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

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5 Acceptance Standard5.1 At an ultra-violet intensity of 1200µW/cm 2 , the maximum acceptable white lightintensity limit varies depending on the meter used. Values for approvedmeters are given below:-(a) Ardrox DLM 1000 8 foot candles(b) Minolta T1 0.3 foot candles(c) Spectronics DSE 100X (Ely Chemical Co.) 2 foot candles(d) Ardrox BC1955 0.9 foot candles(e) Levy Hill Mk. V 0.9 foot candles(f) Levy Hill Mk. VI 0.9 foot candles(g) Elyscan 2 (Ely Chemical Co.) 0.9 foot candles5.2 At any other ultra-violet intensity then the maximum acceptable white lightintensity limit must be calculated from the formula:-Y x ZWhite light intensity shall be less than = ------------ foot candles1200Where Y = maximum ultra-violet light recorded in µW/cm 2 .Z = acceptance limit for white light at a measured ultra-violet intensityof 1200µW/cm 2 for the specific meter used from reference table inparagraph 5.1.5.3 Any lamp having a white light output greater than the limit shall not be used forinspection purposes.6 Identification6.1 All lamps tested and accepted shall be identified in accordance with a localprocedure.NOTES: (1) One foot candle = 10.76 lux.(2) White light photometers are calibrated to a National Standard using TungstenFilament lamps. The spectral output of an ultra-violet lamp is significantlydifferent to that of a Tungsten Filament, and therefore the calibration is notvalid. The major source of discrepancy in this case, will be due to emission ofAN-95 P.331 January 2002
shorter wavelength light.7 CancellationThis Notice cancels Airworthiness Notice No.95, Issue 4, dated 30 June 1999, whichshould be destroyed.Albert K. Y. LAMDirector-General of Civil Aviation31 January 2002 AN-95 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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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 385 and 386: (a)(b)reduction of the generating s
Page 387 and 388: 3.2 Applications for the approval o
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Page 409 and 410: Quality Procedures.6 Suppliers and
Page 411 and 412: Qualification: The proven ability o
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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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Page 439 and 440: its removal from the water.5 Additi
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Page 445 and 446: 3.9 Compliance requirements for hel
Page 447 and 448: 4.5 Type IVA FDR Requirements4.5.1
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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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