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

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4.3 If an aircraft carries ADS-B transmitting equipage which does not comply withthe requirements of paragraph 4.1 or 4.2, the aircraft shall not fly unless theequipage is:(a)(b)deactivated; orset to transmit only a value of zero for the Navigation UncertaintyCategory (NUC P ) or Navigation Integrity Category (NIC).5. Additional Information5.1 GNSS ReceiverAs Selective Availability (SA) aware and Fault Detection and Exclusion (FDE)functionalities will improve accuracy and integrity to the position source ofADS-B, the forward fitment of these functionalities to new aircraft is highlyrecommended.5.2 Operational ApprovalCompliance with the design requirements and standards of this Notice does notconstitute an operational approval. EASA Acceptable Means of ComplianceAMC 20-24 shall be used as the reference acceptance criteria for granting theADS-B operational approval by the Director-General.6. CancellationThis Notice cancels Airworthiness Notice No. 102F Issue 2, dated 28 February 2011,which should be destroyed.Norman LODirector-General of Civil AviationAN-102F P.331 July 2011
CIVIL AVIATION DEPARTMENTHONG KONG, CHINAAirworthiness NoticeNo. 103Issue 131 July 2011THIS NOTICE GIVES DETAILS OF A MANDATORY ACTIONFUEL TANK FLAMMABILITY REDUCTION1. ApplicabilityThis Airworthiness Notice is applicable to all Hong Kong registered aeroplanes, fittedwith Centre Wing Fuel Tank having a fleet average flammability exposure levelexceeding 7%, of which the individual Certificate of Airworthiness was first issued(whether in Hong Kong or elsewhere) on or after 1 February 2012.2. Introduction2.1. This notice provides information pertaining to the introduction ofFlammability Reduction Means for preventing the development of flammableair / fuel vapour mixtures within specific fuel tanks for new productionaeroplanes.2.2. The National Transportation Safety Board (NTSB) investigation of the Boeing747-131 accident on 17 July 1996 (Trans World Airlines Flight 800)determined that the probable cause of the accident was an explosion of thecentre wing fuel tank, resulting from ignition of the flammable air / fuelvapour mixture in the tank. The NTSB recommendations issued after theBoeing 747 accident were to eliminate the flammability exposure of the air /fuel vapour mixture and to make improvements to the safety of specific fueltank designs by reducing the probability of creating an ignition source withinthe fuel tank.2.3. Regulators and industry have done extensive work over the past years in orderto establish by which means fuel tank explosions could be prevented- The traditional certification approach of controlling ignition sourceswithin the fuel system has been reinforced; the relevant requirements ofPart 25 were made more stringent and design reviews were conducted.AN-103 P.131 July 2011
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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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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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Page 431 and 432: unit and any other galley insert wh
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Page 437 and 438: The position of safety belt buckle
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31 July 2011 C1 CIVIL AVIATION DEPARTMENT HONG KONG ...

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