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

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3 Requirements3.1 Containers, whether built into the aircraft or as self-contained units intendedfor transfer from one aircraft to another, shall comply with the requirements.All containers and their means of installation into aircraft shall comply withthe appropriate strength requirements of the appropriate CS/JAR or BCAR foreither:(i)(ii)the flight, ground and emergency alighting loads, orthe flight and ground loads,depending on their intended location in the aircraft, and shall be approved bythe Director-General.NOTE: Containers which comply with the requirements of the National Air SafetySpecification NAS 3610, Revision 6 will be accepted as being in compliance withCS/JAR/BCAR but only for installation in those locations where compliance with theemergency alighting conditions is not required.3.2 Operators shall make adequate provision for care and maintenance ofcontainers under their control and shall, where appropriate, formulate andadopt procedures for ensuring that containers to be used on their aircraft are ofan approved type and in an acceptable condition. These procedures will beexamined by the Director-General as part of the assessment of operator'smaintenance procedures for the issue or variation of an Air Operator'sCertificate.3.3 Organisations responsible for the design of a container and its installationshall provide adequate instructions for its assembly, installation andmaintenance. These instructions shall be included in the operator's loadingmanual or similar document.4 Procedure4.1 When a container is designed for use only in a particular type of aircraft, it andits installation will be considered to be a modification to the aircraft. Theapproval procedure shall be in accordance with the modification approvalprocedures of HKAR-1 Sub-section 1.2-5.4.2 A container designed for use on various types of aircraft will be considered asan accessory. The approval procedure shall be in accordance with theAccessory Approval procedure of HKAR-1 Sub-section 1.4-8.4.2.1 The manner of installation into any particular aircraft will need to becertificated as being in compliance with the appropriate requirements30 May 2006 AN-92 P.2
and with the associated Declaration of Design and Performance, underthe modification approval procedure of HKAR-1 Sub-section 1.2-5.NOTE: A container produced in compliance with CS-ETSO/JAR-TSO C90c or FAA TSOC90c (FAR 37.199) will be accepted on the basis of having been manufactured toprocedures equivalent to HKAR-1 Sub-section 1.4-8.5 Additional Information5.1 CAD approval will be limited to the airworthiness features of the containerwith regard to the aircraft, flight crew and other persons present on the flight.It will not cover the safeguarding of the cargo or, in case of livestock, itswelfare.5.2 It is recommended that containers should be sufficiently robust and simple thatassembly and/or installation into the aircraft would not constitute worknecessitating the signing of a Certificate of Release to Service.5.3 It is strongly recommended that, in view of the mishandling to which suchequipment may be subjected, the instructions provided in accordance withparagraph 3.3 should also contain advice as regards tolerable damage and anyresulting load limitations.5.4 Operators are reminded that they are responsible for safeguarding the aircraftstructure and equipment against the effects of corrosive liquids and any othermaterials which could cause damage or malfunction.5.5 Where restraint of the cargo and container is provided by approved nets,bulkheads, etc. and no reliance is placed on the strength of the container, thensuch containers will not be subject to the above requirements.6 CancellationThis Notice cancels Airworthiness Notice No.92 Issue 4, dated <strong>31</strong> May 2003, whichshould be destroyed.Norman LODirector-General of Civil AviationAN-92 P.330 May 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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(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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Page 353 and 354: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 355 and 356: AIRWORTHINESS NOTICE No. 74APPENDIX
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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Page 371 and 372: 3.3 All aeroplanes defined in parag
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Page 381 and 382: 2 Requirement2.1 Compliance with pa
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Page 387 and 388: 3.2 Applications for the approval o
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Page 403: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 407 and 408: Personnel Certification scheme. In
Page 409 and 410: Quality Procedures.6 Suppliers and
Page 411 and 412: Qualification: The proven ability o
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Page 421 and 422: 3.6 Parts that cannot be returned t
Page 423 and 424: 5.6 Questionable part numbers, frau
Page 425 and 426: case. If such evidence cannot be ob
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Page 429 and 430: 3 Compliancethat these requirements
Page 431 and 432: unit and any other galley insert wh
Page 433 and 434: With effect from 1 January 2009, al
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Page 439 and 440: its removal from the water.5 Additi
Page 441 and 442: 4 Requirement4.1 Performance Levels
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Page 445 and 446: 3.9 Compliance requirements for hel
Page 447 and 448: 4.5 Type IVA FDR Requirements4.5.1
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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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