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

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CIVIL AVIATION DEPARTMENTHONG KONG, CHINAAirworthiness NoticeACCEPTANCE OF AERONAUTICAL PRODUCTSNo. 17AIssue 231 January 20101 Purpose1.1 The purpose of this Airworthiness Notice is to specify the SpecialRequirements that shall be met when importing civil aeronautical Class I, IIand III products to the Hong Kong Special Administrative Region (HKSAR).2 Definition2.1 For the purpose of this Airworthiness Notice the following definitions apply:-(a)(b)(c)Class I Product means a complete aircraft, aircraft engine, orpropeller.Class II Product means a major component of an aircraft, aircraftengine, or propeller, the failure of which would jeopardize the safetyof a Class I product; or any part, material, or appliance, approved andmanufactured under the Hong Kong Technical Standard Order(HTSO) system in the “C” series.Class III Product means any part or component that is not a Class I orClass II product and includes standards parts.(d) Standard Parts are defined in Airworthiness Notice No. 17.3 Acceptance Of Design For Imported Aeronautical Products3.1 The Civil Aviation Department of HKSAR (CAD) will require the informationnecessary to become conversant with the design of aircraft intended for theissue of a Hong Kong Certificate of Airworthiness. CAD may then issueAdditional Requirements to cover certain features that would otherwise notmeet the standards and that are implicit to HKAR-1, HKAR-21 and the AirNavigation (Hong Kong) Order 1995.3.2 Aircraft that are type certificated by the European Aviation Safety Agency(EASA) or the United States Federal Aviation Administration (FAA) areAN-17A P.131 January 2010
accepted by CAD as in full compliance with the basic certification of the HongKong airworthiness standards.3.3 An aircraft engine or propeller that is part of the aircraft is accepted by CADand requires no further approval when listed on the aircraft’s EASA or FAAapproved type certificate data sheet.3.4 An aircraft engine or propeller that is not part of an offered aircraft mayrequire a preliminary CAD investigation to establish the standards for HongKong certification and, where necessary, any Additional Requirements thatmay apply.3.5 An appliance approved under an EASA European Technical Standard Order(ETSO) or FAA Technical Standard Order (TSO) will be accepted provided itis accompanied by the documents specified in Paragraph 4.2 of this Notice.3.6 A replacement or modification part produced under an FAA PartsManufacturer Approval (PMA) will be accepted provided it satisfiesAirworthiness Notice No. 17 and is accompanied by the documents specifiedin Paragraph 4.3 of this Notice.3.7 Noise certification. CAD acknowledges that the FAA does not issue aseparate noise or emission certificate. Noise certification is accomplished aspart of the aircraft type certification as stated on the FAA aircraft typecertificate data sheet. Any change in the product’s type design that effectsnoise or emissions will require re-substantiation of the noise and emissiondata.4 Acceptance of Aeronautical Products4.1 Class I Products4.1.1 New Aircraft4.1.1.1 Each imported aircraft of a type/model/seriesvalidated/accepted by CAD must be accompanied by thefollowing documents:(a) Export Certificate of Airworthiness (Export C of A).The year of manufacture and serial number of theaircraft, as well as the serial number for each aircraftengine and/or propeller, must be stated on the ExportC of A.(b) Statement of non-registration or de-registration.(c) *A copy of the type certificate and type certificatedata sheet.31 January 2010 AN-17A P.2
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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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Page 87 and 88: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 89 and 90: 3.3 Organisations approved to HKAR-
Page 91 and 92: 7 Maintenance of Aircraft - Non-Com
Page 93 and 94: 9.5 Where it is intended to fit par
Page 95 and 96: 1 ApplicabilityAIRWORTHINESS NOTICE
Page 97 and 98: Certificates of Release to Service
Page 99 and 100: 3.2 The organisation will be requir
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Page 139 and 140: 3.2 New Applications for Approvals
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Page 149 and 150: specialist organisation.2.4 Details
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Page 167 and 168: Part II, Chapter 5.7 Coding and reg
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HPMA No. Supp. Item Part Name Part
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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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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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