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

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AIRWORTHINESS NOTICE NO. 35APPENDIX NO. 1Issue 430 May 20051 The concept of allowing engines to run beyond the manufacturer's recommendedoverhaul period depends upon it being possible to assess the condition of the engineby prescribed inspections carried out at defined intervals. It is not intended toprovide a freedom to run until the engine fails.2 Although it is possible to identify engine degradation in many areas of the engine,there are some potential failure modes (e.g. crankshaft cracking, counterweight wear)for which predictive checks would not be effective without engine disassembly.3 For the above reasons, the overhaul period extensions defined in paragraph 3.1.1 and3.1.2 of Airworthiness Notice No. 35 may not be applied unless adequate in servicereliability has been demonstrated, particularly in relation to failures which cannot beprevented by on-wing inspection. Those engine types that are not eligible to makeuse of the provisions of Airworthiness Notice No. 35 are detailed in paragraph 5.4 The UKCAA has sought the advice of the manufacturers of the majority of the pistonengines currently used in light aircraft to try to identify those engine componentswhich service experience has shown to have running time limits beyond which itwould not be reasonable to operate, (i.e. components the failure of which are notsusceptible to prior detection but which would result in either an unacceptably highfailure rate or a hazardous failure). The Director-General has adopted theaforementioned and any limits identified are reflected in paragraph 5 below.5 LimitationsThe provisions of the Airworthiness Notice No. 35 are applicable to all light aircraftpiston engines except where listed below:5.1 Rolls-Royce Gipsy Major Engines - Prior to running beyond 120% of themanufacturer's recommended overhaul period, engines other than Major 10and earlier marks incorporating Modification 2385 (splined propellerattachment) must have the taper portion of the crankshaft "Sulfinuz" treated byModification 2690 or appropriate alternative. In accordance with Rolls-Royce Technical News Sheet G15, engines must not exceed an overhaulperiod of 1000 hours unless Modification 2495 is embodied.5.2 The following engine types have yet to accumulate sufficient serviceexperience to demonstrate acceptable reliability when operating at themanufacturer's recommended overhaul period. Once acceptable reliabilityhas been demonstrated, requests to extend the applicability of AirworthinessNotice No. 35 to include the particular engine type will be considered. In theAN-35 A1 P.130 May 2005
6 Cancellationmean time, the provisions of Airworthiness Notice No. 35 are not applicableto:5.2.1 Societe de Motorisations Aeronautique – All types5.2.2 Rotax – All types5.2.3 Thielert – All types5.2.4 Mid-West Engines – All typesThis Notice Appendix cancels Airworthiness Notice No. 35 Appendix No.1 Issue 3,dated <strong>31</strong> January 2002, which should be destroyed.30 May 2005 AN-35 A1 P.2
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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
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
Page 169 and 170: 1 GeneralAIRWORTHINESS NOTICE NO. 2
Page 175 and 176: List of HKAR-147 approved maintenan
Page 177 and 178: Table 2:Non-Critical HPMA PartsHPMA
Page 179 and 180: HPMA No. Supp. Item Part Name Part
Page 187 and 188: (d)(e)(f)desiring to enhance cooper
Page 189 and 190: (c)(d)(e)in the case of serious non
Page 191 and 192: Certificate of Release to Service a
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Page 197 and 198: Technical Records include but are n
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Page 201 and 202: Authority in respect of any major m
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Page 213: (d)The data obtained during the ins
Page 217 and 218: AIRWORTHINESS NOTICE NO. 35APPENDIX
Page 219 and 220: a pressure gauge (reading up to 140
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Page 225 and 226: and cabin crew seats as applicable,
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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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Page 245 and 246: shall be given in Overhaul Manuals.
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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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