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

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3 Additional Information3.1 When ascertaining that the installed aircraft battery capacity is adequate forcompliance with paragraph 2.3, the following loads should be taken intoaccount:(a)(b)Attitude information (where applicable in accordance with paragraph2.4).Essential Radio Communication.NOTE: For the purpose of calculations it will normally be accepted that intermittentuse of a single VHF communication equipment satisfies this requirement.Utilisation on the basis of a total of 15 minutes reception plus 3 minutestransmission in the 30 minute period would be an acceptable interpretation.(c)(d)(e)(f)Essential cockpit lighting.Pitot Head Heater (applicable only to those aircraft certificated forflight in icing conditions).Any other services essential for the continued safe flight and landing ofthe particular aircraft.Those services that cannot readily be shed when carrying out the drillsrequired under paragraph 2.5.3.1.1 In order to ensure that the essential services, taken into account inaccordance with paragraph 3.1, will function adequately for theprescribed period, the calculation of the duration of battery supplyshould normally be based on the following assumptions:(a)(b)Only 75% of the 'name plate' rating of the battery is available(this is to take into consideration loss of capacity with age, anda realistic state of charge).The voltage/time discharge characteristic of the battery,appropriate to the load of the listed services, is not extendedbeyond a battery terminal voltage of 21.5 volts on a 24 voltsystem, pro rata for 12 volt systems, (this is to ensure that thevoltage available throughout the prescribed period is adequatefor the satisfactory operation of the services).NOTE: Only where compliance with the requirements of this Notice cannotbe shown within the criteria of paragraphs 3.1 and 3.1.1, willconsideration have to be given to the fitment of additional, or largercapacity, batteries to particular aircraft.AN-82 P.330 May 2006
3.2 Applications for the approval of modifications necessary to ensure compliancewith the requirements of this Notice should be made in the manner specified inHKAR-1 Sub-section 1.2-5.4 CancellationThis Notice cancels Airworthiness Notice No.82 Issue 3, dated <strong>31</strong> January 2002,which should be destroyed.Norman LODirector-General of Civil Aviation30 May 2006 AN-82 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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Page 335 and 336: Box 4Box 5The question takes into a
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Page 339 and 340: 4 RequirementPortable oxygen equipm
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Page 347 and 348: (c)The Director-General will not, a
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Page 351 and 352: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 355 and 356: AIRWORTHINESS NOTICE No. 74APPENDIX
Page 359 and 360: 3.4 The periods of operation or ela
Page 361 and 362: AIRWORTHINESS NOTICE NO. 75APPENDIX
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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Page 381 and 382: 2 Requirement2.1 Compliance with pa
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Page 395 and 396: to be operated under IFR with non-i
Page 397 and 398: 3.3 For example, class of emission
Page 399 and 400: 3.2 All aeroplanes flying for the p
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Page 409 and 410: Quality Procedures.6 Suppliers and
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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 and 430: 3 Compliancethat these requirements
Page 431 and 432: unit and any other galley insert wh
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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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