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

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than one quarter of the tread circumferenceor(b)at any place on the circumference the tread pattern is worn to a depth of lessthan 2 mm across the whole width of the tread in contact with the runway.NOTE: This is not a rigid definition and equivalence may be provided if, for example, tyre wear issuch that whilst one groove is less than 2 mm all the others are 3 mm or more.4 CancellationThis notice cancels Airworthiness Notice No. 5 Issue 2, dated 1 November 1996,which should be destroyed.Albert K. Y. LAMDirector-General of civil Aviation30 October 2001 AN-5 P.2
CIVIL AVIATION DEPARTMENTHONG KONG, CHINAAirworthiness NoticeAIRWORTHINESS PUBLICATIONS - GENERAL INFORMATIONNo. 6Issue 1430 May 20081 This Notice gives details of the various airworthiness publications which may ingeneral be available on CAD website at http://www.cad.gov.hk under “Publicationsand press release”. Some of them however may still be obtained in hardcopy formatfrom the CAD Airworthiness Office, 10/F Commercial Building, Airport FreightForwarding Centre, 2 Chun Wan Road, Lantau, Hong Kong (Tel. (852)27697641, Fax.(852)23624250). The prices and versions of those hardcopy format airworthinesspublications are available on the aforementioned CAD website under “Publicationsand press release” then ‘Other Publications for Subscription’.General information on airworthiness publications published by UKCAA, JAA andEASA are described in the Appendix No.1 to this Notice.2 Airworthiness Requirements2.1 Hong Kong Aviation Requirements (HKAR)These comprise minimum requirements and constitute the basis for the issueof approvals and certificates required by the Air Navigation (Hong Kong)Order 1995 as amended (hereinafter referred to as AN(HK)O).HKAR-1 Airworthiness Procedures (CAD 554)HKAR-2 Administrative & Guidance Material (CAD 2)HKAR-21 Certification of Aircraft and Related Products, Parts andAppliances, and of Design and ProductionOrganisations (CAD 21)HKAR-66 Licensing of Maintenance Personnel (Certifying Staff –Maintenance) (CAD 66)HKAR-145 Approved Maintenance Organisations (CAD 145)HKAR-147 Approved Maintenance Training/Examination (CAD147)HKAR-MMEL/MEL Master Minimum Equipment List/Minimum EquipmentList (CAD 549)AN-6 P.130 May 2008
Page 1 and 2: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 3 and 4: NoticeNoIssue Date Subject30 5 30 S
Page 5 and 6: NoticeNoIssue Date Subject65 * 1 31
Page 7 and 8: [ * ] : Airworthiness Notices and/o
Page 9 and 10: 4.1 The contents list is re-issued
Page 11 and 12: INTENTIONALLY LEFT BLANK31 January
Page 13 and 14: Category B Helicopter. A single-eng
Page 15 and 16: together necessary to provide thrus
Page 19 and 20: Schedule 7Schedule 8Schedule 9− A
Page 23 and 24: (b) Assembly - that items are fitte
Page 25 and 26: (b)The holder of a Type Rated HKAR-
Page 27 and 28: combination of theoretical and prac
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Page 31 and 32: 6 HKAR-66 Category B3 Aircraft Main
Page 33 and 34: Certificates of Release to Service
Page 35 and 36: 3 Application3.1 The following appl
Page 37 and 38: Airworthiness Notice No. 4Appendix
Page 39: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 43 and 44: Government Printer, Hong Kong Speci
Page 45 and 46: Airworthiness Notice No. 6Appendix
Page 47 and 48: 6.2 Foreign Airworthiness Directive
Page 49 and 50: 10.2 Light Aircraft Maintenance (CA
Page 51 and 52: No. 21 Helicopter Public Address Sy
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Page 55 and 56: (1)No.(2)English Text(3)Chinese Tex
Page 57 and 58: work detailed in the renewal form w
Page 59 and 60: (e)any parachute including a parasc
Page 63 and 64: (a)an aircraft of the type is regis
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Page 75 and 76: AIRWORTHINESS NOTICE NO. 12APPENDIX
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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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CIVIL AVIATION DEPARTMENTHONG KONG,
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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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AIRWORTHINESS NOTICE NO. 17APPENDIX
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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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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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