31 July 2011 C1 CIVIL AVIATION DEPARTMENT HONG KONG ...

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5 Further Informationhoped that by sharing such data the Director-General and industry canjointly develop a better understanding of maintenance error causationand develop more focused human factors strategies. However, it isappreciated that some information in a MEMS may be consideredsensitive to the organisation affected, and may need to be dis-identifiedbefore being shared with other organisations.5.1 More detailed guidance information is included in UKCAA CAP 716 Issue 2.6 CancellationThis Notice cancels Airworthiness Notice No.71, Issue 2, dated 31 January 2002,which should be destroyed.Norman LODirector-General of Civil AviationAN-71 P.730 September 2006
CIVIL AVIATION DEPARTMENTHONG KONG, CHINAAirworthiness NoticeNo. 72Issue 231 January 2002SAFETY CRITICAL MAINTENANCE TASKS1 A factor in a serious incident involving an oil leakage on a large twin enginedcommercial air transport aircraft was the failure to re-install the drive cover plate onboth engines following maintenance. The Director-General wishes to highlight thepotential safety benefit where companies choose to apply aspects of Extended RangeTwin Operations (ETOPS) maintenance philosophy to multi-system aircraft in order toavoid the possibility of simultaneous incorrect maintenance on two or more safetycritical systems. In this context, such systems are those which have a fundamentalinfluence upon the safe operation of the aircraft, engines and their systems being a casein point.2 Operators and maintenance organisations should consider the following paragraphswhen planning, and accomplishing scheduled and non-scheduled maintenance tasks onmulti-system aircraft.(a)(b)(c)Arrangements should be made to stagger scheduled maintenance tasks onessential or primary systems such that the accomplishment of similar criticaltasks on two or more systems are segregated. Consideration should be givento introducing procedures that will ensure that such tasks are separated by atleast one flight cycle. Where it is not practical to introduce staggeredmaintenance, inspections and functional checks should be performedindependently to ensure system serviceability.Where it is not practical to introduce staggered maintenance at BaseMaintenance inputs or during rectification of Line or Base defects, the use ofseparate work teams together with the accomplishment of appropriate functionalchecks to verify system serviceability should ensure a similar level of systemintegrity.Procedures should be established to provide maintenance and planningpersonnel with guidance on the identification and accomplishment of safetycritical tasks conducted during scheduled and non-scheduled maintenanceactivities. Routine task documentation should identify those tasks which mayhave a critical effect on safety and should clearly identify the individual stagesof such tasks. Maintenance Programme or Maintenance Schedule basic rulesshould provide the necessary standards to ensure the identification of criticalscheduled maintenance tasks.AN-72 P.131 January 2002
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CIVIL AVIATION DEPARTMENTHONG KONG,
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NoticeNoIssue Date Subject30 5 30 S
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NoticeNoIssue Date Subject65 * 1 31
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[ * ] : Airworthiness Notices and/o
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4.1 The contents list is re-issued
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INTENTIONALLY LEFT BLANK31 January
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Category B Helicopter. A single-eng
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together necessary to provide thrus
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Schedule 7Schedule 8Schedule 9− A
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(b) Assembly - that items are fitte
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(b)The holder of a Type Rated HKAR-
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combination of theoretical and prac
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continuation of certification privi
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6 HKAR-66 Category B3 Aircraft Main
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Certificates of Release to Service
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3 Application3.1 The following appl
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Airworthiness Notice No. 4Appendix
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Government Printer, Hong Kong Speci
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Airworthiness Notice No. 6Appendix
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6.2 Foreign Airworthiness Directive
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10.2 Light Aircraft Maintenance (CA
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No. 21 Helicopter Public Address Sy
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4 Requirement4.1 Bilingual Placard4
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(1)No.(2)English Text(3)Chinese Tex
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work detailed in the renewal form w
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(e)any parachute including a parasc
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(a)an aircraft of the type is regis
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(b)A Rating granted in relation to
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* 13.2 Radio-Coupled Automatic Pilo
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Appendix Subject CAAIP Leaflet 11-2
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AIRWORTHINESS NOTICE NO. 12APPENDIX
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9 Due to the complexity and safety
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handling organisations are made awa
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NOTE: Resolution Advisories cannot
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3.3 Organisations approved to HKAR-
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7 Maintenance of Aircraft - Non-Com
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9.5 Where it is intended to fit par
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1 ApplicabilityAIRWORTHINESS NOTICE
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Certificates of Release to Service
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3.2 The organisation will be requir
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one aircraft type or comparable tas
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4 Limited AuthorisationsFlight Crew
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which forms an integral part of the
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4 CancellationThis Notice cancels A
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It must be established by the owner
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this Notice, then the following sta
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7 Lease/Loan/Power-By-The-Hour Powe
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in an aircraft, its engines or prop
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When an aircraft is grounded at a l
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aircraft, engine or propeller Type
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All aircraft components must be rel
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accepted by CAD as in full complian
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(s) Manuals including:(1) * Mainten
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Note: ** Normally only required for
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INTENTIONALLY LEFT BLANK31 January
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3.2 New Applications for Approvals
