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

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CIVIL AVIATION DEPARTMENTHONG KONG, CHINAAirworthiness NoticeNo. 1AIssue 115 February 2009DEFINITIONS1. IntroductionThis Airworthiness Notice is intended to supplement the definitions of terms thatare not included in various airworthiness publications published by CAD.2. DefinitionsThe following terms are defined in current ICAO Standards and RecommendedPractices:Air Operator Certificate. A certificate authorizing an operator to carry outspecified commercial air transport operations.Aircraft Operating Manual. A manual, acceptable to the State of the Operator,containing normal, abnormal and emergency procedures, checklists, limitations,performance information, details of the aircraft systems and other materialrelevant to the operation of the aircraft.Note: The Aircraft Operating Manual is part of the Operations Manual whichcontaining procedures, instructions and guidance for use by operationalpersonnel in the execution of their duties..Altimetry System Error (ASE). The difference between the altitude indicatedby the altimetry display, assuming a correct altimeter barometric setting, and thepressure altitude corresponding to the undisturbed ambient pressure.Auxiliary-Power-Unit (APU). A self-contained power-unit on an aircraftproviding electrical/pneumatic power to aircraft systems during groundoperations.Category A Helicopter. A multi-engine helicopter designed with engine andsystem isolation features specified in Part IVB of ICAO Annex 8 and capable ofoperations using take-off and landing data scheduled under a critical enginefailure concept which assures adequate designated surface area and adequateperformance capability for continued safe flight or safe rejected take-off.AN-1A P.115 February 2009
Category B Helicopter. A single-engine or multi-engine helicopter which doesnot meet Category A standards. Category B helicopters have no guaranteedcapability to continue safe flight in the event of an engine failure, and a forcedlanding is assumed.Critical Power-Unit(s). The power-unit(s) failure of which gives the mostadverse effect on the aircraft characteristics relative to the case underconsideration.Note: On some aircraft there may be more than one equally critical power-unit.In this case, the expression “the critical power-unit” means one of those criticalpower-units.Engine. A unit used or intended to be used for aircraft propulsion. It consists ofat least those components and equipment necessary for functioning and control,but excludes the propeller (if applicable).Final Approach and Take-off Area (FATO). A defined area over which thefinal phase of the approach manoeuvre to hover or landing is completed andfrom which the take-off manoevre is commenced. Where the FATO is to be usedby performance Class 1 helicopters, the defined area includes the rejectedtake-off area available.Fire Resistant. The capability to withstand the application of heat by a flame fora period of 5 minutes.Note: The characteristics of an acceptable flame can be found in ISO 2685.Fireproof. The capability to withstand the application of heat by a flame for aperiod of 15 minutes.Note: The characteristics of an acceptable flame can be found in ISO 2685.Fireproof Material. A material capable of withstanding heat as well as or betterthan steel when the dimensions in both cases are appropriate for the specificpurpose.Flight Recorder. Any type of recorder installed in the aircraft for the purpose ofcomplementing accident/incident investigation.Glider. A non-power-driven heavier-than-air aircraft, deriving its lift in flightchiefly from aerodynamic reactions on surfaces which remain fixed under givenconditions of flight.Ground Handling. Services necessary for an aircraft’s arrival at, and departurefrom, an airport, other than air traffic services.Gyroplane. A heavier-than-air aircraft supported in flight by the reactions of the15 February 2009 AN-1A P.2
Page 1 and 2: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 3 and 4: NoticeNoIssue Date Subject30 5 30 S
Page 5 and 6: NoticeNoIssue Date Subject65 * 1 31
Page 7 and 8: [ * ] : Airworthiness Notices and/o
Page 9 and 10: 4.1 The contents list is re-issued
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Page 15 and 16: together necessary to provide thrus
Page 19 and 20: Schedule 7Schedule 8Schedule 9− A
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Page 27 and 28: combination of theoretical and prac
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Page 33 and 34: Certificates of Release to Service
Page 35 and 36: 3 Application3.1 The following appl
Page 37 and 38: Airworthiness Notice No. 4Appendix
Page 43 and 44: Government Printer, Hong Kong Speci
Page 45 and 46: Airworthiness Notice No. 6Appendix
Page 47 and 48: 6.2 Foreign Airworthiness Directive
Page 49 and 50: 10.2 Light Aircraft Maintenance (CA
Page 51 and 52: No. 21 Helicopter Public Address Sy
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Page 55 and 56: (1)No.(2)English Text(3)Chinese Tex
Page 57 and 58: work detailed in the renewal form w
Page 59 and 60: (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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CIVIL AVIATION DEPARTMENTHONG KONG,
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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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3.2 Fatigue3.3 StressTiredness and
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4 SummaryThe effects of illness, in
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(vi)(vii)(viii)(ix)Drugs for the re
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2.3 Each approved organisation is r
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(paragraph 3).4.3 Overseas Organisa
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7 Concessions against any inspectio
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5 CancellationThis Notice cancels A
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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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