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

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2.4 Both examination centres use identical question bank to generate examinationpapers. The CAD Authorised Examination Centre is providing computerisedexaminations on multiple-choice questions for all HKAR-66 Modules.2.5 Examination results issued by either examination centre are equally acceptedby CAD for the granting of HKAR-66 AML.2 CancellationThis Notice Appendix cancels Airworthiness Notice No. 4 Appendix No. 1 Issue 2,dated 30 May 2008, which should be destroyed.15 February 2009 AN-4 A1 P.2
CIVIL AVIATION DEPARTMENTHONG KONG, CHINAAirworthiness NoticeNo. 5Issue 330 October 2001TYRE WEAR LIMITATIONS1 Introduction1.1 Hong Kong Aviation Requirements require that for certification of new types ofaircraft, the depth of tyre tread below which wet braking friction characteristicsare impaired should be specified at the time of certification; it is also requiredthat it should be possible to determine, in operational conditions, when the treaddepth is worn below this limit.1.2 This Notice provides general guidance on the subject of tyre wear limitationsfor operators of all public transport aeroplanes of more than 5700 kg MaximumTotal Weight Authorised on the Hong Kong Register for which a limiting tyretread depth is not otherwise available.2 Discussion2.1 Accidents and incidents, resulting from both loss of braking friction and loss ofdirectional control on wet runways, continue to occur. While the scheduledaccelerate-stop and landing distances provide some allowance for deteriorationin friction, it has been established that this allowance is not sufficient tomaintain the required level of safety if tyres which are more than 80% worn areused in wet runway operations.2.2 As it is not possible fully to allow for this by increasing the scheduled distances(because of the frequency of incidents caused by loss of directional control,even on the most favourable wheel arrangements), the Director-General favoursthe retention of current scheduled distances, together with a recommendedminimum tread depth applicable to all aircraft tyres.3 RecommendationIn the absence of evidence of the safety of a lower limit for a particularaircraft/tyre/operation combination, it is recommended that a tyre be withdrawn fromservice when it is worn to such an extent that its wet runway performance would beseriously impaired. This may be defined as when:-(a)it is worn such that any groove has a depth of less than 2 mm of tread for moreAN-5 P.130 October 2001
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
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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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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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