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Table 1:Classification of HKAR-1 Ce
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5.1 Users of aircraft components an
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9 CancellationThis Notice cancels N
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specialist organisation.2.4 Details
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5 Guidance4.2.3 Log book entries mu
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of some component parts.2.3 The fun
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4 ApplicationApplicant shall apply
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3 Requirement and Applicability3.1
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e equipped with a ground proximity
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Performance Class 1 helicopter A he
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Part II, Chapter 5.7 Coding and reg
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1 GeneralAIRWORTHINESS NOTICE NO. 2
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List of HKAR-147 approved maintenan
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Table 2:Non-Critical HPMA PartsHPMA
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HPMA No. Supp. Item Part Name Part
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(d)(e)(f)desiring to enhance cooper
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(c)(d)(e)in the case of serious non
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Certificate of Release to Service a
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(g)(h)(i)civil aircraft and/or airc
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Technical Records include but are n
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Party the opportunity to review and
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Authority in respect of any major m
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meanings as specified:(a)(b)(c)(d)(
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2.5.6 Where maintenance involves th
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4.1.1 A statement signed by the cur
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(d)The data obtained during the ins
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6 Cancellationmean time, the provis
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a pressure gauge (reading up to 140
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unchanged. However engine power may
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and cabin crew seats as applicable,
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4 Cancellationoperation is an all-c
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2.6 ICAO has also published guidanc
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(b)(c)Install a means for monitorin
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when installed, shall be monitored.
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4.3 It is recommended that in order
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(c)(d)(e)(f)(g)(h)Ensure that any t
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Minimum (RVSM) compliant aircraft.
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shall be given in Overhaul Manuals.
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(iii)Option Selectable Software (OS
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3.3 Release of Required FLS or DFLD
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een corrupted (e.g. making use of a
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8 Procedure8.1 Configuration Contro
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(f)That connecting a central electr
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2.2 General Tool SelectionThe follo
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2.5 Control and Suitability of Tool
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epair, modification and partial or
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4 ImplementationSub-section 1.2-5,
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and paragraph 11.4 of Document DO-1
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RELATIONSHIP BETWEEN FUNCTION CRITI
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(b)Criticality Categories and Softw
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3.2 Fatigue3.3 StressTiredness and
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4 SummaryThe effects of illness, in
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(vi)(vii)(viii)(ix)Drugs for the re
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2.3 Each approved organisation is r
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(paragraph 3).4.3 Overseas Organisa
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7 Concessions against any inspectio
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Page 301 and 302: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 303 and 304: or revised service information, rev
Page 305 and 306: NOTE: 'Designated' emergency exits
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Page 335 and 336: Box 4Box 5The question takes into a
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Page 339 and 340: 4 RequirementPortable oxygen equipm
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Page 359 and 360: 3.4 The periods of operation or ela
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Page 363 and 364: power switching relays, their physi
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and with the associated Declaration
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Personnel Certification scheme. In
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Quality Procedures.6 Suppliers and
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Qualification: The proven ability o
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continued standard of NDT work carr
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5 Cancellation"guidance" of a Level
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2.5 The test must be performed at a
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shorter wavelength light.7 Cancella
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3.6 Parts that cannot be returned t
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5.6 Questionable part numbers, frau
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case. If such evidence cannot be ob
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This Notice cancels Airworthiness N
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3 Compliancethat these requirements
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unit and any other galley insert wh
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With effect from 1 January 2009, al
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The position of safety belt buckle
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its removal from the water.5 Additi
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4 Requirement4.1 Performance Levels
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equired, the helicopter shall compl
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3.9 Compliance requirements for hel
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4.5 Type IVA FDR Requirements4.5.1
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4.2.3 The following provides guidan
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- Emergency tracheal catheter (or l
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4.7 RNP AR APCHRNP equipages comply
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2.5 ADS-B based surveillance provid
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a. For the purpose of this Article,
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31 July 2011 C1 CIVIL AVIATION DEPARTMENT HONG KONG ...

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