the certificate of registration holder and one copy to the aircraft operator. One copy to the Director and one copy to the maintenance organisation. One copy to the certificate of registration holder and one copy to the Director,. One copy to the Director and one copy to the air operator certificate holder.

9 A test has been carried out on the static pressure system of a Cessna 172 unpressurised aeroplane. During a one-minute period a loss of 80 feet was noted on the altimeter. The static system is: serviceable because the maximum allowable limit is a 100 feet loss. unserviceable because a maximum loss of only 50 feet is permitted. unserviceable because a loss of two percent of the altitude is permitted. serviceable because it is within tho two percent allowable limit.

10.A new type of civil helicopter imported into PNG would bo issued by the CAA with: an import certificate. a type certificate. a supplemental type certificate. a type acceptance certificate.

11Prior to the grant of an airworthiness certificate in the standard category the aircraft must have had a maintenance inspection in accordance with the maintenance programme within: 14 days. 30 days. 60 days. 90 days.

12 Unless revoked by the Director, an AME licence shall remain valid for: the period specified on the document. 24 months, provided work has been performed on aircraft for six months during that period. the lifetime of the holder. five years.

Identify which one of the following activities is required after the completion of a periodic inspection on a gas turbine engine. Test flight. Performance ground run. Taxi check. Conformity inspection.

When storing compressed gas cylinders: oxygen and acetylene cylinders may be stored together provided the acetylene cylinder is stored in the upright positlon. acetylene cylinders should be stored in the horizontal position. acetylene cylinders should be stored in the upright position. oxygen and acetylene cylinders must not be stored together and acetylene cylinders should be stored in the horizontal position.

15 If an aircraft component is purchased from a PNG Part 144 supply organisation, the release documentation you would expect to see with the part is a: CAA Form one - Release note,. CAA Form two - Release note. serviceable part tag. CAA Form 8130.

16 A critical part would be one that. is critical to the operation of an aircra. makes up a powerplant assembly. is listed in the Airworthiness L.imitations Section of a manufacturer's maintenance manual and has a specified replacement lime or inspection interval. is the subject of an airworthiness directi.

17A defect incident would normally be reported to the CAA on a form. cA005. CAA Form two. CA2129. CA2130.

18Identify which of the following avionics equipment must be listed In Section 2 of a form CAA2129. Cellular telephones. Only fixed emergency locator transmitters, not removable ELT's. Passenger entertainment systems (non-transmitter receiver types. Hand held communication units.

19. An aviation maintenance specialist certificate AMS-2 is valid for. the period endorsed on it. the life time of the- holder unless the certificate is suspended or revoked by the Director. five years. 24 months.

20.As a certifying engineer in a Part 145 organisation you are required to: carry your authorisation with you at all times when certifying maintenance. be able to produce your authorisation in a reasonable time should you be requested to do so. only have access to an electronic copy of the authorisation as a hard copy document is not required. carry your AME licence with you at all times when certifying release to service of aircraft.

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

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

23A Part 66 aircraft maintenance engineer licence may be issued in one or more of the following categories?. Aeroplane, rotorcraft, powerplant, avionics. Airframe, powerplant. Mechanical, avionics, lighter than air. Mechanical, electrical, instrument, radio.

24. In order to certify the release-to-service of a repair to a Cessna 206 flight control, the engineer would be required to hold a: Mechanical General (Aeroplanes) Piston Engine Powered rating. Mechanical General (Powerplant) rating. Specific Type Rating. Mechanical General (Aeroplanes) Turbine Engine Powered rating.

25.Which one of the following criteria would an air operator be required to specify in a maintenance programme for their aircraft?. The training requirements for certifying personnel. Procedures for the calibration of special test equipment. Procedures forthe issue of the airworthiness certificate. Instructions for exceeding an inspection interval.

26. The party responsible for ensuring that all applicable ADs relating to an aircraft or its components are complied with is the: Civil Avlation Authority. designated maintenance organisation. operator of that aircraft. Pilot-in-Command of the aircraft operation.

27 When transferring details of maintenance from a technical log to the aircraft logbook, the statement of release-to-service on the technical log: is referenced in the logbook. reissued in the logbook. deleted off the technical log. taken for granted in the logbook.

28.Which ono of the following criteria would be considered a "basic essential" of a Part 145 internal quality assurance system?. Procedures for the performance of periodic inspections. The aircraft maintenance programme. An internal audit programme. Part 66 licensing procedures for certifying staff.

29.Prior to returning an aircraft to service after a 100-hour inspection: it is the responsibility of the pilot to update the existing Technical Log, or enterthe required detail from the aircraft logbook and maintenance records into a new Technical Log. it is the responsibility of the operator to enter the required detail from the aircraft logbook and maintenance records into a new Technical Log. it is the responsibility of the chief engineer to update the existing Technical Log, or enter the required detail from the aircraft logbook and maintenance records into a new Technical Log. it is the responsibility of the licensed aircraft maintenance engineer to enter the required detail from the aircraft logbook and maintenance records Into a new Technical Log.

30. As a certifying engineer you have been rostered on duty for a continuous 20-hour extended shift in order to complete a major check on an aircraft. This roster: is acceptable during periods of high workload. is not acceptable as you may only work 16 hours in a 24 consecutive hour period. is acceptable because only flight crew have duty time limitations. is acceptable provided meal breaks are retained and 8 consecutive hours are free at the ond of the shift.

