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

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(b)(c)(d)(e)(f)The installing organisation – that they have the necessary approvals,competence, facilities, equipment etc. (with respect to the installationin question).Specific aircraft being modified - effect on particular airframe e.g.documents to be amended, maintenance programme amendment.Validation of all proposed documentation changes.Operational considerations – e.g. Crew operating instructions andtraining (including any normal, abnormal and emergency procedures),limitations of use etc.Stakeholders – establish communication links and identify all therelevant parties to ensure full and complete liaison with respect to theirrole in the whole IFE installation.Timeline – identification of specific milestones in the process, e.g.Agreed times to involve/contact Director-General, what should bepresented at these times etc.(g) Development of Scheduled Maintenance and MaintenanceInstructions – who will be responsible for doing this and themethodology to be utilised. (See Appendix No. 1 for guidance.)(h)Ensure all stakeholders understand their role in order to achievecompliance with this Notice.5.5 Considerations for DesignerThe designer for an IFE System should consider, as a minimum, the followingkey areas:(a)(b)(c)Establish communication links with the project manager and therelevant stakeholders.Ensure that all installation instructions, operating conditions andequipment limitations (e.g. European Technical Standard Order (ETSO)and Declaration of Design and Performance (DDP)) are considered andrecorded in the appropriate drawings/manuals etc.It is expected that the designer will provide installation instructions(engineering drawings) that as a minimum equate to the originalaircraft production standards. Statements such as "install inaccordance with industry standard practices" would be unacceptable.It is considered that such statements are inadequate because thestandard practices cannot alone define the location, routing or securityof electrical wiring for example.<strong>31</strong> January 2006 AN-65 P.4
(d)(e)(f)(g)(h)Identify any features that are believed to require new or amendedscheduled maintenance tasks and participate in the scheduledmaintenance task analyses. (See Appendix No. 1 for guidance.)Ensure that all appropriate airworthiness/operational data is producedin sufficient time for the operator to incorporate into relevant manualsprior to entry into service. This should include normal, abnormal andemergency procedures.IFE installations (equipment or wiring) may affect existing TC/STCHolder derived maintenance tasks. The designer should assess, inaccordance with original scheduled AMS development processes, theeffect of the modification on the existing maintenance tasks andinspections, and address accordingly.Validated maintenance instructions to be produced so that the originalinstallation standards are maintained after in-service activities.Establishment of engineering liaison processes to address minorchange requests required during installation, and to monitor and reactto operator in-service reliability feedback.5.6 Considerations for InstallerThe installer of an IFE system should manage, as a minimum, compliancewith the following:(a)(b)(c)(d)Establish communication links with the project manager and therelevant stakeholders.A verified internal competence and capability assessment should becarried out against the specific installation requirements. This shouldcover, as a minimum, any necessary unique skills, technologies, toolsand training. Installer's competence/scope should be described withinthe HKAR-145 Maintenance Organisation Exposition (MOE).The pre-planning function should seek to identify any shortcomingswithin the installation instructions prior to installation on the aircraft,and to report to the relevant stakeholders for resolution.Provide feedback and gain approval of minor installation andinstruction/drawing changes found during installation.5.7 Considerations for OperatorThe operator of an aircraft installed with an IFE system should manage, as aAN-65 P.5<strong>31</strong> January 2006
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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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Page 283 and 284: 3.2 Fatigue3.3 StressTiredness and
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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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2 Requirement2.1 Compliance with pa
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should include adequate battery cap
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(a)(b)reduction of the generating s
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3.2 Applications for the approval o
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3 ComplianceAll applicable aircraft
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5 Additional Information5.1 EASA CS
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to be operated under IFR with non-i
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3.3 For example, class of emission
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3.2 All aeroplanes flying for the p
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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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