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

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5 Compliance for applicable helicopters5.1 All Performance Class 1 and 2 helicopters operating on flights over water at adistance from land corresponding to more than 10 minutes at normal cruisespeed shall be equipped with one automatic ELT and one Survival ELT foreach raft carried (but not more than a total of two Survival ELT are required).5.2 Except as provided for in paragraph 5.1, all Performance Class 1 and 2helicopters shall be equipped with one automatic ELT and one Survival ELT.5.3 All Performance Class 3 helicopters operating on flights over water beyondautorotational or safe forced landing distance from land shall be equipped withone automatic ELT and one Survival ELT for each raft carried (but not morethan a total of two Survival ELT are required).5.4 Except as provided for in paragraph 5.3, all Performance Class 3 helicoptershaving a Maximum Total Weight Authorised of 2730 kg or less shall beequipped with one automatic ELT.5.5 Except as provided for in paragraph 5.3 and 5.4, all Performance Class 3helicopters shall be equipped with one automatic ELT and one Survival ELT.5.6 ELT equipment carried to satisfy the requirements of paragraphs 5.1, 5.2, 5.3,5.4 and 5.5 shall operate in accordance with the relevant provisions of ICAOAnnex 10, Volume III, Part II, Chapter 5 (See paragraph 6 of this notice).5.7 For paragraphs 5.1, 5.2, 5.3, 5.4 and 5.5, the choice of ELT type andplacement of the ELT on helicopters and associated floatable life supportsystems must ensure the greatest chance of ELT activation in the event of anaccident for aircraft operating over water or land. Placement of transmitterunits is a vital factor in ensuring optimal crash and fire protection. Theplacement of the control and switching devices (activation monitors) ofautomatic fixed ELT and their associated operational procedures will also takeinto consideration the need for rapid detection of inadvertent activation andconvenient manual switching by crew members. These should be acceptableto the Director-General.6 Highlights of ICAO Annex 10, Volume III, Part II, Chapter 56.1 ELT shall operate on 406 MHz and 121.5 MHz simultaneously.6.2 The technical characteristics for the 406 MHz component of an integral ELTshall be in accordance with paragraph 5.3 of ICAO Annex 10, Volume III,Part II, Chapter 5.6.3 The technical characteristics for the 121.5 MHz component of an integral ELTshall be in accordance with paragraph 5.2 of ICAO Annex 10, Volume III,<strong>31</strong> January 2007 AN-27 P.4
Part II, Chapter 5.7 Coding and registration of Hong Kong 406 MHz ELT7.1 Details regarding the coding and registration of Hong Kong 406 MHz ELT arecontained in Appendix No. 1 to this notice.8 Cancellation8.1 This Notice cancels Airworthiness Notice No. 27 Issue 4, dated 30 May 2005.Norman LODirector-General of Civil AviationAN-27 P.5<strong>31</strong> January 2007
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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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Page 131 and 132: accepted by CAD as in full complian
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Page 149 and 150: specialist organisation.2.4 Details
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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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