31 Maintenance performed outside the country on a PNG registered aircraft: must be re-inspected and certified when the aircraft returns to its PNG base. can only be released-to-service by the holder of a PNG licence or approval holder. is limited to line maintenance only. could be certified by the holder of an overseas Part 145 company authorisation that is acceptable to the Director.

32Which one of the following documents permits the holder to certify conformity for a major repair. an nspection Authorisation. An AME Licence with the approprlate rating. A design approval Issued by the Director. An AMS-2 Certificate endorsed for conformity inspections.

33 Which one of the following activities may be performed by an engineer who is attending an accident scene?. Turn all electrical switches off in the cockpit. Turn the fuel tank selector to the "OFF" positio. Deactivate the emergency location transmitter. Remove the cockpit voice recorder for safe keeping.

34 Parts that were purchased from a manufacturer who did not hold the appropriate certifications to produce or supply those parts: may be made acceptable if released-to-service on a Form One issued by a Part 145 maintenance organisation. are acceptable If accompanied by a manufacturer's release note. must not be installed on a type certificated product. may be installed on type certificated product if a conformily inspection is carried out by an Inspection Authorisation holder.

35 A person who certifies a maintenance review must send a copy of form CAA43/01 to the Director within. 7 days. 14 days. 28 days. 60 days.

36,. Ex-military parts are acceptable on standard category aircraft if they comply with civil type certification requirementsand: are new or newly overhauled. have been sourced through the proper military channels. have had a conformity inspection carried out by an IA holder. have had a 100-hour Inspection priorto installation.

37 When planning the next 'C' Check on a F28 aircraft you find that a Netherlands CAA airworthiness directive has been issued for that aircraft type. The AD: is NOT required to be actioned. must be complied with only if it is shown in the PNG CAA Register of Airworthiness Directives. must be complied with. must be complied with only if It is an emergency AD.

38. Which one of the following statements best describes a "quality indicator" that should be developed by your company?. The company's exposition (manual). Forms and records used for maintenance. root cause analysis from corrective and preventive action records. cause analysis from corrective and preventive action records.

39.If an STC is carried out that relates to changing the main wheel size to improve grass field operations, and a change to operating limitations results, the release-to-service certification of the modification shall not take place until: a test flight has been carried out. the aircraft technical log has been amended. changes have been incorporated into the flight manual. the manufacturer's maintenance manual has been amended.

40. As a certifying engineer you have just replaced the electrical flap position transmitter and electronic position indicator on an aircraft's flap system. Which parts of the system would require a duplicate inspectio. None, because the actual flap controls were not disturbe. None, because flaps are not considered lo be aircraft control system. Only the electrical flap position transmitter as the control system does not cover electronic component. Both the position transmitter and electronic indicator as both electrical and electronic components are included in a control system.

41.A portable fire extinguisher fitted to an aircraft must be: weighed each 12 months. weighed and pressure tested each 24 months. weighed each 24 months. pressure tested each 12 months.

42.If an aircraft is destroyed in a crash the holder of the certificate of registration is required to notify the Director withi. 28 days. 21 days. 14 days. 7 days.

43. The Identification plate for an aircraft should be attached to the: Instrument panel. fuselage at the base of the fin. underside of the left-hand wing root. arcraft structure at the main point of entrance.

44When conducting an inspection of an aircraft in accordance with a manufacturer's schedule, reference is made to the aircraft Airworthiness Limitations. The Airworthiness Limitations section contained in a manufacturer's maintenance manual would detail: all required repetitive ADs to be performed on the aircraft or Its component. structural inspection intervals and mandatory replacement time. the operational limits for the aircraft. the Minimum Equipment List for the aircraft.

If the module of a gas turbine engine containing the engine data plate is replaced, the old data plate should be. re-attached to the replacement module. left on the original module and a new data plate manufactured and attached to the replacement module. removed and retained with the engine logbook and a new data plate installed. discarded as the new module will have a new data plate.

46.An aircraft maintenance engineers licence in the mechanical category: may be issued with the electrical systems rating without the need for any other rating an the licence. must be endorsed with either avionics or mechanical general ratings before another rating may be endorsed on the licence,. must be endorsed with a type rating at licence issue. other than one endorsed with an aircraft specific type rating, must be endorsed with a mechanical general rating before any other rating can be endorsed.

47 In the course of carrying out a structural inspection of the undercarriage attachment flange for an aircraft on maintenance, you note cracking in the main spar which requires immediate repair of the affected areas as well as the design and installation of a strengthening plate attached to the spar web. This work would be classified underthe CA Rules as: major maintenance. major modification and major repair. major repair and minor modification. minor maintenance and major modification.

48.An entry in maintenance records stating that a propeller has been "overhauled", requires that: the propeller has been bulk stripped, re-assembled and tested and is fit to operate for the remainder of its service life. all moving parts have been replaced, the propeller re-assembled and tested, and time since new returned to zero hours. the propeller has been disassembled, cleaned, inspected, repaired, re-assembled, tested, and its operational life renewed. the propeller has been serviced under Part 43 conditions and its operational life renewed.

49.On a Cessna 172 aeroplane fitted with a 160 HP Lycoming engine, you note that the cylinder head temperature gauge is listed as a defective item in the technical log. This gauge. must be rectified before next flight. must be rectified on return to base. may be listed in the technical log as a deferred maintenance item and the gauge appropriately placarded,. may be rectified at a later date provided an operational restriction is placed on the aircraft limiting maximum power to no more than five minutes continuous.

50. What approval level would a Collins HF-220 high frequency communications system be approved to on the Form CAA2129?. Lovet.one. Level two. Level three. Level four.