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

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Notice.5 ImplementationSoftware in aircraft systems and equipment is subject to the provisions of thisAirworthiness Notice, except for existing systems and equipment, where the provisionsof Airworthiness Notice No.45 have already been adopted.6 CancellationThis Notice cancels Airworthiness Notice No.45A Issue 4, dated 1 January 2002,which should be destroyed.Albert K. Y. LAMDirector-General of Civil Aviation31 January 2003 AN-45A P.4
RELATIONSHIP BETWEEN FUNCTION CRITICALITY CATEGORY AND SOFTWARE LEVELAIRWORTHINESS NOTICE NO. 45AAPPENDIX NO. 1Issue 431 January 2003FAR 25.1309 andJAR 25.1309 definitionsNo significant degradation of aircraftcapability or crew abilityReduction of the aircraft capability or of the crew ability to cope with adverse operatingconditionsPrevention of continued safe flight andlanding of the aircraftEffect onaircraft andoccupants offailureconditions ordesign errorACJ No.1 toJAR 25.1309definitions- Slight reduction of safety margins,- Slight increase in workload, e.g. routinechanges in flight plan, or- Physical effects but no injury to occupants- A significant reduction in safety margins,- A reduction in the ability of the flightcrew to cope with adverse operatingconditions as a result of increase inworkload or as a result of conditionsimpairing their efficiency, or- Injury to occupants- A large reduction in safety margins,- Physical distress or a workload such thatthe flight crew cannot be relied upon toperform their tasks accurately orcompletely, or- Serious injury to, or death of, a relativelysmall proportion of the occupantsLoss of aircraft and/or fatalitiesACJ No.1 to JAR 25.1309definition of Criticality CategoryMinor Effect Major Effect Hazardous/Severe -Major Effect Catastrophic EffectFAR Advisory Circular 25.1309-1Adefinition of Criticality CategoryNon essential Essential CriticalDO-178B/ED-12B Software level* Level D Level C Level B Level A* Note: Using appropriate design and/or implementation techniques, it may be possible to use a Software Level lower than the functional categorisation.CancellationThis Notice Appendix cancels Airworthiness Notice No.45A Appendix No.1 Issue 3, dated 31 January 2002, which should be destroyed.AN-45A A1 P.131 January 2003
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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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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
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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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