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

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5 Reference should also be made to Airworthiness Notice No.12 Appendix No. 69which contains advice on testing criteria for Transponders.NOTE: With the introduction of Mode 'S' Elementary and Enhanced Surveillance functionality,within the transponder, it is envisaged that additional testing of the transponder will berequired on a periodic basis (not to exceed two years).6 Cancellation6.1 This Notice Appendix cancels Airworthiness Notice No. 12 Appendix No. 67 Issue 2,dated 30 May 2008, which should be destroyed.31 July 2011 AN-12 A67 P.2
AIRWORTHINESS NOTICE NO. 12APPENDIX NO. 68Issue 230 September 20061 BackgroundFOREIGN OBJECT DAMAGE TO AIRCRAFT AND ENGINES1.1 Experiences learnt from a foreign CAA that they continue to receive reports ofdamage to aircraft and engines caused by foreign objects. Foreign ObjectDamage (FOD) presents a serious airworthiness threat to any aircraft not tomention the economic impact on the operator. In extreme cases, FOD canlead to an accident and loss of life. FOD damage to airframes and enginescan be extremely expensive to rectify and may result in the aircraft beingremoved from revenue service for significant period of time. There arenumerous reports on record of FOD damage to engines (in particular rotatingassemblies), nose and main landing gear assemblies and aircraft structure.1.2 A research project led by the foreign CAA revealed that a continuing threatexists from varying amounts of FOD present on aircraft maintenance areas andairport manoeuvring areas, including stands, aircraft taxiways and runways.The study showed the aircraft themselves as the main cause of FOD on therunway and this poses the highest immediate risk. Here, parts of aircraftbecome detached or tools and equipment, inadvertently left in the aircraft fallout during takeoff or landing. The largest item found on a runway was awheel chock but metal panels and honeycomb structure were also amongst thelarger items. The FOD found on taxiways and stands came mainly fromairport vehicles and the equipment they tow such as baggage trolleys, steps,cargo equipment etc. The size and shape of some of these foreign objectsmake it likely to cause tyre damage and subsequent tyre burst. The cleaningof aircraft cabins and the transfer of waste from cabin to airside rubbishcontainers is also seen to be a common source of foreign objects in the standareas. Other typical foreign objects consist of such items as oil cans,spanners, pliers, torches, suitcase items (both internal & external), mobileradios, aircraft catering equipment, cutlery, landing gear ground lock pins,thrust reverser lock-out pins and broken parts of ground servicingequipment/vehicles.1.3 Smaller items could be ingested by an engine. In many cases, FOD damageto engine rotating assemblies has led to vibration leading to air turn-backs,diversions and subsequent engine replacement. Boroscope inspections ofengines following reports of engine surging very often reveal internal damageto the enginesuch damage can of course be very expensive to repair.Typically, damage to the aircraft can range from damage to horizontalstabilizer leading edges to pressure hull penetration by objects thrown up fromthe runway, to varying degrees of damage to landing gear assemblies andAN-12 A68 P.130 September 2006
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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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Page 35 and 36: 3 Application3.1 The following appl
Page 37 and 38: Airworthiness Notice No. 4Appendix
Page 39 and 40: CIVIL AVIATION DEPARTMENTHONG KONG,
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
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Page 57 and 58: work detailed in the renewal form w
Page 59 and 60: (e)any parachute including a parasc
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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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AIRWORTHINESS NOTICE NO. 35APPENDIX
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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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