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

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2 Definitions2.1 For the purpose of this Notice the following definitions apply:(a)Aircraft Configuration List (ACL)A list of Line Replaceable Units (LRU) and modules with LoadableSoftware Aircraft Part (LSAP) that are applicable to a specific aircraft.This list may be contained on data supplied by the TC holder in aService Bulletin (SB), Service Information Letter (SIL) or IllustratedParts Catalogue (IPC), or as a separate tracking system.(b)Field Loadable Software (FLS)Software (executable code) that can be loaded without removing thesystem or equipment from the aircraft. FLS can be loaded onto anaircraft system by a maintenance mechanic/technician in accordancewith defined maintenance manual procedures. FLS can be configuredas a component of target hardware and thus affect the part number ofthe target hardware. There are numerous types of FLS, but most canbe categorised as follows:(i)Loadable Software Aircraft Part (LSAP)FLS that is required to meet a specific airworthiness oroperational requirement or regulation and not considered as acomponent of the target hardware, but is considered to be partof the aircraft approved design and therefore an aircraft partrequiring formal controlled release documentation (JAA FormOne, EASA Form 1 or FAA 8130-3) or an equivalent agreedwith the Director-General.(ii)User Modifiable Software (UMS)Software declared by the aircraft TC holder's designorganisation (or STC holder's design organisation) as beingintended for modification by the aircraft operator, usuallywithout review by the Director-General, the aircraft TCholder's (or STC holder's) design organisation or the equipmentmanufacturer, if modified within the constraints establishedduring certification. Should the need arise to modify thesoftware outside of these constraints then the operator will needto seek guidance from the Director-General, the aircraft TCholder's design organisation (or STC holder's designorganisation) and/or the equipment manufacturer on how thisshould be accomplished.30 September 2005 AN-43 P.2
(iii)Option Selectable Software (OSS)LSAP that contains approved and validated components andcombinations of components that may be activated or modifiedby the aircraft operator within defined TC/STC holderboundaries.(c)Database Field Loadable Data (DFLD)Data that is field loadable into target hardware databases.(i)DatabasesA term generally misused to describe the "data" that is fieldloaded into target hardware. However, the database isactually an embedded item that resides within the targethardware and is not, itself, field loadable. The processnormally described as "loading a database" actually loads adata file onto the target hardware's embedded database. Theupdating of the data held on a database, by the uploading of anew data file, will normally be conducted to provide formodifications to operating functions, including the revision ofthe aircraft performance or navigational data. It should benoted that whilst "LSAP" is only associated with FLS(executable code), certain DFLD should be treated in the samemanner, in that they will have their own part number requiringcontrol as an aircraft part and should be accompanied bycontrolled release documentation (JAA Form One, EASA Form1 or FAA 8130-3). The form of release required for differenttypes of DFLD is defined in paragraph 3.(ii)Data FileA specific file that contains the actual data that is the object ofthe database and is field loaded.(d)Target HardwareThe hardware such as LRU and modules that are intended to be loadedwith FLS or DFLD.(i)Examples of target hardware for LSAP (FLS) could be: anElectronic Engine Control (EEC), a Digital Flight DataAcquisition Unit (DFDAU), an Auxiliary Power Unit'sElectronic Control Unit (ECU), a Flight Guidance Computer(FGC), or an Integrated Modular Avionics (IMA) Unit.AN-43 P.330 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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Page 249: CIVIL AVIATION DEPARTMENTHONG KONG,
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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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