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

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(a)(b)(c)(d)operate independently of any other attitude indicating system;be so located on the instrument panel that it will be visible to,and usable by, both pilots from their normal positions;be compatible in presentation with the main attitude indicatingsystem;be fitted with a failure warning device. Alternatively a meansof indicating that the power supply to the instrument isoperating correctly shall be provided.2.3.2 Where the instrument on the Captain's flight instrument panel isutilized:(a)(b)the circuitry to the instrument shall be modified, as necessary,so that transfer to the emergency source of supply isautomatically effected in the event of failure of the mainsupply;the requirements of paragraph 2.3.1(d) shall be met.3 Additional Information3.1 Representations have been made to the Director-General that under conditionsof widespread adverse weather, or heavy traffic density at airports, a period of30 minutes may be a less than desirable time for flight to a suitable airfieldand landing, and clearly this period by itself is inadequate for long rangeaircraft.3.1.1 The basis of Hong Kong certification of all long range, and of certainshort/medium range, aircraft types is that after a period of interruptionof electrical supplies it will be possible for the crew to re-establishsufficient normal, or emergency, generated power to support allnecessary essential services, including the instrument covered by thisNotice, for the remainder of the flight. The prescribed period of 30minutes is considered to be adequate to allow for appropriate crewaction for this class of aircraft.3.1.2 For those shorter range aircraft that are totally dependent on batterypower to support all essential services to the completion of the flight, aperiod of 30 minutes assuming a crew delay time of 10 minutes, is themandatory minimum endurance of the emergency supply for thehorizon instrument prescribed in this Notice. It is, however, stronglyrecommended that in circumstances where the crew do take promptand correct actions in response to warning indications of theinterruption of all generated electrical power, the aircraft installationAN-81 P.330 May 2006
should include adequate battery capacity to provide a 60 minute supplyfor both the subject instrument and the other services essential tocomplete the flight and make a landing.3.2 A number of aircraft types already comply with the requirements of thisNotice, or incorporate other special features which have been considered andaccepted by the Director-General as providing an equivalent level of safety.4 CancellationThis Notice cancels Airworthiness Notice No.81, Issue 4, dated <strong>31</strong> January 2002,which should be destroyed.Norman LODirector-General of Civil Aviation30 May 2006 AN-81 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
Page 331 and 332: (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 355 and 356: AIRWORTHINESS NOTICE No. 74APPENDIX
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 395 and 396: to be operated under IFR with non-i
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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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