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

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(a)(b)(c)(d)Function is the chosen design solution to prevent undesirable failureconsequences e.g. insulation function, cooling function etc.Functional failure is the failure of a chosen design solution to performthe intended function.Failure consequence is the result of the functional failure. The mostsignificant failure consequences are the presence of an ignition, heat orelectric shock source that could lead to smoke/fire or passenger injury.Failure cause is the reason for the functional failure e.g.• Wiring prone to damage;• Components susceptible to fluid spill;• Dust/debris contamination causing overheat;• Components prone to overheat;• Passenger traffic damage;• Components subject to frequent removal/replacement;• Poor electrical bonding;• Mechanical breakdown due to wear.(List not exhaustive.)2.3 Development of Scheduled Maintenance Tasks and SolutionsOnce the functions and functional failures have been identified the series ofquestions contained in the following flowchart should be asked to determinethe applicable and effective scheduled maintenance task and/or solutions tomitigate/prevent the failure of a chosen design solution. This developmentshould be accomplished with the collaborative effort of the TC/STC Holder(s),operator and project manager as appropriate.2.4 Guidance on how to use the FlowchartBox 1Box 2Box 3This question must be asked for each functional failure of thechosen design solution being analysed. The intent is to segregatethe evident and hidden functional failures. The operating crewconsists of qualified flight compartment and cabin attendantpersonnel who are on duty. Normal duties are those dutiesassociated with the routine operation of the aircraft on a dailybasis.Failure consequences to consider are those previously describede.g. ignition, heat or electric shock.The failure in question does not directly affect safety and thereforethe issue is one of reliability and/or passenger convenience. Theanalyst should discuss this with the operator and address the failureas necessary.<strong>31</strong> January 2006 AN-65 A1 P.2
Box 4Box 5The question takes into account failure(s) in which either the singlehidden/dormant failure (from Box 1) or in combination with oneadditional failure could cause one of the identified undesirableconsequences.This is to propose various applicable and effective tasks and/orpreventative actions, either singularly or in combination, for theanalyst to identify:(5a)(5b)(5c)(5d)Inspection – either:• Detailed (An intensive examination of a specific item,installation or assembly to detect damage, failure orirregularity. Available lighting is normallysupplemented with a direct source of good lighting at anintensity deemed appropriate. Inspection aids such asmirrors, magnifying lenses, etc. may be necessary.Surface cleaning and elaborate access procedures maybe required).Or• General Visual (A visual examination of an interior orexterior area, installation or assembly to detect obviousdamage, failure or irregularity. This level ofinspection is made from within touching distance unlessotherwise specified. A mirror may be necessary toenhance visual access to all exposed surfaces in theinspection area. This level of inspection is made undernormally available lighting conditions such as daylight,hangar lighting, flashlight or drop-light and may requireremoval or opening of access panels or doors. Stands,ladders or platforms may be required to gain proximityto the area being checked.)Functional Check• A quantitative check to determine if one or morefunctions of an item performs within specified limits.Restoration Task• That work necessary to return the item to a specificstandard. Restoration may vary from cleaning orreplacement of single parts up to a complete overhaul.Discard• The removal from service of an item at a specified lifelimit.(5e)Update Maintenance Practice/instructions• Amend standard practices (either company orAN-65 A1 P.3<strong>31</strong> January 2006
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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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(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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