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

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(iii)If airborne equipment has only one part number, whichrepresents a specific configuration of software and hardware,the unit identification on the nameplate should be changed ifnew software is loaded. In order for this to be embodied onthe aircraft this should be accomplished in accordance with anaircraft manufacturer's SB. The software part number storedin the target computer after data loading should be verifiedelectronically and confirmed to be an approved configurationas detailed in the SB.(d)Verification that the upgrade actually is needed.(i)(ii)If the system is working as required and the FLS or DFLDupgrade is not introducing a required solution or functionaddition or change, it is not always necessary to upgrade theFLS or DFLD simply for the sake of upgrading. Equally, it ispossible that the upgrade could introduce problems that did notexist before.It is also necessary to check any support agreements to ensurethat customer support for the FLS or DFLD will remain valid.(e)Identify what has changed between the different versions of the FLS orDFLD. This should include identifying and recording within the FLSand DFLD register the problems that have been fixed and whatfunctionality has been added or removed. (See paragraph 1.1(d) ofthis Appendix.)2 Control of FLS or DFLD Tooling2.1 FLS or DFLD can be loaded into the Target Hardware using a variety of toolsas recommended and/or approved by the aircraft or Target Hardwaremanufacturer. These can include Original Equipment Manufacturer (OEM)supplied tools, Commercial Off The Shelf (COTS) tools or in-housedeveloped tools.2.1.1 There are a number of issues associated with FLS or DFLD toolingthat the aircraft operator would need to take into account if analternative to the tooling recommended by the aircraft or TargetHardware manufacturer was to be considered. Prior to seeking theaircraft or Target Hardware manufacturer's approval for any alternativetools' use, the aircraft operator should take the following items intoaccount. These are associated with the general tool selection, and thecontrol and the suitability of those tools.30 September 2005 AN-43 A1 P.4
2.2 General Tool SelectionThe following general issues should be considered when making a FLS orDFLD tool selection:(a)What function is the tool required to perform:(i)(ii)(iii)(iv)Is it simply loading, leaving other tools or processes to performcompatibility checks and validation tasks?Is it loading and validating the final load, leaving initialcompatibility checks to other tools or processes?Is it providing all the tasks associated with loading(compatibility checks, loading and validation) and providing adiagnostic feature?Any other combination of the above should be considered.(b)(c)(d)(e)(f)(g)(h)(i)(j)(k)(l)Is the tool (which could be a laptop) able to be suitably controlled?Does the tool supplier have any previous experience in developingtools for the required purpose?Will the tool supplier provide support and training?Does the tool provide all the needed functionality or will additionaltools or processes be needed?Does the tool provide the necessary confirmation of what has beenloaded onto the aircraft?Do any existing tools that have Director-General's acceptance alreadyprovide the required functionality?How much dependence will be placed on the tool?Will the tool supplier provide support for the tool for the duration of itsuse?Is the tool widely used in the industry and does it have a goodreputation?If the tool is not widely used in the industry, is there any other way toestablish its integrity?Will special training be required to use the tool?AN43 A1 P.530 September 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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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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Page 211 and 212: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 213 and 214: (d)The data obtained during the ins
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Page 219 and 220: a pressure gauge (reading up to 140
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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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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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