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

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5.4 The local attachment factor of 1.33 applies, in addition to the relevantprescribed acceleration forces, to door hinges, catches and restraint meanswhich form part of the equipment structure, and to structure adjacent to therestraint means provided by the galley or similar stowage.5.5 Doors, including their hinges and catches, of catering boxes, etc., must be ofstrength compatible with the placarded contents weight, unless use of the boxis restricted to stowage in completely enclosed galley, or similarcompartments. This also applies to the doors of catering trolleys, but in theircase, the total structure of the trolley must also be shown to be in compliancewith the strength requirements taking into account means of retention of thetrolley in the aircraft.5.6 The design of the trolley should be such that the loads imposed on the aircraftfloor, do not exceed any floor loading limitations.5.7 (a) Duplicated catches must be provided for means of retention for itemswhich are habitually operated during flight, to allow for failure of oneof the catches.(b)Where retention of a unit into its stowage compartment is by turn catch,operating the catch should not release more than one unit.5.8 Where catering trolleys have a facility for the collection of waste, they shallcomply with the fire containment requirements of BCAR Chapter D4-3paragraph 6.4.5.9 Where the basis of type certification of the aircraft requires the provision ofmeans of trolley restraint, in the passenger cabin, capable of withstanding theloads associated with the flight cases, the trolleys shall be provided withattachment means compatible with the anchorage points provided in theaircraft. Such methods of restraint should be engineered so that it can beused by one person and so that its use will be likely to occur by virtue of itssimplicity of operation.5.10 The trolleys must embody a brake system if they are to be removed from theirstowage in flight. In the absence of evidence justifying an equivalentminimum braking force then the braking mechanism must be qualified byloading the trolley to its maximum loaded weight and ensuring that thebraking mechanism holds the trolley on an incline plane of 7.5°.5.11 Trolleys shall carry placarded instructions:(a)(b)that they must be stored and secured during take-off, turbulent weatherand landing;that the gross weight of the unit, or the combined gross weight of theAN-99 P.330 May 2007
unit and any other galley insert when stowed together, must not exceedthe placarded maximum content weight of the compartment wherestowed; and(c)that when removed from their stowage they must not be leftunattended.5.12 The installation of all galley equipment shall be such that the size, weight, andmeans of restraint are compatible with the stowage facility provided, and thatunder design loads the item will not deform in such a manner so as to freeitself from the means of restraint.5.13 Account must be taken of the individual and total electrical power demand ofgalley equipment and an electrical load analysis must be included in designdocumentation.6 CancellationThis Notice cancels Airworthiness Notice No. 99 Issue 8, dated 30 September 2006,which should be destroyed.Norman LODirector-General of Civil Aviation30 May 2007 AN-99 P.4
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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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(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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Page 381 and 382: 2 Requirement2.1 Compliance with pa
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Page 387 and 388: 3.2 Applications for the approval o
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Page 391 and 392: 5 Additional Information5.1 EASA CS
Page 393 and 394: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 395 and 396: to be operated under IFR with non-i
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Page 399 and 400: 3.2 All aeroplanes flying for the p
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Page 421 and 422: 3.6 Parts that cannot be returned t
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Page 425 and 426: case. If such evidence cannot be ob
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Page 429: 3 Compliancethat these requirements
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Page 437 and 438: The position of safety belt buckle
Page 439 and 440: its removal from the water.5 Additi
Page 441 and 442: 4 Requirement4.1 Performance Levels
Page 443 and 444: equired, the helicopter shall compl
Page 445 and 446: 3.9 Compliance requirements for hel
Page 447 and 448: 4.5 Type IVA FDR Requirements4.5.1
Page 451 and 452: 4.2.3 The following provides guidan
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Page 461 and 462: 4.7 RNP AR APCHRNP equipages comply
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31 July 2011 C1 CIVIL AVIATION DEPARTMENT HONG KONG ...

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