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

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manuals for UK engines. Operators must obviously comply with any instruction given,but are additionally advised to inform the engine manufacturer of any conditions of theiroperation which may be at variance with his instructions. The Director-General willprovide assistance if desired in obtaining the manufacturers' assessment of the effects ofoperations on related lives.10 CancellationThis Notice cancels Airworthiness Notice No.44 Issue 3, dated 1 November 1996,which should be destroyed.Albert K. Y. LAMDirector-General of Civil AviationAN-44 P.331 January 2002
CIVIL AVIATION DEPARTMENTHONG KONG, CHINAAirworthiness NoticeNo. 45Issue 431 January 2002SOFTWARE MANAGEMENT1 Introduction1.1 This Notice sets out additional requirements applicable to the certification andcontinued airworthiness control of software used in aircraft equipment andsystems.1.2 Extensive use is now being made in aircraft of software-based equipment andsystems. Typically, software may be used in primary and secondary flightcontrols, engine controls, electrical generation and distribution, brakes, radioand navigation equipment, flight instruments, and automatic flight control. Thesoftware may have a direct influence on aircraft safety. Hence, in meeting theappropriate aircraft requirements and, for Controlled Items, the Requirements ofHKAR-1, it is necessary to investigate the software design and to control itscertification and post-certification configuration in a manner equivalent to thatfor conventional safety-critical systems.1.3 RTCA/EUROCAE document DO-178/ED-12 ∗ , issued May 1982, entitled"Software Considerations in Airborne Systems and Equipment Certification",provides guidance to aircraft manufacturers, equipment manufacturers andaircraft operators on software practices that would support the certification ofsoftware-based equipment and systems. This document is acceptable to theDirector-General as a basis for the certification of the software in aircraftequipment and systems.2 Requirements2.1 General2.1.1 In addition to the normal assessment of system criticality, theresponsible Design Organisation (normally the aircraft manufacturer)shall assign a Software Criticality Category to each software-basedequipment or system which shall relate to the severity of the effect ofpossible software errors within the equipment or system (see Appendixto this Notice). The Software Criticality Category assigned shall beagreed by the Director-General.∗ Obtainable from EUROCAE, 17 Rue Hamelin, 75116 Paris Cedex 16, FranceAN-45 P.131 January 2002
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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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Page 233 and 234: when installed, shall be monitored.
Page 235 and 236: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 237 and 238: 4.3 It is recommended that in order
Page 239 and 240: (c)(d)(e)(f)(g)(h)Ensure that any t
Page 241 and 242: Minimum (RVSM) compliant aircraft.
Page 245 and 246: shall be given in Overhaul Manuals.
Page 251 and 252: (iii)Option Selectable Software (OS
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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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