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

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HPMA No. Supp. Item Part Name Part No. Replacement Make ModelNo. No.For Eligibility EligibilityHPMA/141/0907 3 97 Floor Panel A509262-355 A509262-355 Boeing 747-400HPMA/141/0907 3 98 Floor Panel A509262-357 A509262-357 Boeing 747-400HPMA/141/0907 3 99 Floor Panel A509262-359 A509262-359 Boeing 747-400HPMA/141/0907 3 100 Floor Panel A509262-361 A509262-361 Boeing 747-400HPMA/141/0907 3 101 Floor Panel A509262-363 A509262-363 Boeing 747-400HPMA/141/0907 3 102 Floor Panel A509262-365 A509262-365 Boeing 747-400HPMA/141/0907 3 103 Floor Panel A509262-369 A509262-369 Boeing 747-400HPMA/141/0907 3 104 Spacer A509262-513 A509262-513 Boeing 747-400HPMA/141/0907 3 105 Spacer A509262-514 A509262-514 Boeing 747-400HPMA/141/0907 3 106 Spacer A509262-515 A509262-515 Boeing 747-400HPMA/141/0907 3 107 Spacer A509262-516 A509262-516 Boeing 747-400HPMA/141/0907 3 108 Spacer A509262-517 A509262-517 Boeing 747-400HPMA/141/0907 3 109 Spacer A509262-518 A509262-518 Boeing 747-400HPMA/141/0907 3 110 Spacer A509262-519 A509262-519 Boeing 747-400HPMA/141/0907 3 111 Floor Panel A509262-193 A509262-193 Boeing 747-400HPMA/141/0907 3 112 Floor Panel A509262-195 A509262-195 Boeing 747-400HPMA/141/0907 3 113 Floor Panel A509262-323 A509262-323 Boeing 747-400HPMA/141/0907 3 114 Floor Panel A509262-327 A509262-327 Boeing 747-400HPMA/141/0907 3 115 Floor Panel A509262-367 A509262-367 Boeing 747-400HPMA/141/0907 3 116 Assy-Floor A509262-159 A509262-159 Boeing 747-400PanelHPMA/141/0907 3 117 Assy-Floor A509262-161 A509262-161 Boeing 747-400PanelHPMA/141/0907 3 118 Assy-Floor A509262-257 A509262-257 Boeing 747-400PanelHPMA/141/0907 3 119 Assy-Floor A509262-258 A509262-258 Boeing 747-400PanelHPMA/141/0907 3 120 Assy-Floor A509262-259 A509262-259 Boeing 747-400PanelHPMA/141/0907 3 121 Assy-Floor A509262-260 A509262-260 Boeing 747-400PanelHPMA/141/0907 3 122 Assy-Floor A509262-261 A509262-261 Boeing 747-400PanelHPMA/141/0907 3 123 Assy-Floor A509262-262 A509262-262 Boeing 747-400AN-28 A2 P.7<strong>31</strong> January 2010
HPMA No. Supp. Item Part Name Part No. Replacement Make ModelNo. No.For Eligibility EligibilityPanelHPMA/141/0907 3 124 Assy-Cover A509256-015 A509256-015 Boeing 747-400MountHPMA/141/0907 3 125 Plate A509502-520 A509502-520 Boeing 747-400HPMA/141/0907 4 1 Assy-Doghouse A417156-015 A417156-015 Boeing 747-400<strong>31</strong> January 2010 AN-28 A2 P.8
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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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Page 131 and 132: accepted by CAD as in full complian
Page 133 and 134: (s) Manuals including:(1) * Mainten
Page 135 and 136: Note: ** Normally only required for
Page 137 and 138: INTENTIONALLY LEFT BLANK31 January
Page 139 and 140: 3.2 New Applications for Approvals
Page 141 and 142: Table 1:Classification of HKAR-1 Ce
Page 143 and 144: CIVIL AVIATION DEPARTMENTHONG KONG,
Page 145 and 146: 5.1 Users of aircraft components an
Page 147 and 148: 9 CancellationThis Notice cancels N
Page 149 and 150: specialist organisation.2.4 Details
Page 151 and 152: 5 Guidance4.2.3 Log book entries mu
Page 153 and 154: of some component parts.2.3 The fun
Page 157 and 158: 4 ApplicationApplicant shall apply
Page 159 and 160: 3 Requirement and Applicability3.1
Page 161 and 162: e equipped with a ground proximity
Page 165 and 166: Performance Class 1 helicopter A he
Page 167 and 168: Part II, Chapter 5.7 Coding and reg
Page 169 and 170: 1 GeneralAIRWORTHINESS NOTICE NO. 2
Page 175 and 176: List of HKAR-147 approved maintenan
Page 177 and 178: Table 2:Non-Critical HPMA PartsHPMA
Page 179 and 180: HPMA No. Supp. Item Part Name Part
Page 181: HPMA No. Supp. Item Part Name Part
Page 187 and 188: (d)(e)(f)desiring to enhance cooper
Page 189 and 190: (c)(d)(e)in the case of serious non
Page 191 and 192: Certificate of Release to Service a
Page 193 and 194: (g)(h)(i)civil aircraft and/or airc
Page 197 and 198: Technical Records include but are n
Page 199 and 200: Party the opportunity to review and
Page 201 and 202: Authority in respect of any major m
Page 203 and 204: meanings as specified:(a)(b)(c)(d)(
Page 205 and 206: 2.5.6 Where maintenance involves th
Page 207 and 208: 4.1.1 A statement signed by the cur
Page 213 and 214: (d)The data obtained during the ins
Page 215 and 216: 6 Cancellationmean time, the provis
Page 217 and 218: AIRWORTHINESS NOTICE NO. 35APPENDIX
Page 219 and 220: a pressure gauge (reading up to 140
Page 221 and 222: unchanged. However engine power may
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Page 225 and 226: and cabin crew seats as applicable,
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Page 229 and 230: 2.6 ICAO has also published guidanc
Page 231 and 232: (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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