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

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period for the purposes of this Notice, including recommendations by themanufacturer for reduced overhaul periods with particular types of operationor particular service bulletin/modification configurations.3.1.1 Engines that have reached the operating time or calendar timelimitation of a recommended overhaul period may continue in servicefor a further period of operation not exceeding 20% of therecommended operating time or calendar time, whichever occurs first,subject to (a), (b), (c), (d) and (e).(a)(b)(c)(d)(e)Compliance being shown with the appropriate limitationsspecified in Appendix No.1 paragraph 5 to this Notice.Compliance being shown with any applicable AirworthinessDirective which requires compliance at engine overhaul, unlessotherwise agreed by the Director-General.The engine must have been operated in an aircraft registered inHong Kong for a period of at least 200 hours immediately priorto completion of the engine manufacturer' overhaul periodrecommendation.The engine being inspected in accordance with paragraph 4 inorder to assess its condition immediately prior to the increase,and subsequently at 100 hour or yearly intervals, whicheveroccurs first.The data obtained during the inspections of paragraph 4 beingentered in the engine log book.3.1.2 Engines that have complied with paragraphs 3.1 and 3.1.1, and havecompleted the 120% of the recommended operating time or calendartime, whichever occurs first, may continue in service indefinitely,subject to (a), (b), (c) and (d).(a)(b)(c)The engine being installed in aircraft which is not used for thepurpose of Public Transport or Aerial Work.Compliance being shown with the appropriate limitationsspecified in Appendix No.1 to this Notice.The engine being inspected in accordance with paragraph 4 inorder to assess its condition before exceeding 120% of therecommended operating time or calendar time, whicheveroccurs first, and subsequently being inspected and re-assessedat 100 hour or yearly intervals, whichever occurs first.30 May 2005 AN-35 P.2
(d)The data obtained during the inspections of paragraph 4 beingentered in the engine log book.3.2 In the event that the inspection referred to in paragraphs 3.1.1 and 3.1.2 results inrejection, a thorough engineering investigation must be carried out to establish themaintenance actions required to return the engine to an airworthy condition.4 The inspections referred to in paragraph 3.1.1 and 3.1.2 to assess the condition ofengines shall be in accordance with Appendix No. 3 to this Notice and shall be carriedout by persons or organisations as follows:(a)(b)Engines installed in aircraft that are used for the purpose of Public Transportor Aerial Work by a CAD360 Operator under an Air Operator's Certificate,shall be inspected by a HKAR-145 maintenance organisation appropriatelyapproved for the purpose.All other engines shall be inspected by an appropriately type rated HKAR-66Aircraft Maintenance Licence holder or an organisation specifically approvedfor the purpose.5 In no case shall any mandatory restrictions be exceeded, and the compliance withmandatory bulletins/modifications/inspections shall be completed at the specifiedtime.6 In the case of engines not incorporating all the service bulletins/modifications or partsthat would enable it to qualify for any overhaul period recommended by the enginemanufacturer as defined in paragraph 3.1 of this Notice, or of engine types notincluded in the manufacturers' bulletins, a specific recommendation in writing mustbe sought from the engine manufacturer, and if this is not obtainable, an applicationmust be made to the Director-General. The Director-General need not be consultedin a case where the only question is that an engine manufacturer's documents restrictrecommended overhaul periods to engines embodying only parts specified by theengine manufacturer: the Director-General will not require such restrictions to beapplied provided that all parts are acceptable under the provisions of AirworthinessNotice No. 17, and there has been no adverse experience relating to the use of suchparts.7 For clarity, the requirements of paragraph 3 are presented in tabular form in AppendixNo.2.8 CancellationThis Notice cancels Airworthiness Notice No. 35 Issue 5, dated <strong>31</strong> January 2002,which should be destroyed.Norman LODirector-General of Civil AviationAN-35 P.330 May 2005
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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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Page 163 and 164: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 165 and 166: Performance Class 1 helicopter A he
Page 167 and 168: Part II, Chapter 5.7 Coding and reg
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Page 177 and 178: Table 2:Non-Critical HPMA PartsHPMA
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Page 211: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 215 and 216: 6 Cancellationmean time, the provis
Page 217 and 218: AIRWORTHINESS NOTICE NO. 35APPENDIX
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Page 231 and 232: (b)(c)Install a means for monitorin
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Page 239 and 240: (c)(d)(e)(f)(g)(h)Ensure that any t
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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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