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

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pitch propeller.* 6.3 Piston engines in Aeroplanes.Piston engines not exceeding 500 kW (670 bhp) inAeroplanes/Rotorcraft/Airships.* 6.3.1 Piston engines, in Aeroplanes not exceeding 2730 kg MTWA.* 6.4 Jet-turbine engines in Aeroplanes not exceeding 22.25 kN (5000 lbf) staticthrust including where so endorsed the associated APU installations.* 6.5 Propeller turbine engines in aeroplanes including, where so endorsed, theassociated APU installations:-Garret Airesearch TPE 3<strong>31</strong>* 6.6 Jet turbine engines, in aeroplanes, exceeding 22.25 kN (5000 lbf) static thrustincluding where so endorsed the associated APU installation.7 Certification Privileges - Rotorcraft* 7.1 Piston-engined rotorcraft.7.2 Reserved.* 7.3 Turbine-engined rotorcraft not exceeding 2730 kg MTWA.NOTE: This paragraph includes the Allison 250 and Turbomeca Arriel engines. For anengine annotated #, removal/replacement of main casings including those whoseremoval results in concurrent removal of a rotating assembly from the engine,provided this is accomplished solely by disconnecting at the casing flanges. Nodismantling of main rotating assemblies is permitted.* 7.4 Sikorsky S76 with Turbomeca Arriel #NOTE: For an engine annotated #, removal/replacement of main casings including thosewhose removal results in concurrent removal of a rotating assembly from the engine,provided this is accomplished solely by disconnecting at the casing flanges. Nodismantling of main rotating assemblies is permitted.8 Certification Privileges - Instruments(a)A Rating granted in relation to any of the sub-paragraphs 8.1 to 8.4 inclusive,includes all of the instruments fitted to those aircraft in which are installedsystems defined by or listed in that sub-paragraph excluding those aircraftlisted in paragraph 14, and as limited by paragraph 3 of this Notice.30 September 2008 AN-10 P.4
(b)A Rating granted in relation to sub-paragraph 8.8 relates to Instruments–Direct and remote reading compasses only, but excludes compasses on thoseaircraft listed in paragraph 14, and is limited by sub-paragraph 3.3 of thisNotice.NOTES:(1) A Type Rated Licence which is valid for paragraphs 8.2, 8.3 or 8.4 alsoincludes paragraph 8.1.(2) Where a system is a combined flight director/automatic pilot the rating doesnot include items of equipment associated solely with the automatic pilot.* 8.1 General aircraft instrument systems but excluding instruments installed on anyaircraft which has installed a Flight Director System.8.2 Reserved.* 8.3 Flight Director Systems employing air driven gyroscopes (attitude).* 8.4 Flight Director Systems employing electrically driven gyroscopes (attitude)but excluding those systems defined in sub-paragraph 8.2.8.5 Reserved8.6 Reserved8.7 Reserved* 8.8 'X' Instruments (compasses)Direct and remote reading compasses.9 Certification Privileges - ElectricalA rating granted in relation to any sub-paragraph of paragraph 9 of this Noticeincludes the generation system and the electrical installation in aircraft as defined bythat sub-paragraph, as limited by paragraph 3 of this Notice.NOTES:A Type Rated Licence which is valid for paragraph 9.2 or 9.3 also includes paragraph9.1.* 9.1 Aircraft in which the main generation system output is dc (includingalternators having a self-contained rectifier system) and in which secondaryalternators having an individual power rating not exceeding 1.5 kVA may befitted.* 9.2 Aircraft in which the main generation system output is dc and which haveinstalled 'frequency wild' alternators with an individual power ratingexceeding 1.5 kVA for auxiliary services.AN-10 P.530 September 2008
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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
Page 13 and 14: Category B Helicopter. A single-eng
Page 15 and 16: together necessary to provide thrus
Page 17 and 18: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 19 and 20: Schedule 7Schedule 8Schedule 9− A
Page 23 and 24: (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
Page 29 and 30: continuation of certification privi
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 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
Page 63: (a)an aircraft of the type is regis
Page 67 and 68: * 13.2 Radio-Coupled Automatic Pilo
Page 73 and 74: Appendix Subject CAAIP Leaflet 11-2
Page 75 and 76: AIRWORTHINESS NOTICE NO. 12APPENDIX
Page 77 and 78: 9 Due to the complexity and safety
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Page 91 and 92: 7 Maintenance of Aircraft - Non-Com
Page 93 and 94: 9.5 Where it is intended to fit par
Page 95 and 96: 1 ApplicabilityAIRWORTHINESS NOTICE
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Page 99 and 100: 3.2 The organisation will be requir
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Page 103 and 104: 4 Limited AuthorisationsFlight Crew
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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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AIRWORTHINESS NOTICE NO. 17APPENDIX
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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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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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