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

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4 Details of the operators slide deployment programme should be included in theApproved Maintenance Programme or Schedule.5 Every operator should define its own pass/fail criteria which should be accepted bythe Director-General. The pass/fail criteria should be based on anyrecommendations made by the aircraft or slide manufacturer and would be expectedto include at least the following as failures:• Failure of the automatic deployment system (i.e. manual inflation required);• Failure of the door to fully open;• Door assist failure (if fitted);• Failure to fully inflate;• Failure to fully inflate within 10 seconds (unless otherwise specified by themanufacturer). Timing is from when the door is initially actuated until the slideis deployed in an useable state;• Complete failure of slide lights to illuminate.All the above failures must be reported to the Director-General using the mandatoryoccurrence reporting (MOR) scheme and to the aircraft type certificate holder.6 To assist in the slide deployment failure investigation, unless otherwise agreed by theDirector-General, all slide deployments must be recorded by video and recordings offailed deployments should be held for one year or until any MOR or investigation intothe failure has been closed, whichever occurs later. A copy should be madeavailable to the Director-General on request.7 All slide deployment failures must be investigated to determine the cause of failureand action taken to prevent similar occurrences. The type certificate holder andescape slide manufacturer should be kept informed of failure investigations andprovide assistance where possible. If there are either high levels of slide failures orslide failure causes cannot be determined it may be necessary, in conjunction with theDirector-General to carry out further deployment tests, increase the paragraph 3.2sampling size or remove Minimum Equipment List alleviation until a satisfactorylevel of reliability is achieved.8 For each deployment test the door / slide position, slide part number, pass or failresult, date of manufacture of the slide, failure mode and failure cause should berecorded. Operators should forward a summary of slide deployment testing atregular intervals for each aircraft type to the Director-General. This summaryshould include the following information: Number of aircraft in fleet, number ofdeployments carried out and overall pass rate for fleet.31 May 2003 AN-12A16 P.2
9 Due to the complexity and safety critical nature of escape slide systems it isrecommended that maintenance organisations involved in the installation,maintenance and overhaul of escape slides should implement duplicate orindependent inspections on critical tasks i.e. slide installation, firing mechanismconnections, girt bar installation and rigging, door assist deactivation / slide safety pinremoval. Consideration should also be given to the training and competence ofpersonnel involved with the packing, installation, inspection and overhaul of escapeslides.10 Operators should review all escape slide continued airworthiness instructions from thetype certificate holder and escape slide manufacturer including service bulletins andservice letters and consider embodiment where there may be improvements in escapeslide reliability.When an Operator changes maintenance providers i.e. slide overhauler or aircraftmaintenance organisation it must review the slide deployment programme to monitorthe affects of such changes on the fleet escape slide reliability.11 CancellationThis Notice Appendix cancels Airworthiness Notice No.12 Appendix No.16 Issue 3,dated 31 January 2002, which should be destroyed.AN-12A16 P.331 May 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
Page 25 and 26: (b)The holder of a Type Rated HKAR-
Page 27 and 28: combination of theoretical and prac
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Page 31 and 32: 6 HKAR-66 Category B3 Aircraft Main
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 39 and 40: CIVIL AVIATION DEPARTMENTHONG KONG,
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
Page 53 and 54: 4 Requirement4.1 Bilingual Placard4
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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Page 65 and 66: (b)A Rating granted in relation to
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Page 73 and 74: Appendix Subject CAAIP Leaflet 11-2
Page 75: AIRWORTHINESS NOTICE NO. 12APPENDIX
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Page 83 and 84: handling organisations are made awa
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Page 91 and 92: 7 Maintenance of Aircraft - Non-Com
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Page 95 and 96: 1 ApplicabilityAIRWORTHINESS NOTICE
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Page 103 and 104: 4 Limited AuthorisationsFlight Crew
Page 105 and 106: which forms an integral part of the
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Page 111 and 112: It must be established by the owner
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All aircraft components must be rel
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AIRWORTHINESS NOTICE NO. 17APPENDIX
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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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