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

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equivalent to a SAR 145.50 Maintenance Release.(c)(d)A CAAS Form (AW) 95 Authorised Release Certificate issuedin accordance with this Technical Arrangement will beaccepted by HKCAD as equivalent to HKCAD Form OneAuthorised Release Certificate.A HKCAD Form One Authorised Release Certificate issued inaccordance with this Technical Arrangement will be acceptedby CAAS as equivalent to a CAAS Form (AW) 95 AuthorisedRelease Certificate.2.5.3 The design of any repairs and modifications of an AeronauticalProduct which are not from the original equipment manufacturer shallrequire separate approval by the Responsible Authority.2.5.4 Where maintenance involves the installation of an AeronauticalProduct, the Aeronautical Products being installed must originate froman organisation approved under the provision of an existing TechnicalArrangement entered into by the Responsible Authority, or approvedby or otherwise acceptable to the Responsible Authority.2.5.5 Technical Records shall be kept in accordance with the requirementsof the Responsible Authority.2.6 Mutual Co-operation and Technical Assistance2.6.1 The Parties will provide information regarding the provisions of thisTechnical Arrangement, and will develop appropriate advisorypublications and circulate these publications through establishedmethods in their respective Areas to inform the public of the provisionsof the Technical Arrangement and outline the special requirementsnecessary for persons to perform and certify work under the provisionsof this Technical Arrangement.2.6.2 The Parties agree to provide each other with technical evaluationassistance upon request, to further the purposes and objectives of thisTechnical Arrangement. Such assistance may include, but is notlimited to, reporting on maintenance organisation's continuedcompliance with the requirements of this Technical Arrangement.2.6.3 The Parties will provide each other with any and all regulations,standards, guidance material, policies, practices and interpretationsrelevant to this Technical Arrangement, and will ensure that suchdocuments are updated and provided to the other Party in a timelymanner. In addition, each Party will notify the other Party of anyproposal or initiative to amend such documents and provide the other30 September 2008 AN-30A P.4
Party the opportunity to review and comment on the proposals orinitiatives.2.6.4 Where urgent or unusual situations develop that are within the scope ofthis Technical Arrangement but are not specifically addressed therein,the Parties will review and consult each other, and upon mutualconsent, take appropriate action, including but not limited toamendment or revision to this Technical Arrangement where required.2.6.5 The Parties will by mutual co-operation and with reasonable priornotice, arrange one Party to participate in the other’s inspections andaudits as an observer.2.6.6 Each Party is permitted to request the disclosure or review of any dataconcerning any approval granted under the Technical Arrangement bythe other Party from time to time.2.6.7 Subject to reasonable prior notification, the Parties will endeavour toarrange each other to conduct independent inspections of each other’smaintenance organisations to investigate issues relating to aircraftsafety and the effective application of this Technical Arrangement.2.7 Notification of Non-Compliance2.7.1 Each Party will notify the other Party of any instance of unsatisfactorycompliance with any regulations or any condition set forth in thisTechnical Arrangement that affects the ability of an organisation tocomply with the provisions of this Technical Arrangement.2.7.2 The Overseeing Authority will promptly advise the other Party of anyinvestigations or enforcement action, including revocation orsuspension in respect of maintenance organisations approved inaccordance with this Technical Arrangement.3 Recognition of Maintenance Organisations3.1 The Overseeing Authority will ensure that the following criteria are met byeach organisation authorised to maintain products in accordance with thisTechnical Arrangement.3.2 Except as provided otherwise in accordance with paragraph 2.4.2, themaintenance organisation must be located within the Area of the OverseeingAuthority. Organisations outside the Area of the Overseeing Authority maybe accepted in specific cases by mutual consent of the two OverseeingAuthorities of the respective Party.3.3 Work may be contracted/subcontracted by the maintenance organisation to:AN-30A P.530 September 2008
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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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Page 149 and 150: specialist organisation.2.4 Details
Page 151 and 152: 5 Guidance4.2.3 Log book entries mu
Page 153 and 154: of some component parts.2.3 The fun
Page 155 and 156: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 157 and 158: 4 ApplicationApplicant shall apply
Page 159 and 160: 3 Requirement and Applicability3.1
Page 161 and 162: e equipped with a ground proximity
Page 165 and 166: Performance Class 1 helicopter A he
Page 167 and 168: Part II, Chapter 5.7 Coding and reg
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Page 175 and 176: List of HKAR-147 approved maintenan
Page 177 and 178: Table 2:Non-Critical HPMA PartsHPMA
Page 179 and 180: HPMA No. Supp. Item Part Name Part
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Page 189 and 190: (c)(d)(e)in the case of serious non
Page 191 and 192: Certificate of Release to Service a
Page 193 and 194: (g)(h)(i)civil aircraft and/or airc
Page 197: Technical Records include but are n
Page 201 and 202: Authority in respect of any major m
Page 203 and 204: meanings as specified:(a)(b)(c)(d)(
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Page 207 and 208: 4.1.1 A statement signed by the cur
Page 213 and 214: (d)The data obtained during the ins
Page 215 and 216: 6 Cancellationmean time, the provis
Page 217 and 218: AIRWORTHINESS NOTICE NO. 35APPENDIX
Page 219 and 220: a pressure gauge (reading up to 140
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Page 225 and 226: and cabin crew seats as applicable,
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Page 229 and 230: 2.6 ICAO has also published guidanc
Page 231 and 232: (b)(c)Install a means for monitorin
Page 233 and 234: when installed, shall be monitored.
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Page 239 and 240: (c)(d)(e)(f)(g)(h)Ensure that any t
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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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5 CancellationThis Notice cancels A
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or revised service information, rev
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NOTE: 'Designated' emergency exits
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FAR/JAR 25.812(l)(1) requirement ca
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although not required by this Notic
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and 121-198 respectively. Similar a
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C25inches(Ref para 5.1)(Ref para 4.
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design to ensure repeatable in-serv
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(d)(e)(f)(g)(h)Identify any feature
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Box 4Box 5The question takes into a
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IFE Scheduled Maintenance Tasks and
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4 RequirementPortable oxygen equipm
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CAD Approved Certificate will be re
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2.5 Other potential benefits may ac
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y organisations albeit too often on
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(c)The Director-General will not, a
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(e)(f)the person concerned has atte
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AIRWORTHINESS NOTICE No. 74APPENDIX
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3.4 The periods of operation or ela
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power switching relays, their physi
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(g)a process for conducting periodi
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3.3 All aeroplanes defined in parag
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Figure 2 MINIMUM ACCESS REQUIRED BY
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acks must be in the upright (take-o
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Certificate is made after the 16 Ju
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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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