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

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CIVIL AVIATION DEPARTMENTHONG KONG, CHINAAirworthiness Notice1 ApplicabilityTHIS NOTICE GIVES DETAILS OF A MANDATORY ACTIONPORTABLE OXYGEN EQUIPMENT PRESSURE RELIEFNo. 67Issue 331 January 2002This Airworthiness Notice is applicable to all portable oxygen equipment carried inHong Kong registered aeroplanes certificated in the Transport Category (Passenger)exceeding 5700 kg MTWA and to all aeroplanes manufactured after 1 July 1990exceeding 5700 kg MTWA, in all certification Categories.2 Introduction2.1 In a recent cabin fire-related accident, there were at least two instances ofportable oxygen equipment exploding and forming hazardous projectiles withinthe cabin as a result of direct involvement in the fire. The Director-General isconcerned about any possible risk to the aeroplane occupants or rescuepersonnel from such hazards.2.2 The explosive failure of an oxygen cylinder in a fire may be caused by highinternal pressure generated by the heating of the oxygen, combined with aweakening of the cylinder material. The incorporation of anovertemperature/overpressure relief device should reduce the probability ofsuch a dangerous explosion.2.3 Although protection against rupture is required on the fixed and portable oxygenequipment in all newly designed aeroplanes in accordance with JAR 25.1453and associated ACJ 25.1453, it was not a requirement in the 1950's and 1960'swhen many of the currently used portable oxygen equipment were firstapproved.2.4 The purpose of this Notice is to publish a requirement for the provision of anovertemperature/overpressure relief device on portable oxygen equipment.3 ComplianceAll portable oxygen equipment carried in aeroplanes defined in paragraph 1 above,shall comply with the requirement of this Notice.AN-67 P.131 January 2002
4 RequirementPortable oxygen equipment shall be equipped with an overtemperature/overpressurerelief device in accordance with the requirements of JAR 25.1453(b)(1) and associatedACJ 25.1453.5 Additional InformationCompliance with this requirement would normally be achieved by the provision of adedicated overtemperature/overpressure relief device. However, such a device maynot be necessary if it can be demonstrated by appropriate fire test evidence that thefailure of a part of the equipment (e.g. contents gauge) performs a similar function andsatisfies the requirement of this Notice.6 CancellationThis Notice cancels Airworthiness Notice No.67, Issue 2, dated 1 November 1996,which should be destroyed.Albert K. Y. LAMDirector-General of Civil Aviation31 January 2002 AN-67 P.2
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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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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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Page 297 and 298: 7 Concessions against any inspectio
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Page 305 and 306: NOTE: 'Designated' emergency exits
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Page 329 and 330: design to ensure repeatable in-serv
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Page 335 and 336: Box 4Box 5The question takes into a
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Page 341 and 342: CAD Approved Certificate will be re
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Page 359 and 360: 3.4 The periods of operation or ela
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Page 363 and 364: power switching relays, their physi
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Page 371 and 372: 3.3 All aeroplanes defined in parag
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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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